CN206826920U - A kind of detachable unmanned plane crash-proof bracket - Google Patents
A kind of detachable unmanned plane crash-proof bracket Download PDFInfo
- Publication number
- CN206826920U CN206826920U CN201720655037.7U CN201720655037U CN206826920U CN 206826920 U CN206826920 U CN 206826920U CN 201720655037 U CN201720655037 U CN 201720655037U CN 206826920 U CN206826920 U CN 206826920U
- Authority
- CN
- China
- Prior art keywords
- mounting
- unmanned plane
- mounting cylinder
- mounting blocks
- proof bracket
- 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
- Vibration Dampers (AREA)
Abstract
The utility model discloses a kind of detachable unmanned plane crash-proof bracket, including base, the base lower end is provided with mounting blocks, the mounting blocks side is provided with cross bar, the cross bar includes cross tube and sheer pole, and the cross bar side is provided with mounting cylinder, damper is provided with the mounting cylinder, the mounting cylinder includes upper mounting cylinder and lower mounting cylinder, and the damper includes yielding rubber and damping spring.Beneficial effect is：The detachable unmanned plane crash-proof bracket adds the damper, can effectively slow down influence of the shock on when unmanned plane lands and ground to fuselage, extends service life and the maintenance period of unmanned plane, use cost significantly reduces, meanwhile removing and installing very simple conveniently, practicality is good.
Description
Technical field
Detachable unmanned plane crash-proof bracket field is the utility model is related to, more particularly to a kind of detachable unmanned plane anticollision
Support.
Background technology
At present, the frame installed on unmanned plane is generally no to install damping anticollision device, collision-prevention device additional, therefore in unmanned plane landing or aerial
Catastrophic failure and when falling, frame faces the impact of unmanned aerial vehicle body in which can not buffer well, causes unmanned plane to be damaged
Seriously, and usually frequently land unmanned plane, and certain shock can be caused to fuselage by droping to ground every time in addition, because
This, traditional unmanned plane service life is universal shorter, and the maintenance cycle is shorter, and use cost remains high for a long time.For
The above situation, a kind of detachable unmanned plane crash-proof bracket can be designed to solve the above problems.
Utility model content
The purpose of this utility model is that to solve the above problems and provides a kind of detachable unmanned plane crash-proof bracket.
The utility model is achieved through the following technical solutions above-mentioned purpose：
A kind of detachable unmanned plane crash-proof bracket, including base, the base lower end are provided with mounting blocks, the mounting blocks
Side is provided with cross bar, and the cross bar includes cross tube and sheer pole, and the cross bar side is provided with mounting cylinder, the mounting cylinder
Damper is inside provided with, the mounting cylinder includes upper mounting cylinder and lower mounting cylinder, and the damper includes yielding rubber and damping
Spring.
In order to further improve the practicality of detachable unmanned plane crash-proof bracket, the mounting blocks are cylindrical structural, Gu
Dingan County is in the base lower surface, and its side is provided with mounting hole, and the mounting hole is through hole, and its quantity has two, point
Side upper end and positive lower end of the other position with the mounting blocks, wherein, the central axis of two mounting holes is mutually perpendicular to.
In order to further improve the practicality of detachable unmanned plane crash-proof bracket, the cross tube is embedded in the mounting blocks
Side upper end the mounting hole in and be fixedly connected with the mounting blocks, the sheer pole is being embedded in the mounting blocks just
It is fixedly connected in the mounting hole of face lower end and with the mounting blocks.
In order to further improve the practicality of detachable unmanned plane crash-proof bracket, the upper mounting cylinder quantity has two, point
Not Wei Yu the cross tube both ends, wherein, during two upper mounting cylinders are in centered on the central axis of the mounting blocks
The heart is symmetrical.
In order to further improve the practicality of detachable unmanned plane crash-proof bracket, the lower mounting cylinder quantity also has two,
It is located at the both ends of the sheer pole respectively, wherein, two lower mounting cylinders are in centered on the central axis of the mounting blocks
Central Symmetry is distributed.
In order to further improve the practicality of detachable unmanned plane crash-proof bracket, the damping spring is fixedly mounted on described
On yielding rubber lower surface, the yielding rubber is embedded in the mounting cylinder, and the end of the cross bar is embedded in the damping
It is fixedly connected in rubber and with the damper and the mounting cylinder.
