CN208086037U - A kind of power assisting device that unmanned plane takes off - Google Patents
A kind of power assisting device that unmanned plane takes off Download PDFInfo
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- CN208086037U CN208086037U CN201820549129.1U CN201820549129U CN208086037U CN 208086037 U CN208086037 U CN 208086037U CN 201820549129 U CN201820549129 U CN 201820549129U CN 208086037 U CN208086037 U CN 208086037U
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Abstract
The utility model is related to unmanned aerial vehicle design technical fields, and disclose the power assisting device that unmanned plane takes off, including pedestal, it is installed with bottom plate at the top of the pedestal, the top of the pedestal and it is installed with fixed plate positioned at the both sides of bottom plate, it is installed with buffer spring at the top of the bottom plate, the top of the bottom plate and is installed with limited block positioned at the both sides of buffer spring.The power assisting device that the unmanned plane takes off; fixed seat is installed at the top of platform by shutting down; the leg of unmanned plane can be stuck in the inside of fixed seat; pushing shutdown platform makes shutdown platform reverse snap-gauge block, and snap-gauge cylinder ejector is contacted with snap-gauge block at this time; make it that can not rotate to fix snap-gauge block; when unmanned plane needs lift-off; snap-gauge cylinder is retracted; since the effect of snap-gauge tension spring makes snap-gauge block overturn; platform is shut down under the action of power assistant spring to pop up; due to the effect of inertia, unmanned plane is made to pop up, has achieved the purpose that unmanned plane is assisted to take off.
Description
Technical field
The utility model is related to unmanned aerial vehicle design technical field, specially a kind of power assisting device that unmanned plane takes off.
Background technology
Unmanned plane is a kind of aerial unit using remote control, using unmanned plane carry out remote sensing monitoring be it is a kind of very just
Prompt method, since multi-rotor unmanned aerial vehicle is shorter most of cruise duration, remote sensing monitoring is fixed-wing with unmanned plane majority
Unmanned plane.
The current existing unmanned plane mode of taking off is mainly that pilot manually controls aircraft takeoff, and this mode needs nobody
Machine, which manipulates hand, has very strong manipulation ability and experience, in the environment of weather anomaly, since people is to external environment
The judgement for influencing unmanned plane during flying situation is only capable of through naked-eye observation, if manipulation hand operation error is it is also possible to damage unmanned plane
Even ground staff is damaged, another method machine generally requires longer runway and goes up to the air, in actual monitored environment
It is difficult to meet the needs of to runway in real time, so propose a kind of power assisting device that unmanned plane takes off to solve above-mentioned proposed ask
Topic.
Utility model content
(1) the technical issues of solving
In view of the deficiencies of the prior art, the utility model provides a kind of power assisting device that unmanned plane takes off, and has auxiliary
The advantages that unmanned plane takes off, it is mainly that pilot manually controls aircraft takeoff to solve the current existing unmanned plane mode of taking off,
This mode needs unmanned plane manipulation hand to have very strong manipulation ability and experience, in the environment of weather anomaly,
Since the judgement that people influences external environment unmanned plane during flying situation is only capable of through naked-eye observation, if the operation error of manipulation hand is also
It is possible that damage unmanned plane even damages ground staff, another method machine generally requires longer runway and is risen
Sky is difficult to meet the problem of the needs of to runway in real time in actual monitored environment.
(2) technical solution
To realize that above-mentioned auxiliary unmanned plane takes off purpose, the utility model provides the following technical solutions：A kind of unmanned plane
Winged power assisting device, including pedestal, are installed with bottom plate at the top of the pedestal, the top of the pedestal and positioned at bottom plate
Both sides are installed with fixed plate, are installed with buffer spring at the top of the bottom plate, the top of the bottom plate and are located at
The both sides of buffer spring are installed with limited block, and buffer board, the buffering are installed at the top of the buffer spring
The inside of plate is installed with leader casing, and the internal activity of the leader casing is connected with flexible guide rod, the bottom of the flexible guide rod
Portion is flexibly connected with limited block, and power assistant spring is installed at the top of the buffer board, and the top of the power assistant spring is fixed
Shutdown platform is installed, the bottom for shutting down platform is installed with limited block, the front and the back side for shutting down platform and buffer board
It is installed with directive wheel, the outside of the directive wheel is connected with guide wheel workpiece, and the top for shutting down platform is fixed
Fixed seat is installed, the inner bottom wall of the fixed seat offers sliding slot, and the internal activity of the sliding slot is connected there are two card machine plate,
Two opposite sides of the card machine plate are fixedly connected with fixed spring, and the inside of the fixed plate offers Card trough, described
The inside of fixed plate is fixedly connected with snap-gauge cylinder, and the snap-gauge cylinder is connected with snap-gauge close to the side of guide wheel workpiece
Block, the snap-gauge block internal activity are connected with bull stick, and the snap-gauge block is connected to the inside of Card trough by bar rotation, described
Side of the snap-gauge block far from guide wheel workpiece is fixedly connected with snap-gauge tension spring, and the other end that the snap-gauge tension spring is connect with snap-gauge block is solid
Surely be connected to the inside of Card trough, be fixedly connected with counterweight tank at left and right sides of the pedestal, two counterweight tanks it is interior
Portion is connected with clump weight.
Preferably, the fixed plate is symmetric in the both sides of bottom plate, and the quantity of the buffer spring is no less than four
It is a, and it is uniformly distributed in the top of bottom plate.
Preferably, the quantity of the power assistant spring is no less than two, and is evenly distributed in the top of buffer board, described
The elastic force of power assistant spring is much larger than the elastic force of buffer spring.
Preferably, the limited block is uniformly distributed in buffer board and shuts down the bottom of platform, the diameter for shutting down platform with it is slow
The diameter of punching, size all same.
Preferably, the quantity of the directive wheel is four, is evenly distributed in buffer board and the front and the back side of shutting down platform,
The quantity of the guide wheel workpiece is two.
Preferably, the shape of the snap-gauge block is that a quarter is spherical, and the quantity of the Card trough is two, and symmetrical point
It is distributed in the fixed plate at left and right sides of bottom plate.
Three advantageous effects
Compared with prior art, the utility model provides a kind of power assisting device that unmanned plane takes off, and has following beneficial
Effect：
1, the power assisting device that the unmanned plane takes off is equipped with fixed seat by shutting down at the top of platform, can be by the leg of unmanned plane
Portion is stuck in the inside of fixed seat, push shut down platform so that shutdown platform is reversed snap-gauge block snap-gauge cylinder ejector is contacted with snap-gauge block at this time,
Make it that can not rotate to fix snap-gauge block, when unmanned plane needs lift-off, snap-gauge cylinder is retracted, due to the work of snap-gauge tension spring
With making snap-gauge block overturn, platform is shut down under the action of power assistant spring and is popped up, due to the effect of inertia, unmanned plane is made to pop up,
Achieve the purpose that unmanned plane is assisted to take off.
2, the power assisting device that the unmanned plane takes off makes shutdown platform exist by the collective effect of buffer spring and guide wheel workpiece
It protects it repeatedly to work during being bounced up by power assistant spring not to be damaged, by being installed with counterweight at left and right sides of pedestal
Block avoids moving during bouncing up, and influences bouncing up for unmanned plane, and it is extra during bouncing up on the other hand also to protect
Power make to have shot the user that wounds, it is more convenient to use.
Description of the drawings
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is schematic enlarged-scale view at A in the utility model Fig. 1；
Fig. 3 is schematic enlarged-scale view at B in the utility model Fig. 1.
In figure：1 pedestal, 2 bottom plates, 3 fixed plates, 4 buffer springs, 5 limited blocks, 6 buffer boards, 7 leader casings, 8 flexible guide rods,
Platform, 11 directive wheels, 12 guide wheel workpiece, 13 fixed seats, 14 sliding slots, 15 card machine plates, 16 fixed springs, 17 are shut down in 9 power assistant springs, 10
Card trough, 18 snap-gauge cylinders, 19 snap-gauge blocks, 20 bull sticks, 21 snap-gauge tension springs, 22 counterweight tanks, 23 clump weights.
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.
