CN211442813U - Unmanned aerial vehicle takes off and uses jettison device - Google Patents
Unmanned aerial vehicle takes off and uses jettison device Download PDFInfo
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- CN211442813U CN211442813U CN201922014723.8U CN201922014723U CN211442813U CN 211442813 U CN211442813 U CN 211442813U CN 201922014723 U CN201922014723 U CN 201922014723U CN 211442813 U CN211442813 U CN 211442813U
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a launching device for take-off of an unmanned aerial vehicle, which comprises a launching cradle, a fixed plate is fixedly connected with the inner center of the launching cradle, a first limiting plate is fixedly connected with the left bottom end of the fixed plate, a second limiting plate is fixedly connected with the left center of the first limiting plate, a first motor is fixedly connected with the inner part of the second limiting plate, a first shaft coupling is fixedly connected with the output end of the first motor, a first telescopic rod is fixedly connected with one end of the first shaft coupling, which is far away from the first motor, a first base is fixedly connected with the bottom of the first telescopic rod, a third limiting plate is fixedly connected with the right bottom end of the fixed plate, the first motor can be protected by the arrangement of the second limiting plate matching with the first limiting plate, so that the first motor can not generate shaking, the height adjustment of the left side of the ejection rack is realized.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle takes off and uses jettison device.
Background
Unmanned aircraft, also known as "drones" for short, are unmanned aircraft that are operated by radio remote control devices and self-contained program control devices, and are often more suited to tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + industry is applied, and is really just needed by the unmanned aerial vehicle.
Unmanned aerial vehicle is at present taking photo by plane, agriculture, plant protection, miniature autodyne, express delivery transportation, disaster relief, observe wild animal, control infectious disease, survey and drawing, news report, electric power is patrolled and examined, the relief disaster, the movie & TV is shot, make the application in fields such as romantic, great expansion unmanned aerial vehicle's use itself, unmanned aerial vehicle at present stage takes off and uses jettison device to the planarization requirement on ground, unmanned aerial vehicle takes off when the ground is not very level and uses the jettison device can incline, can influence unmanned aerial vehicle's taking off, unmanned aerial vehicle at present stage takes off and uses with jettison device only can be on level ground, cause very big restriction to the place that unmanned aerial vehicle takes off, therefore, we propose a novel unmanned aerial vehicle takes off and uses jettis.
SUMMERY OF THE UTILITY MODEL
Not enough to prior art, the utility model provides an unmanned aerial vehicle takes off and uses jettison device possesses advantages such as scalable regulation footing, has solved and can appear the problem that the slope influences unmanned aerial vehicle to take off at unevenness ground unmanned aerial vehicle takes off with the device.
The utility model discloses an unmanned aerial vehicle catapult for take-off, including the catapult frame, the inside central authorities fixedly connected with fixed plate of catapult frame, the left side bottom fixedly connected with first limiting plate of fixed plate, the left side central authorities fixedly connected with second limiting plate of first limiting plate, the inside fixedly connected with first motor of second limiting plate, the output fixedly connected with first shaft coupling of first motor, the one end of first shaft coupling far away from first motor fixedly connected with first telescopic link, the bottom fixedly connected with first base of first telescopic link, the right side bottom fixedly connected with third limiting plate of fixed plate, the right side central authorities fixedly connected with fourth limiting plate of third limiting plate, can protect first motor through the second limiting plate that sets up cooperation first limiting plate, make first motor can not appear rocking, can adjust the distance to ground through the left side of the first telescopic link that sets up, the height adjustment of the left side of the ejection rack is realized.
The utility model discloses an unmanned aerial vehicle takes off and uses jettison device, wherein the inside fixedly connected with second motor of fourth limiting plate, the output fixedly connected with second shaft coupling of second motor can protect the second motor through the fourth limiting plate cooperation third limiting plate that sets up, makes the second motor can not appear rocking.
The utility model discloses an unmanned aerial vehicle takes off and uses jettison device, wherein the one end fixedly connected with second telescopic link of second motor is kept away from to the second shaft coupling, the height adjustment on catapult frame right side is realized to the bottom fixedly connected with second base of second telescopic link through the distance on the adjustable catapult frame right side of second telescopic link that sets up and ground, and the cooperation first telescopic link can make unmanned aerial vehicle take off and use jettison device also can use in the ground of unevenness.
