CN207931983U - A kind of unmanned plane undercarriage being easily installed - Google Patents
A kind of unmanned plane undercarriage being easily installed Download PDFInfo
- Publication number
- CN207931983U CN207931983U CN201820281410.1U CN201820281410U CN207931983U CN 207931983 U CN207931983 U CN 207931983U CN 201820281410 U CN201820281410 U CN 201820281410U CN 207931983 U CN207931983 U CN 207931983U
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- Prior art keywords
- unmanned plane
- quick
- cylinder
- snap device
- briquetting
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Abstract
The utility model discloses a kind of unmanned plane undercarriage being easily installed, including unmanned plane, the first quick-snap device is provided with below the unmanned plane, and the lower section of unmanned plane is provided with the second quick-snap device at a side position of the first quick-snap device, the corresponding first quick-snap device in lower surface of the unmanned plane is provided with fixed card slot, and reinforcing rib is connected between the first quick-snap device and the second quick-snap device.The utility model is simple in structure, it is easy to operate, provided with the first quick-snap device, undercarriage can be made easy for removal and installation by the first quick-snap device, reduce the volume of unmanned plane, play the effect convenient for collecting, provided with buffer unit, undercarriage can be made to play cushioning effect by buffer unit, improve stability, the service life for increasing unmanned plane, avoid the problem that unmanned plane in landing because dynamics is excessive cause to unmanned plane caused by counter shake.
Description
Technical field
The utility model is related to unmanned plane undercarriage technical fields more particularly to a kind of unmanned plane being easily installed to rise and fall
Frame.
Background technology
With social development, unmanned plane has been applied to every field, such as takes photo by plane, rescues, goes on patrol, and unmanned plane is rising and falling
When be required for using undercarriage, still, the undercarriage for unmanned plane of taking photo by plane on the market at present is all integrally fixed at the lower surface of unmanned plane,
It can not dismantle, increase volume, be not easy to whole be packaged and collect, now design a unmanned plane undercarriage, it can be with effective solution
Undercarriage is not easy to the problem of dismounting.
Utility model content
The problem of purpose of the utility model is to solve proposed in above-mentioned background technology, and the one kind proposed is convenient for
The unmanned plane undercarriage of installation.
To achieve the goals above, the utility model uses following technical solution：An a kind of unmanned plane being easily installed
Frame, including unmanned plane are fallen, the first quick-snap device is provided with below the unmanned plane, and the lower section of unmanned plane is close to first
The second quick-snap device is provided at one side position of quick-snap device, the lower surface corresponding first of the unmanned plane is fast
Fast clamping close device is provided with fixed card slot, and reinforcement is connected between the first quick-snap device and the second quick-snap device
Muscle, and it is connected with buffer unit below the first quick-snap device, supporting rack is provided with below the buffer unit, it is described
Cushion block is fixed with below supporting rack.
Preferably, the first quick-snap device includes cylinder, fixed link, briquetting, briquetting, the first spring, activity
The outside of bar, the first fixture block, telescopic rod and the second fixture block, the first quick-snap device is provided with cylinder, the cylinder
The second fixture block is provided with above one end, and is fixedly connected by fixed link between cylinder and the second fixture block, the cylinder it is another
It is provided with the first fixture block at the position of corresponding second fixture block in end top, and motion bar is connected between cylinder and the first fixture block,
One end of the cylinder is provided with briquetting, and is provided with the first bullet at a side position of briquetting inside one end of cylinder
Spring, is provided with briquetting inside one end of the cylinder at a side position of the first spring, the fixed link and motion bar it
Between connection expansion link.
Preferably, one end of the briquetting is provided with first connecting rod, and the other end of first connecting rod runs through cylinder and briquetting
It is fixedly connected.
Preferably, notch is offered at the position of the corresponding motion bar of the end surface of the cylinder.
Preferably, it is fixedly connected by the second connecting rod between the motion bar and briquetting.
Preferably, the buffer unit includes second spring, buffer pull rod, supporting rod, snap ring, fixed block, the buffering
The outside of device is provided with fixed block, buffer pull rod is connected on the inside of the fixed block, and the front surface of fixed block is provided with
The side of snap ring, the snap ring is connected with second spring, and the side of the buffer pull rod is provided with supporting rod.
Preferably, it is rotatablely connected by shaft between the buffer pull rod and fixed block, and one end of buffer pull rod and branch
By being welded and fixed between strut.
Preferably, the end surface of the buffer pull rod is provided with connection ring, and one end of the second spring passes through snap ring
It is fixedly connected with fixed block, and the other end of second spring is fixedly connected by connection ring with buffer pull rod.
Compared with prior art, the utility model provides a kind of unmanned plane undercarriage being easily installed, and having following has
Beneficial effect：The utility model is simple in structure, easy to operate, is provided with the first quick-snap device, is attached together by the first rapid card
Setting can make undercarriage easy for removal and installation, reduce the volume of unmanned plane, play the effect convenient for collecting, and be provided with buffering
Device can make undercarriage play cushioning effect, improve stability by buffer unit, increase the whole of unmanned plane and use
Service life, avoid the problem that unmanned plane landing when because dynamics is excessive cause to unmanned plane caused by it is counter shake, be provided with reinforcing rib, pass through
What reinforcing rib can make to connect between the first quick-snap device and the second quick-snap device more stablizes, and avoids the occurrence of shaking
Some potential safety problems is caused to unmanned plane landing.
Description of the drawings
Attached drawing is used to provide a further understanding of the present invention, and a part for constitution instruction, with this practicality
Novel embodiment for explaining the utility model, does not constitute limitations of the present invention together.In the accompanying drawings：
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the structural schematic diagram of the utility model the first quick-snap device；
Fig. 3 is the structural schematic diagram of the utility model fixed card slot；
In figure：1, unmanned plane；2, the first quick-snap device；201, cylinder；202, fixed link；203, briquetting；204、
Briquetting；205, the first spring；206, motion bar；207, the first fixture block；208, telescopic rod；209, the second fixture block；3, buffer unit；
301 second springs；302, buffer pull rod；303, supporting rod；304, snap ring；305, fixed block；4, reinforcing rib；5, the second rapid card
It attaches together and sets；6, fixed card slot；7, supporting rack；8, cushion block.
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.
In the description of the present invention, it should be understood that term "upper", "lower", "front", "rear", "left", "right",
The orientation or positional relationship of the instructions such as "top", "bottom", "inner", "outside" is to be based on the orientation or positional relationship shown in the drawings, and is only
The utility model and simplifying describes for ease of description, do not indicate or imply the indicated device or element must have it is specific
Orientation, with specific azimuth configuration and operation, therefore should not be understood as limiting the present invention.
Embodiment：Referring to Fig.1-3, the utility model provides a kind of technical solution：A kind of unmanned plane being easily installed rises and falls
The lower section of frame, including unmanned plane 1, unmanned plane 1 is provided with the first quick-snap device 2, and the lower section of unmanned plane 1 is fast close to first
The second quick-snap device 5 is provided at one side position of fast clamping close device 2, the lower surface corresponding first of unmanned plane 1 is quick
Clamping close device 2 is provided with fixed card slot 6, and reinforcing rib is connected between the first quick-snap device 2 and the second quick-snap device 5
4, and the lower section of the first quick-snap device 2 is connected with buffer unit 3, the lower section of buffer unit 3 is provided with supporting rack 7, support
The lower section of frame 7 is fixed with cushion block 8.
In order to play the role of being rapidly assembled and disassembled, in the present embodiment, it is preferred that the first quick-snap device 2
Including cylinder 201, fixed link 202, briquetting 203, briquetting 204, the first spring 205, motion bar 206, the first fixture block 207, stretch
The outside of contracting bar 208 and the second fixture block 209, the first quick-snap device 2 is provided with cylinder 201, is set above one end of cylinder 201
Be equipped with the second fixture block 209, and be fixedly connected by fixed link 202 between cylinder 201 and the second fixture block 209, cylinder 201 it is another
It is provided with the first fixture block 207 at the position of corresponding second fixture block 209 above end, and is connected between cylinder 201 and the first fixture block 207
It is connected to motion bar 206, one end of cylinder 201 is provided with briquetting 203, and close to briquetting 203 inside one end of cylinder 201
It is provided with the first spring 205 at one side position, is arranged at a side position of the first spring 205 inside one end of cylinder 201
There is briquetting 204, connection expansion link 208 between fixed link 202 and motion bar 206.
In order to which by briquetting 203 application pressure can be carried out to briquetting 204, in the present embodiment, it is preferred that briquetting
203 one end is provided with first connecting rod, and the other end of first connecting rod is fixedly connected through cylinder 201 with briquetting 204.
In order to allow motion bar 206 to be moved on the surface of cylinder, in the present embodiment, it is preferred that the one of cylinder 201
Notch is offered at the position of the corresponding motion bar of end surfaces 206.
In order to motion bar 206 be driven to operate by briquetting 204, in the present embodiment, it is preferred that motion bar 206 and pressure
It is fixedly connected by the second connecting rod between block 204.
In order to play the effect of buffering, in the present embodiment, it is preferred that buffer unit 3 includes that second spring 301, buffering are drawn
The outside of bar 302, supporting rod 303, snap ring 304, fixed block 305, buffer unit 3 is provided with fixed block 305, fixed block 305
Inside is connected with buffer pull rod 302, and the front surface of fixed block 305 is provided with snap ring 304, and the side of snap ring 304 is connected with
The side of two springs 301, buffer pull rod 302 is provided with supporting rod 303.
In order to allow buffer pull rod 302 in the inside of fixed block 205 activity, the present embodiment, it is preferred that buffer pull rod
It is rotatablely connected by shaft between 302 and fixed block 305, and passes through welding between one end of buffer pull rod 302 and supporting rod 303
It is fixed.
In order to improve buffering effect, in the present embodiment, it is preferred that the end surface of buffer pull rod 302 is provided with connection ring,
One end of second spring 301 is fixedly connected by snap ring 304 with fixed block 305, and the other end of second spring 301 passes through connection
Ring is fixedly connected with buffer pull rod 302.
Undercarriage is passed through the first quick-snap device 2 and unmanned plane 1 by the principles of the present invention and process for using first
It is connected together by fixed card slot 6, undercarriage can be made easy for removal and installation, reduced the volume of unmanned plane 1, play and be convenient for
The effect collected, the first quick-snap device 2, which need to only press briquetting 203 in engaging, makes the first fixture block 207 and fixed card slot 6
Engaged, is then connected with reinforcing rib 4 between the first quick-snap device 2 and the second quick-snap device 5, first can be made
What is connected between quick-snap device 2 and the second quick-snap device 5 more stablizes, and avoids the occurrence of shaking and lands to unmanned plane 1
Some potential safety problems is caused, undercarriage can be made to play cushioning effect finally by buffer unit 3, improve stability, is increased
The service life for having added unmanned plane 1, avoid unmanned plane 1 landing when because dynamics is excessive cause to unmanned plane 1 caused by it is counter shake ask
Topic.
The preferable specific implementation mode of the above, only the utility model, but the scope of protection of the utility model is not
Be confined to this, any one skilled in the art within the technical scope disclosed by the utility model, according to this practicality
Novel technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model
Within enclosing.
Claims (8)
1. a kind of unmanned plane undercarriage being easily installed, including unmanned plane (1), it is characterised in that：The lower section of the unmanned plane (1)
It is provided with the first quick-snap device (2), and the lower section of unmanned plane (1) is close to a side position of the first quick-snap device (2)
Place is provided with the second quick-snap device (5), and the corresponding first quick-snap device (2) in lower surface of the unmanned plane (1) sets
It is equipped with fixed card slot (6), reinforcing rib is connected between the first quick-snap device (2) and the second quick-snap device (5)
(4), it and below the first quick-snap device (2) is connected with buffer unit (3), is provided with below the buffer unit (3)
Supporting rack (7) is fixed with cushion block (8) below support frame as described above (7).
2. a kind of unmanned plane undercarriage being easily installed according to claim 1, it is characterised in that：First rapid card
It includes cylinder (201), fixed link (202), briquetting (203), briquetting (204), the first spring (205), motion bar to attach together and set (2)
(206), the first fixture block (207), telescopic rod (208) and the second fixture block (209), the outside of the first quick-snap device (2)
It is provided with cylinder (201), the second fixture block (209), and cylinder (201) and second are provided with above one end of the cylinder (201)
It is fixedly connected by fixed link (202) between fixture block (209), corresponding second fixture block above the other end of the cylinder (201)
(209) it is provided with the first fixture block (207) at position, and motion bar is connected between cylinder (201) and the first fixture block (207)
(206), one end of the cylinder (201) is provided with briquetting (203), and close to briquetting inside one end of cylinder (201)
(203) the first spring (205) is provided at a side position, one end inside of the cylinder (201) is close to the first spring (205)
A side position at be provided with briquetting (204), connection expansion link (208) between the fixed link (202) and motion bar (206).
3. a kind of unmanned plane undercarriage being easily installed according to claim 2, it is characterised in that：The briquetting
(203) one end is provided with first connecting rod, and the other end of first connecting rod is fixedly connected through cylinder (201) with briquetting (204).
4. a kind of unmanned plane undercarriage being easily installed according to claim 2, it is characterised in that：The cylinder (201)
The corresponding motion bar of end surface (206) position at offer notch.
5. a kind of unmanned plane undercarriage being easily installed according to claim 2, it is characterised in that：The motion bar
(206) it is fixedly connected by the second connecting rod between briquetting (204).
6. a kind of unmanned plane undercarriage being easily installed according to claim 1, it is characterised in that：The buffer unit
(3) include second spring (301), buffer pull rod (302), supporting rod (303), snap ring (304), fixed block (305), the buffering
The outside of device (3) is provided with fixed block (305), buffer pull rod (302) is connected on the inside of the fixed block (305), and solid
The front surface for determining block (305) is provided with snap ring (304), and the side of the snap ring (304) is connected with second spring (301), described
The side of buffer pull rod (302) is provided with supporting rod (303).
7. a kind of unmanned plane undercarriage being easily installed according to claim 6, it is characterised in that：The buffer pull rod
(302) it is rotatablely connected by shaft between fixed block (305), and between one end of buffer pull rod (302) and supporting rod (303)
By being welded and fixed.
8. a kind of unmanned plane undercarriage being easily installed according to claim 6, it is characterised in that：The buffer pull rod
(302) end surface is provided with connection ring, and one end of the second spring (301) passes through snap ring (304) and fixed block (305)
It is fixedly connected, and the other end of second spring (301) is fixedly connected by connection ring with buffer pull rod (302).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820281410.1U CN207931983U (en) | 2018-02-28 | 2018-02-28 | A kind of unmanned plane undercarriage being easily installed |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820281410.1U CN207931983U (en) | 2018-02-28 | 2018-02-28 | A kind of unmanned plane undercarriage being easily installed |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207931983U true CN207931983U (en) | 2018-10-02 |
Family
ID=63653412
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820281410.1U Expired - Fee Related CN207931983U (en) | 2018-02-28 | 2018-02-28 | A kind of unmanned plane undercarriage being easily installed |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207931983U (en) |
-
2018
- 2018-02-28 CN CN201820281410.1U patent/CN207931983U/en not_active Expired - Fee Related
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Legal Events
| 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: 20181002 Termination date: 20190228 |
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| CF01 | Termination of patent right due to non-payment of annual fee |