CN207843346U - A kind of unmanned plane shooting shock bracket - Google Patents
A kind of unmanned plane shooting shock bracket Download PDFInfo
- Publication number
- CN207843346U CN207843346U CN201820220276.4U CN201820220276U CN207843346U CN 207843346 U CN207843346 U CN 207843346U CN 201820220276 U CN201820220276 U CN 201820220276U CN 207843346 U CN207843346 U CN 207843346U
- Authority
- CN
- China
- Prior art keywords
- vibration damper
- damper plate
- unmanned plane
- shock
- holder
- 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
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Abstract
The utility model provides a kind of unmanned plane shooting shock bracket, including：The tripod head frame of video camera is placed set on the lower section of fuselage, is flexibly connected by the bottom of the holder accommodating chamber opened up below holder crane and fuselage by connecting rod connection holder damping device, the damping device above tripod head frame；The raise-lower hydraulic motor of the holder crane is connect with controller；The damping device includes the upper vibration damper plate being connect with the holder crane and the lower vibration damper plate that is connect with the tripod head frame, round rubber shock-absorbing ball is set between the upper vibration damper plate and lower vibration damper plate, groove is set on the upper vibration damper plate and lower vibration damper plate, damping spring is set in the groove, and the rubber shock-absorbing ball is connect by damping spring with upper and lower vibration damper plate.The unmanned plane shoots shock bracket, reduces unmanned plane in flight course, because by gas shock, and causes the drawback of Aerial Images effect difference.
Description
Technical field
The utility model is related to air vehicle technique fields, and in particular to a kind of unmanned plane shooting shock bracket.
Background technology
With gradually going deep into for China's reform, economic construction is grown rapidly, and huge transition occur for the landforms of each department.
Existing aerial remote sens ing technique means can not adapt to the needs of economic development.It is aerial remote sensing platform with UAV
Technology exactly adapts to this needs and a new application technology growing up, can preferably meet China at this stage
Demand to air remote sensing business is updated outmoded geographic data.
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, can not only complete the task of manned aircraft execution, be more suitable for someone's aircraft not
Preferably executing for task.Burst thing is emergent, early warning has prodigious effect.
Existing unmanned plane is usually used in combination with the technology of taking photo by plane, and unmanned plane is in the air in flight course due to by air-flow
Impact influences, and continuously swing vibration, this vibrations and impact force are stronger to the impact endurance test shock of aerial device for meeting, it is difficult to protect
Aerial device shooting effect is demonstrate,proved, causes image high definition than low, and easily causes aerial device damage.
Utility model content
In order to overcome the deficiencies of existing technologies, the utility model provides a kind of unmanned plane shooting shock bracket, reduces nobody
Machine is in flight course, because by gas shock, and causes the drawback of Aerial Images effect difference.
In order to achieve the above object, the utility model is achieved through the following technical solutions：
A kind of unmanned plane shooting shock bracket, including：In the tripod head frame of the lower section of fuselage placement video camera, tripod head frame
Side connects holder damping device by connecting rod, and the damping device is held by the holder opened up below holder crane and fuselage
Receive chamber bottom flexible connection；The raise-lower hydraulic motor of the holder crane is connect with controller；The damping device includes
The upper vibration damper plate being connect with the holder crane and the lower vibration damper plate being connect with the tripod head frame, the upper vibration damper plate subtract under
Rubber shock-absorbing ball is set between shake plate, groove is set on the upper vibration damper plate and lower vibration damper plate, damping bullet is set in the groove
Spring, the rubber shock-absorbing ball are connect by damping spring with upper and lower vibration damper plate.
Preferably, connecting rod is arranged in vertical between the lower vibration damper plate and tripod head frame, the connecting rod subtracts under
Setting tilts reinforcing plate between shaking plate.
Preferably, lightening hole is set on the upper vibration damper plate and lower vibration damper plate, the rubber shock-absorbing ball is hollow shock-absorbing ball.
Preferably, damper is arranged in each apex angle of the tripod head frame bottom end ingress of air side.
Preferably, the round rubber shock-absorbing ball replaces with rectangular rubber shock-absorbing ball.
Preferably, damper includes damper outer barrel, damper inner core and bolster, and damper inner core is arranged in damper
In outer barrel, bolster is folded in the annular gap between damper outer barrel and damper inner core, on the inner wall of damper outer barrel
It is provided with locating slot, locating slot is axially extending along damper outer barrel, and positioning compatible with locating slot is provided on bolster
Protrusion.
