CN109911235A - A kind of unmanned aerial vehicle ejecting buffer protection device - Google Patents

A kind of unmanned aerial vehicle ejecting buffer protection device Download PDF

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Publication number
CN109911235A
CN109911235A CN201910310739.5A CN201910310739A CN109911235A CN 109911235 A CN109911235 A CN 109911235A CN 201910310739 A CN201910310739 A CN 201910310739A CN 109911235 A CN109911235 A CN 109911235A
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China
Prior art keywords
shell
annular magnet
aerial vehicle
unmanned aerial
buffer protection
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CN201910310739.5A
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CN109911235B (en
Inventor
张伟瑞
杜英杰
周行烽
赵大卫
周孝贤
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Chengdu Aeronautic Polytechnic
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Chengdu Aeronautic Polytechnic
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Publication of CN109911235A publication Critical patent/CN109911235A/en
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Publication of CN109911235B publication Critical patent/CN109911235B/en
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Abstract

The present invention relates to air vehicle technique fields; especially a kind of unmanned aerial vehicle ejecting buffer protection device; including shell; the lower surface of the shell is equipped with self balancing device; the inside upper part of the shell, which runs through, mobile column; the outer lower portion of the shell is equipped with operation panel, and the inside bottom surface of the shell is equipped with battery, first annular magnet, the second annular magnet shell body and clamping device, and the drawstring is connected with limited block through through-hole around fixed pulley.Horizontal supporting plate can be in horizontality automatically by the self balancing device that the present invention is equipped with, the first annular magnet and the second annular magnet being equipped with can reduce contact friction force, the clamping device being equipped with, which can be realized, is fixedly clamped to drawstring, it realizes to pop up unmanned plane by the elastic force of spring and emit, entire emission process is steady, and unmanned plane is in horizontality when transmitting, the stability of unmanned plane transmitting can be enhanced, using effect is good, practical, is worth of widely use.

Description

A kind of unmanned aerial vehicle ejecting buffer protection device
Technical field
The present invention relates to air vehicle technique field more particularly to a kind of unmanned aerial vehicle ejecting buffer protection devices.
Background technique
Unmanned plane is because having good using effect to be widely used in our life, such as Aerial photography etc., but The mode of taking off for being current unmanned plane is all directly to take off from ground level mostly, and effect of taking off is poor, when in take-off process not When steady, it is be easy to cause the unbalance of unmanned plane, certain injury is caused to unmanned plane, for this purpose, it is proposed that a kind of unmanned plane bullet It penetrates and uses buffer protection device.
Summary of the invention
The purpose of the present invention is to solve disadvantages existing in the prior art, and a kind of unmanned aerial vehicle ejecting proposed is used and delayed Rush protective device.
To achieve the goals above, present invention employs following technical solutions:
A kind of unmanned aerial vehicle ejecting buffer protection device, including shell are designed, the lower surface of the shell is equipped with from flat Weigh device, and the middle inside of the shell is equipped with intermediate plate by bolt, and the upper surface of the intermediate plate is symmetrically fixedly mounted There is gag lever post, the inside upper part of the shell is through there is mobile column, and the upper end of the mobile column is equipped with top plate, the top plate Lower surface two sides are symmetrically installed with the first guide sleeve for being limited bar grafting, and the outside fixing sleeve of the mobile column is connected to the first ring Shape magnet, the inside upper part of the shell are fixedly installed with the second annular magnet, and the second annular magnet and first annular magnet Mutually exclusive, the outer lower portion of the shell is equipped with operation panel, and the inside bottom surface of the shell is equipped with battery, T Shell body and clamping device, a side lower part of the shell are equipped with through-hole, are equipped with fixed pulley on the inside of the T-type shell, institute It states and convex block is installed in the middle part of the lower surface of top plate, spring, the lower end peace of the convex block are installed between the convex block and T-type shell Equipped with drawstring, the drawstring is connected with limited block, the operation panel, battery and clamping device through through-hole around fixed pulley Between pass through conducting wire connect.
Preferably, the self balancing device includes bottom plate, and the upper surface two sides of the bottom plate are symmetrically installed with vertical support Plate, the lower part between two vertical gripper shoes are equipped with arc panel, the top installation between two vertical gripper shoes There is postive stop baffle, the upper surface of the arc panel is symmetrically installed with support wheel, and the side of the support wheel is rotatably equipped with support Bar, the upper end of the support rod is equipped with horizontal supporting plate, is bolted between the horizontal supporting plate and shell, described Fastening bolt is threaded in the middle part of support rod.
Preferably, the two sides of the bottom plate are symmetrically threaded with adjusting bolt.
Preferably, the clamping device includes the rectangle frame fixed with shell, and the side of the rectangle frame is symmetrically installed with Second guide sleeve, the inside of second guide sleeve are plugged with mobile bar, and one end of the mobile bar is equipped with clamping bar, described The middle part of mobile bar is rotatably equipped with connecting rod by pin shaft, and the inside of the rectangle frame is equipped with electric telescopic rod, described electronic The output end of telescopic rod is rotatablely connected through rectangle frame by one end of pin shaft and connecting rod.
Preferably, the side of the through-hole is equipped with arc angling, and the drawstring is nylon withdrawal line.
A kind of unmanned aerial vehicle ejecting buffer protection device proposed by the present invention, beneficial effect are: the present invention be equipped with from Horizontal supporting plate can be in horizontality automatically by balancing device, and the first annular magnet and the second annular magnet being equipped with can Contact friction force is reduced, the clamping device being equipped with, which can be realized, is fixedly clamped to drawstring, realizes by the elastic force of spring by nothing Man-machine pop-up transmitting, entire emission process is steady, and unmanned plane be in horizontality when transmitting, can enhance unmanned plane emit it is steady Qualitative, using effect is good, practical, is worth of widely use.
Detailed description of the invention
Fig. 1 is a kind of main view schematic diagram of unmanned aerial vehicle ejecting buffer protection device proposed by the present invention;
Fig. 2 is a kind of clamping device structural schematic diagram of unmanned aerial vehicle ejecting buffer protection device proposed by the present invention;
Fig. 3 is that a kind of self balancing device left view graph structure of unmanned aerial vehicle ejecting buffer protection device proposed by the present invention shows It is intended to.
In figure: first annular magnet 1, shell 3, T-type shell 4, operation panel 5, battery 6, erects second annular magnet 2 Allotment fagging 7, horizontal supporting plate 8, adjust bolt 9, support wheel 10, postive stop baffle 11, arc panel 13, bottom plate 14, support rod 15, Fastening bolt 16, limited block 17, drawstring 18, clamping device 19, through-hole 20, intermediate plate 21, fixed pulley 22, spring 23, mobile column 24, gag lever post 25, top plate 26, convex block 27, the first guide sleeve 28, rectangle frame 29, the second guide sleeve 30, mobile bar 31, connecting rod 32, Clamping bar 33, electric telescopic rod 34.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.
Referring to Fig.1-3, a kind of unmanned aerial vehicle ejecting buffer protection device, including shell 3, the lower surface of shell 3 are equipped with Self balancing device, self balancing device include bottom plate 14, and the two sides of bottom plate 14, which are symmetrically threaded with, adjusts bolt 9, can be right Device is balanced fine tuning, enhances stability in use.
The upper surface two sides of bottom plate 14 are symmetrically installed with vertical gripper shoe 7, the lower part installation between two vertical gripper shoes 7 There is arc panel 13, the top between two vertical gripper shoes 7 is equipped with postive stop baffle 11, and the upper surface of arc panel 13 is symmetrically installed There is support wheel 10, the side of support wheel 10 is rotatably equipped with support rod 15, and the upper end of support rod 15 is equipped with horizontal supporting plate 8, It is bolted between horizontal supporting plate 8 and shell 3, the middle part of support rod 15 is threaded with fastening bolt 16, structure letter It is single, it is easy to use, it can be realized autobalance, using effect is good.
The middle inside of shell 3 is equipped with intermediate plate 21 by bolt, and the upper surface of intermediate plate 21 is symmetrically fixedly installed with Gag lever post 25, through there is a mobile column 24, the upper end of mobile column 24 is equipped with top plate 26 for the inside upper part of shell 3, under top plate 26 Surface two sides are symmetrically installed with the first guide sleeve 28 for being limited 25 grafting of bar, and the outside fixing sleeve of mobile column 24 is connected to the first ring Shape magnet 1, the inside upper part of shell 3 are fixedly installed with the second annular magnet 2, and the second annular magnet 2 and first annular magnet 1 Mutually exclusive, the outer lower portion of shell 3 is equipped with operation panel 5, and the inside bottom surface of shell 3 is equipped with battery 6, T-type shell Body 4 and clamping device 19, clamping device 19 include the rectangle frame 29 fixed with shell 3, and the side of rectangle frame 29 is symmetrically installed with Second guide sleeve 30, the inside of the second guide sleeve 30 are plugged with mobile bar 31, and one end of mobile bar 31 is equipped with clamping bar 33, move The middle part of lever 31 is rotatably equipped with connecting rod 32 by pin shaft, and the inside of rectangle frame 29 is equipped with electric telescopic rod 34, electronic to stretch The output end of contracting bar 34 is rotatablely connected through rectangle frame 29 by one end of pin shaft and connecting rod 32, can it is stable to drawstring 18 into Row is fixedly clamped, and stability is high, and clamping effect is good.
One side lower part of shell 3 is equipped with through-hole 20, and the side of through-hole 20 is equipped with arc angling, and drawstring 18 is nylon withdrawal line, The resistance to drawstring 18 can be reduced, improve the service life of drawstring 18.
The inside of T-type shell 4 is equipped with fixed pulley 22, is equipped with convex block 27, convex block 27 and T in the middle part of the lower surface of top plate 26 Spring 23 is installed, the lower end of convex block 27 is equipped with drawstring 18, and drawstring 18 runs through through-hole 20 around fixed pulley 22 between shell body 4 It is connected with limited block 17, is connected between operation panel 5, battery 6 and clamping device 19 by conducting wire.
Working principle: in use, pulling limited block 17 first, limited block 17 drives drawstring 18 mobile, and drawstring 18 passes through convex Block 27 pulls top plate 26, compresses spring 23, when spring 23 reaches maximum compressibility, starts electric telescopic rod 34, electric expansion Bar 34 drives connecting rod 32 mobile, and connecting rod 32 drives mobile bar 31 mobile, and mobile bar 31 drives clamping bar 33 mobile, and drawstring 18 is pressed from both sides It fastens, which is placed on the plane, placed steadily by adjusting bolt 9, while the effect of arc panel 13, level branch Fagging 8 is in horizontality, and horizontality is fixed by fastening bolt 16, and unmanned plane is placed on to the upper table of top plate 26 Face is again started up electric telescopic rod 34 by operation panel 5, and drawstring 18 is unclamped in realization, under the action of spring 23, top plate 26 Move up, realize the ejection of unmanned plane, when the effect of first annular magnet 1 and the second annular magnet 2 makes ejection frictional force compared with It is small, enhancing ejection effect.
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto, Anyone skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention and its Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.