- 3 are please referred to Fig.1, a kind of power assisting device that unmanned plane takes off, including pedestal 1, the top of pedestal 1 are installed with
Bottom plate 2, the top of pedestal 1 and the both sides for being located at bottom plate 2 are installed with fixed plate 3, and fixed plate 3 is symmetric in bottom plate
The quantity of 2 both sides, buffer spring 4 is no less than four, and is uniformly distributed in the top of bottom plate 2, and peace is fixed at the top of bottom plate 2
Equipped with buffer spring 4, the top of bottom plate 2 and it is installed with limited block 5 positioned at the both sides of buffer spring 4, buffer spring 4
Top is installed with buffer board 6, and the inside of buffer board 6 is installed with leader casing 7, and the internal activity of leader casing 7 is connected with
The bottom of flexible guide rod 8, flexible guide rod 8 is flexibly connected with limited block 5, and the top of buffer board 6 is installed with power assistant spring 9,
The quantity of the brute spring of the model 60s i2mn of power assistant spring 9, power assistant spring 9 is no less than two, and is evenly distributed
In the top of buffer board 6, the elastic force of power assistant spring 9 is much larger than the elastic force of buffer spring 4, and the top of power assistant spring 9 is fixedly mounted
Have and shut down platform 10, limited block 5 is uniformly distributed in buffer board 6 and shuts down the bottom of platform 10, shuts down the diameter and buffer board 6 of platform 10
Diameter, size all same, the bottom for shutting down platform 10 are installed with limited block 5, shut down the front and the back side of platform 10 and buffer board 6
It is installed with directive wheel 11, the outside of directive wheel 11 is connected with guide wheel workpiece 12, passes through directive wheel 11 and guide wheel
It is acted on while workpiece 12 and leader casing 7 are with flexible guide rod 8, can effectively ensure that unmanned plane on shutting down platform 10 by upright ejection
Purpose is effectively guaranteed auxiliary unmanned plane and takes off, and the quantity of directive wheel 11 is four, be evenly distributed in buffer board 6 with
The front and the back side of platform 10 are shut down, the quantity of guide wheel workpiece 12 is two, and the top for shutting down platform 10 is installed with fixed seat 13,
The inner bottom wall of fixed seat 13 offers sliding slot 14, and there are two card machine plate 15, two card machine plates 15 for the internal activity connection of sliding slot 14
Opposite side is fixedly connected with fixed spring 16, and the inside of fixed plate 3 offers Card trough 17, and the inside of fixed plate 3 is fixed
It is connected with snap-gauge cylinder 18, the twin shaft double-rod cylinder of the model TN10-100-S of snap-gauge cylinder 18, snap-gauge cylinder 18 is close to lead
The side of wheel workpiece 12 is connected with snap-gauge block 19, and the shape of snap-gauge block 19 is that a quarter is spherical, the quantity of Card trough 17
It is two, and is symmetrically distributed in the fixed plate 3 of 2 left and right sides of bottom plate, 19 internal activity of snap-gauge block is connected with bull stick 20, snap-gauge
Block 19 is rotationally connected with the inside of Card trough 17 by bull stick 20, and side of the snap-gauge block 19 far from guide wheel workpiece 12 is fixedly connected with
Snap-gauge tension spring 21, the other end that snap-gauge tension spring 21 is connect with snap-gauge block 19 are fixedly connected on the inside of Card trough 17, a left side for pedestal 1
Right both sides have been fixedly connected with counterweight tank 22, and the internal activity of two counterweight tanks 22 is connected with clump weight 23, by shutting down platform 10
Top fixed seat 13 is installed, the leg of unmanned plane can be stuck in the inside of fixed seat 13, push and shut down platform 10 and make shutdown platform
10 reverse the ejection of snap-gauge cylinder 18 at this time of snap-gauge block 19 contacts with snap-gauge block 19, makes it that can not turn to fix snap-gauge block 19
Dynamic, when unmanned plane needs lift-off, snap-gauge cylinder 18 is retracted, and since the effect of snap-gauge tension spring 21 makes snap-gauge block 19 overturn, is being helped
Platform 10 is shut down under the action of power spring 9 to pop up, and due to the effect of inertia, unmanned plane is made to pop up, has been reached auxiliary unmanned plane
The purpose taken off makes shutdown platform 10 bounced up by power assistant spring 9 by the collective effect of buffer spring 4 and guide wheel workpiece 12
It protects it repeatedly to work in the process not to be damaged, clump weight 23 is installed with by the left and right sides of pedestal 1, avoid bouncing up
During move, influence bouncing up for unmanned plane, power extra during bouncing up on the other hand also protected to make to have shot
Wound user, more convenient to use.
In conclusion the power assisting device that the unmanned plane takes off, the top by shutting down platform 10 is equipped with fixed seat 13, can incite somebody to action
The leg of unmanned plane is stuck in the inside of fixed seat 13, and pushing shutdown platform 10 makes shutdown platform 10 reverse the snap-gauge cylinder at this time of snap-gauge block 19
18 contact with snap-gauge block 19, make it that can not rotate to fix snap-gauge block 19, when unmanned plane needs lift-off, snap-gauge cylinder 18
It retracts, since the effect of snap-gauge tension spring 21 makes snap-gauge block 19 overturn, shutdown platform 10 pops up under the action of power assistant spring 9,
Due to the effect of inertia, unmanned plane is made to pop up, has achieved the purpose that unmanned plane is assisted to take off.
Also, the power assisting device that the unmanned plane takes off makes to stop by the collective effect of buffer spring 4 and guide wheel workpiece 12
Board 10 is protected it repeatedly to work during being bounced up by power assistant spring 9 and is not damaged, and is fixed by the left and right sides of pedestal 1
Clump weight 23 is installed, avoids moving during bouncing up, bouncing up for unmanned plane is influenced, on the other hand also protects bullet
Extra power makes to have shot the user that wounds during rising, more convenient to use.
It should be noted that the terms "include", "comprise" or its any other variant are intended to the packet of nonexcludability
Contain, so that the process, method, article or equipment including a series of elements includes not only those elements, but also includes
Other elements that are not explicitly listed, or further include for elements inherent to such a process, method, article, or device.
In the absence of more restrictions, the element limited by sentence "including a ...", it is not excluded that including the element
Process, method, article or equipment in there is also other identical elements.
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 power assisting device that unmanned plane takes off, including pedestal (1), it is characterised in that：Peace is fixed at the top of the pedestal (1)
Equipped with bottom plate (2), the top of the pedestal (1) and it is installed with fixed plate (3), the bottom positioned at the both sides of bottom plate (2)
It is installed with buffer spring (4) at the top of plate (2), the top of the bottom plate (2) and solid positioned at the both sides of buffer spring (4)
Dingan County is equipped with limited block (5), is installed with buffer board (6) at the top of the buffer spring (4), the buffer board (6) it is interior
Portion is installed with leader casing (7), and the internal activity of the leader casing (7) is connected with flexible guide rod (8), the flexible guide rod
(8) bottom is flexibly connected with limited block (5), and power assistant spring (9) is installed at the top of the buffer board (6), described to help
It being installed at the top of power spring (9) and shuts down platform (10), the bottom for shutting down platform (10) is installed with limited block (5),
The platform (10) of shutting down is installed with directive wheel (11) with the front of buffer board (6) and the back side, the directive wheel (11)
Outside is connected with guide wheel workpiece (12), and fixed seat (13) is installed at the top of the shutdown platform (10), described solid
The inner bottom wall of reservation (13) offers sliding slot (14), and the internal activity connection of the sliding slot (14) is there are two card machine plate (15), and two
The opposite side of a card machine plate (15) is fixedly connected with fixed spring (16), and the inside of the fixed plate (3) offers card
The inside of board slot (17), the fixed plate (3) is fixedly connected with snap-gauge cylinder (18), and the snap-gauge cylinder (18) is close to guide wheel work
The side of part (12) is connected with snap-gauge block (19), and snap-gauge block (19) internal activity is connected with bull stick (20), the card
Plate (19) is rotationally connected with the inside of Card trough (17) by bull stick (20), and the snap-gauge block (19) is far from guide wheel workpiece (12)
Side be fixedly connected with snap-gauge tension spring (21), the other end that the snap-gauge tension spring (21) connect with snap-gauge block (19) is fixedly connected
Inside in Card trough (17) has been fixedly connected with counterweight tank (22), two counterweight tanks at left and right sides of the pedestal (1)
(22) internal activity is connected with clump weight (23).
2. the power assisting device that a kind of unmanned plane according to claim 1 takes off, it is characterised in that：The fixed plate (3) is in
The both sides of bottom plate (2) are symmetrically distributed in, the quantity of the buffer spring (4) is no less than four, and is uniformly distributed in bottom plate (2)
Top.
