阅读说明：本技术 百向平桨直升飞行器 (Multi-direction flat-blade helicopter ) 是由 罗灿 于 2018-05-28 设计创作，主要内容包括：本发明涉及一种百向平桨直升飞行器,包括机身、发动机、传动系统、顶桨旋翼、百向传动器、百向平桨、操纵控制系统等,该飞行器依靠顶桨旋翼提供升力。该飞行器设置了百向平桨,在动力从传动系统传动到百向平桨的传动路径中设置了五种百向传动器中的一种,使百向传动器中的百向合动器轴保持竖直,在动力传动过程中百向平桨可以受控地水平转动、实现百向平桨推力水平变向。这种转动与变向是受百向操控装置控制的,每一种百向传动器具有特定的控制方法。百向平桨可以发挥三种作用：1平衡顶桨旋翼反作用力力矩,2控制偏航,3提供飞行器前飞推进力。(The invention relates to a hundred-direction flat-blade helicopter which comprises a helicopter body, an engine, a transmission system, a top blade rotor, a hundred-direction driver, a hundred-direction flat blade, an operation control system and the like. The aircraft is provided with the hundred-direction flat paddles, one of five hundred-direction drivers is arranged in a transmission path from a transmission system to the hundred-direction flat paddles, so that a hundred-direction clutch shaft in the hundred-direction driver is kept vertical, and the hundred-direction flat paddles can be controlled to horizontally rotate in the power transmission process to realize horizontal direction change of thrust of the hundred-direction flat paddles. The rotation and the direction change are controlled by a hundred-direction control device, and each hundred-direction actuator has a specific control method. The hundred-direction flat paddle can play three roles: the method comprises the steps of 1 balancing the reaction force moment of a top propeller rotor, 2 controlling yaw, and 3 providing the forward flight propelling force of the aircraft.)

1. The vertical lift aircraft with the hundred-directional flat propellers comprises an aircraft body, an engine, a transmission system, a top propeller rotor, a hundred-directional driver, the hundred-directional flat propellers, a control system and the like, wherein the top propeller rotor can be a single rotor or a double rotor and comprises a total pitch variable mechanism, a periodic pitch variable mechanism and the like, the hundred-directional driver comprises a hundred-directional control device thereof, the hundred-directional flat propellers can be a single propeller or a double propeller and comprises a pitch variable mechanism and the like, the aircraft provides lift force by depending on the top propeller rotor, and the vertical lift aircraft is characterized in that the aircraft is provided with the hundred-directional flat propellers, one of five hundred-directional drivers such as a same-directional transfer propeller driver, a same-directional double-control propeller driver, a double-directional transfer propeller driver, a reverse double-directional double-control propeller driver and the like is arranged in a transmission path from the transmission system to the hundred-directional propeller, so that a hundred-directional clutch shaft in the hundred-directional, the input end of the hundred-direction driver is connected with the transmission system, the output end of the hundred-direction driver is connected with the hundred-direction flat propeller, the hundred-direction flat propeller and the output end of the hundred-direction driver can rotate around the axle of the hundred-direction clutch, the hundred-direction control device is arranged to control the rotation, the hundred-direction flat propeller can horizontally rotate and the hundred-direction flat propeller can controllably change the axial direction in the process that power is transmitted to the hundred-direction flat propeller through the hundred-direction driver, and therefore the thrust horizontal direction change of the hundred-direction flat propeller is achieved.

2. The vertical lift aircraft with hundred-directional flat propellers of claim 1, further characterized in that the change of the axial direction of the hundred-directional flat propellers of the aircraft, namely the turnover of the output end of the hundred-directional driver is controlled by a hundred-directional control device, the turnover is controlled by controlling a turnover control end for a same-directional transfer hundred-directional driver or a reverse transfer hundred-directional driver, the turnover is controlled by controlling a central input end for a same-directional transfer double-control hundred-directional driver or a reverse transfer double-control hundred-directional driver in a first application mode, the turnover is controlled by controlling a turnover control end in a second application mode, the turnover is controlled by controlling an input end in a third application mode, the turnover is controlled by controlling a turnover control end in a fourth application mode, and the turnover is controlled by controlling a turnover input end or a turnover control end for a double-directional driver.

3. The vertical lift aircraft with the hundreds of flat propellers, as claimed in claim 1, is provided with a single rotor top propeller, and the hundreds of flat propellers can play three roles by controlling variable pitch of the hundreds of flat propellers and controlling the axial directional steering of the hundreds of flat propellers: 1, balanced top oar rotor reaction force moment, 2, control driftage, 3, provide the aircraft forward propulsion, set up this aircraft of coaxial anti-oar bispin top oar, hundred can exert two kinds of effects to the flat oar: the method comprises the steps of 1, controlling yaw and 2, providing the front flying propelling force of the aircraft, wherein various functions of the hundred-direction flat paddles can be independently used or can be superposed with functions of other equipment of the aircraft.

Technical Field

The invention relates to an aircraft capable of vertically lifting and flying in a horizontal direction, in particular to a helicopter which is provided with a multi-direction flat propeller, provides lift force by depending on a top propeller rotor, and can provide variable-direction flat propulsion force by axially pointing to the multi-direction flat propeller capable of horizontally rotating.

Background

The existing common helicopter adopts a top propeller rotor to lift, a top propeller rotor cone tilts through a periodic torque variation to horizontally fly, the forward, backward, leftward and rightward translational thrust force depends on the periodic torque variation of the top propeller rotor, and the push-pull force of a flat-propeller tail propeller is only used for balancing the top propeller horizontal torque and adjusting and controlling yaw. When the helicopter flies forwards, the propeller disc of the top propeller rotor tilts forwards to provide forward component force, and at the moment, the propeller disc of the top propeller rotor also tilts downwards, so that the lift efficiency is low and the oil consumption is high when the helicopter flies forwards. If the helicopter depends on the top propeller rotor to provide lift force and the flat propeller rotor to provide the flat thrust to fly, the lift efficiency of the aircraft in the forward flight can be improved. The helicopter is propelled by coaxial reverse double-rotor top propellers, provides vertical lift, lift control, yaw control, roll control, left and right side flight control, pitching control and front and back flight control, and propels the helicopter forward by variable total pitch tail propellers with axial direction unchanged, fixed and backward when the helicopter flies forward in cruising. The method can improve the lift efficiency of the helicopter in forward flight. But yaw control is not flexible enough. But also is only suitable for double-rotor top-paddle helicopters and is not suitable for single-rotor top-paddle helicopters.

