CN211139663U - Catch formula VTOL formula unmanned aerial vehicle - Google Patents
Catch formula VTOL formula unmanned aerial vehicle Download PDFInfo
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- CN211139663U CN211139663U CN201922330538.XU CN201922330538U CN211139663U CN 211139663 U CN211139663 U CN 211139663U CN 201922330538 U CN201922330538 U CN 201922330538U CN 211139663 U CN211139663 U CN 211139663U
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- fixedly connected
- unmanned aerial
- aerial vehicle
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- fuselage
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Abstract
The utility model discloses a formula of arresting VTOL formula unmanned aerial vehicle, the reciprocating impact tunnel drilling machine comprises a machine body, turn right in proper order wing and the fin that the symmetry set up around fixedly connected with from a left side in the fuselage outside, wing lower extreme fixedly connected with connecting rod, the screw that the connecting rod upper end was rotated and is connected with the bilateral symmetry and sets up, turn right in proper order fixedly connected with singlechip and battery from a left side at the inside top lower extreme of fuselage, fixedly connected with signalling and receiving module on the singlechip, the micro motor that bottom upper end fixedly connected with bilateral symmetry set up in the fuselage. This formula of arresting VTOL formula unmanned aerial vehicle catches through the net transmitter of arresting in fuselage below installation, has improved unmanned aerial vehicle's functionality, is convenient for in time catch the operation after the discovery target, has improved unmanned aerial vehicle's practicality, improves the accuracy of the position of arresting, shortens the time of arresting, improves the integrality and the security of camera, and the protection casing is transparent design, does not influence the shooting effect of camera.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a formula of arresting VTOL formula unmanned aerial vehicle.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, and has the advantages of small volume, low manufacturing cost, convenient use, low requirement on the operational environment, strong battlefield viability and the like.
Unmanned aerial vehicle is in police usefulness, city management, agriculture, geology, weather, look a plurality of fields such as screen shooting and by wide use, but current unmanned aerial vehicle function singleness generally can only carry out the transmission of image, can not grab the operation, and the practicality is low, and the camera exposes externally, damages easily, reduces life's shortcoming.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a formula of arresting is played perpendicularly and is fallen formula unmanned aerial vehicle to propose the function singleness in solving above-mentioned background, generally can only carry out the transmission of image, can not arrest the operation, the practicality is low, and the camera exposes externally, damages easily, reduces life's problem.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a formula of arresting VTOL formula unmanned aerial vehicle, includes the fuselage, wing and the fin that the symmetry set up around turning right from a left side in proper order fixedly connected with in the fuselage outside, wing lower extreme fixedly connected with connecting rod, the screw that is connected with bilateral symmetry setting is rotated to the connecting rod upper end, the inside top lower extreme of fuselage turns right from a left side in proper order fixedly connected with singlechip and battery, fixedly connected with signalling and receiving module on the singlechip, the micro motor that bottom upper end fixedly connected with bilateral symmetry set up in the fuselage.
Preferably, the equal fixedly connected with of fuselage left and right sides lower extreme front and back symmetry setting mount pad, it is connected with the axis of rotation to rotate between mount pad and another corresponding mount pad, the axis of rotation lower extreme fixedly connected with connecting seat and undercarriage in proper order, be provided with the belt between axis of rotation and micro motor.
Preferably, the undercarriage is of an isosceles trapezoid structure, the width of the lower end of the undercarriage is larger than that of the undercarriage body, the distance from the undercarriage to the other undercarriage is larger than the sum of the heights of the undercarriage and the other undercarriage, and the tail wing is designed in an inclined mode.
Preferably, the camera and the capture net emitter are fixedly connected to the middle of the lower end of the machine body from left to right in sequence, the protective cover is fixedly connected to the outer side of the camera at the lower end of the machine body and made of transparent acrylic, the height of the camera and the height of the capture net emitter are smaller than that of the undercarriage, and the diameters of the camera and the capture net emitter are smaller than the width of the upper end of the undercarriage.
Preferably, the capturing net emitter is internally and fixedly connected with a small gas cylinder, the lower end of the capturing net emitter is movably connected with a capturing net, the lower end of the capturing net emitter is provided with symmetrically arranged limiting grooves, and the capturing net is fixedly connected with limiting blocks which are clamped and connected with the limiting grooves.
Compared with the prior art, the beneficial effects of the utility model are that:
1. according to the capture type vertical take-off and landing unmanned aerial vehicle, the capture net emitter is arranged below the unmanned aerial vehicle body, so that the functionality of the unmanned aerial vehicle is improved, capture operation can be performed in time after a target is found, and the practicability of the unmanned aerial vehicle is improved;
2. according to the capture type vertical take-off and landing unmanned aerial vehicle, the shooting direction of the camera is consistent with the transmitting direction of the capture net transmitter, and after a target is found, the capture net transmitter can be directly opened for capture, so that the accuracy of a capture position is improved, and the capture time is shortened;
3. this formula of arresting VTOL formula unmanned aerial vehicle is provided with the protection casing in the camera outside, effectively protects the camera, improves the integrality and the security of camera, and the protection casing is transparent design, does not influence the shooting effect of camera.
Drawings
FIG. 1 is a schematic perspective view of the present invention;
FIG. 2 is a schematic front view of the present invention;
FIG. 3 is a schematic side view of the present invention;
FIG. 4 is a schematic sectional view of the present invention;
fig. 5 is an enlarged schematic structural diagram of a in fig. 4 according to the present invention.
In the figure: 1. a body; 2. an airfoil; 3. a tail wing; 4. a connecting rod; 5. a propeller; 6. a single chip microcomputer; 7. a storage battery; 8. a signal transmitting and receiving module; 9. a micro motor; 10. a mounting seat; 11. a rotating shaft; 12. a connecting seat; 13. a landing gear; 14. a belt; 15. a camera; 16. catching a net emitter; 17. a protective cover; 18. a small gas cylinder; 19. catching the net; 20. a limiting groove; 21. and a limiting block.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-5, the present invention provides a technical solution: a catching type vertical lifting unmanned aerial vehicle comprises a body 1, wings 2, a tail wing 3, a connecting rod 4, propellers 5, a single chip microcomputer 6, a storage battery 7, a signal transmitting and receiving module 8, a micro motor 9, a mounting seat 10, a rotating shaft 11, a connecting seat 12, an undercarriage 13, a belt 14, a camera 15, a catching net emitter 16, a protective cover 17, a small gas cylinder 18, a catching net 19, a limiting groove 20 and a limiting block 21, wherein the wings 2 and the tail wing 3 which are symmetrically arranged front and back are fixedly connected with the outer side of the body 1 from left to right in sequence, the lower end of each wing 2 is fixedly connected with the connecting rod 4, the upper end of each connecting rod 4 is rotatably connected with the propellers 5 which are symmetrically arranged left and right, the single chip microcomputer 6 and the storage battery 7 are fixedly connected with the inner top of the body 1 from left to right in sequence, the signal transmitting and receiving module 8 is fixedly connected with, the single chip microcomputer 6 and the storage battery 7 are electrically connected with the camera 15, the micro motor 9 and the capturing net emitter 16, the model of the single chip microcomputer 6 is STC89C52, the model of the storage battery 76-CNF-38 is SPIDER-N, and the installation mode and the circuit connection are not described in detail;
furthermore, the lower ends of the left side and the right side of the unmanned aerial vehicle body 1 are fixedly connected with mounting seats 10 which are symmetrically arranged in the front-back direction, a rotating shaft 11 is rotatably connected between the mounting seat 10 and the other corresponding mounting seat 10, the lower end of the rotating shaft 11 is sequentially and fixedly connected with a connecting seat 12 and an undercarriage 13, a belt 14 is arranged between the rotating shaft 11 and the micro motor 9, and the rotating shaft 11 is driven to rotate by the micro motor 9, so that the undercarriage 13 is accommodated, the occupied area of the unmanned aerial vehicle during working is reduced, and the safety is higher;
furthermore, the undercarriage 13 is in an isosceles trapezoid structure, the width of the lower end of the undercarriage 13 is greater than that of the airframe 1, the distance between the undercarriage 13 and the other undercarriage 13 is greater than the sum of the heights of the undercarriage 13 and the other undercarriage 13, the empennage 3 is in an inclined design, and the undercarriage 13 adopts the isosceles trapezoid design, so that the supporting performance of the airframe 1 is improved, and the stability of the airframe 1 is ensured;
furthermore, a camera 15 and a catching net emitter 16 are fixedly connected to the middle of the lower end of the unmanned aerial vehicle body 1 from left to right in sequence, a protective cover 17 is fixedly connected to the outer side of the camera 15 at the lower end of the unmanned aerial vehicle body 1, the protective cover 17 is made of transparent acrylic, the heights of the camera 15 and the catching net emitter 16 are both smaller than the height of the undercarriage 13, the diameters of the camera 15 and the catching net emitter 16 are both smaller than the width of the upper end of the undercarriage 13, and the functionality of the unmanned aerial vehicle is improved through the design of the catching net emitter 16;
furthermore, a small gas bottle 18 is fixedly connected in the catching net emitter 16, a catching net 19 is movably connected at the lower end of the catching net emitter 16, limiting grooves 20 which are symmetrically arranged are formed in the lower end of the catching net emitter 16, limiting blocks 21 which are connected with the limiting grooves 20 in a clamping mode are fixedly connected at the upper end of the catching net 19, and the limiting blocks 21 are pushed out of the limiting grooves 20 through the impact force of the small gas bottle 18, so that the catching net 19 falls down to perform catching operation.
