CN219970017U - Anti-interference device of composite wing unmanned aerial vehicle - Google Patents

Anti-interference device of composite wing unmanned aerial vehicle Download PDF

Info

Publication number
CN219970017U
CN219970017U CN202321251075.8U CN202321251075U CN219970017U CN 219970017 U CN219970017 U CN 219970017U CN 202321251075 U CN202321251075 U CN 202321251075U CN 219970017 U CN219970017 U CN 219970017U
Authority
CN
China
Prior art keywords
unmanned aerial
aerial vehicle
plate
wing unmanned
interference device
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202321251075.8U
Other languages
Chinese (zh)
Inventor
尚威威
李杨霞
程继伟
贾艺飞
窦晓阳
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanxi Guanghan Yunchuang Digital Technology Co ltd
Original Assignee
Shanxi Guanghan Yunchuang Digital Technology Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shanxi Guanghan Yunchuang Digital Technology Co ltd filed Critical Shanxi Guanghan Yunchuang Digital Technology Co ltd
Priority to CN202321251075.8U priority Critical patent/CN219970017U/en
Application granted granted Critical
Publication of CN219970017U publication Critical patent/CN219970017U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

The utility model discloses an anti-interference device of a compound wing unmanned aerial vehicle, which relates to the technical field of unmanned aerial vehicles and comprises a machine body, wherein connecting blocks are fixedly arranged on two sides of the machine body, a fixed plate is fixedly arranged on the outer side of each connecting block, a protection plate is movably arranged on the back surface of each fixed plate, a diversion trench is formed in the top of the surface of each protection plate, an arc-shaped curved surface is arranged on the surface of each diversion trench, and the cross section of each diversion trench is rectangular. This compound wing unmanned aerial vehicle anti-interference device connects and fixes the fixed plate through installation connecting block convenient to use person, and after the fixed plate installation, the user is convenient for install drive arrangement and guard plate, and the user is installed the guard plate through, can prevent effectively after the installation that the organism from appearing producing the phenomenon of damage because of receiving the collision of flying bird in the in-process of flight, has promoted the stability of device in the use and security thereof effectively.