The utility model discloses an unmanned aerial vehicle takes off and uses jettison device, wherein a plurality of group's of top fixedly connected with spring of fixed plate, a plurality of group the spring becomes the equidistance and distributes, the top fixedly connected with of spring plays the board, a set of extension board of both ends fixedly connected with of play board, the bullet when can realizing unmanned aerial vehicle takes off through the play board cooperation spring that sets up launches.
The utility model discloses an unmanned aerial vehicle takes off and uses jettison gear, wherein first screw thread through-hole has been seted up at the top of extension board, second screw thread through-hole has been seted up at the top of launching cradle under first screw thread through-hole, first screw thread through-hole is unanimous with second screw thread through-hole, first screw thread through-hole and bolt looks adaptation realize the catapulting of diving board to unmanned aerial vehicle through the first screw thread through-hole and the second screw thread through-hole cooperation bolt compressible spring that set up.
The utility model discloses an unmanned aerial vehicle takes off and uses jettison device, wherein the casing has been placed at the top of diving board, the inside fixedly connected with organism of casing, four apex angle fixedly connected with oar wings of casing, the top fixedly connected with signal receiver of casing, the bottom fixedly connected with cloud platform camera of casing can protect the organism through the casing that sets up, can carry out wireless control to unmanned aerial vehicle through the signal receiver who sets up, can make unmanned aerial vehicle accomplish through the cloud platform camera that sets up and shoot the work.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses a first motor and second motor can be protected to the first limiting plate, second limiting plate, third limiting plate and the fourth limiting plate that set up, make first motor and second motor can not appear rocking, can adjust the distance on launching rack left side and ground according to the ground actual conditions through the first telescopic link that sets up, can adjust the distance on launching rack right side and ground according to the face condition and the distance on launching rack left side and ground through the second telescopic link that sets up, make the launching rack top keep the level.
2. The utility model discloses a compressible bullet board of first screw thread through-hole and the cooperation of second screw thread through-hole bolt that set up, bullet board cooperation spring through setting up can realize the ejection when unmanned aerial vehicle takes off, can protect the signal receiver through setting up to the organism through the casing that sets up and can carry out long-range wireless control to unmanned aerial vehicle, can make unmanned aerial vehicle accomplish through the cloud platform camera that sets up and shoot the work.
Drawings
The accompanying drawings, which are included to provide a further understanding of the application and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the application and together with the description serve to explain the application and not to limit the application. In the drawings:
fig. 1 is a schematic view of a vertical section structure of the ejection rack of the present invention;
FIG. 2 is a schematic top view of the housing of the present invention;
fig. 3 is a schematic view of the vertical section structure of the extension plate of the present invention.
In the figure: 01. an ejection rack; 02. a fixing plate; 03. a spring plate; 04. a spring; 05. an extension plate; 06. a bolt; 07. a first limit plate; 08. a second limiting plate; 09. a first motor; 10. a first coupling; 11. a first telescopic rod; 12. a first base; 13. a third limiting plate; 14. a fourth limiting plate; 15. a second motor; 16. a second coupling; 17. a second telescopic rod; 18. a second base; 19. a housing; 20. a body; 21. a paddle wing; 22. a signal receiver; 23. a pan-tilt camera; 24. a first threaded through hole; 25. a second threaded through hole.
Detailed Description
In the following description, numerous implementation details are set forth in order to provide a more thorough understanding of the present invention. It should be understood, however, that these implementation details should not be used to limit the invention. That is, in some embodiments of the invention, details of these implementations are not necessary. In addition, some conventional structures and components are shown in simplified schematic form in the drawings.
In addition, the descriptions related to "first", "second", etc. in the present invention are only for description purposes, not specifically referring to the order or sequence, and are not intended to limit the present invention, but only to distinguish the components or operations described in the same technical terms, and are not to be construed as indicating or implying any relative importance or implicit indication of the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In addition, the technical solutions in the embodiments may be combined with each other, but it must be based on the realization of those skilled in the art, and when the technical solutions are contradictory or cannot be realized, the combination of the technical solutions should not be considered to exist, and is not within the protection scope of the present invention.