Beneficial effect is：The detachable unmanned plane crash-proof bracket adds the damper, can effectively slow down unmanned plane
Influence of the shock on during landing and ground to fuselage, extends service life and the maintenance period of unmanned plane, and use cost is notable
Reduce, meanwhile, remove and install very simple conveniently, practicality is good.
Brief description of the drawings
Fig. 1 is a kind of structural representation of detachable unmanned plane crash-proof bracket described in the utility model；
Fig. 2 is a kind of cut-away view of detachable unmanned plane crash-proof bracket described in the utility model.
Description of reference numerals is as follows：
1st, base；2nd, mounting blocks；3rd, cross tube；4th, sheer pole；5th, upper mounting cylinder；6th, lower mounting cylinder；7th, damping spring；
8th, yielding rubber；9th, mounting hole.
Embodiment
The utility model is described in further detail below in conjunction with the accompanying drawings：
As Figure 1-Figure 2, a kind of detachable unmanned plane crash-proof bracket, including base 1, the lower end of base 1 are provided with installation
Block 2, the side of mounting blocks 2 are provided with cross bar, and cross bar, which is used to install, is fixedly mounted cylinder, cross bar are embedded in mounting blocks 2 during use,
Cross bar is taken out when not in use, is removed and installed conveniently, cross bar includes cross tube 3 and sheer pole 4, and cross bar side is provided with installation
Cylinder, mounting cylinder are fixed and are set in crossbar end, are put during use, remove, easy installation and removal, install when not in use
Cylinder is used to install fixed damper, is provided with damper in mounting cylinder, when damper is used to buffer unmanned plane landing with ground it
Between collision, protect unmanned plane from damage, mounting cylinder includes upper mounting cylinder 5 and lower mounting cylinder 6, and damper includes yielding rubber
8 and damping spring 7.
In order to further improve the practicality of detachable unmanned plane crash-proof bracket, mounting blocks 2 are cylindrical structural, fixed peace
On the lower surface of base 1, its side is provided with mounting hole 9, and mounting hole 9 is through hole, and its quantity has two, respectively position and installation
The side upper end and positive lower end of block 2, wherein, the central axis of two mounting holes 9 is mutually perpendicular to, and cross tube 3 is embedded in installation
It is fixedly connected in the mounting hole 9 of the side upper end of block 2 and with mounting blocks 2, sheer pole 4 is embedded in the positive lower end of mounting blocks 2
It is fixedly connected in mounting hole 9 and with mounting blocks 2, the upper quantity of mounting cylinder 5 has two, respectively positioned at the both ends of cross tube 3, wherein,
Two upper mounting cylinders 5 are centrosymmetric distribution centered on the central axis of mounting blocks 2, and the lower quantity of mounting cylinder 6 also has two, divided
Not Wei Yu sheer pole 4 both ends, wherein, two lower mounting cylinders 6 are centrosymmetric point centered on the central axis of mounting blocks 2
Cloth, damping spring 7 are fixedly mounted on the lower surface of yielding rubber 8, and yielding rubber 8 is embedded in mounting cylinder, the end edge of cross bar
It is fixedly connected in yielding rubber 8 and with damper and mounting cylinder.
General principle, principal character and advantage of the present utility model has been shown and described above.The technical staff of the industry
It should be appreciated that the utility model is not restricted to the described embodiments, the simply explanation described in above-described embodiment and specification is originally
The principle of utility model, on the premise of the spirit and scope of the utility model is not departed from, the utility model also has various change
And improvement, these changes and improvements are both fallen within claimed the scope of the utility model.The utility model requires protection scope
Defined by appended claims and its effect thing.
Claims (6)
1. a kind of detachable unmanned plane crash-proof bracket, including base, it is characterised in that：The base lower end is provided with mounting blocks,
The mounting blocks side is provided with cross bar, and the cross bar includes cross tube and sheer pole, and the cross bar side is provided with mounting cylinder,
Damper is provided with the mounting cylinder, the mounting cylinder includes upper mounting cylinder and lower mounting cylinder, and the damper includes damping
Rubber and damping spring.
A kind of 2. detachable unmanned plane crash-proof bracket according to claim 1, it is characterised in that：The mounting blocks are cylinder
Shape structure, it is fixedly mounted in the base lower surface, its side is provided with mounting hole, and the mounting hole is through hole, its quantity
There are two, respectively side upper end and positive lower end of the position with the mounting blocks, wherein, the central axis phase of two mounting holes
It is mutually vertical.
