CN208086036U - A kind of movable unmanned helicopter airplane parking area of laser aiming - Google Patents
A kind of movable unmanned helicopter airplane parking area of laser aiming Download PDFInfo
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- CN208086036U CN208086036U CN201820373191.XU CN201820373191U CN208086036U CN 208086036 U CN208086036 U CN 208086036U CN 201820373191 U CN201820373191 U CN 201820373191U CN 208086036 U CN208086036 U CN 208086036U
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- parking area
- airplane parking
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- berth
- unmanned helicopter
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Abstract
A kind of movable unmanned helicopter airplane parking area of laser aiming, idler wheel is installed in the shaft of the application movement airplane parking area main body both sides, respectively there are one hydraulic stems at four angles of mobile airplane parking area main body, lift the upper end that berth is mounted on the telescopic rod of hydraulic stem, there is the H-type mark of landing point in the middle part of lifting berth, the middle part of H-type mark is Laser emission mouth, lifting berth both sides, respectively there are one solar panels, respectively there are a pair of of horizontal rotation motor in the both sides in lifting berth, the horizontal rotation machine shaft for rotating horizontally motor is connected by connecting rod, there is vertical electric rotating machine in the side of solar panel, vertical electric rotating machine shaft is connected with bar middle part is correspondingly connected with.The usable laser of the application carries out the movable unmanned helicopter airplane parking area of landing guiding; using laser beam high directivity, wave beam is narrow, anti-interference ability powerful feature, also, airplane parking area itself is removable; landing plane can automatic leveling, to substantially increase the adaptability under complex environment.
Description
Technical field
The utility model is related to unmanned plane stopping pad fields, stop more particularly to a kind of movable unmanned helicopter of laser aiming
Machine level ground.
Background technology
With the continuous development of unmanned air vehicle technique, unmanned plane has higher requirement in landing to visual environment, manually
Landing needs winged hand to confirm the environment of drop point with avoiding obstacles using onboard image equipment and select relatively flat earth's surface, but
At night or in visual poor environment（Such as haze）The security risk landed manually is larger, it is therefore desirable to which design makes accordingly
With the movable unmanned helicopter airplane parking area of laser aiming.
Utility model content
Above-mentioned in order to solve the problems, such as, the utility model provides a kind of movable unmanned helicopter shutdown of laser aiming
Level ground, usable laser carries out the movable unmanned helicopter airplane parking area of landing guiding, narrow, anti-using laser beam high directivity, wave beam
Interference performance powerful feature, also, airplane parking area itself is removable, landing plane can automatic leveling, to substantially increase complicated ring
Adaptability under border, for this purpose, the utility model provides a kind of movable unmanned helicopter airplane parking area of laser aiming, including
Mobile airplane parking area main body, idler wheel, hydraulic stem, solar panel and lifting berth, the mobile airplane parking area main body both sides turn
Idler wheel is installed, respectively there are one hydraulic stem, the lifting berth is mounted on liquid at four angles of the mobile airplane parking area main body on axis
The upper end of the telescopic rod of compression bar, the lifting berth internal control coremaking piece have Attitude Measuring Unit, have had in the middle part of the lifting berth
The H-type mark of point drops, and the middle part of the H-type mark is Laser emission mouth, and laser emitter is provided in the Laser emission mouth,
Respectively there are one solar panel, respectively there are a pair of of horizontal rotation motor in the both sides in the lifting berth for the lifting berth both sides,
The horizontal rotation machine shaft for rotating horizontally motor is connected by connecting rod, is had in the side of the solar panel perpendicular
Direct rotary electric rotating machine, the vertical electric rotating machine shaft are connected with bar middle part is correspondingly connected with.
Further improvement of the utility model, respectively there are one LED light, LED light can be at four angles in the lifting berth
Night reacts the position of airplane parking area and carries out drop point determination.
Further improvement of the utility model, the mobile airplane parking area main body both sides respectively have retaining mechanism locking mechanism and
The locking mechanism of fastener structures, the retaining mechanism is traction lock padlock locking structure, and the fastener structures of the retaining mechanism are to lead
Draw lock fastener structures, the utility model can be with the multiple connected uses of blocking.
Further improvement of the utility model, the laser emitter laser wavelength are the laser of 10.6 micron wavebands,
The laser of 10.6 micron wavebands can use under conditions of poor visibility.