Referring to fig. 1-3, the launching device for take-off of unmanned aerial vehicle of the present invention comprises a launching cradle 01, a fixed plate 02 is fixedly connected to the inner center of the launching cradle 01, a first limiting plate 07 is fixedly connected to the left bottom end of the fixed plate 02, a second limiting plate 08 is fixedly connected to the left center of the first limiting plate 07, a first motor 09 is fixedly connected to the inner portion of the second limiting plate 08, a first coupler 10 is fixedly connected to the output end of the first motor 09, a first telescopic rod 11 is fixedly connected to the end of the first coupler 10 far from the first motor 09, a first base 12 is fixedly connected to the bottom of the first telescopic rod 11, a third limiting plate 13 is fixedly connected to the right bottom of the fixed plate 02, a fourth limiting plate 14 is fixedly connected to the right center of the third limiting plate 13, the first motor 09 can be protected by the cooperation of the second limiting plate 08, the first motor 09 is prevented from shaking, the distance from the left side of the ejection rack 01 to the ground can be adjusted through the first telescopic rod 11, and the left side of the ejection rack 01 can be adjusted in height.
The second motor 15 is fixedly connected to the inside of the fourth limiting plate 14, the second coupling 16 is fixedly connected to the output end of the second motor 15, and the second motor 15 can be protected by the fourth limiting plate 14 matched with the third limiting plate 13, so that the second motor 15 cannot shake.
One end fixedly connected with second telescopic link 17 that second motor 15 was kept away from to second shaft coupling 16, the bottom fixedly connected with second base 18 of second telescopic link 17, the adjustable ejector rack 01 right side of second telescopic link 17 through the setting apart from ground, realize the height adjustment on ejector rack 01 right side, cooperation first telescopic link 11 can make unmanned aerial vehicle take off with jettison gear also can use on the ground of unevenness.
The top fixedly connected with of fixed plate 02 a plurality of group spring 04, a plurality of group spring 04 become the equidistance and distribute, and the top fixedly connected with of spring 04 plays board 03, plays a set of extension board 05 of both ends fixedly connected with of board 03, plays the ejection when board 03 cooperation spring 04 that sets up can realize unmanned aerial vehicle and take off.
First screw thread through-hole 24 has been seted up at the top of extension board 05, and second screw thread through-hole 25 has been seted up at the top of launching cradle 01 under first screw thread through-hole 24, and first screw thread through-hole 24 is unanimous with second screw thread through-hole 25, and first screw thread through-hole 24 and bolt 06 looks adaptation realize playing the ejection of bullet board 03 to unmanned aerial vehicle through the first screw thread through-hole 24 and the cooperation bolt 06 compressible spring 04 that set up.
When using the utility model discloses the time:
the method comprises the steps of firstly starting a first motor 09, driving a first coupler 10 to rotate by the first motor 09, driving a first telescopic rod 11 to stretch by the rotation of the first coupler 10, adjusting the distance between the left side of an ejection rack 01 and the ground according to the ground condition, turning off the first motor 09, starting a second motor 15, driving a second coupler 16 to rotate by the second motor 15, driving a second telescopic rod 17 to stretch by the rotation of the second coupler 16, adjusting the distance between the right side of the ejection rack 01 and the ground according to the ground condition and the distance between the left side of the ejection rack 01 and the ground, and keeping the top end of the ejection rack 01 horizontal.
The board 03 is played in the downward compression makes spring 04 compressed, rotatory bolt 06 makes the board 03 of playing fixed, place unmanned aerial vehicle on playing the board 03, rotatory bolt 06 makes the board 03 of playing released, spring 04 drives the board 03 rebound, play the board 03 rebound and accomplish unmanned aerial vehicle's ejection and take off, but through the signal receiver 22 long-range wireless control unmanned aerial vehicle of setting, can make unmanned aerial vehicle accomplish through the cloud platform camera 23 that sets up and shoot the work.
The above description is only an embodiment of the present invention, and is not intended to limit the present invention. Various modifications and changes may occur to those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention should be included in the scope of the claims of the present invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle takes off and uses jettison gear, includes jettison rack (01), its characterized in that: the utility model discloses a launch frame, including launch frame (01), the first limiting plate of inside central fixedly connected with fixed plate (02) of left side bottom fixedly connected with (07) of fixed plate (02), the left side central fixedly connected with second limiting plate (08) of first limiting plate (07), the first motor (09) of inside fixedly connected with of second limiting plate (08), the first shaft coupling (10) of output fixedly connected with of first motor (09), the first telescopic link (11) of one end fixedly connected with of keeping away from first motor (09) of first shaft coupling (10), the first base (12) of bottom fixedly connected with of first telescopic link (11), the right side bottom fixedly connected with third limiting plate (13) of fixed plate (02), the right side central fixedly connected with fourth limiting plate (14) of third limiting plate (13).
2. The catapult device for take-off of the unmanned aerial vehicle as claimed in claim 1, wherein: the inside fixedly connected with second motor (15) of fourth limiting plate (14), the output fixedly connected with second shaft coupling (16) of second motor (15).
3. The catapult device for take-off of the unmanned aerial vehicle as claimed in claim 2, wherein: one end, far away from the second motor (15), of the second coupler (16) is fixedly connected with a second telescopic rod (17), and the bottom of the second telescopic rod (17) is fixedly connected with a second base (18).
4. The catapult device for take-off of the unmanned aerial vehicle as claimed in claim 1, wherein: the top fixedly connected with of fixed plate (02) a plurality of group spring (04), a plurality of group spring (04) become the equidistance and distribute, the top fixedly connected with of spring (04) plays board (03), the both ends fixedly connected with of playing board (03) a set of extension board (05).
5. The launch device for takeoff of unmanned aerial vehicle as claimed in claim 4, wherein: first screw thread through-hole (24) have been seted up at the top of extension board (05), second screw thread through-hole (25) have been seted up at the top of launching cradle (01) under first screw thread through-hole (24), first screw thread through-hole (24) are unanimous with second screw thread through-hole (25), first screw thread through-hole (24) and bolt (06) looks adaptation.
6. The launch device for takeoff of unmanned aerial vehicle as claimed in claim 4, wherein: a machine shell (19) is placed at the top of the elastic plate (03), an organism (20) is fixedly connected inside the machine shell (19), paddle wings (21) are fixedly connected to four top corners of the machine shell (19), a signal receiver (22) is fixedly connected to the top of the machine shell (19), and a holder camera (23) is fixedly connected to the bottom of the machine shell (19).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922014723.8U CN211442813U (en) | 2019-11-20 | 2019-11-20 | Unmanned aerial vehicle takes off and uses jettison device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922014723.8U CN211442813U (en) | 2019-11-20 | 2019-11-20 | Unmanned aerial vehicle takes off and uses jettison device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211442813U true CN211442813U (en) | 2020-09-08 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922014723.8U Expired - Fee Related CN211442813U (en) | 2019-11-20 | 2019-11-20 | Unmanned aerial vehicle takes off and uses jettison device |
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| Country | Link |
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| CN (1) | CN211442813U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112960134A (en) * | 2021-03-25 | 2021-06-15 | 杭州科技职业技术学院 | Unmanned aerial vehicle bears support |
| CN113148216A (en) * | 2021-06-02 | 2021-07-23 | 南京联汇智能科技有限公司 | Ejection type unmanned aerial vehicle |
| CN115924056A (en) * | 2022-12-13 | 2023-04-07 | 华能(广东)能源开发有限公司汕头电厂 | Catapult-assisted take-off unmanned aerial vehicle |
-
2019
- 2019-11-20 CN CN201922014723.8U patent/CN211442813U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112960134A (en) * | 2021-03-25 | 2021-06-15 | 杭州科技职业技术学院 | Unmanned aerial vehicle bears support |
| CN113148216A (en) * | 2021-06-02 | 2021-07-23 | 南京联汇智能科技有限公司 | Ejection type unmanned aerial vehicle |
| CN115924056A (en) * | 2022-12-13 | 2023-04-07 | 华能(广东)能源开发有限公司汕头电厂 | Catapult-assisted take-off unmanned aerial vehicle |
| CN115924056B (en) * | 2022-12-13 | 2024-05-14 | 华能(广东)能源开发有限公司汕头电厂 | Catapult-assisted take-off unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210803 Address after: 430000 Pengcheng international 1-a-1707, No. 1, Luoyu Road, Hongshan District, Wuhan City, Hubei Province Patentee after: Wuhan Tianbo Technology Co.,Ltd. Address before: 552100 Dafen formation, Dazhai village, xiongjiachang Township, Zhijin County, Zunyi City, Guizhou Province Patentee before: Huang Cong |
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| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200908 Termination date: 20211120 |