Claims (5)

1. a kind of unmanned aerial vehicle ejecting buffer protection device, including shell (3), which is characterized in that the lower surface of the shell (3) Self balancing device is installed, the middle inside of the shell (3) is equipped with intermediate plate (21) by bolt, the intermediate plate (21) Upper surface be symmetrically fixedly installed with gag lever post (25), the inside upper part of the shell (3) is through having mobile column (24), the shifting The upper end of dynamic column (24) is equipped with top plate (26), and the lower surface two sides of the top plate (26), which are symmetrically installed with, to be limited bar (25) and insert The outside fixing sleeve of the first guide sleeve (28) connect, the mobile column (24) is connected to first annular magnet (1), the shell (3) Inside upper part be fixedly installed with the second annular magnet (2), and the second annular magnet (2) and first annular magnet (1) are mutually arranged Reprimand, the outer lower portion of the shell (3) are equipped with operation panel (5), and the inside bottom surface of the shell (3) is equipped with battery (6), a side lower part of T-type shell (4) and clamping device (19), the shell (3) is equipped with through-hole (20), the T-type shell (4) Inside be equipped with fixed pulley (22), be equipped with convex block (27) in the middle part of the lower surface of the top plate (26), the convex block (27) and T It is equipped between shell body (4) spring (23), the lower end of the convex block (27) is equipped with drawstring (18), and the drawstring (18) bypasses Fixed pulley (22) is connected with limited block (17) through through-hole (20), the operation panel (5), battery (6) and clamping device (19) it is connected between by conducting wire.
2. unmanned aerial vehicle ejecting buffer protection device according to claim 1, which is characterized in that the self balancing device packet It includes bottom plate (14), the upper surface two sides of the bottom plate (14) are symmetrically installed with vertical gripper shoe (7), two vertical gripper shoes (7) lower part between is equipped with arc panel (13), and the top between two vertical gripper shoes (7) is equipped with postive stop baffle (11), the upper surface of the arc panel (13) is symmetrically installed with support wheel (10), the side rotational installation of the support wheel (10) Have support rod (15), the upper end of the support rod (15) is equipped with horizontal supporting plate (8), the horizontal supporting plate (8) and shell (3) it is bolted between, is threaded with fastening bolt (16) in the middle part of the support rod (15).
3. unmanned aerial vehicle ejecting buffer protection device according to claim 2, which is characterized in that the two of the bottom plate (14) Side, which is symmetrically threaded with, adjusts bolt (9).
4. unmanned aerial vehicle ejecting buffer protection device according to claim 1, which is characterized in that the clamping device (19) Including the rectangle frame (29) fixed with shell (3), the side of the rectangle frame (29) is symmetrically installed with the second guide sleeve (30), institute The inside for stating the second guide sleeve (30) is plugged with mobile bar (31), and one end of the mobile bar (31) is equipped with clamping bar (33), The middle part of the mobile bar (31) is rotatably equipped with connecting rod (32) by pin shaft, and the inside of the rectangle frame (29) is equipped with electronic The output end of telescopic rod (34), the electric telescopic rod (34) is turned through rectangle frame (29) by one end of pin shaft and connecting rod (32) Dynamic connection.
5. unmanned aerial vehicle ejecting buffer protection device according to claim 1, which is characterized in that the one of the through-hole (20) Side is equipped with arc angling, and the drawstring (18) is nylon withdrawal line.
CN201910310739.5A 2019-04-17 2019-04-17 Buffering protection device for unmanned aerial vehicle ejection Active CN109911235B (en)

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Application Number Priority Date Filing Date Title
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112660407A (en) * 2021-01-13 2021-04-16 陆颖怡 High-pressure pneumatic boosting take-off device of light unmanned aerial vehicle
CN112960134A (en) * 2021-03-25 2021-06-15 杭州科技职业技术学院 Unmanned aerial vehicle bears support
CN113619732A (en) * 2021-08-13 2021-11-09 中国船舶科学研究中心 Ejection type buoy laying device
CN115489749A (en) * 2022-11-16 2022-12-20 成都航空职业技术学院 Fixed wing unmanned aerial vehicle launches take-off and land integrated system

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3911663A1 (en) * 1989-04-10 1989-12-14 Richard Kuenanz Muscle-powered short-flight aircraft
CN2223042Y (en) * 1995-05-02 1996-03-27 李义 Adjustable dynamic self-balance-stable chair
CN104436554A (en) * 2014-11-05 2015-03-25 菏泽恒泰健身器材制造有限公司 Pop-up flip device
CN108248887A (en) * 2018-01-22 2018-07-06 成都草寓科技有限公司 One kind emits equipment for small drone
CN109176584A (en) * 2018-10-22 2019-01-11 安徽航大智能科技有限公司 A kind of new energy electric machine casing gripping body

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3911663A1 (en) * 1989-04-10 1989-12-14 Richard Kuenanz Muscle-powered short-flight aircraft
CN2223042Y (en) * 1995-05-02 1996-03-27 李义 Adjustable dynamic self-balance-stable chair
CN104436554A (en) * 2014-11-05 2015-03-25 菏泽恒泰健身器材制造有限公司 Pop-up flip device
CN108248887A (en) * 2018-01-22 2018-07-06 成都草寓科技有限公司 One kind emits equipment for small drone
CN109176584A (en) * 2018-10-22 2019-01-11 安徽航大智能科技有限公司 A kind of new energy electric machine casing gripping body

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112660407A (en) * 2021-01-13 2021-04-16 陆颖怡 High-pressure pneumatic boosting take-off device of light unmanned aerial vehicle
CN112960134A (en) * 2021-03-25 2021-06-15 杭州科技职业技术学院 Unmanned aerial vehicle bears support
CN113619732A (en) * 2021-08-13 2021-11-09 中国船舶科学研究中心 Ejection type buoy laying device
CN115489749A (en) * 2022-11-16 2022-12-20 成都航空职业技术学院 Fixed wing unmanned aerial vehicle launches take-off and land integrated system

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