A kind of 3. detachable unmanned plane crash-proof bracket according to claim 1 or 2, it is characterised in that：The cross tube edge
It is fixedly connected in the mounting hole of the side upper end of the mounting blocks and with the mounting blocks, the sheer pole is embedded in
It is fixedly connected in the mounting hole of the positive lower end of the mounting blocks and with the mounting blocks.
A kind of 4. detachable unmanned plane crash-proof bracket according to claim 1, it is characterised in that：The upper mounting cylinder quantity
Have two, respectively positioned at the both ends of the cross tube, wherein, two upper mounting cylinders using the central axis of the mounting blocks as
Center is centrosymmetric distribution.
A kind of 5. detachable unmanned plane crash-proof bracket according to claim 1, it is characterised in that：The lower mounting cylinder quantity
Also there are two, respectively positioned at the both ends of the sheer pole, wherein, two lower mounting cylinders are with the central axis of the mounting blocks
Centered on be centrosymmetric distribution.
A kind of 6. detachable unmanned plane crash-proof bracket according to claim 1, it is characterised in that：The damping spring is fixed
On the yielding rubber lower surface, the yielding rubber is embedded in the mounting cylinder, and the end of the cross bar is inlayed
It is fixedly connected in the yielding rubber and with the damper and the mounting cylinder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720655037.7U CN206826920U (en) | 2017-06-07 | 2017-06-07 | A kind of detachable unmanned plane crash-proof bracket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720655037.7U CN206826920U (en) | 2017-06-07 | 2017-06-07 | A kind of detachable unmanned plane crash-proof bracket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206826920U true CN206826920U (en) | 2018-01-02 |
Family
ID=60772486
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720655037.7U Expired - Fee Related CN206826920U (en) | 2017-06-07 | 2017-06-07 | A kind of detachable unmanned plane crash-proof bracket |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206826920U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108674677A (en) * | 2018-05-28 | 2018-10-19 | 河南农贝得农业科技有限公司 | A kind of dismountable unmanned plane anticollision damping device |
-
2017
- 2017-06-07 CN CN201720655037.7U patent/CN206826920U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108674677A (en) * | 2018-05-28 | 2018-10-19 | 河南农贝得农业科技有限公司 | A kind of dismountable unmanned plane anticollision damping device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN203854854U (en) | Rotary wing type unmanned plane with damping landing gear | |
| CN206049792U (en) | The shockproof balance system of new vehicle | |
| CN206826920U (en) | A kind of detachable unmanned plane crash-proof bracket | |
| CN204175860U (en) | A kind of vibration damper | |
| CN205277784U (en) | Take vibration damper's water pump | |
| CN202220823U (en) | Damper and damping support | |
| CN211253002U (en) | Unmanned aerial vehicle rises and falls and uses shock absorber support | |
| CN202703233U (en) | Rear suspended left supporting frame for engine | |
| CN205311896U (en) | Unmanned aerial vehicle multi -level buffer undercarriage | |
| CN205345324U (en) | Bottom protection frame is protected to unmanned aerial vehicle elasticity | |
| CN217022870U (en) | Unmanned aerial vehicle anticollision structure | |
| CN204137320U (en) | Unmanned fog machine alighting gear | |
| CN207944282U (en) | A kind of rail traffic damping device | |
| CN210949287U (en) | Fan vibration damping base | |
| CN206000936U (en) | A kind of water purifier base buffer unit | |
| CN203297263U (en) | Shock absorbing bolt structure | |
| CN207173556U (en) | Vehicle body supporting plate | |
| CN208486185U (en) | A kind of road and bridge paravent | |
| CN203868234U (en) | Strengthened type vehicle shock absorber | |
| CN207826532U (en) | A kind of power-line patrolling unmanned plane undercarriage | |
| CN208221460U (en) | A kind of mass center experimental provision of multidirectional buffering | |
| CN202499275U (en) | Hydraulic damping undercarriage of unmanned plane | |
| CN216233076U (en) | Thread protection device convenient for changing main wheel shaft of airplane | |
| CN204526709U (en) | A kind of fixing lower of automobile absorber | |
| CN205101448U (en) | Modular bumper shock absorber subassembly |
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: 20180102 Termination date: 20190607 |