CN213948765U - Unmanned aerial vehicle structure - Google Patents
Unmanned aerial vehicle structure Download PDFInfo
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- CN213948765U CN213948765U CN202023306986.5U CN202023306986U CN213948765U CN 213948765 U CN213948765 U CN 213948765U CN 202023306986 U CN202023306986 U CN 202023306986U CN 213948765 U CN213948765 U CN 213948765U
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- unmanned aerial
- aerial vehicle
- casing
- fixed
- vehicle structure
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Abstract
The utility model relates to an unmanned aerial vehicle structure, which comprises a housing, the bottom of casing is close to both sides edge and all installs the horizontal pole, two bottoms of horizontal pole all are fixed with the telescopic link, four the sleeve is all installed to the outside between each two of telescopic link, two telescopic bottom is close to four corners and all is fixed with the spring, and eight all welds under each four of spring has the foot rest, the bottom center department of casing installs the distancer. The utility model discloses, through the horizontal pole of chassis bottom installation to can play the effect of fixed stay bottom telescopic link, can play the effect of improving the height through adjusting four telescopic links, two telescopic bottoms are close to four corners and all are fixed with the spring, and the effect of spring can cushion the impact force that descends, and the effect of foot rest is the power dispersion that receives when making unmanned aerial vehicle descend, protects unmanned aerial vehicle's device normal operating.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to unmanned aerial vehicle structure.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. A drone is an unmanned aerial vehicle that is operated using a radio remote control device and a self-contained program control device. Unmanned aerial vehicles are in fact a general term for unmanned aerial vehicles, and can be defined from a technical perspective as follows: unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned paravane, etc. Compared with manned aircraft, it has the advantages of small volume, low cost, convenient use, low requirement on the operational environment, strong battlefield viability and the like.
But among the prior art, current unmanned aerial vehicle can lean on the foot rest to descend after taking off and landing, let foot rest direct contact ground have the impact force bounce-back, long-time taking off and landing can lead to the unmanned aerial vehicle device to damage, if the place of descending is rugged and uneven, then can directly make unmanned aerial vehicle damage after descending and lead to unable taking off, current unmanned aerial vehicle if stop in an area and shoot, only can lean on the rotation camera to shoot, the height of foot rest is fixed unchangeable, so the high effect that leads to shooting does not reach.
SUMMERY OF THE UTILITY MODEL
The utility model provides an unmanned aerial vehicle structure has solved above technical problem.
The utility model provides a scheme as follows of above-mentioned technical problem: the utility model provides an unmanned aerial vehicle structure, includes the casing, the bottom of casing is close to both sides edge and all installs the horizontal pole, two bottoms of horizontal pole all are fixed with the telescopic link, four the sleeve is all installed to the outside between each two of telescopic link, two telescopic bottom is close to four corners and all is fixed with the spring, and eight all welds under each four of spring has the foot rest, the bottom center department of casing installs the distancer.
The utility model has the advantages that: through the horizontal pole of chassis bottom installation to can play the effect of fixed stay bottom telescopic link, can play the effect that improves the height through adjusting four telescopic links, two telescopic bottoms are close to four corners and all are fixed with the spring, and the effect of spring is the impact force that can cushion the decline, and the effect of foot rest is the power dispersion that receives when making unmanned aerial vehicle descend, protects unmanned aerial vehicle's device normal operating.
On the basis of the technical scheme, the utility model discloses can also do following improvement.
Further, four sides of the casing are close to top edge and all weld there is the connecting rod, and four the movable rod, four are installed to one side of connecting rod the bracing piece is all installed to the one end of movable rod, and four the inside center department of bracing piece all is provided with motor, four the output shaft of motor all is fixed with the rotary rod, four the both sides of rotary rod all are fixed with the screw.
The beneficial effect of adopting the further scheme is that: can make unmanned aerial vehicle part folding, motor and screw can let unmanned aerial vehicle take off.
Furthermore, a rotating firmware is installed at the bottom of the casing close to one side edge, and a camera is installed at the bottom of the rotating firmware.
The beneficial effect of adopting the further scheme is that: can make unmanned aerial vehicle have the function of shooting.
Further, a heat exhaust area is arranged at the center of the top of the machine shell.
The beneficial effect of adopting the further scheme is that: can prevent that the inside heat of unmanned aerial vehicle machine from damaging machine internals.
Furthermore, a switch is installed at the edge of the outer surface center of the casing close to one side, and an indicator lamp is installed at the edge of the outer surface center of the casing close to the other side.
The beneficial effect of adopting the further scheme is that: the setting of switch can make things convenient for the start-up of artificial control unmanned aerial vehicle, and the pilot lamp can conveniently indicate the artificial unmanned aerial vehicle of controlling.
Further, a fixed block is installed at the top of the machine shell close to one side edge, and an antenna is installed at the top of the fixed block.
The beneficial effect of adopting the further scheme is that: make things convenient for wireless connection to control unmanned aerial vehicle.
Further, a base is fixed on the inner bottom surface of the inner portion of the shell close to the inner wall of one side, and a storage battery is mounted at the top of the base.
The beneficial effect of adopting the further scheme is that: the battery can provide electric support for unmanned aerial vehicle.
The above description is only an overview of the technical solution of the present invention, and in order to make the technical means of the present invention clearer and can be implemented according to the content of the description, the following detailed description is made with reference to the preferred embodiments of the present invention and accompanying drawings. The detailed description of the present invention is given by the following examples and the accompanying drawings.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the invention and together with the description serve to explain the invention without undue limitation to the invention. In the drawings:
fig. 1 is a front sectional view of an unmanned aerial vehicle structure of the present invention;
fig. 2 is a side sectional view of an unmanned aerial vehicle structure according to the present invention;
fig. 3 is the utility model relates to a top view of unmanned aerial vehicle structure.
In the drawings, the components represented by the respective reference numerals are listed below:
1. a housing; 2. a cross bar; 3. a telescopic rod; 4. a sleeve; 5. a spring; 6. a foot rest; 7. a range finder; 8. a connecting rod; 9. a movable rod; 10. a support bar; 11. a motor; 12. rotating the rod; 13. a propeller; 14. rotating the fastener; 15. a camera; 16. a heat discharge zone; 17. a switch; 18. an indicator light; 19. a fixed block; 20. an antenna; 21. a base; 22. and (4) a storage battery.
Detailed Description
The principles and features of the present invention are described below in conjunction with the accompanying fig. 1-3, the examples given are intended to illustrate the present invention and are not intended to limit the scope of the invention. The invention is described in more detail in the following paragraphs by way of example with reference to the accompanying drawings. The advantages and features of the present invention will become more fully apparent from the following description and appended claims. It should be noted that the drawings are in simplified form and are not to precise scale, and are provided for convenience and clarity in order to facilitate the description of the embodiments of the present invention.
It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When a component is referred to as being "connected" to another component, it can be directly connected to the other component or intervening components may also be present. When a component is referred to as being "disposed on" another component, it can be directly on the other component or intervening components may also be present. The terms "vertical," "horizontal," "left," "right," and the like as used herein are for illustrative purposes only.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.
The effect that its whole embodiment 1 reaches does, horizontal pole 2 through the installation of casing 1 bottom, thereby can play the effect of fixed stay bottom telescopic link 3, can play the effect that improves the height through adjusting four telescopic links 3, the bottom of two sleeves 4 is close to four corners and all is fixed with spring 5, the impact force that can cushion the decline is used as of spring 5, the power dispersion that receives when foot rest 6 is used as messenger's unmanned aerial vehicle descends, unmanned aerial vehicle's device normal operating is protected, distancer 7 is installed at the bottom center department of casing 1, can conveniently measure unmanned aerial vehicle's altitude of flight.
Embodiment 2, as shown in fig. 1 to 3, four side surfaces of a casing 1 are welded with connecting rods 8 near top edges, one side of each connecting rod 8 is provided with a movable rod 9, one end of each movable rod 9 is provided with a support rod 10, the center of the inside of each support rod 10 is provided with a motor 11, output shafts of the four motors 11 are fixed with rotating rods 12, two sides of each rotating rod 12 are fixed with propellers 13, the bottom of the casing 1 near one side edge is provided with a rotating firmware 14, the bottom of the rotating firmware 14 is provided with a camera 15, the center of the top of the casing 1 is provided with a heat discharging area 16, the center of the outer surface of the casing 1 near one side edge is provided with a switch 17, the center of the outer surface of the casing 1 near the other side edge is provided with an indicator light 18, the top of the casing 1 near one side edge is provided with a fixed block 19, and the top of the fixed block 19 is provided with an antenna 20, a base 21 is fixed on the inner bottom surface of the casing 1 near one side of the inner wall, and a storage battery 22 is mounted on the top of the base 21.
The whole embodiment 2 achieves the effect that through the connecting rods 8 welded on the four side surfaces of the machine shell 1 and the movable rod 9 arranged at one side of the connecting rod 8, so that the unmanned aerial vehicle can be conveniently and manually stored, the motor 11, the rotating rod 12 and the propeller 13 can enable the unmanned aerial vehicle to take off, the rotating firmware 14 is arranged at the bottom of the unmanned aerial vehicle shell 1, the rotating firmware 14 can adjust the angle of the camera 15, thereby facilitating the artificial shooting, the heat discharging area 16 is arranged at the center of the top of the unmanned aerial vehicle shell 1, can make things convenient for the inside heat of unmanned aerial vehicle machine to discharge, the effect of switch 17 and pilot lamp 18 is the start-up that makes things convenient for artificial operation unmanned aerial vehicle, and fixed block 19 at 1 top of unmanned aerial vehicle casing can play fixed antenna 20's effect, and antenna 20 can make artificial wireless control unmanned aerial vehicle, and the inside battery 22 of casing 1 provides electric power for unmanned aerial vehicle motor 11 and supports.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention in any way; the present invention can be smoothly implemented by those skilled in the art according to the drawings and the above description; however, those skilled in the art should understand that changes, modifications and variations made by the above-described technology can be made without departing from the scope of the present invention, and all such changes, modifications and variations are equivalent embodiments of the present invention; meanwhile, any changes, modifications, evolutions, etc. of the above embodiments, which are equivalent to the actual techniques of the present invention, still belong to the protection scope of the technical solution of the present invention.
Claims (7)
1. An unmanned aerial vehicle structure, includes casing (1), its characterized in that: horizontal pole (2), two are all installed near both sides edge to the bottom of casing (1) two bottoms of horizontal pole (2) all are fixed with telescopic link (3), four sleeve (4), two are all installed to the outside between each two of telescopic link (3) the bottom of sleeve (4) is close to four corners and all is fixed with spring (5), and eight all welds under the bottom between each four of spring (5) has foot rest (6), distancer (7) are installed to the bottom center department of casing (1).
2. An unmanned aerial vehicle structure according to claim 1, wherein: four sides of casing (1) are close to top edge and all weld connecting rod (8), and four movable rod (9), four are installed to one side of connecting rod (8) the bracing piece (10) is all installed to the one end of movable rod (9), and four the inside center department of bracing piece (10) all is provided with motor (11), four the output shaft of motor (11) all is fixed with rotary rod (12), four the both sides of rotary rod (12) all are fixed with screw (13).
3. An unmanned aerial vehicle structure according to claim 1, wherein: the bottom of casing (1) is close to one side edge and installs rotating firmware (14), camera (15) are installed to the bottom of rotating firmware (14).
4. An unmanned aerial vehicle structure according to claim 1, wherein: and a heat exhaust area (16) is arranged at the center of the top of the machine shell (1).
5. An unmanned aerial vehicle structure according to claim 1, wherein: switch (17) are installed near one side edge in the surface center of casing (1), indicator (18) are installed near opposite side edge in the surface center of casing (1).
6. An unmanned aerial vehicle structure according to claim 1, wherein: the top of the machine shell (1) is provided with a fixed block (19) near one side edge, and the top of the fixed block (19) is provided with an antenna (20).
7. An unmanned aerial vehicle structure according to claim 1, wherein: the inner bottom surface of the shell (1) is fixed with a base (21) close to the inner wall of one side, and a storage battery (22) is installed at the top of the base (21).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023306986.5U CN213948765U (en) | 2020-12-31 | 2020-12-31 | Unmanned aerial vehicle structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023306986.5U CN213948765U (en) | 2020-12-31 | 2020-12-31 | Unmanned aerial vehicle structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213948765U true CN213948765U (en) | 2021-08-13 |
Family
ID=77197338
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023306986.5U Expired - Fee Related CN213948765U (en) | 2020-12-31 | 2020-12-31 | Unmanned aerial vehicle structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213948765U (en) |
-
2020
- 2020-12-31 CN CN202023306986.5U patent/CN213948765U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210813 Termination date: 20211231 |
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| CF01 | Termination of patent right due to non-payment of annual fee |