CN207917135U - A kind of safe floor stand of Small Civil unmanned plane - Google Patents

A kind of safe floor stand of Small Civil unmanned plane Download PDF

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Publication number
CN207917135U
CN207917135U CN201820193874.7U CN201820193874U CN207917135U CN 207917135 U CN207917135 U CN 207917135U CN 201820193874 U CN201820193874 U CN 201820193874U CN 207917135 U CN207917135 U CN 207917135U
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China
Prior art keywords
unmanned plane
spring
fixedly connected
support frame
safe floor
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CN201820193874.7U
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Chinese (zh)
Inventor
郑向东
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Sichuan Sanchuan Aviation Technology Co ltd
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Chengdu Yu Feng Technology Co Ltd
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Priority to CN201820193874.7U priority Critical patent/CN207917135U/en
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Abstract

The utility model discloses a kind of safe floor stands of Small Civil unmanned plane, including unmanned plane main body and support frame, the unmanned plane main body is mounted on the inner hub location of support frame, the upper surface of the support frame is fixedly connected with annular fixinig plate, it is fixedly connected with the first fixation spring tab between first spring and annular fixinig plate, it is fixedly connected with second spring between support fixed plate and the bottom of support frame, the bottom on the chassis is fixedly connected with damping base, the bottom face of the damping base is equipped with third spring, the bottom of the third spring is equipped with pedestal.The safe floor stand of Small Civil unmanned plane is reasonable for structure; using simple; the protective device of a damping, buffering is provided for unmanned plane; it is out of control fall into behind ground due to be package state; the extent of injury to human body can greatly be reduced; the problem of being effectively reduced casualties, while unmanned plane also being protected to be unlikely to directly to hit damage, improves service efficiency.

Description

A kind of safe floor stand of Small Civil unmanned plane
Technical field
The utility model is related to air vehicle technique field, specially a kind of safe floor stand of Small Civil unmanned plane.
Background technology
This several years development of unmanned plane increases when geometry is presented in China, and certain warp is brought in the behind of rapid growth It helps benefit, while also bringing huge security risk, it is more and more civilian as unmanned plane is creeped the continuous promotion of height There is a series of problems, such as out of control in unmanned plane, and after unmanned plane occurs out of control, falling into ground pounds to the common people, and consequence can't bear to set Think, suchlike event also constantly occurs, and how to solve existing safety problem, and designs a kind of effective protection dress It sets, at there is problem to be solved.
Utility model content
The purpose of this utility model is to provide a kind of safe floor stands of Small Civil unmanned plane, to solve above-mentioned background skill The problem of being proposed in art.
To achieve the above object, the utility model provides the following technical solutions:A kind of Small Civil unmanned plane landing safely Frame, including unmanned plane main body and support frame, the unmanned plane main body are mounted on the inner hub location of support frame, the support frame Upper surface be fixedly connected with annular fixinig plate, the end face of the annular fixinig plate is equipped with buffering spacer, and buffering spacer is set It sets in the edge of annular fixinig plate, the bottom of the support frame is fixedly connected with chassis, among the inner wall of the support frame Position is fixedly connected with support fixed plate, and the upper surface of the support fixed plate is fixedly connected with the first spring, first bullet It is fixedly connected with the first fixation spring tab between spring and annular fixinig plate, it is fixed between support fixed plate and the bottom of support frame It is connected with second spring, the bottom on the chassis is fixedly connected with damping base, and the bottom face of the damping base is equipped with The bottom of three springs, the third spring is equipped with pedestal.
Preferably, the support frame is arranged in camber line hemispherical, and inside it by the installation of unmanned plane main body, and upper and lower side Face is flat mouth structure.
Preferably, the annular fixinig plate is circular ring structure, and is in inner and outer ring twin nuclei, and is fixed and connected by buffering spacer It connects.
Preferably, the buffering spacer is provided with 4 altogether in the end face of annular fixinig plate, and evenly distributed.
Preferably, the support fixed plate is evenly distributed altogether in the inside of support frame and is equipped with 4, and each support is solid The upper and lower end face of fixed board is fixedly connected with the first spring, second spring.
Preferably, the bottom on the chassis is evenly distributed altogether and is equipped with 4 damping bases.
Compared with prior art, the utility model has the beneficial effects that:The safe floor stand structure of the Small Civil unmanned plane Rationally, using simple, the protective device of a damping, buffering is provided for unmanned plane, it is out of control fall into ground after due to being package State, can greatly reduce the extent of injury to human body, be effectively reduced casualties, while also protecting unmanned plane The problem of being unlikely to directly to hit damage, improves service efficiency.
Description of the drawings
Fig. 1 is the utility model side sectional view;
Fig. 2 is the utility model vertical view.
In figure:1 buffering spacer, 2 first fixation spring tabs, 3 annular fixinig plates, 4 unmanned plane main bodys, 5 first springs, 6 supports Fixed plate, 7 support frames, 8 second springs, 9 damping bases, 10 pedestals, 11 third springs, 12 chassis.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work The every other embodiment obtained, shall fall within the protection scope of the present invention.
In the description of the utility model, it should be noted that the side of the instructions such as term "vertical", "upper", "lower", "horizontal" Either position relationship is orientation based on ... shown in the drawings or position relationship for position, is merely for convenience of describing this practicality and simplification is retouched State, rather than indicate either to imply that signified device or element must have a particular orientation, with specific azimuth configuration and Operation, therefore should not be understood as limiting the present invention.In addition, " first ", " second ", " third ", " the 4th " are only used for Purpose is described, and should not be understood as indicating or implying relative importance.
In the description of the utility model, it is also necessary to which explanation " is set unless otherwise specific regulation and limitation, term Set ", " installation ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, Or be integrally connected, it can be mechanical connection, can also be electrical connection, can be directly connected to, can also be by intermediate matchmaker It is situated between and is connected, can is the connection inside two elements.It for the ordinary skill in the art, can be as the case may be Understand the concrete meaning of above-mentioned term in the present invention.
- 2 are please referred to Fig.1, the utility model provides a kind of technical solution:A kind of safe floor stand of Small Civil unmanned plane, Including unmanned plane main body 4 and support frame 7, the support frame 7 is arranged in camber line hemispherical, and unmanned plane main body 4 is mounted on it Inside, and upper and lower end face is flat mouth structure, is played a protective role, the unmanned plane main body 4 is mounted in the inside of support frame 7 The upper surface of heart position, the support frame 7 is fixedly connected with annular fixinig plate 3, and the annular fixinig plate 3 is circular ring structure, and It is fixedly connected in inner and outer ring twin nuclei, and by buffering spacer 1, plays the role of being fixedly connected, the end face of the annular fixinig plate 3 Buffering spacer 1 is installed, and buffering spacer 1 is arranged in the edge of annular fixinig plate 3, the buffering spacer 1 is solid in annular The end face of stator 3 is provided with 4 altogether, and evenly distributed, plays the role of bumper and absorbing shock.
The bottom of the support frame 7 is fixedly connected with chassis 12, and the bottom on the chassis 12 is evenly distributed altogether and is equipped with 4 A damping base 9 plays cushioning effect, and position is fixedly connected with support fixed plate 6 among the inner wall of the support frame 7, described Support fixed plate 6 is evenly distributed altogether in the inside of support frame 7 and is equipped with 4, and the upper and lower end face of each support fixed plate 6 is equal It is fixedly connected with the first spring 5, second spring 8, plays the role of being fixedly connected, the upper surface of the support fixed plate 6, which is fixed, to be connected It is connected to the first spring 5, the first fixation spring tab 2, the support are fixedly connected between first spring 5 and annular fixinig plate 3 Second spring 8 is fixedly connected between fixed plate 6 and the bottom of support frame 7, the bottom on the chassis 12 is fixedly connected with damping The bottom face of pedestal 9, the damping base 9 is equipped with third spring 11, and the bottom of the third spring 11 is equipped with pedestal 10.
Operation principle:The safe floor stand of this kind of unmanned plane by the hemispherical of support frame 7 wrap up form can effectively by Unmanned plane main body 4 is wrapped up wherein, while the annular fixinig plate 3 installed above it will not shut top, this would not be influenced The steady air current of unmanned plane main body 4 in use has same using effect, while this kind of safe floor stand is in inside The first spring 5 and second spring 8 of installation can play effective shock-absorbing protecting after unexpected landing occurs to unmanned plane main body 4 Effect, use are more efficient.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art, It is appreciated that can these embodiments be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaiied Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.