Further improvement of the utility model, the Attitude Measuring Unit are a rectangular circuit board, the rectangular circuit board
Front includes GPS antenna, power conversion chip, three-axis gyroscope, magnetic sensor, three axis accelerometer, USB interface and inserts
Needle interface, the GPS antenna bottom are GPS antenna feed point, and the rectangular circuit board reverse side includes communication chip and microcontroller,
And fixed by four fixed hole positions, the rectangular circuit board side has two rows of spare interfaces, GPS chip and GPS antenna to be used for
The time service and positioning of system, power conversion chip generate the voltage needed for Attitude Measuring Unit work, usb communication chip and USB
Interface is used for the output of posture and location information, and posture blending algorithm is added using three-axis gyroscope, magnetic sensor and three axis
The output of speedometer calculates the real-time attitude of platform.Contact pin interface is the expansion interface reserved.
The utility model provides a kind of movable unmanned helicopter airplane parking area of laser aiming, car body, traction lock, berth, four
A hydraulic stem, two blocks of solar-powered collapsible plates, the rotary shaft for connecting solar panel, berth, laser emitter, four positions
Indicator light and built-in Attitude Measuring Unit module composition, using laser beam high directivity, wave beam is narrow, strong antijamming capability, special
It is not the laser of 10.6 micron wavebands to use under conditions of poor visibility, then coordinates airplane parking area itself removable and rise
Drop plane can automatic leveling, solar panel can carry out rotary turning by vertical electric rotating machine, need to be arranged one in this way
Face solar panel just can be carried out solar power generation in expansion and closure situation, substantially increase and stop under complex environment
The adaptability on machine level ground.
Description of the drawings
FIG. 1 is a schematic structural view of the utility model one；
Fig. 2 is the utility model structure diagram two；
Fig. 3 is the utility model Attitude Measuring Unit chip schematic diagram one；
Fig. 4 is the utility model Attitude Measuring Unit chip schematic diagram two；
It illustrates:
1, mobile airplane parking area main body；2, idler wheel；3, traction lock padlock locking structure；4, traction lock fastener structures；5, hydraulic pressure
Bar；6, solar panel；7, vertical electric rotating machine shaft；8, rotate horizontally machine shaft；9, lift berth；10, laser hair
Loophole；11, rectangular circuit board；12, fixed hole position；13, communication chip；14, microcontroller；15, GPS antenna feed point；16, three axis
Gyroscope；17, magnetic sensor；18, GPS antenna；19, USB interface；20, power conversion chip；21, spare interface；22,
Three axis accelerometer.
Specific implementation mode
The utility model is described in further detail with specific implementation mode below in conjunction with the accompanying drawings：
The utility model provides a kind of movable unmanned helicopter airplane parking area of laser aiming, and usable laser carries out landing guiding
Movable unmanned helicopter airplane parking area, using laser beam high directivity, wave beam is narrow, anti-interference ability powerful feature, also, airplane parking area
Itself is removable, landing plane can automatic leveling, to substantially increase the adaptability under complex environment.
As a kind of embodiment of the utility model, the utility model provides a kind of movable unmanned helicopter shutdown of laser aiming
Level ground, including mobile airplane parking area main body 1, idler wheel 2, hydraulic stem 5, solar panel 6 and lifting berth 9, the mobile airplane parking area
Idler wheel 2 is installed, respectively there are one hydraulic stems 5 at four angles of the mobile airplane parking area main body 1, described in the shaft of 1 both sides of main body
The upper end that berth 9 is mounted on the telescopic rod of hydraulic stem 5 is lifted, there is the H-type mark of landing point at 9 middle part of lifting berth, described
Lifting 9 internal control coremaking piece of berth has Attitude Measuring Unit, and the middle part of the H-type mark is Laser emission mouth 10, the laser hair
Laser emitter is provided in loophole 10, respectively there are one solar panel 6, the lifting berths 9 for 9 both sides of lifting berth
Both sides respectively have it is a pair of rotate horizontally motor, the horizontal rotation machine shaft 8 for rotating horizontally motor is connected by connecting rod,
There is vertical rotation electric rotating machine in the side of the solar panel 6, the vertical electric rotating machine shaft 7 and is correspondingly connected in bar
Portion is connected.
As a kind of specific embodiment of the utility model, the utility model provides a kind of laser aiming as shown in Figs. 1-2
Movable unmanned helicopter airplane parking area, including mobile airplane parking area main body 1, idler wheel 2, hydraulic stem 5, solar panel 6 and lifting pool
Position 9 is equipped with idler wheel 2 in the shaft of mobile 1 both sides of airplane parking area main body, and four angles of the mobile airplane parking area main body 1 are each
There are one hydraulic stem 5, the lifting berth 9 is mounted on the upper end of the telescopic rod of hydraulic stem 5, four angles in the lifting berth 9
Each there are one LED light, and LED light can react the position of airplane parking area at night and carry out drop point determination, in the middle part of the lifting berth 9
There are the H-type mark of landing point, 9 internal control coremaking piece of the lifting berth to have Attitude Measuring Unit, the middle part of the H-type mark is sharp
Light emitting mouth 10, laser emitter is provided in the Laser emission mouth 10, and the laser emitter laser wavelength is 10.6 micro-
The laser of the laser of VHF band, 10.6 micron wavebands can use under conditions of poor visibility, and 9 both sides of the lifting berth are each
There are one solar panel 6, respectively there are a pair of of horizontal rotation motor, the horizontal rotation motor in the both sides in the lifting berth 9
Horizontal rotation machine shaft 8 by connecting rod be connected, have vertical electric rotating machine, institute in the side of the solar panel 6
It states vertical electric rotating machine shaft 7 and is connected with bar middle part is correspondingly connected with, respectively there are retaining mechanism in the mobile airplane parking area main body both sides
The locking mechanism of locking mechanism and fastener structures, the retaining mechanism is traction lock padlock locking structure 3, the button of the retaining mechanism
Part structure is traction lock fastener structures 4, and the utility model can be with the multiple connected uses of blocking.
Attitude Measuring Unit described in the utility model is as shown in Figures 3 and 4 a rectangular circuit board, and the rectangular circuit board is just
Face includes GPS antenna, power conversion chip, three-axis gyroscope, magnetic sensor, three axis accelerometer, USB interface and contact pin
Interface, the GPS antenna bottom are GPS antenna feed point, and the rectangular circuit board reverse side includes GPS chip and microcontroller, and
It is fixed by four fixed hole positions, the rectangular circuit board side has two rows of spare interfaces, GPS chip and GPS antenna for being
The time service and positioning of system, power conversion chip generate the voltage needed for Attitude Measuring Unit work, and usb communication chip and USB connect
Mouth is used for the output of posture and location information, and posture blending algorithm is accelerated using three-axis gyroscope, magnetic sensor and three axis
The output of degree meter calculates the real-time attitude of platform.Contact pin interface is the expansion interface reserved.
The utility model characteristics of components：Berth center depicts the H-type mark for indicating landing point, circle marker region
One laser emitter of center of circle positioned inside, the direction of the launch is vertical with berth upper surface and points into the sky, the length of transmitter
Degree is not more than the thickness in berth so that it can be embedded in the interlayer of berth without causing surface bulge.The four of berth upper surface
A endpoint is respectively there are one high-brightness LED, the boundary for indicating airplane parking area.Four endpoints of berth lower surface respectively connect there are one liquid
Compression bar may be implemented the lifting in berth and be adjusted to the horizontal reference in berth, to ensure aircraft for adjusting height
Berth is parallel with local level when landing.The lower surface in berth is equipped with attitude measurement module, is used to measure in real time
The posture in berth, if discovery and the angled deviation of local level, control hydraulic stem and be adjusted.Berth both sides are respectively provided with
Solar panels provide electric energy for whole system, and two pieces of solar panels are attached by specific two degrees of freedom rotary shaft respectively,
Solar panels may be implemented opening and closing movement under the drive of trunnion axis, and plate is opened when work, when not working solar panels merge with
Reduce volume；The rotation along axial direction may be implemented in solar panels under the drive of vertical axes, by being carried to the tracking of light source
The transfer efficiency of high solar plate.Car body front end is equipped with the protruding end of traction lock, and body rear end is equipped with traction lock
Lock ring, front and back car body can be attached by this traction locker and be formed a team, carried out by headstock traction traveling to designated position
Deployment.
When normal work, airplane parking area is drawn to designated position by headstock first, deploying solar plate simultaneously enters working condition,
Berth pushes to height appropriate by hydraulic stem, and the level in berth is kept under the auxiliary of attitude measurement module.When there is nobody
When machine approaching touch down, by the laser seeker or infrared thermoviewer of aircraft bottom（Since the energy of laser beam is stronger, at
As the very high white point of brightness can be formed on instrument, so being easy for that it can be positioned）Receive what airplane parking area emitted
Laser can also be according to the LED lamplight of airplane parking area quadrangle to drop point site in descent to complete from motion tracking and land
It is further confirmed that.
The above descriptions are merely preferred embodiments of the present invention, is not to make any other to the utility model
The limitation of form, and according to any modification or equivalent variations made by the technical essence of the utility model, it is new to still fall within this practicality
Type range claimed.