The invention aims to provide another solving method, and the helicopter provides vertical lift force by utilizing a top propeller rotor wing, and provides lifting control, rolling control, left and right side flight control, pitching control and front and back flight control. Meanwhile, a hundred-direction flat propeller (tail propeller) which is driven by a hundred-direction driver and can change the axial direction and the distance is arranged, so that the hundred-direction flat propeller not only can balance the reaction moment when a top propeller rotor actively rotates, but also can participate in yaw control, and can provide a variable-direction driving force to propel the aircraft to fly forwards when the aircraft flies forwards. This is a hundred-way flat-blade helicopter. The multi-direction flat-blade helicopter is suitable for a double-rotor blade-pushing aircraft and a single-rotor blade-pushing aircraft, the yaw control of the multi-direction flat-blade helicopter is more flexible, and the lift efficiency of the helicopter during forward flight can be very high.

Disclosure of Invention

The invention relates to a vertical lift aircraft with hundred directions of flat propellers, which comprises an aircraft body, an engine, a transmission system, a top propeller rotor wing, a hundred direction driver, a hundred direction flat propeller (tail propeller), an operation control system and the like. The top propeller rotor can be a single rotor or a double rotor, comprises a total distance variable mechanism, a periodic distance variable mechanism and the like, and also comprises an operation control device thereof. The hundred-direction driver comprises a hundred-direction control device, the hundred-direction control device is a control device which finally controls the output end of the hundred-direction driver to rotate around a hundred-direction clutch shaft by controlling a turnover control end (or a central input end or an input end or a turnover input end) of the hundred-direction driver, and the control device is generally a rack and pinion device or a link mechanism and the like which obtains power from a transmission system, or a servo motor device and the like with independent power. The hundred-direction flat paddle can be a single paddle or a double paddle, comprises a variable pitch mechanism and further comprises a variable pitch control device. The aircraft relies on a top paddle rotor to provide lift. The invention relates to a hundred-direction flat-paddle helicopter which is characterized in that a hundred-direction driver is arranged in a transmission system of a hundred-direction flat paddle (tail paddle), the output end of the hundred-direction driver is connected with the hundred-direction flat paddle, the axial direction of the hundred-direction flat paddle can be changed, and the direction of the thrust (or the pull) of the hundred-direction flat paddle can be changed in the horizontal plane.

The invention relates to a hundred-direction flat-blade helicopter which is provided with a hundred-direction flat blade (tail blade), wherein one of five hundred-direction drivers, namely a same-direction transfer hundred-direction driver, a same-direction transfer double-control hundred-direction driver, a double-flow hundred-direction driver, a reverse transfer double-control hundred-direction driver and the like, is arranged in a transmission path from a transmission system to the hundred-direction flat blade. And the shaft of the unidirectional clutch in the unidirectional driver is kept vertical, the input end of the unidirectional driver is connected with the transmission system, the output end of the unidirectional driver is connected with the unidirectional flat blade, and the unidirectional flat blade and the output end can rotate around the shaft of the unidirectional clutch. A hundred-direction control device is arranged to control the turnover, the hundred-direction flat paddles can horizontally rotate in the process that power is transmitted to the hundred-direction flat paddles through the hundred-direction driver, the axial direction of the hundred-direction flat paddles can be controllably changed, and the thrust of the hundred-direction flat paddles can be changed in the horizontal plane. See fig. 1, 2, 3. The turnover of the output end of the unidirectional driver is controlled by the unidirectional control device, so that the axial direction of the unidirectional flat paddle and the axial direction of the unidirectional clutch are controlled to form a 90-degree included angle with the axial direction of the unidirectional clutch to rotate around the axial direction of the unidirectional clutch in a horizontal plane at the same time of power transmission. The axial direction of the hundred-direction flat paddles can point to the left, the rear, the right and other directions of the aircraft, so that the propelling force of the flat paddles can point to the right, the rear, the left and other directions of the aircraft. Such a flat blade, which is axially oriented and can be rotated horizontally about the axis of the blade actuator, is called a blade actuator. The multi-directional flat propeller can be a propeller or a ducted fan, and can be a single propeller or a single-propeller ducted fan, or a double-propeller or double-propeller ducted fan. The relationship between the double paddles can be coaxial contra-rotation (or coaxial contra-rotation or coaxial contra-paddles). Similar to the arrangement of a torque converter in a tail rotor of a common helicopter, the hundred-direction flat blade of the hundred-direction flat blade helicopter comprises a variable pitch device, so that the wing surface of a rotor wing or a blade of the rotor wing can be variable in pitch, and the propelling force of the hundred-direction flat blade can be adjusted or made to be zero. In the invention, the torque converter and the variable-pitch operation control device thereof have the same axial direction as the axial direction of the hundred-direction flat paddles and can rotate around the axle of the hundred-direction clutch along with the output end of the hundred-direction driver and the hundred-direction flat paddles. The pitch range of the hundred-direction flat paddle is generally larger than or equal to zero and can be smaller than zero under special conditions. When the pitch of the hundreds of flat blades can be changed to a value less than zero, the thrust of the hundreds of flat blades (tail blades) is converted into the pulling force.

The hundred-direction driver can be one of five hundred-direction drivers, namely a same-direction transfer hundred-direction driver, a same-direction transfer double-control hundred-direction driver, a double-flow hundred-direction driver, a reverse transfer hundred-direction driver or a reverse transfer double-control hundred-direction driver. The common characteristic of the five hundred-direction drivers is that the structures of the five hundred-direction drivers are all provided with a hundred-direction clutch, the structures of the five hundred-direction drivers can ensure that the axial direction of an output end forms a certain included angle with the axis of the hundred-direction clutch while driving, and the axial direction of the output end can be circulated around the axis of the hundred-direction clutch and can be controlled in circulation, so that the rotatable direction-changing driving is formed. After the hundred direction clutch shafts are set, the hundred direction control devices are respectively controlled by using respective specific control methods, so that the output end can axially point to and rotate around the hundred direction clutch shafts, and the rotating control can be independent from the rotating direction-changing transmission without mutual interference. The hundred-direction control device is a control device which finally controls the output end of the hundred-direction driver to rotate around the axis of the hundred-direction clutch by controlling the turnover control end (or the central input end or the turnover input end) of the hundred-direction driver, and generally is a gear and rack device or a link mechanism which obtains power from a transmission system, or is a servo motor device with independent power, and the like. The five hundred-direction drivers can drive high power and high transmission efficiency, and the controllable range of the turnover angle when the output end points to the shaft of the hundred-direction clutch in a turnover mode is large.