Claims (6)

1. a kind of safe floor stand of Small Civil unmanned plane, including unmanned plane main body (4) and support frame (7), it is characterised in that:Institute The inner hub location that unmanned plane main body (4) is mounted on support frame (7) is stated, the upper surface of the support frame (7) is fixedly connected with The end face of annular fixinig plate (3), the annular fixinig plate (3) is equipped with buffering spacer (1), and buffering spacer (1) is arranged in ring The edge of shape fixinig plate (3), the bottom of the support frame (7) are fixedly connected with chassis (12), the support frame (7) it is interior Position is fixedly connected with support fixed plate (6) among wall;
The upper surface of the support fixed plate (6) is fixedly connected with the first spring (5), and first spring (5) is fixed with annular The first fixation spring tab (2) is fixedly connected between piece (3), it is fixed between the support fixed plate (6) and the bottom of support frame (7) It is connected with second spring (8), the bottom of the chassis (12) is fixedly connected with damping base (9), the bottom of the damping base (9) End face is equipped with third spring (11), and the bottom of the third spring (11) is equipped with pedestal (10).
2. a kind of safe floor stand of Small Civil unmanned plane according to claim 1, it is characterised in that:The support frame (7) it is in that camber line hemispherical arranges, and unmanned plane main body (4) is installed inside it, and upper and lower end face is flat mouth structure.
3. a kind of safe floor stand of Small Civil unmanned plane according to claim 1, it is characterised in that:The annular is fixed Piece (3) is circular ring structure, and is in inner and outer ring twin nuclei, and is fixedly connected by buffering spacer (1).
4. a kind of safe floor stand of Small Civil unmanned plane according to claim 1, it is characterised in that:The buffering spacer (1) it is provided with 4 altogether in the end face of annular fixinig plate (3), and evenly distributed.
5. a kind of safe floor stand of Small Civil unmanned plane according to claim 1, it is characterised in that:The support is fixed Plate (6) is evenly distributed altogether in the inside of support frame (7) and is equipped with 4, and each the upper and lower end face of support fixed plate (6) with First spring (5), second spring (8) are fixedly connected.
6. a kind of safe floor stand of Small Civil unmanned plane according to claim 1, it is characterised in that:The chassis (12) Bottom it is evenly distributed and 4 damping bases (9) are installed altogether.
CN201820193874.7U 2018-02-05 2018-02-05 A kind of safe floor stand of Small Civil unmanned plane Active CN207917135U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820193874.7U CN207917135U (en) 2018-02-05 2018-02-05 A kind of safe floor stand of Small Civil unmanned plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820193874.7U CN207917135U (en) 2018-02-05 2018-02-05 A kind of safe floor stand of Small Civil unmanned plane

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CN207917135U true CN207917135U (en) 2018-09-28

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108100238A (en) * 2018-02-05 2018-06-01 成都市煜沣科技有限公司 A kind of safe floor stand of Small Civil unmanned plane

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108100238A (en) * 2018-02-05 2018-06-01 成都市煜沣科技有限公司 A kind of safe floor stand of Small Civil unmanned plane

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GR01 Patent grant
GR01 Patent grant
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TR01 Transfer of patent right

Effective date of registration: 20200819

Address after: 610000 Qingyang District, Chengdu, Sichuan Province, Qingyang District, Chengdu Jiao long industrial port Qingyang Park Huanghai Road (No.)

Patentee after: SICHUAN SACHUAN AVIATION MACHINERY EQUIPMENT Co.,Ltd.

Address before: 610041 No. 9, No. 6, No. 6, 89 cooperative road, hi tech Zone, Chengdu, Sichuan.

Patentee before: CHENGDU YUFENG TECHNOLOGY Co.,Ltd.

CP03 Change of name, title or address
CP03 Change of name, title or address

Address after: Building 7, No. 551, Wanglong Road, High-tech Industrial Park, Xindu District, Chengdu, Sichuan 610000

Patentee after: Sichuan Sanchuan Aviation Technology Co.,Ltd.

Address before: Block 2 (No.), Huanghai Road, Qingyang Park, Qingyang Park, Chengdu Jiaolong Industrial Port, Qingyang District, Chengdu City, Sichuan Province 610000

Patentee before: SICHUAN SACHUAN AVIATION MACHINERY EQUIPMENT CO.,LTD.