CN207389537U - A kind of unmanned plane shock-proof machine frame - Google Patents
A kind of unmanned plane shock-proof machine frame Download PDFInfo
- Publication number
- CN207389537U CN207389537U CN201721354295.8U CN201721354295U CN207389537U CN 207389537 U CN207389537 U CN 207389537U CN 201721354295 U CN201721354295 U CN 201721354295U CN 207389537 U CN207389537 U CN 207389537U
- Authority
- CN
- China
- Prior art keywords
- supporting leg
- pedestal
- unmanned plane
- machine frame
- proof machine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Landscapes
- Toys (AREA)
Abstract
The utility model is related to unmanned air vehicle technique fields, disclose a kind of unmanned plane shock-proof machine frame, including pedestal, the pedestal is circumferentially uniformly arranged at least three supporting legs, the supporting leg is connected with base rotation, each respectively it is connected between supporting leg and pedestal by a spring, the angle α between the supporting leg and pedestal is acute angle.The utility model enables unmanned plane to obtain certain elastic buffer in landing, avoids collision or bounces, to protect the sophisticated electronics on unmanned plane overall structure and machine.
Description
Technical field
The utility model is related to unmanned air vehicle technique field more particularly to a kind of unmanned plane shock-proof machine frames.
Background technology
Unmanned plane is the not manned vehicle manipulated by radio robot or airborne computer stored program controlled,
Unmanned plane is simple in structure, use cost is low, burst thing meet an urgent need, early warning play the role of it is very big.When unmanned plane lands, due to
Own wt, the sinking speed control reasons such as error occur to bounce after colliding or land with ground etc., foot stool it is strong
Vibration can cause airborne sophisticated electronics to break down, thus need to ensure can have buffering during unmanned plane landing.
Utility model content
The goal of the invention of the utility model is：In view of the above problems, a kind of unmanned plane shock-proof machine frame is provided, is made
Unmanned plane landing when can obtain certain elastic buffer, avoid collision or bounce, with protect unmanned plane overall structure with
And the sophisticated electronics on machine.
The technical solution adopted in the utility model is such：A kind of unmanned plane shock-proof machine frame, including pedestal, the pedestal
At least three supporting legs circumferentially are uniformly arranged, the supporting leg is connected with base rotation, is respectively passed through between each supporting leg and pedestal
A piece spring is connected, and the angle α between the supporting leg and pedestal is acute angle.
A kind of unmanned plane shock-proof machine frame described in the utility model offers on the pedestal scarce corresponding to each supporting leg
Mouthful, the supporting leg upper end is installed in notch, and there are one inclined confined planes, the upper ends of the supporting leg for the bottom tool of the notch
Tool is there are one protrusion, and there are one clinoplain corresponding with confined planes, the confined planes and clinoplains for the protrusion tool
During contact or when supporting leg is contacted with the lower edge of confined planes, it can limit rotational angle of the supporting leg compared with pedestal.
A kind of unmanned plane shock-proof machine frame described in the utility model, the both sides of the notch and the upper end of supporting leg open up
There is pin hole, an axis pin is installed in the pin hole, to realize that supporting leg is connected with base rotation.
A kind of unmanned plane shock-proof machine frame described in the utility model offers groove on the pedestal.
A kind of unmanned plane shock-proof machine frame described in the utility model, the supporting leg include epimere and hypomere, the hypomere phase
For epimere to the outer expandable of pedestal, and the angle between epimere and hypomere is obtuse angle.
A kind of unmanned plane shock-proof machine frame described in the utility model is fixedly installed spring base, the bullet on the pedestal
Spring abutment is corresponded with every spring, and one end of spring is fixedly connected with spring base, the friendship of the epimere and hypomere of another end and supporting leg
It is fixedly connected at boundary.
A kind of unmanned plane shock-proof machine frame described in the utility model, the pedestal is corner star, right on each angle
One supporting leg should be set.
In conclusion by adopting the above-described technical solution, the beneficial effects of the utility model are：The utility model structure
Simple and practical, supporting leg is realized using axis pin with pedestal and is rotatablely connected, overhanging to the maximum of supporting leg by the confined planes on pedestal
Angle is limited, and spring is connected between the spring base on supporting leg and pedestal, after unmanned plane goes up to the air, under the action of the spring,
Supporting leg is shunk to pedestal medial movement, but supporting leg and pedestal angle are acute angle, and when unmanned plane lands, supporting leg is moved to chassis outer side
Dynamic expansion a distance, while spring elongation, can absorb vibration during unmanned plane landing, effectively prevent unmanned plane judder
And damage airborne equipment.
Description of the drawings
Fig. 1 is the first axonometric schematic diagram of the utility model；
Fig. 2 is second of axonometric schematic diagram of the utility model；
Fig. 3 is supporting leg link position partial enlarged view in the utility model；
Fig. 4 is supporting leg link position partial sectional view in the utility model.
It is marked in figure：1 is pedestal, and 2 be supporting leg, and 201 be epimere, and 202 be hypomere, and 3 be spring, and 4 be notch, and 5 be /V
Face, 6 be protrusion, and 7 be pin hole, and 8 be axis pin, and 9 be groove, and 10 be spring base.
Specific embodiment
Below in conjunction with the accompanying drawings, the utility model is described in detail.
In order to make the purpose of the utility model, technical solutions and advantages more clearly understood, below in conjunction with attached drawing and implementation
Example, is further elaborated the utility model.It should be appreciated that specific embodiment described herein is only used to explain
The utility model is not used to limit the utility model.
As shown in Figures 1 to 4, a kind of unmanned plane shock-proof machine frame, the top of shock-proof machine frame are used to install unmanned rack（In figure not
It shows）, including pedestal 1, groove 9 is uniformly provided on pedestal 1, pedestal 1 is alleviated while 1 structural strength of pedestal is ensured
Weight, the pedestal 1 is circumferential to be uniformly arranged at least three supporting legs 2, and pedestal 1 is specifically configured to corner starriness herein, every
A supporting leg 2 is correspondingly arranged on one angle so that entire shock-proof machine frame structure is more steady, ensures the stabilization of unmanned plane landing
Property, the supporting leg 2 are rotatablely connected with pedestal 1, are respectively connected between each supporting leg 2 and pedestal 1 by a spring 3, institute
It is acute angle to state the angle α between supporting leg 2 and pedestal 1.
Further, jagged 4 are opened up corresponding to each supporting leg 2 on the pedestal 1, notch 4 is opened in corner star bottom
Each angle end of seat 1,2 upper end of supporting leg are installed in notch 4, and there are one inclined limits for the bottom tool of the notch 4
Plane 5, the upper end tool of the supporting leg 2 is there are one protrusion 6, and there are one inclination corresponding with confined planes 5 is flat for the tool of protrusion 6
Face when the confined planes 5 are contacted with clinoplain or when supporting leg 2 is contacted with the lower edge of confined planes 5, can limit 2 phase of supporting leg
For the rotational angle of pedestal 1；The both sides of the notch 4 and the upper end of supporting leg 2 offer pin hole 7, pacify in the pin hole 7
An axis pin 8 is filled, to realize that supporting leg 2 is rotatablely connected with pedestal 1；Supporting leg 2 is rotatably dispose in notch 4 so that supporting leg 2 and pedestal
Rotation connection between 1 is more stablized, so that supporting leg 2 is compared with the tool of pedestal 1, there are two the limit positions rotated for the setting of confined planes 5
It puts, limits rotational angle of the supporting leg 2 compared with pedestal 1 well.
Further, the supporting leg 2 includes epimere 201 and hypomere 202, and the hypomere 202 is compared with epimere 201 to pedestal
1 outer expandable, and the angle between epimere 201 and hypomere 202 is obtuse angle；Spring base 10 is fixedly installed on the pedestal 1,
The spring base 10 is corresponded with every spring 3, one end of spring 3 is fixedly connected with spring base 10, another end and supporting leg 2 it is upper
Section 201 is fixedly connected with the intersection of hypomere 202；So set, when unmanned plane lands, hypomere 202 contacts ground so that entire
, can be more successfully to 1 outer expandable of pedestal when supporting leg 2 rotates, spring 3 is connected to the boundary of epimere 201 and hypomere 202
Place so that the stretching of spring 3 is more smooth with shrinking.
After unmanned plane goes up to the air, under the action of 3 pulling force of spring, supporting leg 2 is shunk to 1 medial movement of pedestal, confined planes 5
Lower edge is contacted with supporting leg 2, and /V is carried out to supporting leg 2, and when unmanned plane lands, supporting leg 2 expands one section to 1 outside of pedestal is mobile
Distance, while extension spring 3 can absorb vibration during unmanned plane landing, effectively prevent unmanned plane judder and damage machine
Equipment is carried, the tapered plane of protrusion 6 can be contacted with confined planes 5, and confined planes 5 can carry out /V to supporting leg 2.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
All any modification, equivalent and improvement made within the spirit and principle of utility model etc., should be included in the utility model
Protection domain within.
Claims (7)
1. a kind of unmanned plane shock-proof machine frame, it is characterised in that：Including pedestal（1）, the pedestal（1）Circumferentially it is uniformly arranged at least three
A supporting leg（2）, the supporting leg（2）With pedestal（1）Rotation connection, each supporting leg（2）With pedestal（1）Between respectively pass through one
Spring（3）It is connected, the supporting leg（2）With pedestal（1）Between angle α be acute angle.
2. a kind of unmanned plane shock-proof machine frame according to claim 1, it is characterised in that：The pedestal（1）It is upper to correspond to often
A supporting leg（2）It opens up jagged（4）, the supporting leg（2）Upper end is installed on notch（4）It is interior, the notch（4）Bottom have one
A inclined confined planes（5）, the supporting leg（2）Upper end tool there are one protrusion（6）, the protrusion（6）Tool there are one with
Confined planes（5）Corresponding clinoplain, the confined planes（5）When being contacted with clinoplain or supporting leg（2）With confined planes（5）Under
When edge contacts, it can limit supporting leg（2）Compared with pedestal（1）Rotational angle.
3. a kind of unmanned plane shock-proof machine frame according to claim 2, it is characterised in that：The notch（4）Both sides and
Supporting leg（2）Upper end offer pin hole（7）, the pin hole（7）A piece axis pin of interior installation（8）, to realize supporting leg（2）With pedestal
（1）Rotation connection.
4. a kind of unmanned plane shock-proof machine frame according to claim 1, it is characterised in that：The pedestal（1）On open up it is free
Heart slot（9）.
5. a kind of unmanned plane shock-proof machine frame according to claim 1, it is characterised in that：The supporting leg（2）Including epimere
（201）And hypomere（202）, the hypomere（202）Compared with epimere（201）To pedestal（1）Outer expandable, and epimere（201）
With hypomere（202）Between angle be obtuse angle.
6. a kind of unmanned plane shock-proof machine frame according to claim 5, it is characterised in that：The pedestal（1）Upper fixed setting
There is spring base（10）, the spring base（10）With every spring（3）It corresponds, spring（3）One end and spring base（10）Gu
Fixed connection, another end and supporting leg（2）Epimere（201）And hypomere（202）Intersection be fixedly connected.
7. a kind of unmanned plane shock-proof machine frame according to claim 1, it is characterised in that：The pedestal（1）For corner star,
A supporting leg is correspondingly arranged on each angle（2）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721354295.8U CN207389537U (en) | 2017-10-20 | 2017-10-20 | A kind of unmanned plane shock-proof machine frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721354295.8U CN207389537U (en) | 2017-10-20 | 2017-10-20 | A kind of unmanned plane shock-proof machine frame |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207389537U true CN207389537U (en) | 2018-05-22 |
Family
ID=62329057
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721354295.8U Expired - Fee Related CN207389537U (en) | 2017-10-20 | 2017-10-20 | A kind of unmanned plane shock-proof machine frame |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207389537U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113467162A (en) * | 2021-07-12 | 2021-10-01 | 山西迪奥普科技有限公司 | Five-piece camera with adjustable shooting angle |
-
2017
- 2017-10-20 CN CN201721354295.8U patent/CN207389537U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113467162A (en) * | 2021-07-12 | 2021-10-01 | 山西迪奥普科技有限公司 | Five-piece camera with adjustable shooting angle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| KR101633921B1 (en) | Switchboards equipped with a Triaxial twist | |
| US20150354748A1 (en) | Motion simulator | |
| CN207389537U (en) | A kind of unmanned plane shock-proof machine frame | |
| JP6946604B2 (en) | A pan head and an unmanned aerial vehicle with the pan head | |
| KR101601803B1 (en) | Switchboard seismic equipment and seismic switchboard with this | |
| JP2007230734A (en) | Base isolation device of cargo handling machine | |
| CN108083138B (en) | The general unloading bracket of hung antenna | |
| WO2017008530A1 (en) | Landing gear for unmanned aerial vehicle | |
| JP2019133629A (en) | Server rack, server rack moving system, and installation method therefor | |
| KR102406119B1 (en) | Attachment and transfer device having this | |
| JP2016199343A (en) | Support structure of belt conveyer | |
| CN209433873U (en) | A kind of hard disc of computer bracing means | |
| KR101090842B1 (en) | Table having folding structure | |
| CN204679908U (en) | A kind of cooling pad foot device | |
| CN209265347U (en) | A kind of computer vibration abatement | |
| KR101757700B1 (en) | Switchboard having earthquake proof device | |
| KR101751752B1 (en) | Device safety for harrow | |
| CN210084433U (en) | Transfer table | |
| KR101757704B1 (en) | Switchboard having earthquake proof device | |
| CN205453664U (en) | Low phase noise missile -borne anti vibration frequency synthesizer | |
| KR101814518B1 (en) | Lifting apparatus | |
| CN205663819U (en) | Cabinet body's shock insulation lower margin structure | |
| CN207840590U (en) | A kind of integrated machine accessory automatic assembly equipment | |
| CN112303173A (en) | Shock attenuation formula installation base for sweet potato pump | |
| KR101029305B1 (en) | Folding type table |
Legal Events
| 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: 20180522 Termination date: 20211020 |