The co-rotating hundreds-directional transmission structure is shown in figure 4. The equidirectional transfer-hundred-direction driver consists of an equidirectional transfer case, a reverser and a hundred-direction clutch. The equidirectional transfer case is a single-row planet row, and is characterized in that the planet row meets the condition I: the kinematic characteristic equation is in the form of a homodromous transfer case kinematic equation NA1-k NB1- (1-k) NC1 being 0, wherein 0< k < 1.0. In the equidirectional transfer case planet row, a component A1 corresponding to NA1 is used as the input end of the equidirectional transfer case, the input end of the equidirectional transfer case is also used as the input end of the equidirectional transfer case, the other two components are used as the equidirectional transfer case transfer ends, the transfer end B1 is connected with a central wheel B2 of the hundred-direction transfer case, and the transfer end C1 is connected with a central wheel C2 of the hundred-direction transfer case. The first type of the commutator is a one-way commutator which is used in one of two connections between a transfer end of a equidirectional transfer case and a central wheel of a hundred-directional clutch and can change the absolute value of the rotating speed of the connection transmission in a constant rotating direction, namely, two rotating speeds of coaxial and same rotation are converted into two rotating speeds of coaxial and reverse rotation. The second type is a two-way commutator which is used in two connections and can convert two rotating speeds of the two connection transmissions from coaxial co-rotation to coaxial counter-rotation. The unidirectional clutch is a single-row planetary row, the shaft of the planetary row is the shaft of the unidirectional clutch, the planetary row can be a bevel gear single-layer planetary row, and the unidirectional clutch is characterized in that the planetary row meets the second condition: the motion characteristic equation is in the form of NA2-0.5 NB2- (1-0.5) NC 2-0 after finishing deformation, and a planet carrier j2 corresponding to NA2 is also A2 as a turnover control end, and the turnover control end is also a turnover control end of the equidirectional transfer hundred-direction transmission. One planetary gear in the hundred-direction clutch is taken as an output end and is called a single-path output end, two planetary gears are taken as output ends and are called double-path output ends, and the output rotating speed is the output end autorotation rotating speed NX2 which is also the output end of the same-direction transfer hundred-direction transmission. The vertical lift aircraft with the hundred-direction flat paddles adopts a same-direction transfer hundreds-direction driver with an axially directed turnover control end and completely independent turnover turning transmission end. Referring to fig. 4, the homodromous transfer case adopts a variable linear speed double-layer planetary row, and transmits an input rotating speed NA1 to an output end NX2 through a horizontal paraxial bevel gear which is powered from a transmission system to an input end a 1. The single-way commutator in the figure takes the form of a bevel gear planet row with a fixed planet carrier. In the figure, a shaft of the hundred-direction clutch is kept vertical, an outer gear ring is arranged on a planet carrier turnover control end 5, a paraxial gear 8 meshed with the outer gear ring can input a rotating speed NA2 to the turnover control end (in the embodiment 1, the paraxial gear 8 is controlled and controlled by a servo motor), a paraxial connecting gear 7 which can adjust two rotating speeds of a double-path output end and convert the two rotating speeds into two rotating speeds of coaxial reverse propellers can also rotate around the axle of the hundred-direction clutch along with the output end, the two rotating speeds of the double-path output end 6 can be connected with the double-rotor coaxial reverse propeller hundred-direction flat propeller after being converted into the two rotating speeds of the coaxial reverse propeller, and the turnover angle range of the hundred-direction flat propeller. The condition that the axially directed revolving operation of the output end of the power transmission is completely independent from the revolving direction-changing transmission is that the same-direction transfer case motion equation NA1-k NB1- (1-k) NC1 is 0, and k is 0.5. The rotating speed NA1 is input at the input end of the equidirectional transfer unidirectional transmission, the rotating speed NX2 can be output at the output end, and the rotating speed NA2 of the transfer control end can be controlled to axially point around the axis of the unidirectional clutch for transfer. The turnover rotating speed of the output end is small, and the turnover amplitude of the turnover control end is not large. The hundred-direction control device for controlling the turnover can be a servo motor device, or a gear rack device, or a link mechanism.

The structure of the equidirectional split double-control hundred-direction driver is shown in figure 5. The equidirectional transfer double-control one-hundred-direction driver consists of an equidirectional transfer case, a reverser, an equidirectional clutch and a one-hundred-direction clutch. The equidirectional transfer case is a single-row planet row, and is characterized in that the planet row meets the condition I: the motion characteristic equation is in a form of a homodromous transfer case motion equation NA1 being 0.5 NB1+0.5 NC1 after finishing deformation, in a homodromous transfer case planet row, a component A1 corresponding to NA1 is used as an input end of a homodromous transfer case, the component A1 is also used as an input end of a homodromous transfer case, the other two components are used as transfer ends of the homodromous transfer case, a transfer end B1 is connected with an input end output end B2 of the homodromous transfer case, and a transfer end C1 is connected with an input end output end C2 of the homodromous transfer case. The first type of the commutator is a one-way commutator which is used in one of two connections between a transfer end of a equidirectional transfer case and an input end of a equidirectional clutch and can change the absolute value of the rotating speed of the connection transmission in a constant rotating direction, namely, two rotating speeds of coaxial and same rotation are converted into two rotating speeds of coaxial and reverse rotation. The second type is a two-way commutator which is used in two connections and can convert two rotating speeds of the two connection transmissions from coaxial co-rotation to coaxial counter-rotation. The syntropy clutch is single row planet row, and its planet row can be change linear speed double-deck star planet row or ordinary cylindrical gear double-deck star planet row, and the form that its motion characteristic equation was out of shape in the arrangement accords with condition two for its planet row characteristics: the motion equation NA2 of the homodromous clutch is 0.5 × NB2+0.5 × NC2, a central wheel A2 corresponding to the NA2 serves as a central input end, B2 and C2 are two input ends and two output ends of the homodromous clutch, the two input ends serve as input ends and are respectively connected with two transfer ends of the homodromous transfer, and two connections serving as output ends and central wheels of the homodromous transfer are called rear ends. The rear end is connected with two connection modes: in the first connection mode, the transmission ratios of the two rear-end connections are both n or-n, that is, the two original rotation speeds in the same direction are connected and transmitted and then keep in the same direction, and the two original rotation speeds in the opposite direction are connected and transmitted and then keep in the opposite direction. In the second connection mode, one of the transmission ratios of the two rear-end connections is n, and the other transmission ratio is-n, namely, the two rotation speeds which are originally in the same direction are converted into the opposite directions after being connected and transmitted, and the two rotation speeds which are originally in the opposite directions are converted into the same direction after being connected and transmitted. The unidirectional clutch is a single-row planetary row, the shaft of the planetary row is the shaft of the unidirectional clutch, the planetary row can be a bevel gear single-layer planetary row, and the unidirectional clutch is characterized in that the planetary row meets the condition three: the form of the motion characteristic equation after finishing deformation is NA 3-0.5-NB 3+ 0.5-NC 3, and a planet carrier j3 corresponding to NA3 is also A3 as a turnover control end, which is also a turnover control end of the equidirectional transfer double-control hundred-direction transmission. One or two planetary wheels in the hundred-direction clutch are used as output ends, and the output rotating speed is output end autorotation rotating speed NX3 which is also the output end of the homodromous double-control hundred-direction transmission. The component 12 in fig. 5 uses a planet wheel as an output end, called a one-way output end, and the rear end connection in the figure is in a first connection mode. The connection modes of the rear end connection of the equidirectional transfer double-control hundred-direction driver are different, and the corresponding application modes are different. The corresponding connection mode has a first application mode: the input end A1 inputs a rotating speed NA1 which can be transmitted to the output end to form an output rotating speed NX3, the output end is axially directed and can rotate around the shaft of the unidirectional clutch, so that the rotating control end can be kept free (the rotating control end can be omitted at the moment), the rotating speed NA3 axially directed at the output end can be adjusted by adjusting the rotating speed NA2 of the central input end, the rotating can be controlled, and NA2 is in direct proportion to NA 3. Corresponding to the first connection mode, the method also has a second application mode: the input end A1 inputs a rotating speed NA1, the rotating speed NA1 can be transmitted to the output end to form an output rotating speed NX3, the axial direction of the output end can be rotated around the shaft of the unidirectional clutch, the central input end is kept free, the axial direction of the output end can be adjusted by adjusting the rotating speed NA3 of the rotating control end, and the rotation can be controlled. Corresponding to the second connection mode, there is a third application mode: the rotating speed NA2 is input at the central input end A2 and can be transmitted to the output end to form an output rotating speed NX3, the output end is axially directed and can rotate around the shaft of the unidirectional clutch, so that the rotating control end can be kept free, the rotating speed NA3 axially directed at the output end can be adjusted by adjusting the rotating speed NA1 of the input end, the rotating can be controlled, and NA1 is in direct proportion to NA 3. And corresponding to the second connection mode, a fourth application mode is also provided: the rotating speed NA2 is input at the central input end A2 and can be transmitted to the output end to form the output rotating speed NX3, the axial direction of the output end can be rotated around the shaft of the unidirectional clutch, so that the input end is kept free, the axial direction of the output end can be adjusted by adjusting the rotating speed NA3 of the rotating control end, and the rotation can be controlled. The four application modes can realize that the axial direction of the output end forms an included angle of 90 degrees with the shaft of the unidirectional clutch, the axial direction of the output end can be circulated around the shaft of the unidirectional clutch, the circulation is controllable, and the circulation control and the direction-changing transmission which can be circulated are mutually independent. The hundred-direction flat-paddle helicopter generally adopts a same-direction transfer double-control hundred-direction driver with a first connection mode and a first application mode in the rear end connection. Referring to fig. 5, the equidirectional transfer case adopts a variable linear speed double-layer star planetary row, the one-way commutator adopts a bevel gear form, the equidirectional clutch adopts a variable linear speed double-layer star planetary row, an outer gear ring is arranged at a central input end 7, an output end is controlled to rotate by inputting NA2 through a paraxial gear 8 meshed with the outer gear ring, the rear end is connected in a first connection mode, the one-way clutch adopts a bevel gear single-layer star planetary row, and the one-way output end 12 is used for connecting one-way flat paddles. The rotating speed of the output end turnover is small, and the turnover amplitude of the control turnover is not large. The hundred-direction control device for controlling the turnover can be a servo motor device, or a gear rack device, or a link mechanism.

The dual flow hundred drive is shown in fig. 6. The double-flow one-hundred-direction transmission is composed of a double-flow variable speed transmission and a one-hundred-direction clutch, and has a specific connection mode and a transmission path. The double-flow variable-speed transmission device is characterized in that a planet row component is arranged at a reverse input end, the rotating speed of the input end is transferred into two rotating speeds with the same rotating speed and the opposite rotating directions through a transfer case and is transmitted to the double-flow variable-speed transmission device, a planet row component is arranged at a same input end, the rotating speed of the input end is transferred into two rotating speeds with the same rotating speed and the same rotating directions through the transfer case and is transmitted to the other component of the planet row of the double-flow variable-speed transmission device, and the connection from the reverse input end and the same input. The two planetary rows of the double-flow variable-speed driver can adopt variable linear speed double-layer planetary rows or common cylindrical gear single-layer planetary rows, when the double-flow variable-speed driver adopts the two double-layer planetary rows, the two motion characteristic equations are a, Nq1, (a-1), Nj1+ Nt1 and a, Nq2, (a-1), Nj2+ Nt2, two input ends are respectively connected to two sun gears and two planet carriers of two planet rows through a transfer gear, two inner gear rings of the two planet rows are used as two output ends, when two single-star planetary rows are used, the two kinematic characteristic equations in the double-flow variable-speed transmission are (1+ a) × Nj1 ═ a × Nq1+ Nt1 and (1+ a) × Nj2 ═ Nq2+ Nt2, the two input ends are respectively connected to the two sun wheels and the two ring gears of the two planetary rows through the transfer gears, and the two planet carriers of the two planetary rows serve as the two output ends. The single-row bevel gear single-layer star planet row is adopted as the unidirectional clutch, the planet row shaft is the shaft of the unidirectional clutch, the motion characteristic equation of the unidirectional clutch is in a form that Nj3 is 0.5 Nt3+0.5 Nq3 after arrangement and deformation, a planet carrier j3 corresponding to Nj3 is used as a turnover control end, an Ethernet wheel t3 and an inner gear ring q3 are used as the input ends of the unidirectional clutch and are respectively connected with two output ends of a double-flow variable speed driver, and two connections between the two output ends of the double-flow variable speed driver and the two input ends of the unidirectional clutch are called rear end connections. One or more groups of planet wheels can be arranged on the planet carrier of the hundred-direction clutch, one or two planet wheels are used as the output end of the hundred-direction clutch, the output end of the whole double-flow hundred-direction clutch is also the output end of the whole double-flow hundred-direction clutch, and the output rotating speed is the rotation rotating speed Nx3 of the planet wheels. One planet wheel is taken as an output end and is called a one-way output end, and two planet wheels which coaxially rotate reversely are taken as output ends and are called two-way output ends. Setting the absolute value of the transmission ratio of the rear end connection as n, wherein the rear end is connected with two modes, namely a first mode: the transmission ratio of the two rear ends is n or-n. And a second connection mode: the transmission ratios of the two rear end connections are n and-n respectively. The rear end is connected with a double-flow hundred-direction driver adopting a first connection mode, the reverse input end is a turnover input end of the double-flow hundred-direction driver, the turnover input end can be called z, the rotating speed is called Nz, the same-direction input end is a driving input end of the double-flow hundred-direction driver, the rotating speed is called c, and the rotating speed is called Nc. The rear end is connected with a double-flow hundred-direction driver adopting a second connection mode, the homodromous input end is a turnover input end of the double-flow hundred-direction driver and can be called z, the rotating speed of the double-flow hundred-direction driver is called Nz, the reverse input end is a driving input end of the double-flow hundred-direction driver and can be called c, and the rotating speed of the double-flow hundred-direction driver is called Nc. The rear end connection of the double-flow hundred-direction driver in fig. 6 adopts a second connection mode, and the output end 9 in the figure adopts two planetary wheels as a double-path output end, and can also adopt a single-path output end for connecting a hundred-direction flat paddle. When the rotation speeds Nc and Nz of two rotating members of the transmission input end and the turnover input end are determined, the rotation speeds of all the rotating members in the system are determined, and the planetary wheel rotation speed Nx3 at the output end is also determined. The power can be transmitted from the transmission input end rotating speed Nc to the output end autorotation rotating speed Nx3, the output end of the planet wheel of the single-layer planet row of the bevel gear of the unidirectional clutch can be controlled to be in controlled turnover around the axis of the unidirectional clutch in the axial direction perpendicular to the axis of the unidirectional clutch by controlling the value of Nz, the turnover rotating speed is in direct proportion to Nz, and the purpose that the output end can be in controlled turnover around the axis of the unidirectional clutch in the axial direction is achieved. When the revolution speed Nc, Nj3 of the two rotating members of the transmission input end and the revolution control end are determined, the rotation speed of all the rotating members in the system is determined, and the planet wheel rotation speed Nx3 of the output end is also determined. The input Nc and the power can be transmitted from the transmission input end rotating speed Nc to the output end autorotation rotating speed Nx3, the planetary gear output end of the single-layer planetary row of the bevel gear of the unidirectional clutch can be controlled to be in controlled turnover around the axis of the unidirectional clutch in the axial direction perpendicular to the axis of the unidirectional clutch by controlling the value of Nj3, and the turnover rotating speed Nj3 realizes the purpose that the output end can be in turnover around the axis of the unidirectional clutch and the turnover can be controlled. In the two control modes, the turnover control and the turnover turning transmission are independent and do not interfere with each other. The turnover rotating speed of the output end is small, and the turnover amplitude of the turnover control end is not large. The hundred-direction control device for controlling the turnover can be a servo motor device, or a gear rack device, or a link mechanism.

The reverse transfer hundred-way transmission structure is shown in figure 7. The reverse transfer one-hundred-way transmission consists of an issuing transfer case and a one-hundred-way clutch. The reverse transfer case is a single-row planet row, and is characterized in that the planet row meets the condition I: the kinematic characteristic equation is in the form of inverse transfer case kinematic equation NA1 (1+ k) NB1-k NC1 after finishing deformation, k > 1.0. In the reverse transfer case planet row, a component A1 corresponding to NA1 is used as the input end of a reverse transfer case, which is also the input end of a reverse transfer case hundred-direction transmission, the other two components are used as the transfer ends of the reverse transfer case, a transfer end B1 is connected with a hundred-direction clutch central wheel B2, and a transfer end C1 is connected with a hundred-direction clutch central wheel C2. The unidirectional clutch is a single-row planetary row, the shaft of the planetary row is the shaft of the unidirectional clutch, the planetary row can be a bevel gear single-layer planetary row, and the unidirectional clutch is characterized in that the planetary row meets the second condition: the motion characteristic equation is in the form of NA2-m NB3- (1-m) NC 3-0 after arrangement and deformation, 0< m <1.0, and a planet carrier j2 corresponding to NA2 is also A2 as a turnover control end, which is also a turnover control end of the reverse split-gear transmission, one or two planet wheels in the split-gear transmission are used as output ends, the output rotating speed is output end self-rotating speed NX2, and the output end of the reverse split-gear transmission is also used as an output end of the reverse split-gear transmission. The revolution of the output end can be controlled by controlling the revolution speed NA2 of the revolution control end with smaller torque. The counter transfer hundreds transmission adopted by the hundreds flat-blade helicopter is shown in figure 7. In the figure, a reverse transfer case adopts a variable linear speed double-layer star planetary row, a unidirectional clutch adopts a bevel gear single-layer star planetary row, a turnover control end 6 is provided with an outer gear ring, the turnover is controlled by inputting NA2 to the turnover control end through a paraxial gear 8 meshed with the outer gear ring, and a single-path output end 7 is used for connecting a unidirectional flat paddle. The condition that the difference between the forward torque and the reverse torque of the output end axially directed to the epicyclic control is the minimum is that k in a reverse transfer case motion equation NA1 ═ (1+ k) × NB1-k × NC1, and m in a hundred transfer case motion equation NA2 ═ m ═ NB2+ (1-m) × NC2 ═ 0.5. The rotating speed NA1 is input at the input end of the reverse transfer hundred-direction transmission, the rotating speed NX2 can be output at the output end, and the rotating speed NA2 of the transfer control end can be controlled to axially point around the shaft of the hundred-direction transmission for transfer. The turnover rotating speed of the output end is small, and the turnover amplitude is not large. The hundred-direction control device for controlling the turnover can be a servo motor device, or a gear rack device, or a link mechanism.