The working principle is as follows: firstly, a limiting block 21 on a catching net 19 is plugged into a limiting groove 20 at the lower end of a catching net emitter 16, the unmanned aerial vehicle is placed on the ground through an undercarriage 13, then the unmanned aerial vehicle is connected with an external control terminal through a signal transmitting and receiving module 8, the machine body 1 is driven to ascend under the action of a propeller 5, a micro motor 9 is started, a rotating shaft 11 is driven to rotate under the action of a belt 14, a connecting seat 12 at the lower end of the rotating shaft 11 rotates inwards to store the undercarriage 13, a camera 15 shoots in real time and sends a shot picture to the external control terminal, after a catching target is found, the catching net emitter 16 is opened through a singlechip 6, the limiting block 21 is pushed out from the limiting groove 20 under the action of pressure of a small air bottle 18, the catching net 19 moves downwards to catch the target, then the unmanned aerial vehicle is controlled to return, and when the unmanned aerial vehicle approaches the ground, the micro motor 9 is controlled by the single chip microcomputer 6 to rotate reversely, so that the undercarriage 13 is put down, and the stability of the unmanned aerial vehicle is ensured.
It should be finally noted that the above only serves to illustrate the technical solution of the present invention, and not to limit the scope of the present invention, and that simple modifications or equivalent replacements performed by those skilled in the art to the technical solution of the present invention do not depart from the spirit and scope of the technical solution of the present invention.
Claims (5)
1. The utility model provides a formula of arresting VTOL formula unmanned aerial vehicle, includes the fuselage, its characterized in that: the fuselage outside turns right wing and the fin that symmetry set up around fixedly connected with in proper order from a left side, wing lower extreme fixedly connected with connecting rod, the screw that is connected with bilateral symmetry and sets up is rotated to the connecting rod upper end, turn right fixedly connected with singlechip and battery in proper order from a left side to the inside top lower extreme of fuselage, fixedly connected with signal transmission and receiving module on the singlechip, the micro motor that bottom upper end fixedly connected with bilateral symmetry set up in the fuselage.
2. A capture type vertical take-off and landing unmanned aerial vehicle according to claim 1, wherein: the fuselage left and right sides lower extreme equal fixedly connected with front and back symmetry set up the mount pad, it is connected with the axis of rotation to rotate between mount pad and another corresponding mount pad, the axis of rotation lower extreme fixedly connected with connecting seat and undercarriage in proper order, be provided with the belt between axis of rotation and micro motor.
3. A capture type vertical take-off and landing unmanned aerial vehicle according to claim 2, wherein: the undercarriage is of an isosceles trapezoid structure, the width of the lower end of the undercarriage is larger than that of the undercarriage body, the distance from the undercarriage to the other undercarriage is larger than the sum of the heights of the undercarriage and the other undercarriage, and the tail wing is designed in an inclined mode.
4. A capture type vertical take-off and landing unmanned aerial vehicle according to claim 2, wherein: the camera is fixedly connected with the middle of the lower end of the machine body in sequence from left to right, the outer side of the camera at the lower end of the machine body is fixedly connected with a protective cover, the protective cover is made of transparent acrylic, the height of the camera and the height of the catching net transmitter are smaller than that of the undercarriage, and the diameters of the camera and the catching net transmitter are smaller than the width of the upper end of the undercarriage.
5. A capture type vertical take-off and landing unmanned aerial vehicle according to claim 4, wherein: the catching net type gas cylinder is characterized in that a small gas cylinder is fixedly connected in the catching net transmitter, a catching net is movably connected at the lower end of the catching net transmitter, limiting grooves which are symmetrically arranged are formed in the lower end of the catching net transmitter, and limiting blocks which are connected with the limiting grooves in a clamping mode are fixedly connected to the catching net.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922330538.XU CN211139663U (en) | 2019-12-23 | 2019-12-23 | Catch formula VTOL formula unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922330538.XU CN211139663U (en) | 2019-12-23 | 2019-12-23 | Catch formula VTOL formula unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211139663U true CN211139663U (en) | 2020-07-31 |
Family
ID=71746698
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922330538.XU Expired - Fee Related CN211139663U (en) | 2019-12-23 | 2019-12-23 | Catch formula VTOL formula unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211139663U (en) |
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2019
- 2019-12-23 CN CN201922330538.XU patent/CN211139663U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200731 Termination date: 20201223 |
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| CF01 | Termination of patent right due to non-payment of annual fee |