阅读说明：本技术 一种无源单人穿戴踏翼飞行器 (Passive single-person wearable pedal-wing aircraft ) 是由 万定仁 于 2020-05-13 设计创作，主要内容包括：一种无源单人穿戴踏翼飞行器,其特征在于：其包含<Image he="52" wi="51" file="DSA0000208758490000011.GIF" imgContent="drawing" imgFormat="GIF" orientation="portrait" inline="no"></Image>加强关节翼；<Image he="53" wi="51" file="DSA0000208758490000012.GIF" imgContent="drawing" imgFormat="GIF" orientation="portrait" inline="no"></Image>可调节框架；<Image he="52" wi="51" file="DSA0000208758490000013.GIF" imgContent="drawing" imgFormat="GIF" orientation="portrait" inline="no"></Image>翼迎角控制和阻尼滑动套；<Image he="54" wi="51" file="DSA0000208758490000018.GIF" imgContent="drawing" imgFormat="GIF" orientation="portrait" inline="no"></Image>多功能操控杆；<Image he="53" wi="52" file="DSA0000208758490000017.GIF" imgContent="drawing" imgFormat="GIF" orientation="portrait" inline="no"></Image>推拉吊环杆；<Image he="53" wi="52" file="DSA0000208758490000015.GIF" imgContent="drawing" imgFormat="GIF" orientation="portrait" inline="no"></Image>并串式铰簧驱动、储存、缓冲器；<Image he="54" wi="52" file="DSA00002087584900000110.GIF" imgContent="drawing" imgFormat="GIF" orientation="portrait" inline="no"></Image>后踏式驱动支架；<Image he="52" wi="51" file="DSA0000208758490000019.GIF" imgContent="drawing" imgFormat="GIF" orientation="portrait" inline="no"></Image>离合、档位、传动结构；<Image he="53" wi="52" file="DSA0000208758490000016.GIF" imgContent="drawing" imgFormat="GIF" orientation="portrait" inline="no"></Image>后踏往复式钢索驱动扇形轮；<Image he="53" wi="52" file="DSA0000208758490000014.GIF" imgContent="drawing" imgFormat="GIF" orientation="portrait" inline="no"></Image>人体结构辅助架；多数结构采用双单元多构件相互关联又互不影响设计,如某单元或构件出故障并不影响飞行或降落,动力来源：利用人体踩踏输出动能来振动双翼,在地面储存动能以满足其起飞较大动能的需求,辅助架辅助飞行续能；其包含有扑翼、三角翼和固定滑翔翼的特点,故又可称之为‘三合一’单人穿戴飞行器,其有结构简单精巧,方便操控,重量轻等优点,可作为交通、旅游、娱乐、健身等工具。(A passive single-person wearing pedal-wing aircraft is characterized in that: which comprises Strengthening the joint wing; an adjustable frame; a wing attack angle control and damping sliding sleeve; a multifunctional joystick; pushing and pulling the suspension loop rod; parallel-serial type hinge spring driverA moving, storing, buffering device; a rear pedal type driving bracket; clutch, gear and transmission structure; back stepping reciprocating steel cable to drive sector wheel; a human body structure auxiliary frame; most structures adopt a design that double units and multiple components are mutually associated and do not influence each other, for example, if a certain unit or component fails, the flight or landing is not influenced, and a power source is as follows: the double wings are vibrated by outputting kinetic energy through treading of a human body, the kinetic energy is stored on the ground to meet the requirement of large takeoff kinetic energy, and the auxiliary frame assists in flying energy continuation; it includes the characteristics of flapping wings, delta wings and fixed gliding wings, so that it can be called as three-in-one single-person wearable aircraft, and its structure is simple and exquisite, convenient to operate and control, light in weight and can be used as means for traffic, travelling, recreation and body-building, etc..)

1. A passive single-person wearing pedal-wing aircraft is characterized in that: which comprisesStrengthening the joint wing;an adjustable frame;a wing attack angle control and damping sliding sleeve;

2. A passive single-person wearable tread aircraft, in accordance with claim 1, said:strengthening the joint wing: adopt 'primary and secondary wing' wing body and the design of three section wing stem, every aileron has adjustable damping spring, and its function is the biggest pressure differential that produces when letting flapping from top to bottom, and female wing adopts the trapezoidal wing stem of three section, can divide into in wing root, the wing (power arm) and fin, and the wing root has rotatable 60 degrees to the straight spring damping joint, can change flapping radian radius and length from top to bottom, its function: the symmetrical adjustment is gear adjustment, which can be divided into a first gear and a second gear, the asymmetrical adjustment is left-right balance adjustment and fine adjustment, and the control arms are arranged on the left side and the right side of the wing; the wing middle part root is a sliding lever slideway, the wing middle part and the tail wing are connected by a reinforced damping buffering joint, the wing middle part and the tail wing are composed of a positioning joint, a reinforced buffering joint, a buffering arm, a damping arm, a buffering damping spring, an adjustable PE wheel and other components, the joint is a damper when lifting the wing, the joint is a buffer when flapping the wing, and each buffering and damping arm is provided with an adjustable screw and can adjust the buffering and damping angles.

