CN205256688U - Unmanned vehicles and tripod head control circuit board thereof - Google Patents
Unmanned vehicles and tripod head control circuit board thereof Download PDFInfo
- Publication number
- CN205256688U CN205256688U CN201521007102.2U CN201521007102U CN205256688U CN 205256688 U CN205256688 U CN 205256688U CN 201521007102 U CN201521007102 U CN 201521007102U CN 205256688 U CN205256688 U CN 205256688U
- Authority
- CN
- China
- Prior art keywords
- circuit board
- control circuit
- head control
- cradle head
- board body
- 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.)
- Active
Links
Landscapes
- Mounting Of Printed Circuit Boards And The Like (AREA)
Abstract
The utility model discloses an unmanned vehicles and tripod head control circuit board thereof. This tripod head control circuit board includes: a control circuit board body is located for setting up tripod head control circuit two first buffering holes on the control circuit board body, first buffering hole is used for the installation to prevent the bolster of cloud platform vibrations two of the first side of control circuit board body be equipped with between the first buffering hole be used for right the control circuit board body carries out spacing fixed first fixed recess. The utility model discloses an unmanned vehicles and tripod head control circuit board thereof has simple structure, is convenient for fix, easily dismouting and low cost's beneficial effect.
Description
Technical field
The utility model relates to unmanned vehicle control field, particularly relates to a kind of many rotor flyingsDevice and cradle head control circuit board thereof.
Background technology
Unmanned plane be a kind of dynamic, can control, can carry multiple-task equipment, carry out multipleBusiness also can reusable aircraft. Can utilize wireless remote control device and the control device of self to enterThe not manned vehicle that row is controlled, for example depopulated helicopter, unmanned fixed-wing aircraft, unmanned parasolEtc.. This unmanned plane can be for carry filming apparatus, for taking photo by plane, survey and draw, investigating etc.
The The Cloud Terrace of unmanned plane be for install video camera use support and maintain stable workbench,Video camera is arranged on The Cloud Terrace. By the adjustment to The Cloud Terrace, to adjust the camera lens of video camera, with realityThe now correct shooting to target. But in prior art, fixing but to the installation of cradle head control circuit boardBe varied, majority arranges complex structure, and is difficult for fixing, and sometimes occurs cradle head control electricityRoad plate slips etc., cause circuit breaking, when serious, even cause aircraft flight center of gravity to change,Affect flight safety.
In view of this, be necessary to provide a kind of new unmanned vehicle and cradle head control circuit board thereof,To solve the above-mentioned problems in the prior art.
Utility model content
The utility model is just based on above one or more problems, provide a kind of unmanned vehicle andIts cradle head control circuit board, in order to solve the cradle head control circuit board fixed knot occurring in prior artStructure complexity, is difficult for the problem fixing, not easy to assemble and cost is high.
A kind of cradle head control circuit board, comprising: for the control circuit board of cradle head control circuit is setBody, is located at two the first cushion holes on described control circuit board body, described the first cushion holeFor the bolster of anti-The Cloud Terrace vibrations is installed, in two institutes of described control circuit board body the first sideState between the first cushion hole, be provided with for described control circuit board body is fixedOne fixed groove.
Preferably, second side relative with described the first side of described cradle head control circuit board body establishedHave the second fixed groove, the bottom land of described the second fixed groove is provided with a jut.
Preferably, in described jut, be provided with a fixing hole.
Preferably, at described second fixed groove of the second side of described cradle head control circuit board bodyTwo cell wall sides be respectively equipped with second cushion hole, described in two described the second cushion holes and twoThe first cushion hole joins end to end and is a rectangular shape.
Preferably, the bottom land of described the first fixed groove is provided with semicircle holddown groove.
Preferably, described semicircle holddown groove and described fixing hole are oppositely arranged.
Preferably, the cross section that two cell walls of described jut and described the second fixed groove form is WShape shape.
Preferably, the back side of described control circuit board body is provided with electric contact contact site, and described electricity touchesPoint contact site is provided with multiple contact points.
Preferably, described electric contact contact site is in the center at the back side of described control circuit board bodyRegion.
A kind of unmanned vehicle, comprises aircraft body, is located at the The Cloud Terrace on described aircraft bodyControl circuit board, wherein, described cradle head control circuit board is the cradle head control as described in front any oneCircuit board.
Unmanned vehicle of the present utility model and cradle head control circuit board thereof have simple in structure, are convenient toFixing, be easy to dismounting and beneficial effect with low cost.
Brief description of the drawings
Fig. 1 is the structural representation of the cradle head control circuit board preferred embodiment of the utility model unmanned planeFigure;
Fig. 2 is the structure schematic diagram of the cradle head control circuit board of Fig. 1.