3. the power assisting device that a kind of unmanned plane according to claim 1 takes off, it is characterised in that：The power assistant spring (9)
Quantity be no less than two, and be evenly distributed in the top of buffer board (6), the elastic force of the power assistant spring (9) is much larger than
The elastic force of buffer spring (4).
4. the power assisting device that a kind of unmanned plane according to claim 1 takes off, it is characterised in that：The limited block (5) is equal
The even bottom for being distributed in buffer board (6) and shutting down platform (10), it is the diameter of diameter and the buffer board (6) for shutting down platform (10), big
Small all same.
5. the power assisting device that a kind of unmanned plane according to claim 1 takes off, it is characterised in that：The directive wheel (11)
Quantity is four, is evenly distributed in buffer board (6) and the front and the back side of shutting down platform (10), the number of the guide wheel workpiece (12)
Amount is two.
6. the power assisting device that a kind of unmanned plane according to claim 1 takes off, it is characterised in that：The snap-gauge block (19)
Shape is that a quarter is spherical, and the quantity of the Card trough (17) is two, and is symmetrically distributed in consolidating at left and right sides of bottom plate (2)
On fixed board (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820549129.1U CN208086037U (en) | 2018-04-18 | 2018-04-18 | A kind of power assisting device that unmanned plane takes off |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820549129.1U CN208086037U (en) | 2018-04-18 | 2018-04-18 | A kind of power assisting device that unmanned plane takes off |
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| Publication Number | Publication Date |
|---|---|
| CN208086037U true CN208086037U (en) | 2018-11-13 |
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ID=64055441
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820549129.1U Active CN208086037U (en) | 2018-04-18 | 2018-04-18 | A kind of power assisting device that unmanned plane takes off |
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| CN (1) | CN208086037U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111216668A (en) * | 2018-11-23 | 2020-06-02 | 比亚迪股份有限公司 | Vehicle collision processing method and unmanned aerial vehicle fixing device |
| CN112660407A (en) * | 2021-01-13 | 2021-04-16 | 陆颖怡 | High-pressure pneumatic boosting take-off device of light unmanned aerial vehicle |
| CN113492993A (en) * | 2021-09-08 | 2021-10-12 | 佐力西(江苏)物联科技有限公司 | Thing networking unmanned aerial vehicle auxiliary device |
-
2018
- 2018-04-18 CN CN201820549129.1U patent/CN208086037U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111216668A (en) * | 2018-11-23 | 2020-06-02 | 比亚迪股份有限公司 | Vehicle collision processing method and unmanned aerial vehicle fixing device |
| CN112660407A (en) * | 2021-01-13 | 2021-04-16 | 陆颖怡 | High-pressure pneumatic boosting take-off device of light unmanned aerial vehicle |
| CN113492993A (en) * | 2021-09-08 | 2021-10-12 | 佐力西(江苏)物联科技有限公司 | Thing networking unmanned aerial vehicle auxiliary device |
| CN113492993B (en) * | 2021-09-08 | 2021-11-16 | 佐力西(江苏)物联科技有限公司 | Thing networking unmanned aerial vehicle auxiliary device |
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Legal Events
| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210702 Address after: 050000 No. 401, unit 3, building 5, No. 96, Shizheng Road, Qiaodong District, Shijiazhuang City, Hebei Province Patentee after: Ha Long Address before: 561000 Huangguoshu (Sichuan Chongqing) e-commerce Industrial Park, Anshun economic and Technological Development Zone, Guizhou Province Patentee before: GUIZHOU ZINGTO AVIATION TECHNOLOGY Co.,Ltd. |
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| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220915 Address after: 2nd Floor, Building 33, Ludao V Valley Science and Technology Park, No. 181, Shibai South Street, Luquan District, Shijiazhuang City, Hebei Province, 050000 Patentee after: HEBEI ZINGTO AVIATION TECHNOLOGY CO.,LTD. Address before: 050000 No. 401, unit 3, building 5, No. 96, Shizheng Road, Qiaodong District, Shijiazhuang City, Hebei Province Patentee before: Ha Long |
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| TR01 | Transfer of patent right |