the structure of the reverse transfer double-control hundred-direction driver is shown in figure 8. The reverse transfer double-control one-hundred-direction driver consists of a reverse transfer case, a single-way speed changer, a same-direction clutch and a one-hundred-direction clutch. The reverse transfer case is a single-row planet row, and is characterized in that the planet row meets the condition I: the kinematic characteristic equation is in the form of inverse transfer case kinematic equation NA1 (1+ k) NB1-k NC1 after finishing deformation, k > 1.0. In the reverse transfer case planet row, a component A1 corresponding to NA1 is used as the input end of a reverse transfer case, which is also the input end of a reverse transfer case double-control one-hundred-direction transmission, the other two components are used as the transfer ends of the reverse transfer case, a transfer end B1 is connected with the input end output end B2 of a homodromous transmission, and a transfer end C1 is connected with the input end output end C2 of the homodromous transmission. The syntropy clutch is single row planet row, and its planet row can be change linear speed double-deck star planet row or ordinary cylindrical gear double-deck star planet row, and the form that its motion characteristic equation was out of shape in the arrangement accords with condition two for its planet row characteristics: the motion equation NA2 of the homodromous clutch is 0.5 × NB2+0.5 × NC2, a central wheel A2 corresponding to the NA2 serves as a central input end, B2 and C2 are two input ends and two output ends of the homodromous clutch, the two input ends serve as input ends and are respectively connected with two transfer ends of the reverse transfer case, and the two connections serving as output ends and the central wheel of the hundred-directional clutch are called rear end connections. The rear end is connected with two connection modes: in the first connection mode, the transmission ratios of the two rear-end connections are both n or-n, that is, the two original rotation speeds in the same direction are connected and transmitted and then keep in the same direction, and the two original rotation speeds in the opposite direction are connected and transmitted and then keep in the opposite direction. In the second connection mode, one of the transmission ratios of the two rear-end connections is n, and the other transmission ratio is-n, namely, the two rotation speeds which are originally in the same direction are converted into the opposite directions after being connected and transmitted, and the two rotation speeds which are originally in the opposite directions are converted into the same direction after being connected and transmitted. The unidirectional clutch is a single-row planetary row, the shaft of the planetary row is the shaft of the unidirectional clutch, the planetary row can be a bevel gear single-layer planetary row, and the unidirectional clutch is characterized in that the planetary row meets the condition three: the form of the motion characteristic equation after finishing deformation is NA3 ═ 0.5 × NB3+0.5 × NC3, and the carrier j3 corresponding to NA3 is also A3 as an epicyclic control end. The transmission is also a revolution control end of the reverse transfer double-control one-hundred-direction transmission, one or two planetary wheels in the one-hundred-direction transmission are used as output ends, and the output rotating speed is output end rotation rotating speed NX3 which is also the output end of the reverse transfer double-control one-hundred-direction transmission. The component 11 in fig. 8 uses a planet wheel as an output end, called a one-way output end, and the rear end connection in the figure is in a first connection mode. The reverse transfer double-control hundred-direction driver has different connection modes connected with the rear end and different corresponding application modes. The corresponding connection mode has a first application mode: the input end A1 inputs a rotating speed NA1 which can be transmitted to the output end to form an output rotating speed NX3, the output end is axially directed and can rotate around the shaft of the unidirectional clutch, so that the rotating control end can be kept free (the rotating control end can be omitted at the moment), the rotating speed NA2 of the central input end can be adjusted by small torque, the rotating speed NA3 axially directed at the output end can be adjusted, the rotating can be controlled, and NA2 is in direct proportion to NA 3. Corresponding to the first connection mode, the method also has a second application mode: the input end A1 inputs a rotating speed NA1 which can be transmitted to the output end to form an output rotating speed NX3, the axial direction of the output end can be rotated around the shaft of the unidirectional clutch, so that the central input end is kept free, the axial direction of the output end can be adjusted by adjusting the rotating speed NA3 of the rotating control end with small torque, and the rotation can be controlled. Corresponding to the second connection mode, there is a third application mode: the rotating speed NA2 is input at the central input end A2 and can be transmitted to the output end to form the output rotating speed NX3, the output end is axially directed and can rotate around the shaft of the unidirectional clutch, so that the rotating control end is kept free, the rotating speed NA1 of the input end can be adjusted by small torque, the rotating speed NA3 axially directed at the output end can be adjusted, the rotation can be controlled, and NA1 is in direct proportion to NA 3. And corresponding to the second connection mode, a fourth application mode is also provided: the rotating speed NA2 is input at the central input end A2 and can be transmitted to the output end to form the output rotating speed NX3, the axial direction of the output end can be rotated around the shaft of the unidirectional clutch, so that the input end is kept free, the axial direction of the output end can be adjusted by adjusting the rotating speed NA3 of the rotating control end with small torque, and the rotation can be controlled. The four application modes can realize that the axial direction of the output end forms an included angle of 90 degrees with the shaft of the unidirectional clutch, and the axial direction of the output end can be circulated around the shaft of the unidirectional clutch and has controllable unidirectional transmission. The hundred-direction flat-paddle helicopter generally adopts a reverse transfer double-control hundred-direction driver with the rear end connected in a first connection mode and a first application mode. Referring to fig. 8, the reverse transfer case adopts a variable linear speed double-layer star planetary row, the homodromous clutch adopts a variable linear speed double-layer star planetary row, an outer gear ring is arranged at a central input end 6, an NA2 is input through a paraxial gear 7 meshed with the outer gear ring to control output end turnover, the rear end connection is a first connection mode, the unidirectional clutch adopts a bevel gear single-layer star planetary row, and a single-path output end 11 is used for connecting a unidirectional flat paddle. The revolving speed of the output end is small, and the revolving amplitude is not large. The hundred-direction control device for controlling the turnover can be a servo motor device, or a gear rack device, or a link mechanism.

The effect of the hundred-way feathering in a hundred-way feathering helicopter is similar to the effect of a conventional tail rotor in a conventional helicopter, as is the case when the hundred-way feathering is directed axially to the right for balancing the top rotor reaction force moment. But also has the difference, and different with ordinary tail rotor, the axial direction of hundred to the flat oar can adjust its axial point and rotate around the axle of hundred to the ware of closing, so has more different functions and effects. The method comprises the following specific steps:

For a hundred-direction flat-blade helicopter provided with a single-rotor-blade top blade, the top blade rotor blade is arranged to rotate clockwise, and the top blade rotor blade comprises a collective pitch device and a periodic pitch device. By controlling the pitch change of the hundred-direction flat paddles and controlling the axial directional steering of the hundred-direction flat paddles, the hundred-direction flat paddles can play three roles: the method comprises the steps of 1, balancing the reaction force moment of a top propeller rotor, 2, controlling yaw, and 3, and providing forward flight propelling force of an aircraft. And 1, balancing the moment of the reaction force of the top propeller rotor, wherein the moment of the reaction force is anticlockwise when the top propeller rotor is hovered by the aircraft and actively rotates clockwise. The hundred-direction flat paddles can adjust the axial direction to the right, adjust the variable pitch of the flat paddles to enable the thrust to push the machine body leftwards, and balance the reaction force moment of the top paddle rotor wing. 2, when the top propeller rotor of the aircraft rotates actively, the variable pitch of the hundreds direction flat propeller can be adjusted to adjust the thrust like the tail propeller of the common helicopter, so that the moment of the hundreds direction flat propeller relative to the mass center of the aircraft is changed, and the aim of controlling the aircraft to yaw is fulfilled. The axial direction of the hundred-direction flat paddles can be adjusted to rotate, the direction of thrust is changed, the direction of moment is changed, and yaw is controlled more quickly. When the hundred-direction flat paddles are axially directed to the left and the thrust to the right, the aircraft can quickly yaw to the left. And 3, providing forward flight propelling force of the aircraft, wherein when the rotor wing of the front-flying top propeller of the aircraft rotates forwards actively, the axial direction of the hundred-direction flat propeller can point to the right rear side, the variable-pitch output thrust of the hundred-direction flat propeller can be adjusted, lateral component force can be generated to balance the moment of the reaction force of the rotor wing of the top propeller, and meanwhile, forward component force and the forward component force of the rotor wing of the top propeller are generated to jointly propel the aircraft to fly forwards. See fig. 1. When the front top propeller rotor of the aircraft passively rotates like a rotor of a self-rotating gyroplane, the axial direction of the hundred-direction flat propellers can point to the rear, the effect of forward propulsion is exerted, and the forward propulsion is independently provided for the aircraft. Meanwhile, the axial direction of the hundred-direction flat paddles can also finely adjust and deflect leftwards and rightwards, so that a yaw control effect is provided for the flying vehicle in the front flight. The function of the hundreds direction flat paddle is completely different from that of the tail rotor of the common helicopter. When the top propeller rotor of the aircraft is provided with the speed changer and can actively rotate at a low speed, the reaction force moment of the top propeller rotor is smaller. At the moment, the axial direction of the hundred-direction flat paddles can point to the rear and slightly lean to the right, the hundred-direction flat paddles mainly play a role in forward propulsion force, play a role in balancing the counter-force moment of the top paddle rotor wings and play a role in yaw control. The function of the hundred-direction flat-blade helicopter is completely different from that of a common helicopter.

For a hundred-direction flat-rotor helicopter provided with coaxial reverse double rotors, a flat rotor (tail rotor) is not needed for balancing the reaction force moment of a top-rotor. If the top propeller rotor wing comprises the periodic pitch changing device and the total pitch changing device, the mutual relation of the double rotor wings is coaxial reversal, the top propeller double rotor wing does not need to be provided with a differential pitch changing device, and the structure can be simplified. By controlling the pitch of the hundred-direction flat paddles and controlling the axial directional steering of the hundred-direction flat paddles, the hundred-direction flat paddles can play two roles: controlling yaw, and providing the front flying propelling force of the aircraft by 2. 1, a common coaxial counter-rotor dual-rotor helicopter generates a yaw moment to the left and the right through differential variable pitch. In the invention, the axial direction of the hundred-direction flat paddles can be adjusted to turn around, the direction of thrust can be changed, the direction of moment can be changed, and yaw can be effectively controlled. When the hundreds of flat paddles are axially directed to the left and thrust to the right, the aircraft may yaw to the left. When the paddle is pointed axially to the right and the thrust is to the left, the aircraft can yaw to the right. Therefore, a differential pitch-changing device in the coaxial contra-rotating dual-rotor wing can be cancelled when necessary, and the structure is simplified. 2, provide the aircraft and fly forward propulsive force, no matter top oar bispin wing initiative is rotatory, low-speed initiative is rotatory under the derailleur is adjusted, still passively rotates like the autogyro rotor, the axial direction of hundred to flat oar can point to the rear, adjusts the effect of propulsive force forward of variable-pitch production thrust performance, provides the aircraft and flies forward propulsive force. See fig. 2. Meanwhile, the axial direction of the hundred-direction flat paddles can also finely adjust and deflect leftwards and rightwards, so that a yaw control effect is provided. The function of controlling the yaw is that the function of the hundred-direction flat rotor is completely different from the function of the double-top rotor fixed tail rotor propulsion helicopter in the research.

The hundred-direction flat paddles can be arranged at the front end of the aircraft besides being arranged at the rear end of the aircraft to be used as tail paddles. Unlike the tail rotor, the fore-end paddle generally provides a pulling force, and the axial direction of the paddle becomes a direction that can rotate around the vertical paddle shaft to the right, the front, the left, and other directions. The function of the multi-directional flat paddle is basically the same, and the multi-directional flat paddle can balance the reaction force moment of a top paddle rotor wing, control yaw, provide the forward flying tension of an aircraft and the like. The various functions of the paddle can be used independently or can be superposed with the functions of other equipment devices of the aircraft. For example, the forward thrust of the feathering blade may be superimposed with the forward component of the forward flight generated by the forward tilt of the top rotor disk as the top rotor actively rotates. The invention is called a hundred-direction flat-blade helicopter because when the top blade rotor rotates passively, the hundred-direction flat blades can provide forward-flight propelling force to make the helicopter fly forward, and the helicopter in the flight state is not only a helicopter. The shaft of the unidirectional clutch can be finely adjusted according to actual requirements, is not required to be arranged vertically absolutely, and can be slightly inclined forwards, backwards, leftwards or rightwards according to actual requirements.

Compared with the common single-rotor top propeller helicopter, the multi-direction flat-propeller helicopter provided by the invention has the advantages that the multi-direction flat propellers are arranged, and when the top propeller rotor actively rotates, the yaw control force is improved, and the forward flight propelling force is increased. When the top propeller rotor wing passively rotates, the front-flying propelling force of the aircraft can be provided, the yaw control force is provided, and the front-flying lifting force efficiency of the aircraft can be improved. Compared with the double-rotor top propeller reinforced fixed tail rotor propulsion helicopter which is researched, the yaw control capability is provided, the lateral flight capability of the aircraft is improved, and a differential variable pitch device in the double rotors can be omitted when necessary.

The invention relates to a hundred-direction flat-blade helicopter, which has the advantages that: it is proposed to connect the output end of the hundred-direction driver to the hundred-direction flat paddle by arranging the hundred-direction driver in the drive system of the hundred-direction flat paddle. The output end of the hundred-direction driver is controlled to rotate around the axle of the hundred-direction clutch through the hundred-direction control device, so that the axial direction of the hundred-direction flat paddle can be controlled to rotate around the axle of the hundred-direction clutch in the process of driving the power to the hundred-direction flat paddle, and the power points to the required direction. The aircraft has the advantages that the performances of yaw control and the like are improved, the forward flight propelling force is increased, particularly, the performance that the multi-direction flat propellers flexibly change direction to propel the aircraft to fly forwards when the top propeller rotor rotates passively is realized, and the lift efficiency of the aircraft to fly forwards can be improved.

Drawings

Fig. 1 is a schematic view of a single-rotor top-paddle vertical lift aircraft with the top paddle pointing in the axial direction of the top paddle when the front top paddle rotor is actively rotating. The aircraft comprises an aircraft body 1, a top propeller rotor 2, a hundred-direction flat propeller disc cone 3, a hundred-direction driver 4 and a hundred-direction clutch shaft which are vertical. The single rotor top paddles rotate clockwise in the figure.

Fig. 2 is a schematic top view of a hundred-direction flat-blade helicopter with the hundred-direction flat blades pointing axially when the front top-flying rotor rotates passively. The aircraft comprises an aircraft body 1, a top propeller rotor disk cone 2, a hundred-direction flat propeller disk cone 3, a hundred-direction driver 4 and a hundred-direction clutch shaft which are vertical.

Fig. 3 is a schematic side view of a single-rotor top paddle vertical lift aircraft with the axial direction of the hundred flat paddles pointing when the front top paddle rotor rotates passively. The aircraft comprises an aircraft body 1, a top propeller rotor 2, a hundred-direction flat propeller disc cone 3, a hundred-direction driver 4 and a hundred-direction clutch shaft which are vertical. Wherein part of power is transmitted to the hundred-direction flat paddle from the transmission system through the tail beam and the hundred-direction driver.

Fig. 4 is a schematic diagram of the equidirectional transfer hundreds-directional transmission, and is a schematic diagram of the embodiment 1 of the invention as in fig. 1, 2 and 3. The equidirectional transfer case adopts a variable linear speed double-layer star planet row, and the unidirectional combiner adopts a bevel gear single-layer star planet row with the characteristic parameter of 1.0. The axial line of a paraxial bevel gear 1 which inputs NA1 to the input end is kept horizontal, the homodromous transfer case 2, the one-way commutator 3 and the universal joint case shaft 4 are kept vertical, an outer gear ring is arranged on the turnover control end 5, the two-way output end 6 and a paraxial connection 7 which is used for adjusting two rotating speeds of the two-way output end and converting the two rotating speeds into two rotating speeds of coaxial reverse rotation also revolve around the universal joint case shaft, and a paraxial input gear 8 which is meshed with the outer gear ring can input NA2 to the turnover control end to control turnover. The autorotation rotating speeds of the two planetary wheels output by the two-way output end are finally converted into two coaxial reverse rotating speeds which can be connected to a coaxial reverse hundred-direction flat paddle.

Fig. 5 is a schematic diagram of the equidirectional transfer double-control hundred-direction driver. The input end 1, one transfer end 2, the other transfer end 3, a bevel gear 4 fixed by a bearing, one input end and output end 5 of a homodromous clutch, the other input end and output end 6 of the homodromous clutch, an outer gear ring is arranged at a central input end 7, a paraxial gear 8 meshed with the outer gear ring at the central input end can input rotating speed NA2 to the central input end, one central wheel 9 of a hundred-direction clutch, the other central wheel 10 of the hundred-direction clutch, a turnover control end 11 and a one-way output end 12. Wherein the equidirectional transfer case composed of the components 1, 2 and 3 adopts a variable linear speed double-layer star planet row. 5. The homodromous clutch composed of the components shown in 6 and 7 adopts a variable linear speed double-layer star planet row. Wherein the back end connection is a first connection mode. The central wheels 9 and 10 of the bevel gear single-layer star planet row adopted by the unidirectional clutch have the same tooth number, and the single-path output end 12 is used for connecting the unidirectional flat paddle. The part shown in 4 is a bevel gear fixed by a bearing of the one-way commutator.

FIG. 6 is a schematic view of a dual flow hundred direction actuator according to the present invention. The device comprises a reverse input end 1, a same-direction input end 2, a sun gear (a central wheel) 3, a planet carrier 4, an inner gear ring (another central wheel) 5, a central wheel 6 of a unidirectional clutch, another central wheel 7 of the unidirectional clutch, a turnover control end 8 and an output end 9. Wherein the components shown in 3, 4 and 5 form a variable linear speed double-layer planet row. Wherein the back end connection adopts a second connection mode. 6. The counter actuator consisting of the components shown in 7, 8 and 9 adopts a bevel gear single-layer star planetary row, and the component shown in 9 in the counter actuator is a double-path output end.

Fig. 7 is a schematic view of a reverse transfer hundreds transmission of the invention. The input end 1, one of the split ends 2, the other of the split ends 3, one of the central wheels 4, the other of the central wheels 5 and the turnover control end 6 are provided with an external gear ring, and the output end 7 and a paraxial gear 8 meshed with the external gear ring can input rotating speed NA2 to the turnover control end. Wherein the reverse transfer case composed of the components 1, 2 and 3 adopts a variable linear speed double-layer star planet row. The central wheels 4 and 5 of the bevel gear single-layer star planet row adopted by the unidirectional clutch have the same tooth number, and 7 is a single-path output end for connecting the unidirectional flat paddle.

Fig. 8 is a schematic diagram of a reverse transfer double-control hundred-direction driver according to the invention. The input end 1, one transfer end 2, the other transfer end 3, one input end output end 4 of the homodromous clutch, the other input end output end 5 of the homodromous clutch, the central input end 6 is provided with an outer gear ring, a paraxial gear 7 meshed with the outer gear ring of the central input end can input rotating speed NA2 to the central input end, one central wheel 8 of the unidirectional clutch, the other central wheel 9 of the unidirectional clutch, an epicyclic control end 10 and a unidirectional output end 11. Wherein the reverse transfer case composed of the components 1, 2 and 3 adopts a variable linear speed double-layer star planet row. 4. 5 and 6 adopts a variable linear speed double-layer star planet row. Wherein the back end connection is a first connection mode. The central wheels 8 and 9 of the bevel gear single-layer star planet row adopted by the unidirectional clutch have the same tooth number, and 11 is a single-path output end for connecting the unidirectional flat paddle.

The top paddle rotor in fig. 2 and the hundred-direction flat paddles in fig. 1, 2 and 3 are all drawn as triangles to illustrate the cone of the paddle wheel when the rotor is under force. The components in fig. 4 are illustrated in a simplified overall configuration. The rows of planet components in fig. 5, 6, 7, 8 are illustrated schematically in half-frame construction, as is conventional in the industry. The components are only schematic in relation to each other and do not reflect actual dimensions.

Detailed Description