Detailed description of the invention
Below in conjunction with drawings and Examples, the utility model is elaborated. Need to illustrateThat, if do not conflicted, each feature in the utility model embodiment and embodiment can be mutualIn conjunction with, all within protection domain of the present utility model.
Refer to Fig. 1 and Fig. 2, Fig. 1 be the utility model unmanned plane cradle head control circuit boardThe structural representation of good embodiment; Fig. 2 is the structure signal of the cradle head control circuit board of Fig. 1Figure. Unmanned vehicle of the present utility model, comprises aircraft body, is located at described aircraft bodyOn cradle head control circuit board. As illustrated in fig. 1 and 2, the utility model preferred embodiment providesCradle head control circuit board, comprising: for the control circuit board body 10 of cradle head control circuit is set,Be located at two the first cushion hole 12a, 12b on described control circuit board body 10, described firstCushion hole 12a, 12b are for installing the bolster of anti-The Cloud Terrace vibrations, at described control circuit board originallyBetween two described the first cushion hole 12a, 12b of body 10 first sides, be provided with for to described controlThe first fixed groove 13 that circuit board body 10 fixes.
Cradle head control circuit board of the present utility model has simple in structure, is convenient to fix, and is easy to dismountingAnd beneficial effect with low cost.
Further, relative with described the first side of described cradle head control circuit board body 10Two sides are provided with the second fixed groove, and the bottom land of described the second fixed groove is provided with a jut 11. InstituteState and in jut 11, be provided with a fixing hole 14. This fixing hole 14 is for further fixing cradle head controlCircuit board body 11, is inserted and flies again through fixing hole 14 by screw or expansion bar plastic partRealize in hole corresponding on row device body.
Preferably, at described second fixed groove of the second side of described cradle head control circuit board bodyTwo cell wall sides be respectively equipped with the second cushion hole 12c, a 12d, two described the second cushion holes12c, 12d are connected successively and are a rectangular shape with two described the first cushion hole 12a, 12b head and the tail.
Preferably, the bottom land of described the first fixed groove is provided with semicircle holddown groove 18. Semicircle solidDetermine groove 18 and can be used as and strengthen fixing or expansion is fixing, as required with screw etc. through being fixed toOn aircraft body. Described semicircle holddown groove 18 is oppositely arranged with described fixing hole 14.
Preferably, the cross section that two cell walls of described jut 11 and described the second fixed groove formBe W shape shape.
Please, with further reference to Fig. 2, the back side of described control circuit board body is provided with electric contact contact site15, described electric contact contact site 14 is provided with multiple contact points, touches with the electricity of carry-on settingPoint contact, as the power supply interface of control circuit board body, without external wire, makes structure letterSingle. Preferably, described electric contact contact site is in the center at the back side of described control circuit board bodyRegion.
Unmanned vehicle of the present utility model, comprises aircraft body, is located at described aircraft bodyOn cradle head control circuit board, wherein, described cradle head control circuit board is previously described The Cloud Terrace controlCircuit board processed.
Unmanned vehicle of the present utility model is owing to having above-mentioned cradle head control circuit board, thereby hasSimple in structure, be convenient to fix, be easy to dismounting and beneficial effect with low cost.
Although described the preferred embodiment of the utility model embodiment, the technology in this areaOnce personnel the basic creative concept of cicada, can to these embodiment make other change andAmendment. So claims are intended to be interpreted as comprising preferred embodiment and fall into this practicalityAll changes and the amendment of new embodiment scope.
To a kind of unmanned plane tracking provided by the utility model and system, carry out in detail aboveThin introduction, has applied specific case herein principle of the present utility model and embodiment has been carried outSet forth, the explanation of above embodiment is just for helping to understand method of the present utility model and core thereofThought; Meanwhile, for one of ordinary skill in the art, according to thought of the present utility model,In detailed description of the invention and range of application, all will change, in sum, this descriptionBe only embodiment of the present utility model, not thereby limit the scope of the claims of the present utility model, allEquivalent structure or the conversion of equivalent flow process that utilizes the utility model description and accompanying drawing content to do,Or be directly or indirectly used in other relevant technical fields, be all in like manner included in of the present utility modelIn scope of patent protection. Should not be construed as restriction of the present utility model.
Claims (10)
1. a cradle head control circuit board, is characterized in that, comprising: for cradle head control electricity is setThe control circuit board body on road, two first that are located on described control circuit board body are delayedPunching, described the first cushion hole is for the bolster of anti-The Cloud Terrace vibrations is installed, in described controlBetween two described the first cushion holes of circuit board body the first side processed, be provided with for to describedThe first fixed groove that control circuit board body fixes.
2. cradle head control circuit board as claimed in claim 1, is characterized in that, described The Cloud Terrace controlSecond side relative with described the first side of circuit board body processed is provided with the second fixed groove,The bottom land of described the second fixed groove is provided with a jut.