3. A passive single-person wearable pedal aircraft, as claimed, said: the reinforced damping buffer joint comprises a positioning joint, a reinforced damping joint, a buffer arm, a damping arm, a buffer damping spring, an adjustable PE wheel and other members, and as the members are important wear members, the functions of each member are separately designed, and the positioning joint only has a positioning function; the ultimate buffering function is achieved when the buffering joint is a flapping wing; when the wing is lifted, the joint is a damper, when the wing is flapping, the joint is a buffer, each buffering and damping arm is provided with an adjustable screw, the buffering and damping angle can be adjusted, and the force of the buffering and damping arms can be adjusted to form a PE wheel.

4. A passive single-person wearable pedal aircraft, as claimed in, wherein: in the above-mentioned manner,the adjustable frame: the upper back strap plate of the frame is adjusted by screws; the two sides of the middle part are provided with driving hanging wheel rails, and wing attack angle control and damping sliding sleeve fixing teeth are arranged at the upper parts of the rails; the left side and the right side are symmetrically provided with a control rod, a belt board mounting column and a fixing column, and the fixing column is provided with a mounting groove and a fixing tooth socket for adjusting the size of the control rod and the belt board so as to be convenient for people of different body types to wear; the lower part of the middle of the frame is provided with an adjustable cable guide wheel at a corresponding position.

5. A passive single-person wearable pedal aircraft, as claimed in, wherein: in the above-mentioned manner,wing angle of attack control and damping sliding sleeve: the upper part of the sliding sleeve is a synchronous shaft with a fixed wheel and a brake wheel, the upper teeth of the hanging wheel track are occluded between the fixed wheel and the frame, only the brake block is pushed to brake the brake wheel, the sliding sleeve is fixed on the frame, otherwise, the sliding is carried out, the lower synchronous shaft is the same, except that the lower synchronous shaft is not fixed on the frame but fixed on a 'U' -shaped groove of the push-pull hanging ring rod, the brake block is only pushed to ensure that the lower synchronous shaft is fixed on the frame and the push-pull hanging ring rod to be converted, the two brake blocks are mutually associated, one of the two brake blocks is a time-delay conversion brake block to prevent dislocation, a brake cable is used for braking, and the multifunctional control rod is used for front knob; the outside of the wing attack angle control and damping sliding sleeve is in occlusion with a sector gear on a parallel-serial hinge spring drive, storage and buffer, and when the sliding sleeve is fixed on a frame, the sliding sleeve is in a wing working state and a state of pushing a push-pull lifting ring rod to rotate a wing, and is fixed on the push-pull lifting ring rod in a translational wing state; a damping spring is arranged between the cylindrical teeth of the sliding sleeve and the sliding sleeve, a common spring is arranged on the upper part of the sliding sleeve, a controllable gas spring is arranged on the lower part of the sliding sleeve, the damping spring has the functions that thrust is generated when the flapping wing generates lift force, a certain attack angle is generated when the wing and the flapping wing are lifted, the lift force lost when the wing is lifted is reduced, forward thrust is increased when the wing is lifted, and the gas spring is controlled to determine the damping magnitude, namely, whether the sliding sleeve flies upwards or forwards is controlled; the structure is a symmetrical structure.

6. Root of herbaceous plantA passive single-person wearable pedal aircraft, as claimed, wherein: in the above-mentioned manner,a multifunctional joystick; the left side is provided with an operating panel, the side surface of the panel is provided with a clutch and gear operating handle which controls a clutch, gear and transmission structure to push a cable handle, and a brake cable is used for braking, so that first-gear transmission, second-gear transmission and neutral gear can be realized; the front side of the control plate is provided with a common brake handle mounting rod, the brake handle is connected with directional brake handles at two sides of the parallel-serial hinge spring driving, storing and buffering device, and a brake cable is used for braking and has the function of fixing the gliding wing by switching the flapping wing; the right side is provided with a multifunctional control rod, the root part of the rod body is provided with a self-locking forward and reverse gear set which consists of a bilateral reverse gear and two pairs of unilateral reverse gears, one of the bilateral reverse gears is fixed, the other one of the bilateral reverse gears can move left and right, the unilateral reverse gears are pressed by a spring, a square shaft is arranged in the middle of the reverse gear set, the bilateral reverse gears are fixed with the control rod, a round-rotating square conversion pad is arranged between the bilateral reverse gears and the square shaft and can rotate independently, a jackscrew is fixed and cannot move left and right, the bilateral movable unilateral reverse gears are synchronously rotated with the square shaft, and the two pairs of unilateral reverse gears move left and right and are mutually associated to achieve the functions of forward reverse locking and reverse forward locking of the up-down swinging control rod; the square shaft is provided with two transmission gears at corresponding positions, the transmission gears are meshed with a U-shaped groove pushing gear tooth hole of a push-pull lifting ring rod, and a push-pull driver is used, the function is generally used in the lifting and triangular wing states, so the lifting rod can be called as a lifting rod, the function I is a function I, a function II is a function II, a function III is a function III, a fixed drive and a function III are locked, the control rod is in a failure state in a normal state, the drive and the function IV; this structure is a single structure.

7. A passive single-person wearable pedal aircraft, as claimed in, wherein: in the above-mentioned manner,

8. A passive single-person wearable pedal aircraft, as claimed in, wherein: in the above-mentioned manner,a parallel-serial type hinge spring driving, storing and buffering device; a double-group three-nine-joint hinge spring is adopted, so that kinetic energy which is released by 0.6-0.4 horsepower per second for 2-3 minutes can be stored; the double-group three-parallel nineteen-linkage hinge springs are released when taking off, three plane scroll springs are connected in parallel in a 'convex' strip box, nineteen 'convex' strip boxes are connected in series to form a group, and then the two groups are connected in parallel to form the double-group three-parallel nineteen-linkage hinge springs; the two groups of hinge springs are internally provided with a positioning shaft and a rotating shaft, and the outside of the two groups of hinge springs is provided with a fixed shaft which is connected by a bridge; directional brake pads are arranged in the inner shafts of the strip boxes at the outer ends of the two groups of hinged springs, and directional brake actuators are arranged at corresponding positions of the outer shafts of the hinged springs and have the functions of flapping-wing conversion fixed wings and delta wings; the rotating shaft is connected with an eccentric shaft bearing force terminal on the rotary driving handle driving sliding lever; the wing root fixing shaft and the joint damping straight spring are arranged in the middle of the hinge spring group; a cylindrical tooth fan-shaped positioning wheel is arranged towards the inner side and meshed with the cylindrical teeth outside the sliding sleeve, and the function of the positioning wheel is fixed wing, rotating wing and wing attack angle damping; the eccentric shaft bearing force terminal is a left eccentric bearing force terminal and a right eccentric bearing force terminal which are designed on a sliding bearing, and the bearing radius is changed, so that the flapping wing speed is high, and the wing lifting speed is low; the left and right sides of the structure are mirror images.

9. A passive single-person wearable pedal aircraft, as claimed in, wherein: the hinge springs are connected in series; the structure of the spring is that a plurality of plane spiral springs and a specially-made convex barrel form a series-connected spring, the number and the size of the parallel plane spiral springs determine the magnitude of the pre-stored torque force of the spring, the number of the series-connected convex barrel determines the pre-stored stroke of the spring, the more the springs are connected in series, the longer the pre-stored stroke is, and the defects that the pre-stored torque force and the pre-stored stroke are limited by the size of the traditional barrel are overcome.

10. A passive single-person wearable pedal aircraft, as claimed in, wherein: in the above-mentioned manner,a rear-pedal type adjustable driving bracket; the main functions of the device are supporting and fixing, and the angle can be adjusted; the middle part is a clutch, gear and reverse actuator on the upper side of the reverse gear on three sides of the input shaft of the transmission structure; the lower part is provided with a clutch, gear and transmission structure mounting bracket; it is a symmetrical structure.

11. A passive single-person wearable pedal aircraft, as claimed in, wherein: in the above-mentioned manner,

12. According to the claimsThe passive single-person wearing pedal-wing aircraft is characterized in that: in the above-mentioned manner,

13. A passive single-person wearable pedal aircraft, as claimed in, wherein: in the above-mentioned manner,an auxiliary frame for adjusting human body structure; the device consists of a sliding rod, a sliding terminal, a pedal, a joint and the like; the pedal is connected with a pedal sector forward and backward steel cable driving wheel steel cable; the joints are provided with a abandoning and starting switch, so that the legs of the human body can only do treading actions no matter the human body is upright or prone after the starting, the legs can move freely after the abandoning of the function, and the main function is to solve the problem that the human body structure is not suitable for flying; this structure is a mirror image structure.

Technical Field

The invention relates to a passive single-person wearing pedal-wing aircraft, which comprises the characteristics of flapping wings, delta wings and fixed gliding wings, so the passive single-person wearing pedal-wing aircraft can be called as a three-in-one single-person wearing aircraft, has the advantages of simple and exquisite structure, convenient operation and control, light weight and the like, and can be used as tools for transportation, travel, entertainment, body building and the like.

Background

The energy efficiency of the flapping wing flight mode is several times that of a fixed wing aircraft and a rotary wing aircraft, and even larger, however, the flapping wing manned flight has not been realized so far. Human beings do not stop the manpower flight research and manufacture ever and do not stop afterwards, and countless modern, recent and ancient research and manufacture people, such as the following "western costs prize" (centuries data), cannot fly to the sky?

