Fixed wing VTOL unmanned aerial vehicle
阅读说明:本技术 固定翼垂直起降无人机 (Fixed wing VTOL unmanned aerial vehicle ) 是由 梁煜 单肖文 于 2020-07-30 设计创作,主要内容包括:本发明公开了一种固定翼垂直起降无人机,包括机身主体、外翼、尾翼、驱动部,外翼设置有两个,对称设置于机身主体两侧,尾翼呈V型对称连接于机身主体的尾部,驱动部用于提供飞行动力,与机身主体和/或外翼连接。本发明中,无人机能够在驱动部的驱动下进行起降、悬停、飞行,通过在机身主体尾端设置V型尾翼,降低无人机飞行控制的难度并增加俯仰配平能力,从而提高无人机的俯仰偏航稳定性及操控性,并且通过尾翼的风标效应,减小了无人机的迎风面积,提高了无人机的抗风性。(The invention discloses a fixed-wing vertical take-off and landing unmanned aerial vehicle which comprises a main body, two outer wings, tail wings and driving parts, wherein the two outer wings are symmetrically arranged on two sides of the main body, the tail wings are symmetrically connected to the tail part of the main body in a V shape, and the driving parts are used for providing flight power and are connected with the main body and/or the outer wings. According to the unmanned aerial vehicle, the unmanned aerial vehicle can take off and land, hover and fly under the driving of the driving part, the V-shaped empennage is arranged at the tail end of the main body of the unmanned aerial vehicle, the flying control difficulty of the unmanned aerial vehicle is reduced, and the pitching balancing capacity is improved, so that the pitching yawing stability and the controllability of the unmanned aerial vehicle are improved, the windage area of the unmanned aerial vehicle is reduced through the weathercock effect of the empennage, and the wind resistance of the unmanned aerial vehicle is improved.)
1. Fixed wing VTOL unmanned aerial vehicle, its characterized in that includes:
a main body of the body;
two outer wings are arranged and symmetrically arranged on two sides of the fuselage main body;
two empennages are arranged and symmetrically connected to the tail part of the machine body main body in a V shape;
and the driving part is used for providing flight power and is connected with the fuselage main body and/or the outer wing.
2. The fixed-wing VTOL unmanned aerial vehicle of claim 1, wherein the outer wing is fused with the fuselage body.
3. The fixed-wing VTOL UAV of claim 2, wherein the upper contour lines of the outer wing and the fuselage body are S-shaped.
4. The fixed-wing VTOL unmanned aerial vehicle of claim 1, wherein the drive section comprises a plurality of rotors, the rotors being rotatable.
5. The fixed-wing VTOL UAV of claim 4, wherein the rotor is mounted at the outer wing leading edge and the aft end of the fuselage body.
6. The fixed-wing VTOL UAV of claim 5, wherein each of the outer wings has the rotor connected thereto, the rotor being symmetric with respect to the fuselage body.
7. A fixed-wing VTOL UAV according to any of claims 4-6, wherein the rotor can tilt with respect to the fuselage body and/or the outer wing to change its plane of rotation.
8. The fixed-wing VTOL UAV of any of claims 4-6, wherein the rotor is foldable.
9. The fixed-wing VTOL UAV of any one of claims 5-6, wherein a tail section extends from the tail of the fuselage body, the tail wing and the rotor wing being mounted to the tail section.
10. The fixed-wing VTOL unmanned aerial vehicle of claim 1, further comprising an energy system housed within the outer wing and/or the fuselage body.
Technical Field
The invention relates to the technical field of flight equipment, in particular to a fixed-wing vertical take-off and landing unmanned aerial vehicle.
Background
The body of the traditional fixed-wing unmanned aerial vehicle hovers in a vertical state, the wind resistance of the body is poor, the length of the body of the unmanned aerial vehicle is limited to avoid side turning, and the aerodynamic layout of the unmanned aerial vehicle is limited; or although vertical take-off and landing are adopted, the flying wing layout of the airframe, wings and other pneumatic components of the fixed-wing unmanned aerial vehicle is unreasonable, so that the unmanned aerial vehicle has low pneumatic efficiency and poor stability and operability during flying.
Disclosure of Invention
The present invention is directed to solving at least one of the problems of the prior art. Therefore, the invention provides a fixed-wing vertical take-off and landing unmanned aerial vehicle which can improve the flight stability of the unmanned aerial vehicle.
One embodiment of the present invention provides a fixed-wing vertical take-off and landing unmanned aerial vehicle, including:
a main body of the body;
two outer wings are arranged and symmetrically arranged on two sides of the fuselage main body;
two empennages are arranged and symmetrically connected to the tail part of the machine body main body in a V shape;
and the driving part is used for providing flight power and is connected with the fuselage main body and/or the outer wing.
The fixed-wing vertical take-off and landing unmanned aerial vehicle in the embodiment of the invention at least has the following beneficial effects:
according to the unmanned aerial vehicle, the unmanned aerial vehicle can take off and land, hover and fly under the driving of the driving part, the V-shaped empennage is arranged at the tail end of the main body of the unmanned aerial vehicle, the flying control difficulty of the unmanned aerial vehicle is reduced, and the pitching balancing capacity is improved, so that the pitching yawing stability and the controllability of the unmanned aerial vehicle are improved, the windage area of the unmanned aerial vehicle is reduced through the weathercock effect of the empennage, and the wind resistance of the unmanned aerial vehicle is improved.
According to the fixed-wing VTOL UAV of other embodiments of the present invention, the outer wing is fused with the fuselage body.
According to the fixed-wing VTOL UAV of other embodiments of the present invention, the upper side contour lines of the outer wing and the fuselage body are S-shaped.
According to other embodiments of the invention, the drive portion comprises a plurality of rotary wings, and the rotary wings can rotate.
According to other embodiments of the invention, the fixed-wing VTOL UAV has the rotor wings mounted on the leading edge of the outer wing and the tail end of the fuselage body.
According to the fixed-wing VTOL UAV of other embodiments of the present invention, each outer wing is connected with the rotor, and the rotors are symmetrical relative to the main body.
According to the fixed-wing VTOL UAV of other embodiments of the present invention, the rotor can tilt relative to the fuselage body and/or the outer wing to change the rotation plane of the rotor.
According to the fixed-wing VTOL drones of further embodiments of the present invention, the rotor can be folded.
According to the fixed-wing VTOL UAV, the tail part of the main body extends out of the tail section, and the tail wing and the rotor wing are installed on the tail section.
According to other embodiments of the invention, the fixed-wing VTOL UAV further comprises an energy system, wherein the energy system is accommodated in the outer wing and/or the fuselage body.
Drawings
FIG. 1 is a schematic structural view of a fixed-wing VTOL UAV of the present invention in a flight state;
FIG. 2 is a schematic structural view of a fixed-wing VTOL UAV of the present invention in another flight state;
FIG. 3 is a schematic structural view of the fixed-wing VTOL UAV of the present invention in other flight states;
FIG. 4 is a schematic structural view of the fixed-wing VTOL UAV of the present invention in other flight states;
fig. 5 is a schematic structural diagram of the fixed-wing VTOL UAV of the present invention in other flight states.
Description of reference numerals:
a
a
drive
Detailed Description
The concept and technical effects of the present invention will be clearly and completely described below in conjunction with the embodiments to fully understand the objects, features and effects of the present invention. It is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments, and those skilled in the art can obtain other embodiments without inventive effort based on the embodiments of the present invention, and all embodiments are within the protection scope of the present invention.
In the description of the embodiments of the present invention, if an orientation description is referred to, for example, the orientations or positional relationships indicated by "upper", "lower", "front", "rear", "left", "right", etc. are based on the orientations or positional relationships shown in the drawings, only for convenience of describing the present invention and simplifying the description, but not for indicating or implying that the referred device or element must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the present invention.
In the description of the embodiments of the present invention, if a feature is referred to as being "disposed", "fixed", "connected", or "mounted" to another feature, it may be directly disposed, fixed, or connected to the other feature or may be indirectly disposed, fixed, connected, or mounted to the other feature. In the description of the embodiments of the present invention, if "a number" is referred to, it means one or more, if "a plurality" is referred to, it means two or more, if "greater than", "less than" or "more than" is referred to, it is understood that the number is not included, and if "greater than", "lower" or "inner" is referred to, it is understood that the number is included. If reference is made to "first" or "second", this should be understood to distinguish between features and not to indicate or imply relative importance or to implicitly indicate the number of indicated features or to implicitly indicate the precedence of the indicated features.
Fig. 1 is a schematic structural diagram illustrating a flight state of a fixed-wing vertical take-off and landing drone, and referring to fig. 1, the fixed-wing vertical take-off and landing drone in this embodiment includes a
In this embodiment, unmanned aerial vehicle can take off and land, hover, fly under the drive of
In addition, in this embodiment,
In this embodiment, the
In addition, it should be noted that, unmanned aerial vehicle in this embodiment adopts and fuses wing body and the 300 compound mode of V type fin, the unmanned aerial vehicle that mixes wing body and fuses outer wing overall arrangement can improve more than 50% than conventional VTOL unmanned aerial vehicle lift-drag ratio under the same speed, when unmanned aerial vehicle meets the crosswind, because the extra aerodynamic force that fin 300 weathercock effect produced changes flight resistance into, because the pneumatic overall arrangement lift-drag ratio of unmanned aerial vehicle in this embodiment is great, unmanned aerial vehicle's resistance is compared in other aerodynamic force a lot less, thereby unmanned aerial vehicle's wind-resistance has been improved.
The driving
All be connected with
In addition, in this embodiment, the rear portion of the
In fig. 1, a state diagram of the vertical take-off and landing and hovering phases of the drone is shown, the rotation plane of the
In addition,
Fig. 2 shows unmanned aerial vehicle is at VTOL or hover state to the structural sketch of the state transition state that flies of level, and this in-process, front and
Fig. 3 shows unmanned aerial vehicle at the structural schematic diagram of the flat state of flying, after unmanned aerial vehicle accelerates to predetermineeing speed,
Because
In addition, in this embodiment, the
It should be noted that the tilting and folding of
In addition, still can install the cloud platform on the unmanned aerial vehicle, carry on the camera element on the cloud platform, the record can be shot to unmanned aerial vehicle's the condition of cruising to the camera element, still can set up control element, GPS inductive element etc. on the unmanned aerial vehicle, is convenient for acquire unmanned aerial vehicle's flight information and positional information.
The embodiments of the present invention have been described in detail with reference to the accompanying drawings, but the present invention is not limited to the above embodiments, and various changes can be made within the knowledge of those skilled in the art without departing from the gist of the present invention. Furthermore, the embodiments of the present invention and the features of the embodiments may be combined with each other without conflict.
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