With immediate prior art ratio, the technical solution of the utility model has following advantageous effect：
A kind of unmanned plane provided by the utility model shoots shock bracket, includes placing video camera set on the lower section of fuselage
Tripod head frame, connection includes upper vibration damper plate above tripod head frame, lower vibration damper plate and the rubber shock-absorbing ball between upper and lower vibration damper plate
Holder damping device reduces unmanned plane in flight course, because by air-flow impact vibration, and causes the video camera for being set to tripod head frame
The drawback of Aerial Images effect difference；
The damping device is flexibly connected by the bottom of the holder accommodating chamber opened up below holder crane and fuselage, institute
The raise-lower hydraulic motor for stating holder crane is connect with controller, when unmanned plane is by big gas shock, will place video camera
Tripod head frame the holder accommodating chamber that opens up below fuselage is withdrawn by the crane, avoid aerial device from damaging；
Groove is set on the upper vibration damper plate and lower vibration damper plate, damping spring, the rubber shock-absorbing are set in the groove
Ball is connect by damping spring with upper and lower vibration damper plate, and the damping performance of damping device is greatly improved.
Description of the drawings
Fig. 1 is the schematic diagram of the unmanned plane shooting shock bracket in a kind of embodiment of the utility model；
Fig. 2 is the side sectional view of the vibration damper plate in a kind of embodiment of the utility model；
Fig. 3 is the schematic diagram of the unmanned plane shooting shock bracket in the utility model another embodiment；
Fig. 4 is the vertical view of the vibration damper plate in the utility model another embodiment；
Fig. 5 is the schematic diagram of tripod head frame bottom end ingress of air side in a kind of embodiment of the utility model；
Fig. 6 is the structural schematic diagram of the damper in a kind of embodiment of the utility model；
Fig. 7 is the side sectional view of the damper in a kind of embodiment of the utility model；
1- video cameras, 2- tripod head frames, 3- holder cranes, the upper vibration damper plates of 4-, vibration damper plate under 5-, 6- rubber shock-absorbing balls, 7-
Groove, 8- damping springs, 9- connecting rods, 10- reinforcing plates, 11- lightening holes, 12- dampers, 13- damper outer barrels, 14- dampings
Device inner core, 15- bolsters, 16- positioning protrusion.
Specific implementation mode
The technical solution of the utility model is described further below in conjunction with the accompanying drawings：
A kind of unmanned plane as shown in Figs. 1-2 shoots shock bracket, including：Video camera 1 is placed set on the lower section of fuselage
Tripod head frame 2, the top of tripod head frame 2 connect holder damping device by connecting rod 9, the damping device by holder crane 3 with
The bottom flexible connection of the holder accommodating chamber opened up below fuselage；The raise-lower hydraulic motor and controller of the holder crane 3
Connection；The damping device includes the upper vibration damper plate 4 being connect with the holder crane 3 and is connect down with the tripod head frame 2
Rubber shock-absorbing ball 6, the upper vibration damper plate 4 and lower vibration damper plate 5 is arranged in vibration damper plate 5 between the upper vibration damper plate 4 and lower vibration damper plate 5
Upper setting groove 7, the groove 7 is interior to be arranged damping spring 8, and the rubber shock-absorbing ball 6 passes through damping spring 8 and upper and lower vibration damper plate
Connection；
As a preferred embodiment, being arranged in vertical connecting rod between the lower vibration damper plate 5 and tripod head frame 2
9, it is obliquely installed reinforcing plate 10 between the connecting rod 9 and lower vibration damper plate 5.
Preferably, in order to increase the contact area of vibration damper plate and the shock-absorbing ball, and then increase the cushion performance of shock-absorbing ball,
As shown in figure 3, the round rubber shock-absorbing ball replaces with rectangular rubber shock-absorbing ball.
As a preferred embodiment, in order to reduce the weight of shooting shock bracket, as shown in figure 4, subtracting on described
It shakes and lightening hole 11 is set on plate 4 and lower vibration damper plate 5, the rubber shock-absorbing ball 6 is hollow shock-absorbing ball.
As a preferred embodiment, in order to optimize the damping performance of the shooting shock bracket, as shown in figure 5,
Damper 12 is arranged in each apex angle of 2 bottom end ingress of air side of tripod head frame；
As shown in fig. 6-7, the damper 12 includes damper outer barrel 13, damper inner core 14 and silica gel bolster 15,
Damper inner core 14 is arranged in damper outer barrel 13, and the bolster 15 is folded in damper outer barrel 13 and damper inner core 14
Between annular gap in, locating slot, axial direction of the locating slot along damper outer barrel 13 are provided on the inner wall of damper outer barrel 13
Extend, positioning protrusion 16 compatible with locating slot is provided on bolster 15, damper has excellent anti-twisting property.
Above example is only to illustrate the technical solution of the utility model rather than its limitations, although with reference to above-mentioned implementation
The utility model is described in detail in example, and those of ordinary skill in the art still can be to the tool of the utility model
Body embodiment is modified or replaced equivalently, these without departing from the spirit and scope of the utility model any modification or wait
With replacement, within the claims for applying for pending the utility model.
Claims (6)
1. a kind of unmanned plane shoots shock bracket, including：The tripod head frame of video camera is placed set on the lower section of fuselage, feature exists
In tripod head frame top connects holder damping device by connecting rod, and the damping device passes through below holder crane and fuselage
The bottom of the holder accommodating chamber opened up is flexibly connected；The raise-lower hydraulic motor of the holder crane is connect with controller；It is described
Damping device includes the upper vibration damper plate being connect with the holder crane and the lower vibration damper plate that is connect with the tripod head frame, it is described on
Round rubber shock-absorbing ball is set between vibration damper plate and lower vibration damper plate, groove is set on the upper vibration damper plate and lower vibration damper plate, it is described
Damping spring is set in groove, and the rubber shock-absorbing ball is connect by damping spring with upper and lower vibration damper plate.
2. unmanned plane as described in claim 1 shoots shock bracket, which is characterized in that between the lower vibration damper plate and tripod head frame
It is arranged in vertical connecting rod, setting inclination reinforcing plate between the connecting rod and lower vibration damper plate.
3. unmanned plane as described in claim 1 shoots shock bracket, which is characterized in that on the upper vibration damper plate and lower vibration damper plate
Lightening hole is set, and the rubber shock-absorbing ball is hollow shock-absorbing ball.
4. unmanned plane as described in claim 1 shoots shock bracket, which is characterized in that the round rubber shock-absorbing ball replaces with
Rectangular rubber shock-absorbing ball.
5. unmanned plane as claimed in claim 4 shoots shock bracket, which is characterized in that tripod head frame bottom end ingress of air one
Damper is arranged in each apex angle of side.
6. unmanned plane as claimed in claim 5 shoots shock bracket, which is characterized in that damper includes damper outer barrel, subtracts
Device inner core and silica gel bolster are shaken, damper inner core is arranged in damper outer barrel, and bolster is folded in damper outer barrel and subtracts
It shakes in the annular gap between device inner core, locating slot is provided on the inner wall of damper outer barrel, locating slot is along damper outer barrel
It is axially extending, positioning protrusion compatible with locating slot is provided on bolster.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820220276.4U CN207843346U (en) | 2018-02-08 | 2018-02-08 | A kind of unmanned plane shooting shock bracket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820220276.4U CN207843346U (en) | 2018-02-08 | 2018-02-08 | A kind of unmanned plane shooting shock bracket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207843346U true CN207843346U (en) | 2018-09-11 |
Family
ID=63411766
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820220276.4U Expired - Fee Related CN207843346U (en) | 2018-02-08 | 2018-02-08 | A kind of unmanned plane shooting shock bracket |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207843346U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112594325A (en) * | 2020-12-08 | 2021-04-02 | 重庆工程职业技术学院 | Damper with efficient shock absorption function for aerial photography equipment |
| CN113081278A (en) * | 2021-04-07 | 2021-07-09 | 哈尔滨医科大学 | Orthopedics positioning robot base with shock-absorbing function |
-
2018
- 2018-02-08 CN CN201820220276.4U patent/CN207843346U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112594325A (en) * | 2020-12-08 | 2021-04-02 | 重庆工程职业技术学院 | Damper with efficient shock absorption function for aerial photography equipment |
| CN113081278A (en) * | 2021-04-07 | 2021-07-09 | 哈尔滨医科大学 | Orthopedics positioning robot base with shock-absorbing function |
| CN113081278B (en) * | 2021-04-07 | 2022-11-22 | 哈尔滨医科大学 | Orthopedics positioning robot base with shock-absorbing function |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180911 Termination date: 20200208 |