The western skis prize awards:

the american helicopter association (american helicoptersociety) on day 7/12 in 2013 indicates that a human-powered helicopter manufactured by the canadian team AeroVelo is a work that has historically won the $ 25 million engineering jackpot on the 1 st time. The winning Atlas (Atlas) man-powered helicopter has 4 rotors with a diameter of 20.4 meters, a widest part of 58 meters, a total length of about 49.4 meters, and a weight of only 52 kilograms, and one person pedals a carbon fiber bicycle to drive the rotors to rotate. It flies in 6 months and 13 days, rises to 3.3 meters from the ground, stays in the air for 64.11 seconds, and lands 7 meters away from the takeoff. After about one month technical review, the helicopter association officially awarded the prize in 2013, 7 and 11 months. The design team AeroVelo consists of approximately 20 students and young experts at the university of toronto (university of toronto). The design team created one of the people cameron robertson who said that about 1 horse power was required to "drive" the helicopter, while the average person might only be able to send out about half horse power, so the "pilot" needs to be robust while not weighing more than 73 kg. This helicopter is "piloted" by the captain of the team, toddler (ToddReichert). He was 31 years old now and is an aerodynamic specialist and a fast skating team. The american helicopter association executed the new society of law on richeck hickey (MikeHirschberg)2013, 7 months and 12 days: "this has been considered an impossible task. "

Most of the conclusions are drawn that the manpower flight is not realizable, just like the first perpetual motion machine, so the perpetual motion machine cannot be realized and is limited by the law of conservation of energy, but the perpetual motion machine cannot be limited by the sentence of 'unrealizable' and cannot be limited by the manpower flight like the law of conservation of energy, and the manpower flight is possible as long as the aircraft is light enough and flexible enough to overcome the defect that the human body structure is not suitable for flying.

Disclosure of Invention

In view of the above, the present invention provides a passive single-person wearable pedal-wing aircraft, comprising:

strengthening the joint wing;

an adjustable frame;

a wing attack angle control and damping sliding sleeve;a multifunctional joystick;

pushing and pulling the suspension loop rod;a parallel-serial type hinge spring driving, storing and buffering device;a rear pedal type driving bracket;

clutch, gear and transmission structure;back stepping reciprocating steel cable to drive sector wheel;

a human body structure auxiliary frame; most structures adopt a design that double units and multiple components are mutually associated and do not influence each other, for example, if a certain unit or component fails, the flight or landing is not influenced, and a power source is as follows: the double wings are vibrated by outputting kinetic energy through treading of a human body, the kinetic energy is stored on the ground to meet the requirement of large takeoff kinetic energy, and the auxiliary frame assists in flying energy continuation; it includes the characteristics of flapping wings, delta wings and fixed gliding wings, so that it can be called as three-in-one single-person wearable aircraft, and its structure is simple and exquisite, convenient to operate and control, light in weight and can be used as means for traffic, travelling, recreation and body-building, etc..

Drawings

Fig. 1, fig. 2, fig. 3, and fig. 4 are schematic perspective views of a passive single-person wearing pedal-wing aircraft according to the present invention, fig. 1 is a rear view of a flat wing, fig. 2 is a right view of an angle of attack wing, fig. 3 is a front view of the angle of attack wing, and fig. 4 is a partially enlarged view of human wearing effect; FIG. 5 and FIG. 6 are schematic perspective views of two pedaling modes of a passive single-person wearing pedal-wing aircraft according to the present invention; FIG. 7 is a schematic view of a reinforced knuckle wing structure; FIGS. 18 and 19 are views showing the state of the flapping wings; FIG. 8 is an exploded view of a mechanical structure of a passive single-person-worn pedal-wing aircraft, wherein the structures are labeled as follows:

strengthening the joint wing;

an adjustable frame;

a wing attack angle control and damping sliding sleeve;a multifunctional joystick;pushing and pulling the suspension loop rod;

a parallel-serial type hinge spring driving, storing and buffering device;

a rear pedal type driving bracket;clutch, gear and transmission structure;back stepping reciprocating steel cable to drive sector wheel;

human body structure auxiliary frame.

The following are marked three-dimensional schematic diagrams and descriptions of various structural components of the passive single-person wearable pedal aircraft machinery of the invention:

figure 7 is a view of the present invention showing a passive single-person wearing treaded aircraft,

the reinforced joint wing has a perspective view, and the structural components in the figure are marked as follows:

Strengthening joint, middle wing (power arm), root, back wing and tail wing.

Figure 7-1 is a view showing a passive single-person-worn pedal-wing aircraft according to the present invention,

schematic perspective view of reinforced jointThe structural components in the figure are labeled as follows:

the damping device comprises a damping angle adjusting screw, a damping prismatic spring, a PE wheel capable of adjusting spring force, a positioning joint and a damping spring.