Description

Anti-interference device of composite wing unmanned aerial vehicle
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to an anti-interference device of a compound wing unmanned aerial vehicle.
Background
Unmanned aerial vehicle is abbreviated as "unmanned aerial vehicle", english abbreviation "UAV", is unmanned aerial vehicle that utilizes radio remote control equipment and self-contained program control device to operate, can divide into from technical angle definition: unmanned fixed wing aircraft, unmanned multi-rotor aircraft, unmanned helicopter, unmanned parachute wing aircraft, and the like.
The Chinese patent discloses a compound wing unmanned aerial vehicle (grant bulletin No. CN 106394856B), the technology of the patent comprises a wing body fusion body, a fixed wing part, a multi-rotor wing part, a landing gear, a propeller and a power mechanism, wherein the fixed wing part comprises two fixed wings which are respectively arranged at two sides of the wing body fusion body; the multi-rotor part comprises a plurality of rotor mechanisms which are symmetrically arranged at two sides of the wing body fusion body, each rotor mechanism comprises a connecting rod and a rotor, the connecting rods are connected with the fixed wings, the rotors are horizontally arranged on the connecting rods, the connecting rods are provided with mounting shafts which are perpendicular to the axial direction of the connecting rods, and the end parts of the mounting shafts are provided with first inclined planes; the fixed wing is provided with a connecting hole matched with the mounting shaft, the hole wall of the connecting hole is provided with a clamping groove, a telescopic buckle is arranged in the clamping groove, and the mounting shaft is provided with a groove matched with the telescopic buckle. The fixed wing part and the multi-rotor wing part of the unmanned aerial vehicle can realize rapid mounting and dismounting of the unmanned aerial vehicle, but the existing compound wing unmanned aerial vehicle is not provided with an anti-interference device in the use process, so that the device is easily damaged due to the influence of flying birds in the flight process, the working efficiency and the working progress of the device in the use process are seriously influenced, and inconvenience is brought to users.
Disclosure of Invention
The utility model aims to provide an anti-interference device of a compound wing unmanned aerial vehicle, which aims to solve the technical problems that the prior compound wing unmanned aerial vehicle provided in the background art is not provided with the anti-interference device in the use process, so that the device is easily damaged due to the influence of flying birds in the flight process, the working efficiency and the working progress of the device in the use process are seriously influenced, and inconvenience is brought to users.
In order to achieve the above purpose, the specific technical scheme of the utility model is as follows: the utility model provides a compound wing unmanned aerial vehicle anti-interference device, includes the organism, the equal fixed mounting in both sides of organism has the connecting block, the outside fixed mounting of connecting block has the fixed plate, the back movable mounting of fixed plate has the guard plate, the guiding gutter has been seted up at the top on guard plate surface, the surface of guiding gutter is provided with the arc curved surface, the cross-sectional shape of guiding gutter is the rectangle, the setting quantity of guard plate is two, the front fixed mounting of organism has the power pack.
Preferably, a protective door is movably arranged on the surface of the power box, and a driving device is arranged at the top of the fixing plate.
Preferably, the top of the driving device is fixedly connected with a rotating shaft, and the surface of the rotating shaft is fixedly provided with a mounting cylinder.
Preferably, the outside of the installation cylinder is fixedly provided with a propeller, the bottom of the machine body is fixedly provided with a bottom plate, and the surface of the bottom plate is fixedly provided with a protection pad.
Preferably, an electric plate is fixedly arranged at the middle part of the back of the machine body, and a camera is fixedly arranged at the middle part of the back of the electric plate.
Preferably, the back of the electric plate and the outer side of the camera are fixedly provided with a protective cover, and the length of the protective cover is larger than that of the camera.
Preferably, the bottom of guard plate inner chamber and extend to the front threaded connection of fixed plate have the threaded rod, the setting quantity of threaded rod is four.
The anti-interference device of the composite wing unmanned aerial vehicle has the following advantages:
1. this compound wing unmanned aerial vehicle anti-interference device connects and fixes the fixed plate through installation connecting block convenient to use person, and after the fixed plate installation, the user is convenient for install drive arrangement and guard plate, and the user is installed the guard plate through, can prevent effectively after the installation that the organism from appearing producing the phenomenon of damage because of receiving the collision of flying bird in the in-process of flight, has promoted the stability of device in the use and security thereof effectively.
2. This compound wing unmanned aerial vehicle anti-interference device opens and changes and maintains its inside battery to power pack through installing the guard gate convenient to use person, and the setting convenient to use person through the installation section of thick bamboo installs and fixes the screw, can reduce the vibrations that the organism appears in the in-process that descends effectively through the setting of protection pad, monitors the environment when being convenient for the organism when using through the installation camera, can protect the camera effectively through the installation protection casing, and fixed and spacing to the fixed plate through installation threaded rod convenient to use person.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the drawings that are needed in the embodiments will be briefly described below, it being understood that the following drawings only illustrate some examples of the present utility model and therefore should not be considered as limiting the scope, and other related drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a perspective view of the overall structure of the present utility model;
FIG. 2 is a rear perspective view of the structure of the present utility model;
FIG. 3 is a partial bottom perspective view of the structure of the present utility model;
FIG. 4 is an enlarged view of the structure A of the structure of the present utility model;
the figure indicates: 1. a body; 2. a connecting block; 3. a fixing plate; 4. a protection plate; 5. a diversion trench; 6. a power supply box; 7. a protective door; 8. a driving device; 9. a rotating shaft; 10. a mounting cylinder; 11. a propeller; 12. a bottom plate; 13. a protective pad; 14. an electric plate; 15. a camera; 16. a protective cover; 17. a threaded rod.
Detailed Description
Hereinafter, only certain exemplary embodiments are briefly described. As will be recognized by those of skill in the pertinent art, the described embodiments may be modified in numerous different ways without departing from the spirit or scope of the embodiments of the present utility model. Accordingly, the drawings and description are to be regarded as illustrative in nature and not as restrictive.
In the description of the embodiments of the present utility model, it should be understood that the terms "length," "vertical," "horizontal," "top," "bottom," and the like indicate an orientation or a positional relationship based on that shown in the drawings, and are merely for convenience in describing the embodiments of the present utility model and to simplify the description, rather than to indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the embodiments of the present utility model.
Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more such feature. In the description of the embodiments of the present utility model, the meaning of "plurality" is two or more, unless explicitly defined otherwise.
In the embodiments of the present utility model, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured" and the like are to be construed broadly and include, for example, either permanently connected, removably connected, or integrally formed; the device can be mechanically connected, electrically connected and communicated; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two elements or the interaction relationship of the two elements. The specific meaning of the above terms in the embodiments of the present utility model will be understood by those of ordinary skill in the art according to specific circumstances.
The following disclosure provides many different implementations, or examples, for implementing different configurations of embodiments of the utility model. In order to simplify the disclosure of embodiments of the present utility model, components and arrangements of specific examples are described below. Of course, they are merely examples and are not intended to limit embodiments of the present utility model. Furthermore, embodiments of the present utility model may repeat reference numerals and/or letters in the various examples, which are for the purpose of brevity and clarity, and which do not themselves indicate the relationship between the various embodiments and/or arrangements discussed.
For a better understanding of the objects, structure and function of the utility model, a further detailed description of the utility model is provided below with reference to the accompanying drawings.
As shown in fig. 1-4, the anti-interference device of the compound wing unmanned aerial vehicle comprises a machine body 1, wherein connecting blocks 2 are fixedly arranged on two sides of the machine body 1, a fixed plate 3 is fixedly arranged on the outer side of each connecting block 2, a protection plate 4 is movably arranged on the back surface of each fixed plate 3, a diversion trench 5 is formed in the top of the surface of each protection plate 4, arc-shaped curved surfaces are arranged on the surface of each diversion trench 5, the cross section of each diversion trench 5 is rectangular, the number of the protection plates 4 is two, and a power supply box 6 is fixedly arranged on the front surface of the machine body 1.
Specifically, the surface of the power supply box 6 is movably provided with a protective door 7, and the top of the fixed plate 3 is provided with a driving device 8.
Through above-mentioned technical scheme, through installing guard gate 7 convenient to use person opens power pack 6 and changes and maintains its inside battery.
Specifically, the top of drive arrangement 8 fixedly connected with pivot 9, the fixed mounting of surface of pivot 9 has a mounting cylinder 10.
Through above-mentioned technical scheme, through the setting of installation section of thick bamboo 10, the user of being convenient for installs and fixes screw 11.
Specifically, the outside of the installation cylinder 10 is fixedly provided with a propeller 11, the bottom of the machine body 1 is fixedly provided with a bottom plate 12, and the surface of the bottom plate 12 is fixedly provided with a protection pad 13.
Through the technical scheme, the vibration of the machine body 1 in the falling process can be effectively reduced through the arrangement of the protection pad 13.
Specifically, the electric plate 14 is fixedly installed in the middle of the back of the machine body 1, and the camera 15 is fixedly installed in the middle of the back of the electric plate 14.
Through above-mentioned technical scheme, be convenient for organism 1 monitor the environment when using through installation camera 15.
Specifically, the back of the electric plate 14 and the outer side of the camera 15 are fixedly provided with a protective cover 16, and the length of the protective cover 16 is greater than that of the camera 15.
Through above-mentioned technical scheme, can protect camera 15 effectively through installation protection casing 16.
Specifically, the bottom of the inner cavity of the protection plate 4 and the front surface extending to the fixing plate 3 are in threaded connection with threaded rods 17, and the number of the threaded rods 17 is four.
Through above-mentioned technical scheme, through the installation threaded rod 17, the user of being convenient for fixes fixed plate 3 spacing.
The working principle of the anti-interference device of the composite wing unmanned aerial vehicle is as follows: through installing connecting block 2 to fixed plate 3 connect and fix, after fixed plate 3 installs, the user installs drive arrangement 8 and guard plate 4, the user is through installing guard plate 4, can prevent after the installation that organism 1 from appearing producing the phenomenon damaged because of receiving the collision of flying bird in the in-process of flight, open power pack 6 and change and maintain its inside battery through installing guard gate 7 convenient to use person, install and fix screw 11 through setting up of installation section of thick bamboo 10, can reduce the vibrations that organism 1 appears at the in-process of descending through protection pad 13, can make organism 1 monitor the environment when using through installing camera 15, can protect camera 15 through installing protection casing 16, can fix and spacing fixed plate 3 through installing threaded rod 17 user.
It will be understood that the utility model has been described in terms of several embodiments, and that various changes and equivalents may be made to these features and embodiments by those skilled in the art without departing from the spirit and scope of the utility model. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the utility model without departing from the essential scope thereof. Therefore, it is intended that the utility model not be limited to the particular embodiment disclosed, but that the utility model will include all embodiments falling within the scope of the appended claims.

Claims (7)

1. The utility model provides a compound wing unmanned aerial vehicle anti-interference device, includes organism (1), its characterized in that: the utility model discloses a machine body, including connecting block (2), fixed plate (3), guiding gutter (5) have been seted up at the top on guard plate (4) surface, the surface of guiding gutter (5) is provided with the arc curved surface, the cross-sectional shape of guiding gutter (5) is the rectangle, the setting quantity of guard plate (4) is two, the front fixed mounting of machine body (1) has power pack (6).
2. The composite wing unmanned aerial vehicle anti-interference device of claim 1, wherein: the surface of the power box (6) is movably provided with a protective door (7), and the top of the fixed plate (3) is provided with a driving device (8).
3. The composite wing unmanned aerial vehicle anti-interference device of claim 2, wherein: the top of the driving device (8) is fixedly connected with a rotating shaft (9), and the surface of the rotating shaft (9) is fixedly provided with a mounting cylinder (10).
4. A compound wing unmanned aerial vehicle anti-interference device according to claim 3, wherein: the outer side of the installation cylinder (10) is fixedly provided with a propeller (11), the bottom of the machine body (1) is fixedly provided with a bottom plate (12), and the surface of the bottom plate (12) is fixedly provided with a protection pad (13).
5. The composite wing unmanned aerial vehicle anti-interference device of claim 1, wherein: an electric plate (14) is fixedly arranged at the middle part of the back of the machine body (1), and a camera (15) is fixedly arranged at the middle part of the back of the electric plate (14).
6. The composite wing unmanned aerial vehicle anti-interference device of claim 5, wherein: the back of electric plate (14) and be located the outside fixed mounting of camera (15) protection casing (16), the length of protection casing (16) is greater than the length of camera (15).
7. The composite wing unmanned aerial vehicle anti-interference device of claim 1, wherein: the front thread connection that just extends to fixed plate (3) in the bottom of guard plate (4) inner chamber has threaded rod (17), the setting quantity of threaded rod (17) is four.
CN202321251075.8U 2023-05-22 2023-05-22 Anti-interference device of composite wing unmanned aerial vehicle Active CN219970017U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202321251075.8U CN219970017U (en) 2023-05-22 2023-05-22 Anti-interference device of composite wing unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202321251075.8U CN219970017U (en) 2023-05-22 2023-05-22 Anti-interference device of composite wing unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN219970017U true CN219970017U (en) 2023-11-07

Family

ID=88594033

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202321251075.8U Active CN219970017U (en) 2023-05-22 2023-05-22 Anti-interference device of composite wing unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN219970017U (en)

Similar Documents

Publication Publication Date Title
CN205931257U (en) A motor cabinet for having more rotor unmanned vehicles
CN219970017U (en) Anti-interference device of composite wing unmanned aerial vehicle
CN113247258A (en) Unmanned aerial vehicle without rotor wing
CN107108011B (en) Unmanned plane and its horn mechanism
CN220682659U (en) Unmanned aerial vehicle anticollision safety cover
CN212850145U (en) Motor positioning mechanism
CN215098249U (en) Small-size VTOL aircraft structure
CN208102331U (en) A kind of multi-rotor unmanned aerial vehicle
CN212022976U (en) Helicopter and tail assembly thereof
CN215245561U (en) Scalable protection device of unmanned aerial vehicle
CN215514154U (en) Unmanned aerial vehicle flight buffer stop
CN207346070U (en) Based shell, rack and unmanned plane
CN214397263U (en) Fireproof plate for engine compartment of helicopter
CN214986027U (en) Variable-speed steering tail rotor of unmanned helicopter convenient to disassemble and assemble
CN219339750U (en) Rotor wing protection cover for unmanned aerial vehicle
CN112124559A (en) Aircraft wing for aerospace
CN215591016U (en) Anti-interference fixed wing type aerial survey unmanned aerial vehicle
CN205675251U (en) A kind of double-deck rotor wing unmanned aerial vehicle motor cabinet
CN220189817U (en) Energy storage battery protector
CN220448159U (en) Fuselage bearing type single-rotor unmanned aerial vehicle
CN218317317U (en) Indoor unmanned aerial vehicle with vision camera
CN214930661U (en) Be applied to drum drive structure of aircraft
CN214824086U (en) Adjustable bracket for helicopter
CN215944885U (en) Pin-connected panel VTOL unmanned aerial vehicle
CN214957210U (en) Aircraft quick detach battery structure

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant