CN207089639U - A kind of new unmanned plane foot stool and unmanned plane - Google Patents
A kind of new unmanned plane foot stool and unmanned plane Download PDFInfo
- Publication number
- CN207089639U CN207089639U CN201720727005.3U CN201720727005U CN207089639U CN 207089639 U CN207089639 U CN 207089639U CN 201720727005 U CN201720727005 U CN 201720727005U CN 207089639 U CN207089639 U CN 207089639U
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- China
- Prior art keywords
- unmanned plane
- foot stool
- damping
- support
- damping part
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Abstract
The utility model discloses a kind of unmanned plane foot stool, including：Support foot rest and damping foot stool；Two support feets that the support foot rest includes the connection member at top and connecting portion both sides extend separately down, the connecting portion of the support foot rest are used to connect unmanned aerial vehicle body, and the support feet is used to support unmanned plane upright.The utility model also provides a kind of unmanned plane, including any one unmanned plane foot stool that the application provides.The utility model is advantageous to increase the distance of fuselage bottom from the ground, so as to prevent in unmanned plane descent, fuselage inner bottom part camera and sensing unit collide with bottom surface protrusion by setting support foot rest and damping foot stool on unmanned plane；Impulsive force during unmanned plane landing can effectively be slowed down, extend unmanned plane service life；The utility model structure is frivolous, has a graceful figure, and Material Strength is high, under the premise of the navigation performance of unmanned plane is not damaged, effectively enhances damping, shatter-resistant performance.
Description
Technical field
It the utility model is related to unmanned air vehicle technique field, more particularly to a kind of new unmanned plane foot stool and unmanned plane.
Background technology
Unmanned plane is the not manned aircraft manipulated using wireless remote control device and the program control facility provided for oneself.Unmanned plane with
Its take action flexibly, landing environmental requirement it is relatively low, and with good operating characteristics etc., be widely used in take photo by plane, monitor, investigating,
The numerous areas such as search and rescue.Existing unmanned plane typically all has foot stool, in order to which unmanned plane is when landing, can pass through its foot stool
To unmanned plane standing support.
However, at UAV Landing, particularly when unmanned plane breaks down quickly. in unmanned plane in actual use
When falling, due to speed when unmanned plane lands, it is larger that the earth's surface of landing point can pass to unmanned plane body by foot stool
Impulsive force.This impulsive force easily damages the valuable part in unmanned plane, or the uav bottom foot stool that fractures, cause unmanned plane without
Method safe landing.
To solve this problem, existing unmanned plane is general all by the more thick and heavy of foot rest structure design, to ensure foot stool
Intensity, still, thick and heavy foot rest structure can increase the weight of unmanned plane, influence the flying distance of unmanned plane, in addition, thick and heavy pin
Frame structure also influences the attractive in appearance of unmanned plane.Therefore, the prior art is defective, it is necessary to improve.
Utility model content
The purpose of this utility model is overcome the deficiencies in the prior art, there is provided a kind of new unmanned plane foot stool and unmanned plane.
The technical solution of the utility model is as follows：
The utility model provides a kind of unmanned plane foot stool first, including：Support foot rest installed in unmanned aerial vehicle body bottom
With the damping foot stool installed in uav bottom surrounding；The support foot rest includes connection member and the connecting portion both sides at top
Two support feets extended separately down, the connecting portion of the support foot rest are used to connect unmanned aerial vehicle body, and the support feet is used for
Support unmanned plane upright.
Further, the connecting portion of the support foot rest is horizontal positioned U-typed structure, the two of the "u"-shaped
End extends two support feets for forming "eight" shape separately down, and the bottom of the support feet outwards turns down.At the top of the support feet
Distance apart from ground is 30-60mm, as a preferred embodiment, selecting 45mm herein.
Further, the damping foot stool is tortuous wavy shaped configuration, and the bottom of the damping foot stool is to horizontal direction
Turnover.
Further, the damping foot stool is the string configuration for stretching out, bending；The damping part is along length side
To the hole provided with some hollow outs.
More preferably, the damping foot stool includes extension component and damping part, one end and the unmanned plane bottom of the extension
Portion is connected, and the other end is connected with damping part.
Preferably, the structure of the damping part is tortuous wavy shaped configuration, and the bottom of the damping part is to level
Direction turns down.
Preferably, the structure of the damping part is with stretching out extension component junction, bending from damping part
String configuration；The damping part is provided with the hole of some hollow outs along its length.
Further, the damping part is additionally provided with adapter sleeve, the adapter sleeve and damping portion with extension component junction
Part is connected, and the extension component other end is stretched into adapter sleeve.
Further, the damping foot stool overturns connection with uav bottom or is fixedly connected.
The utility model also provides a kind of unmanned plane, including any one unmanned plane foot stool that the application provides.
Using such scheme, the utility model on unmanned plane by setting support foot rest and damping foot stool, support foot rest
Be advantageous to increase fuselage bottom distance from the ground, so as to prevent in unmanned plane descent, fuselage inner bottom part camera and quick
Feel part to collide with bottom surface protrusion, cause unmanned plane to damage；Damping foot stool can effectively slow down the vibrations of unmanned plane descent；
Because support foot rest and damping foot stool are dispersedly distributed in uav bottom surrounding, support foot rest and damping foot stool coordinate together,
More stable landing can be formed when unmanned plane lands, can effectively slow down impulsive force during unmanned plane landing, protect unmanned plane
Internal precision element, extend unmanned plane service life；Unmanned plane foot rest structure in the utility model is frivolous, has a graceful figure, knot
Structure itself uses high intensity material, effectively enhances damping, the support performance of unmanned plane, and does not damage the navigation of unmanned plane
Performance.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is explosive view of the present utility model；
Fig. 3 is front view of the present utility model.
Embodiment
Below in conjunction with the drawings and specific embodiments, the utility model is described in detail.
Referring to figs. 1 to shown in Fig. 3, the utility model provides a kind of unmanned plane foot stool, including：Installed in unmanned aerial vehicle body 1
The support foot rest 5 of bottom and the damping foot stool 6 installed in uav bottom surrounding；The support foot rest 5 includes the connection at top
Two support feets 52 that part 51 and the both sides of connecting portion 51 extend separately down, the connecting portion 51 of the support foot rest 5 are used to connect
Unmanned aerial vehicle body 1 is connect, the support feet 52 is used to support unmanned plane upright.
Specifically, the connecting portion 51 of the support foot rest 5 is horizontal positioned U-typed structure, the "u"-shaped
Both ends extend two support feets 52 to form "eight" shape separately down, and the bottom of the support feet 52 outwards turns down.Unmanned plane drops
When falling, the support feet 52 of this structure can produce the deformation of bending, and recover rapidly, and this deformation is advantageous to slow down unmanned plane drop
Impulsive force when falling.The distance d of the top of support feet 52 from the ground scope is 30-60mm, as a preferred embodiment, select herein
Select 45mm.Increase support feet 52 is highly advantageous for increasing the distance of the bottom of fuselage 1 from the ground, so as to prevent unmanned plane from landing
Cheng Zhong, the inner bottom part camera of fuselage 1 and sensing unit collide with bottom surface protrusion, cause unmanned plane to damage.
The damping foot stool 6 can be fixedly connected on uav bottom, can also overturn and connect with uav bottom.When subtracting
When shake foot stool 6 is fixedly connected on uav bottom, the supporting construction of damping foot stool 6 can be preferably maintained；When damping foot stool 6 with
During uav bottom upset connection, the fold inward of damping foot stool 6 can be facilitated packaging and the transport of unmanned plane.The shock-absorbing foot
Frame 6 can be single shock-damping structure or the composite construction including extension component 61 and damping part 62.
When damping foot stool 6 is single shock-damping structure, the structure of the damping foot stool 6 is tortuous wavy shaped configuration,
The bottom of the damping foot stool 6 turns down to horizontal direction.This structure is advantageous to allow damping foot stool 6 as spring, absorbs nothing
The impulsive force brought during man-machine landing, damping effect is produced, and effectively protect the fine structure inside unmanned plane.The shock-absorbing foot
The structure of frame 6 can also be the string configuration for stretching out, bending；The damping foot stool 6 is provided with some engrave along its length
Empty hole.When unmanned plane lands, the damping foot stool 6 of this structure can produce the deformation of bending, and recover rapidly, this deformation
Be advantageous to slow down impulsive force during unmanned plane landing.
When damping foot stool 6 includes extension component 61 and damping part 62, one end of the extension component 61 and unmanned plane
Bottom is connected, and the other end is connected with damping part 62.The junction of extension component 61 is additionally provided with adapter sleeve, the adapter sleeve and damping
Part is connected, and the described one end of extension component 61 away from unmanned plane is stretched into adapter sleeve.Extension component 61 is advantageous to increase nobody
Machine and the distance on ground, when avoiding the unmanned plane from dropping to out-of-flatness ground, bottom surface projection is wounded the fuselage of unmanned plane, so as to protect
Unmanned plane internal precision part.The damping part 62 can be tortuous wavy shaped configuration, the bottom of the damping foot stool 6 to
Horizontal direction turns down.The damping part 6 can also be stretch out from damping part 62 ' and the junction of extension component 61,
The string configuration of bending；The damping part 62 ' is provided with the hole of some hollow outs along its length.These structures are advantageous to increase
The damping performance of strong unmanned plane.
It is noted that unmanned plane foot rest structure provided by the utility model is frivolous, it has a graceful figure, structure itself uses
High intensity material, effectively enhances damping, the support performance of unmanned plane, and does not damage the navigation performance of unmanned plane.This reality
A kind of unmanned plane, including above-mentioned unmanned plane foot stool are also provided with new.
As a kind of embodiment, unmanned plane includes：1, four, fuselage, 3, four propellers 4 of engine of horn 2, four；Institute
State four horns 2 and be distributed in the both sides of fuselage 1 two-by-two, the end of four horns 2 is respectively equipped with engine 3, four engines 3
Top be respectively equipped with propeller 4.Unmanned plane also includes support foot rest 5 and damping foot stool 6, wherein, support foot rest 5 is arranged on machine
The bottom of body 1, the frame of shock-absorbing foot 6 are arranged on the lower section of engine 3.
The number of the damping foot stool 6 can decide as circumstances require, and can increase the number of damping foot stool 6 for enhancing damping performance, be
The number of damping foot stool 6 can be reduced by mitigating unmanned plane weight.Unmanned plane selects two damping foot stools 6 herein, and is attached separately to nothing
The lower section of engine 3 of man-machine front end, to keep the balance of unmanned plane, support foot rest 5 is arranged on the position rearward of unmanned aerial vehicle body 1
Bottom.When unmanned plane lands, firm three-legged structure is formed between a support foot rest 5 and two damping foot stools 6, it is common real
Existing unmanned plane stable landing.
Optimizing as one kind, damping foot stool 6 includes extension component 61 and damping part 62 herein, and the one of the extension 61
End is connected with uav bottom, and the other end is connected with damping part.The junction of extending portion part 61 is additionally provided with adapter sleeve, the adapter sleeve
It is connected with damping part, the described one end of extension component 61 away from unmanned plane is stretched into adapter sleeve.Extension component 61 is advantageous to increase
Big unmanned plane and the distance on ground, when avoiding the unmanned plane from dropping to out-of-flatness ground, bottom surface projection is wounded the fuselage 1 of unmanned plane,
So as to protect unmanned plane internal precision part.Waveform damping part 62 is advantageous to allow damping foot stool 6 as spring, absorbs nothing
The impulsive force brought during man-machine landing, damping effect is produced, and effectively protect the fine structure inside unmanned plane.
In summary, the utility model on unmanned plane by setting support foot rest and damping foot stool, support foot rest favourable
In the distance of increase fuselage bottom from the ground, so as to prevent in unmanned plane descent, fuselage inner bottom part camera and sensitive portion
Part collides with bottom surface protrusion, causes unmanned plane to damage；Damping foot stool can effectively slow down the vibrations of unmanned plane descent；Due to
Support foot rest and damping foot stool are dispersedly distributed in uav bottom surrounding, and support foot rest and damping foot stool coordinate together, in nothing
More stable landing can be formed during man-machine landing, can effectively slow down impulsive force during unmanned plane landing, protect inside unmanned plane
Precision element, extend unmanned plane service life；Unmanned plane foot rest structure in the utility model is frivolous, has a graceful figure, and structure is certainly
Body uses high intensity material, effectively enhances damping, the shatter-resistant performance of unmanned plane, and does not damage the navigation of unmanned plane
Energy.
Preferred embodiment of the present utility model is these are only, is not limited to the utility model, it is all in this practicality
All any modification, equivalent and improvement made within new spirit and principle etc., should be included in guarantor of the present utility model
Within the scope of shield.
Claims (10)
- A kind of 1. unmanned plane foot stool, it is characterised in that including：Installed in the support foot rest of unmanned aerial vehicle body bottom and installed in nothing The damping foot stool of people's motor spindle surrounding；The support foot rest includes the connection member at top and connecting portion both sides are prolonged separately down Two support feets stretched, the connecting portion of the support foot rest are used to connect unmanned aerial vehicle body, and the support feet is used to support unmanned plane Uprightly.
- 2. unmanned plane foot stool according to claim 1, it is characterised in that the connecting portion of the support foot rest is horizontal positioned U-typed structure, the both ends of the "u"-shaped extend two support feets to form "eight" shape, the support feet separately down Bottom outwards turn down.
- 3. unmanned plane foot stool according to claim 1, it is characterised in that the damping foot stool includes extension component and damping Part, one end of the extension are connected with uav bottom, and the other end is connected with damping part.
- 4. unmanned plane foot stool according to claim 3, it is characterised in that the structure of the damping part is tortuous wave Shape structure, the bottom of the damping part turn down to horizontal direction.
- 5. unmanned plane foot stool according to claim 3, it is characterised in that the structure of the damping part is from damping part The string configuration for stretching out, bending is acted with extension component junction；The damping part is provided with some engrave along its length Empty hole.
- 6. the unmanned plane foot stool according to any one in claim 4-5, it is characterised in that the damping part and extension Part junction is additionally provided with adapter sleeve, and the adapter sleeve is connected with damping part, and the extension component other end stretches into adapter sleeve It is interior.
- 7. unmanned plane foot stool according to claim 1, it is characterised in that the damping foot stool is tortuous waveform knot Structure, the bottom of the damping foot stool turn down to horizontal direction.
- 8. unmanned plane foot stool according to claim 1, it is characterised in that the damping foot stool is to stretch out, bend String configuration；The damping part is provided with the hole of some hollow outs along its length.
- 9. according to the unmanned plane foot stool described in claim 7-8 any one, it is characterised in that the damping foot stool and unmanned plane Bottom reversed connects.
- 10. a kind of unmanned plane, it is characterised in that including the unmanned plane foot stool described in claim 1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720727005.3U CN207089639U (en) | 2017-06-21 | 2017-06-21 | A kind of new unmanned plane foot stool and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720727005.3U CN207089639U (en) | 2017-06-21 | 2017-06-21 | A kind of new unmanned plane foot stool and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207089639U true CN207089639U (en) | 2018-03-13 |
Family
ID=61553093
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720727005.3U Expired - Fee Related CN207089639U (en) | 2017-06-21 | 2017-06-21 | A kind of new unmanned plane foot stool and unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207089639U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108528685A (en) * | 2018-04-27 | 2018-09-14 | 宋忠春 | A kind of multi-functional undercarriage of unmanned plane |
-
2017
- 2017-06-21 CN CN201720727005.3U patent/CN207089639U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108528685A (en) * | 2018-04-27 | 2018-09-14 | 宋忠春 | A kind of multi-functional undercarriage of unmanned plane |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| 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: 20180313 Termination date: 20180621 |