Claims (7)
1. a kind of movable unmanned helicopter airplane parking area of laser aiming, including mobile airplane parking area main body（1）, idler wheel（2）, hydraulic stem
（5）, solar panel（6）With lifting berth（9）, it is characterised in that：The mobile airplane parking area main body（1）In the shaft of both sides
Idler wheel is installed（2）, the mobile airplane parking area main body（1）Four angles respectively there are one hydraulic stem（5）, the lifting berth（9）
Mounted on hydraulic stem（5）Telescopic rod upper end, the lifting berth（9）Internal control coremaking piece has Attitude Measuring Unit, the liter
Berth drops（9）There is the H-type mark of landing point at middle part, and the middle part of the H-type mark is Laser emission mouth（10）, the Laser emission
Mouthful（10）Inside it is provided with laser emitter, the lifting berth（9）Respectively there are one solar panels for both sides（6）, the lifting
Berth（9）Both sides respectively have and a pair of rotate horizontally motor, the horizontal rotation machine shaft for rotating horizontally motor（8）Pass through company
Extension bar is connected, the solar panel（6）Side in have vertical electric rotating machine, the vertical electric rotating machine shaft（7）With
It is correspondingly connected in the middle part of bar and is connected.
2. a kind of movable unmanned helicopter airplane parking area of laser aiming according to claim 1, it is characterised in that：The lifting
Berth（9）Four angles respectively there are one LED light.
3. a kind of movable unmanned helicopter airplane parking area of laser aiming according to claim 1, it is characterised in that：The movement
Airplane parking area main body（1）Respectively there are the locking mechanism and fastener structures of retaining mechanism in both sides.
4. a kind of movable unmanned helicopter airplane parking area of laser aiming according to claim 3, it is characterised in that：The locking
The locking mechanism of mechanism is traction lock padlock locking structure（3）, the fastener structures of the retaining mechanism are traction lock fastener structures.
5. a kind of movable unmanned helicopter airplane parking area of laser aiming according to claim 1, it is characterised in that：The laser
Transmitter laser wavelength is the laser of 10.6 micron wavebands.
6. a kind of movable unmanned helicopter airplane parking area of laser aiming according to claim 1, it is characterised in that：The posture
Measuring unit is a rectangular circuit board（11）, the rectangular circuit board（11）Front includes GPS antenna（18）, power conversion chip
（20）, three-axis gyroscope（16）, magnetic sensor（17）, three axis accelerometer（22）, USB interface（19）And contact pin interface,
The GPS antenna（18）Bottom is GPS antenna feed point（15）, the rectangular circuit board（11）Reverse side includes communication chip（13）With
Microcontroller（14）, and pass through four fixed hole positions（12）It is fixed.
7. a kind of movable unmanned helicopter airplane parking area of laser aiming according to claim 6, it is characterised in that：The rectangle
Circuit board（11）There are two rows of spare interfaces in side（21）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820373191.XU CN208086036U (en) | 2018-03-20 | 2018-03-20 | A kind of movable unmanned helicopter airplane parking area of laser aiming |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820373191.XU CN208086036U (en) | 2018-03-20 | 2018-03-20 | A kind of movable unmanned helicopter airplane parking area of laser aiming |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208086036U true CN208086036U (en) | 2018-11-13 |
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ID=64059618
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820373191.XU Active CN208086036U (en) | 2018-03-20 | 2018-03-20 | A kind of movable unmanned helicopter airplane parking area of laser aiming |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208086036U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108357690A (en) * | 2018-03-20 | 2018-08-03 | 金陵科技学院 | A kind of movable unmanned helicopter airplane parking area of laser aiming |
| CN113085702A (en) * | 2021-03-26 | 2021-07-09 | 国家电网有限公司 | Movable intelligent take-off and landing platform of vertical take-off and landing fixed wing unmanned aerial vehicle for electric power inspection |
-
2018
- 2018-03-20 CN CN201820373191.XU patent/CN208086036U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108357690A (en) * | 2018-03-20 | 2018-08-03 | 金陵科技学院 | A kind of movable unmanned helicopter airplane parking area of laser aiming |
| CN113085702A (en) * | 2021-03-26 | 2021-07-09 | 国家电网有限公司 | Movable intelligent take-off and landing platform of vertical take-off and landing fixed wing unmanned aerial vehicle for electric power inspection |
| CN113085702B (en) * | 2021-03-26 | 2023-01-24 | 国家电网有限公司 | Movable intelligent take-off and landing platform of vertical take-off and landing fixed wing unmanned aerial vehicle for electric power inspection |
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