Figure 7-2 is a view showing a passive single-person wearing treading aircraft,the reinforced joint is a perspective view, and the structural components in the figure are marked as follows:

a sliding lever slideway, a wing control handle, a wing root straight spring damping wheel,

in the above-mentioned manner,

strengthening the joint wing: referring to fig. 7, 7-1 and 7-2, the design of 'primary and secondary wing' body and three-section wing stem is adopted, each secondary wing is provided with an adjustable damping spring, the function is to generate the maximum pressure difference when flapping up and down, the primary wing adopts three-section trapezoidal wing stem and can be divided into a wing root, a wing middle (power arm) and a tail wing, the wing root is provided with a straight spring damping joint capable of rotating 60 degrees, the radius and the length of the radian of flapping up and down can be changed, and the function is as follows: the symmetrical adjustment is gear adjustment, which can be divided into a first gear and a second gear, the asymmetrical adjustment is left-right balance adjustment and fine adjustment, and the control arms are arranged on the left side and the right side of the wing; the wing middle part root is a sliding lever slideway, the wing middle part and the tail wing are connected by a reinforced damping buffering joint, the wing middle part and the tail wing are composed of a positioning joint, a reinforced buffering joint, a buffering arm, a damping arm, a buffering damping spring, an adjustable PE wheel and other components, the joint is a damper when lifting the wing, the joint is a buffer when flapping the wing, and each buffering and damping arm is provided with an adjustable screw and can adjust the buffering and damping angles.

FIGS. 9 and 9-1 show a passive single-person wearing pedal-wing aircraft,the adjustable frame is a schematic perspective view, and the structural components in the figure are marked as follows:

a sling mount, a driving hanging wheel track, a sliding sleeve fixed tooth, a safety belt main buckle, a control rod, a belt board mounting column, a control rod, a belt board fixing column, a waist protection plate, a waist belt main buckle, a cable guide wheel and a belt board,

a slidable fixing groove is installed on the base,the teeth are fixed.

In the above-mentioned manner,the adjustable frame: referring to fig. 9 and 9-1, the upper strap plate of the frame is adjusted by screws; the two sides of the middle part are provided with driving hanging wheel rails, and wing attack angle control and damping sliding sleeve fixing teeth are arranged at the upper parts of the rails; the left side and the right side are symmetrically provided with a control rod, a belt board mounting column and a fixing column, and the fixing column is provided with a mounting groove and a fixing tooth socket for adjusting the size of the control rod and the belt board so as to be convenient for people of different body types to wear; the lower part of the middle of the frame is provided with an adjustable cable guide wheel at a corresponding position.

FIGS. 10 and 10-1 show a passive single-person wearing pedal-wing aircraft,the wing attack angle control and damping sliding sleeve is a schematic perspective view, and the structural components in the drawing are marked as follows:

a fixed wheel, a sliding sleeve, a column tooth, a cable control handle, a synchronous shaft, a sliding brake wheel, an angle-variable damping spring, an angle-variable damping gas spring,

The time-delay conversion brake block is provided with a brake block,a brake pad.

In the above-mentioned manner,wing angle of attack control and damping sliding sleeve: referring to fig. 10 and 10-1, the upper part of the sliding sleeve is a synchronizing shaft with a fixed wheel and a brake wheel, the upper teeth of the hanging wheel track are occluded between the fixed wheel and the frame, only the brake block is needed to be pushed to brake the brake wheel, the sliding sleeve is fixed on the frame, otherwise, the lower synchronizing shaft slides, the lower synchronizing shaft is the same, the difference is that the lower synchronizing shaft is not fixed on the frame but fixed on a 'U' -shaped groove of a push-pull hanging ring rod, the lower synchronizing shaft can be switched between the frame and the push-pull hanging ring rod only by pushing the brake block, the two brake blocks are mutually associated, one of the brake blocks is a time-delay switching brake block to prevent dislocation, a brake cable is used for braking, and the front twist handle of the multifunctional control rod is; the outside of the wing attack angle control and damping sliding sleeve is in occlusion with a sector gear on a parallel-serial hinge spring drive, storage and buffer, and when the sliding sleeve is fixed on a frame, the sliding sleeve is in a wing working state and a state of pushing a push-pull lifting ring rod to rotate a wing, and is fixed on the push-pull lifting ring rod in a translational wing state; a damping spring is arranged between the cylindrical teeth of the sliding sleeve and the sliding sleeve, a common spring is arranged on the upper part of the sliding sleeve, a controllable gas spring is arranged on the lower part of the sliding sleeve, the damping spring has the functions that thrust is generated when the flapping wing generates lift force, a certain attack angle is generated when the wing and the flapping wing are lifted, the lift force lost when the wing is lifted is reduced, forward thrust is increased when the wing is lifted, and the gas spring is controlled to determine the damping magnitude, namely, whether the sliding sleeve flies upwards or forwards is controlled; the structure is a symmetrical structure.

FIGS. 11 and 11-1 show a passive single-person wearing pedal-wing aircraft,

the multifunctional control rod is a schematic perspective view, and structural components in the figure are marked as follows:

firstly, a front twisting handle (a translational wing elevation angle synchronous conversion twisting handle), a rear twisting handle (a forward and reverse gear wheel reversing twisting handle), a control rod, a subsidiary crutch mounting rod, a self-locking forward and reverse gear wheel group, a clutch and gear control handle, a waist belt plate, a locking plate with adjustable size, a control handle, a square shaft and a push wheel of the third,the common brake handle is provided with a rod,the pushing wheel is arranged on the upper portion of the frame,the control gear piece is arranged on the gear box,

a rotating wheel is arranged at the bottom of the rotating wheel,and installing a fixing screw.

In the above-mentioned manner,a multifunctional joystick; referring to fig. 11 and 11-1, the left side is a control plate, the side of the plate is a clutch and gear control handle, which controls the clutch, gear and transmission structure to push a cable handle, and the brake cable to brake can be divided into first gear transmission, second gear transmission and neutral gear; the front side of the control plate is provided with a common brake handle mounting rod, the brake handle is connected with directional brake handles at two sides of the parallel-serial hinge spring driving, storing and buffering device, and a brake cable is used for braking and has the function of fixing the gliding wing by switching the flapping wing; the right side is provided with a multifunctional control rod, the root part of the rod body is provided with a self-locking forward and reverse gear set which consists of a bilateral reverse gear and two pairs of unilateral reverse gears, one of the bilateral reverse gears is fixed, the other one of the bilateral reverse gears can move left and right, the unilateral reverse gears are pressed by a spring, a square shaft is arranged in the middle of the reverse gear set, the bilateral reverse gears are fixed with the control rod, a round-rotating square conversion pad is arranged between the bilateral reverse gears and the square shaft and can rotate independently, a jackscrew is fixed and cannot move left and right, the bilateral movable unilateral reverse gears are synchronously rotated with the square shaft, and the two pairs of unilateral reverse gears move left and right and are mutually associated to achieve the functions of forward reverse locking and reverse forward locking of the up-down swinging control rod; two transmission gears are arranged at corresponding positions of the square shaft, the transmission wheel is meshed with a tooth hole of a U-shaped groove pushing wheel of a push-pull lifting ring rod, and a push-pull driver has the function of The lifting rod is generally used in a lifting and delta wing state, and can be called as a lifting rod, wherein the lifting rod has a first function, a vertical translation driving function and double wings, a second function, a vertical rolling driving function and double wings, and a third function, a fixed driving function and double wings are locked; this structure is a single structure.

Figure 12 is a view of the present invention showing a passive single-person-worn pedal aircraft,the push-pull lifting ring rod is a three-dimensional schematic diagram, and the structural components in the diagram are marked as follows:

the lifting wheel, the drive frame angle adjusting screw, the drive ring, the push-pull U-shaped groove and the push-pull wheel tooth hole.

In the above-mentioned manner,push-and-pull hanging ring rod: referring to fig. 13, for connecting the driver and the frame, the root of the hanging wheel is a 'U' shaped slot with a tooth hole of the pushing wheel for pushing and pulling the driver and the wing attack angle control and damping sliding sleeve; this structure is a mirror image structure.

Figure 13 is a view of the present invention showing a passive single-person-worn pedal aircraft,the parallel-serial type hinge spring driving, storing and buffering device is a three-dimensional schematic diagram, and the structural components in the diagram are marked as follows:

a synchronous rotating shaft, a rotary driving handle, a hinge spring positioning shaft, a bearing, a hinge spring strip box, a directional brake sheet, a brake handle, a damping straight spring of the wing root, a tooth sector positioning wheel of a column shape and a wing root fixed shaft, A back wing mounting plate is arranged on the back wing,

wing root damping straight spring adjusterThe screw is arranged on the screw rod and is connected with the screw rod,

the driving outer sleeve is bridged and connected with the driving outer sleeve,the lever is slid to move the lever,the eccentric shaft bears a force terminal,

the positioning wheel is arranged on the base plate,

a plane scroll spring is connected in parallel with the flat spiral spring,the 'convex' barrel can be connected in series.

In the above-mentioned manner,

a parallel-serial type hinge spring driving, storing and buffering device; referring to FIG. 13, a double set of three and nineteen jointed spring is used which can store kinetic energy at 0.6-0.4 horsepower per second for 2-3 minutes; the double-group three-parallel nineteen-linkage hinge spring is released when the aircraft takes off, three plane scroll springs are connected in parallel in a 'convex' strip box, nineteen 'convex' strip boxes are connected in series to form a group, and then the two groups are connected in parallel to form the aircraft engine, the number of the parallel plane scroll springs can be selected according to the required torque force, the more the number is, the larger the torque force is, the more the number is, the serial connection number of the 'convex' strip boxes determines the stroke of the spring, and the more the serial connection is, the longer the stroke is; the two groups of hinge springs are internally provided with a positioning shaft and a rotating shaft, and the outside of the two groups of hinge springs is provided with a fixed shaft which is connected by a bridge; directional brake pads are arranged in the inner shafts of the strip boxes at the outer ends of the two groups of hinged springs, and directional brake actuators are arranged at corresponding positions of the outer shafts of the hinged springs and have the functions of flapping-wing conversion fixed wings and delta wings; the rotating shaft is connected with an eccentric shaft bearing force terminal on the rotary driving handle driving sliding lever; the wing root fixing shaft and the joint damping straight spring are arranged in the middle of the hinge spring group; then the inner side is positioned in a cylindrical sector shape The wheel is meshed with the outer cylindrical teeth of the sliding sleeve and has the functions of fixed wing, rotating wing and wing attack angle damping; the eccentric shaft bearing force terminal is a left eccentric bearing force terminal and a right eccentric bearing force terminal which are designed on a sliding bearing, and the bearing radius is changed, so that the flapping wing speed is high, and the wing lifting speed is low; the left and right sides of the structure are mirror images.

The hinge springs are connected in series; referring to fig. 13, the structure of the spring is that a plurality of spiral springs and specially-made convex-shaped barrels can be connected in series, the number and size of the parallel spiral springs determine the magnitude of the pre-stored torque force of the spring, and the number of the series convex-shaped barrels determines the stroke of the pre-stored torque force.

Figure 14 is a view of the present invention showing a passive single-person-worn pedal aircraft,

the back-stepping type driving bracket is a schematic perspective view, and the structural components in the drawing are marked as follows:

the chain pitch adjusting device comprises a reverse gear reverse actuator, an angle adjusting screw hole, a driving fixed bearing, a clutch, gear and transmission structure mounting bracket, a clutch, gear and transmission structure bearing mounting plate and a chain pitch adjusting screw.

In the above-mentioned manner,a rear-pedal type adjustable driving bracket; please refer to fig. 14, which mainly functions to support and fix, and adjust the angle; the middle part is a clutch, gear and reverse actuator on the upper side of the reverse gear on three sides of the input shaft of the transmission structure; the lower part is provided with a clutch, gear and transmission structure mounting bracket; it is a symmetrical structure.

FIG. 15 and FIG. 15-1 show a passive single-person wearing pedal-wing aircraft,the three-dimensional schematic diagram of the clutch, gear and transmission structure is characterized in that the structural components are marked as follows:

kinetic energy input shaft, bilateral retrograde tooth kinetic energy output shaft, bearing sleeve flange, bearing, hinged spring strip box inner shaft, anda retrograde chain wheel with a slot on one side, an independent chain at gear position, a chain wheel pushing and associating plate, a retrograde tooth shaft wheel at three sides, a pushing shaft at the r,the pushing execution piece is pushed to the front end of the machine body,

the rope handle is pushed and sent out,a pedal steel cable sector drive wheel bearing,

the chain wheel is prevented from falling off,the movable unilateral retrograde gear wheel is provided with a gear wheel,the movable unilateral retrograde roller cone spring.

In the above-mentioned manner,

clutch, gear and transmission structure; referring to fig. 15 and 15-1, the middle of the output shaft is a bilateral retrograde gear shaft wheel; the middle of the input shaft is provided with a three-side retrograde tooth shaft wheel; the chain transmission adopts a first-gear independent chain and a second-gear independent chain, the input and output chain wheels both adopt separable single-side reverse gear wheels, the chain wheels can slide left and right, the middle part is provided with a chain wheel pushing column and a relevant plate to form a transmission chain set, two groups of chain wheels share one pushing column and the relevant plate is fixed together, a shaft is arranged in the middle, a middle shaft is rotated to push the two groups of transmission chain sets to slide left and right, a brake cable is braked and controlled on a left control plate, when the chain wheels are pushed to the left, the left chain set is combined with the right chain set into a first gear, the other direction is a second gear, the middle part is a neutral position, the torque of the input chain wheel is larger than that of the output chain set into the first gear, otherwise, the double chains; it is of a double structure.

FIG. 16 is a drawing of the present inventionProvides a passive single-person wearing pedal-wing aircraft,

the back stepping reciprocating type steel cable driving sector wheel is a schematic perspective view, and the structural components in the figure are marked as follows:

the reverse gear transmission device comprises a pedal reciprocating sector steel cable driving wheel, a return wheel strip spring, a fixed unilateral reverse gear and a steel cable.

In the above-mentioned manner,back stepping on the sector forward and backward steel cable driving wheel; referring to fig. 16, a pedal sector reciprocating steel cable driving wheel is adopted, a fixed reverse gear is arranged on the outer side, a return wheel plane spiral spring and a barrel are arranged on the inner side, and the arc length of a sector wheel is the stroke of the pedal steel cable plus the stroke of driving the vertical movement; this structure is a mirror image structure.

Figure 17 is a view of the present invention showing a passive single-person wearing treaded aircraft,

the human body structure auxiliary frame is a schematic perspective view, and the structural components in the figure are marked as follows:

the automatic foot pedal device comprises a switch, a joint, an auxiliary spring, a shank bandage, a waistband board connector, a sliding rod bearing, a steel rope fixing end and an automatic foot pedal.

In the above-mentioned manner,

an auxiliary frame for adjusting human body structure; please refer to fig. 18, which is composed of a slide rod, a slide terminal, a pedal, a joint, etc.; the pedal is connected with a pedal sector forward and backward steel cable driving wheel steel cable; the joints are provided with a abandoning and starting switch, so that the legs of the human body can only do treading actions no matter the human body is upright or prone after the starting, the legs can move freely after the abandoning of the function, and the main function is to solve the problem that the human body structure is not suitable for flying; this structure is a mirror image structure.

The flapping wings are aircrafts manufactured by human beings in a flight mode simulating birds or insects;

the fixed glider is arranged at high altitude, and under the condition of no wind, the glider obtains forward power by means of self gravity in downward gliding flight;

the delta wing depends on the fixed wing, and under the condition of wind, the kite principle is utilized to generate lift force under the action of constantly changing gravity center and attack angle so as to fly upwards.

The flapping wing has the advantages of energy efficiency in flying, but in the flying stage, the flapping wing needs great kinetic energy as other aircrafts, so the flapping wing aircraft takes off by adopting the storage prestress hinged spring, is made of light materials, has the weight of less than 17kg as well as the weight of about 70kg of human body, has the total weight of 87kg, has the wing area load rate of about 12kg and is in defense with hawks, so the flapping speed is low in the absence of power, the sinking speed is also slow, and the flapping wing aircraft can land safely. The flight has three modes (flapping wings, fixed gliding wings and delta wings), the pedal wings can adopt two modes, please refer to fig. 5 and fig. 6, the horizontal vertical pedal wings generally keep horizontal flight, the output force of the inclined vertical pedal wings is larger, because a part of the self weight is used, the flight is more suitable for ascending flight, the three flight modes and the two pedal wing modes can be randomly switched, and the operation is simple.

Description of the operation

First step, wear the aircraft: locking plate handles on the waistband plates on the two sides are broken off by two hands, the size is adjusted, the locking plate handles are automatically locked by loosening the hands, the pedal plate is buckled, and a safety belt and a small binding belt are fastened;

step two, preparation and energy continuation: adjusting the attack angle and the position of the wing by using the control lever, adjusting the braking state (the wing has a small angle to buffer and is externally fixed), abandoning the auxiliary frame (the leg can move freely), setting the flapping wing gear on the 1 gear, setting the transmission gear on the 2 gear, stepping on the original place for about 500 steps, selecting the 1 gear for the transmission gear to continue for about 300 steps, and continuing for driving for about 6-4 minutes;

thirdly, taking off and flying: the transmission gear is pushed to a neutral position, the leg part does not have any load except the elastic force of a steel cable return rope at the moment, the running is carried out for about 10 meters, if wind exists, the running is carried out against the wind, the speed is enough to release the brake, the kinetic energy in the driver is released to start flapping wings, the attack angle and the position of the wings are adjusted by using the control lever, meanwhile, the transmission gear is pushed to a 1 gear, the oblique and vertical pedaling wings are adopted to drive to continue energy continuation, the wing control handle is used for controlling balance to start flying, at the moment, the auxiliary frame can be started, the pedaling mode and the flying mode are selected, and the flapping wing gear is selected; the brake is that the fixed wing glides, utilize control lever to adjust wing position and attack angle to make it rise to become the delta wing in the course of gliding;

Step four, landing: the brake is in a fixed gliding state, treading is performed to supply driving energy, after continuous energy supply is finished, an auxiliary frame is abandoned, a transmission gear is pushed to a neutral gear, the direction is adjusted by using a wing control handle to select landing, when 5-3 meters away from the ground, the brake is released, driving, storage and buffer kinetic energy are stored, the brake is released, the brake is operated for 3-2 times, and the wing is braked again, and meanwhile, the position and the attack angle of the wing are adjusted to land.

Description of the embodiments

The aircraft has the advantages of simple and exquisite structure, flexibility, convenient operation and control, light weight and the like, and can be used as tools for transportation, travel, entertainment, body building and the like. Can install electronic helping hand additional, also can reequip unmanned aerial vehicle or military aircraft, partial braking can change into pneumatic or hydraulic braking. Because the wing adopts the design that the wing can be conveniently disassembled, the shape of a bird wing can be simulated, one machine is matched with a plurality of wings, and speed type double wings or load type double wings are selected and matched according to the requirements.

The above description is only an embodiment of the present invention, and is not intended to limit the scope of the present invention, and the present invention is not limited by the additional assistance, any modification, and change of application, and all the suburb structures or suburb changes made by using the contents of the present specification and the accompanying drawings, or directly or indirectly applied to other related technical fields, are included in the scope of the present invention.