3. cradle head control circuit board as claimed in claim 2, is characterized in that, described jutIn be provided with a fixing hole.
4. cradle head control circuit board as claimed in claim 2, is characterized in that, at described The Cloud TerraceTwo cell wall sides of described second fixed groove of the second side of control circuit board body are established respectivelyThere is second cushion hole, two described the second cushion holes and two described the first cushion holesJoin end to end and be a rectangular shape.
5. cradle head control circuit board as claimed in claim 3, is characterized in that, described first is solidThe bottom land of determining groove is provided with semicircle holddown groove.
6. cradle head control circuit board as claimed in claim 5, is characterized in that, described semicircleHolddown groove and described fixing hole are oppositely arranged.
7. cradle head control circuit board as claimed in claim 4, is characterized in that, described jutThe cross section forming with two cell walls of described the second fixed groove is W shape shape.
8. cradle head control circuit board as claimed in claim 1, is characterized in that, described control electricityThe back side of road plate body is provided with electric contact contact site, and described electric contact contact site is provided with multipleContact point.
9. cradle head control circuit board as claimed in claim 8, is characterized in that, described electric contactContact site is in the central area at the back side of described control circuit board body.
10. a unmanned vehicle, comprises aircraft body, is located at the cloud on described aircraft bodyPlatform control circuit board, is characterized in that, described cradle head control circuit board is as claim 1To the cradle head control circuit board described in 9 any one.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201521007102.2U CN205256688U (en) | 2015-11-27 | 2015-11-27 | Unmanned vehicles and tripod head control circuit board thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201521007102.2U CN205256688U (en) | 2015-11-27 | 2015-11-27 | Unmanned vehicles and tripod head control circuit board thereof |
Publications (1)
Publication Number | Publication Date |
---|---|
CN205256688U true CN205256688U (en) | 2016-05-25 |
Family
ID=55998233
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201521007102.2U Active CN205256688U (en) | 2015-11-27 | 2015-11-27 | Unmanned vehicles and tripod head control circuit board thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN205256688U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107478224A (en) * | 2017-08-17 | 2017-12-15 | 深圳市道通智能航空技术有限公司 | Inertial measuring unit and plant equipment |
US11041726B2 (en) | 2017-08-17 | 2021-06-22 | Autel Robotics Co., Ltd. | Inertial measurement apparatus and mechanical device |
-
2015
- 2015-11-27 CN CN201521007102.2U patent/CN205256688U/en active Active
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107478224A (en) * | 2017-08-17 | 2017-12-15 | 深圳市道通智能航空技术有限公司 | Inertial measuring unit and plant equipment |
WO2019033753A1 (en) * | 2017-08-17 | 2019-02-21 | 深圳市道通智能航空技术有限公司 | Inertial measuring device and mechanical equipment |
US11041726B2 (en) | 2017-08-17 | 2021-06-22 | Autel Robotics Co., Ltd. | Inertial measurement apparatus and mechanical device |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2019212892A3 (en) | Market based detect and avoid (daa) solutions | |
US11677275B2 (en) | Wireless power transfer network management | |
CN205256688U (en) | Unmanned vehicles and tripod head control circuit board thereof | |
CN105867436B (en) | Unmanned vehicle and its clouds terrace system | |
CN104776861B (en) | Flexible calibration device for calibrating wind tunnel vision measurement system | |
WO2013177065A3 (en) | Server-based hierarchical mass storage system | |
CN204465646U (en) | Mobile terminal | |
US10111355B1 (en) | Equipment module adapter blocks | |
CN103259196A (en) | Framework of an electrical panel or enclosure | |
US10675990B2 (en) | Drone docking system | |
CN204477650U (en) | A kind of wear type The Cloud Terrace being convenient to install | |
US10080303B2 (en) | Interlock bracket unit | |
CN203868650U (en) | Suspension bracket for multiple projectors | |
CN204137327U (en) | The Micro Aerial Vehicle of a kind of quick shooting compare rule orthogonal projection figure | |
CN204279925U (en) | The unmanned vehicle that alighting gear quick release is changed | |
CN204518279U (en) | Vehicle detection controller | |
CN202693242U (en) | Multipurpose fixture for routine experiment of inertial navigation system | |
CN204836796U (en) | PCB panel of quick concatenation | |
CN211364931U (en) | Multi-body detachable unmanned aerial vehicle | |
CN204291704U (en) | A kind of wire-management device and a kind of rack | |
CN203181402U (en) | Ion fan fixing device | |
CN206020771U (en) | The attitude-control device that many camera lens three-dimensional lives of unmanned plane shoot | |
CN203930505U (en) | A kind of CMOS road Identification device | |
CN204496858U (en) | A kind of display screen section difference regulating device | |
CN204965717U (en) | Remote control system |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant |