CN207173991U - Can automatically keep level and adjust height aircraft landing platform - Google Patents
Can automatically keep level and adjust height aircraft landing platform Download PDFInfo
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- CN207173991U CN207173991U CN201720459061.3U CN201720459061U CN207173991U CN 207173991 U CN207173991 U CN 207173991U CN 201720459061 U CN201720459061 U CN 201720459061U CN 207173991 U CN207173991 U CN 207173991U
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- landing platform
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Abstract
Keep level and the aircraft landing platform of height can be adjusted automatically the utility model discloses a kind of, including mobile platform, landing platform and control system, there is gyroscope automatic control module in control system；Landing stage+module in one tilt forward and back adjustment motor on, tilt forward and back adjustment motor be installed on one tilt adjustment motor on；The adjustment motor that tilts is installed on a hoistable platform, and hoistable platform is installed on mobile platform by pressure liftable bar；Height induction device is installed on landing platform, gyroscope automatic control module is also installed on landing platform.The utility model is by the way that landing stage+module is adjusted on motors two, the posture of different directions is adjusted by two motors or two or more motor, reach and remain that landing platform is in horizontality, and by pressure liftable bar landing platform can be kept to be in fixed height above sea level automatically, it so can ensure that aircraft can also Normal Take-Off And Landing even in IFR conditions.
Description
Technical field
It the utility model is related to vehicles equipment technology field, and in particular to one kind is used for aircraft（Such as aircraft）Rising
The platform of drop.
Background technology
With the development of scientific and technological level, the scope of activities of people is more and more wider, and more and more frequently, because aircraft transports
Rapidity, therefore be also applied to more and more widely in the daily routines of people.At present, the landing of most of aircraft is all
It is to be carried out by airstrip or landing platform, because landing platform construction cost is lower, because face is using more and more extensive.Rise
Drop platform is typically mounted at a bigger moveable platform（Such as vehicle formula or boat form mobile platform）On, it can so improve
Its adaptability.However, because mobile platform is when on land or sea, under the conditions of landform, wave, tidewater, wind etc., platform
Floating or left left front rear-inclined can be descended with wave or environmentally, the landing to aircraft causes great obstacle, or causes to fly
Row device can not landing, or even cause security incident, therefore serious potential safety hazard be present.
Utility model content
The technical problems to be solved in the utility model is to provide a kind of more reasonable structure, can keep landing platform steady automatically
Aircraft landing platform.
In order to solve the above technical problems, the utility model adopts the following technical scheme that：One kind can keep level and tune automatically
The aircraft landing platform of whole height, including mobile platform, landing platform and control system, landing stage+module is in mobile platform
On, there is at least one landing platform on a mobile platform, there is gyroscope automatic control module, its feature in control system
It is：The landing stage+module is tilted forward and back on adjustment motor in one, is tilted forward and back adjustment motor and is installed on one and tilts
Adjust on motor, tilt forward and back the horizontal adjusting mechanism that adjustment motor collectively forms landing platform with the adjustment motor that tilts；
The adjustment motor that tilts is installed on a hoistable platform, and hoistable platform is installed on mobile platform by elevating mechanism, lifting
Mechanism and hoistable platform form the height regulating mechanism of landing platform together；Tilt forward and back adjustment motor, tilt adjustment horse
Control system is connected up to elevating mechanism；Height induction device, gyroscope automatic control module are installed on landing platform
It is installed on landing platform.
Preferably, the adjustment motor that tilts is installed on hoistable platform by a support, the anteversion and retroversion slop regulation
Whole motor is installed on the horizontal L-type installing plate of a horizontal edge-on installation, and the horizontal L-type installing plate connection, which tilts, adjusts horse
The power transmission shaft reached；In on a vertically installed vertical L-type installing plate, the vertical L-type installing plate connects the landing stage+module
Tilt forward and back the power transmission shaft of adjustment motor.
Further, the power transmission shaft structure of the power transmission shaft for tilting forward and back adjustment motor and the adjustment motor that tilts
Into being mutually perpendicular to structure.
Further, the elevating mechanism is pressure liftable bar, and the drive mechanism of pressure liftable bar connects control system.
When mobile platform is with wave or when environmentally descending floating, the height induction device of landing platform can allow pressure liftable bar
The height of adjust automatically landing platform, landing platform is set to remain fixed height above sea level movement；When platform is because of wave or ring
During the run-off the straight of border, the gyroscope automatic control module of landing platform will send signal driving and tilt adjustment motor with before
Hypsokinesis skew adjustment motor does suitable operating, so as to adjust landing platform, landing platform is remained horizontality.
The present invention is by the way that landing stage+module on two adjustment motors, is adjusted by two motors or two or more motor
The posture of different directions, reach and remain that landing platform is in horizontality, and can be kept automatically by pressure liftable bar
Landing platform is in fixed height above sea level, so can ensure that aircraft can also normally rise even in IFR conditions
Drop.
Brief description of the drawings
Fig. 1 is the utility model overall structure diagram；
Fig. 2 is the utility model normal condition structural representation；
Fig. 3 is that the utility model is the structural representation for keeping level altitude；
Fig. 4 is the structural representation that the utility model is keep level state.
In figure, 1 is mobile platform, and 2 be pressure liftable bar, and 3 be hoistable platform, and 4 be the adjustment motor that tilts, before 5 are
Hypsokinesis skew adjustment motor, 6 be landing platform, and 7 be horizontal L-type installing plate, and 8 be vertical L-type installing plate.
Embodiment
In the present embodiment, reference picture 1, Fig. 2, Fig. 3 and Fig. 4, it is described can automatically keep level and adjust height aircraft
Landing platform, including mobile platform 1, landing platform 6 and control system, landing platform 6 are installed on mobile platform 1, control system
There is gyroscope automatic control module in system；The landing stage+module is tilted forward and back on adjustment motor 5 in one, anteversion and retroversion slop regulation
Whole motor 5 is installed on one and tilted on adjustment motor 4, tilts forward and back adjustment motor and the adjustment motor that tilts collectively forms
The horizontal adjusting mechanism of landing platform；The adjustment motor that tilts is installed on a hoistable platform 3, and hoistable platform 3 passes through lifting
Mechanism is installed on mobile platform 1, and elevating mechanism and hoistable platform form the height regulating mechanism of landing platform together；Anteversion and retroversion
Skew adjustment motor, the adjustment motor that tilts connect control system with elevating mechanism；Height is installed on landing platform to sense
Device, gyroscope automatic control module are also installed on landing platform.
The adjustment motor 4 that tilts is installed on hoistable platform 3 by a support, is tilted forward and back adjustment motor 5 and is installed on
On the horizontal L-type installing plate 7 of one horizontal edge-on installation, the horizontal L-type installing plate 7 connects the transmission for the adjustment motor 4 that tilts
Axle；The landing platform 6 is installed on a vertically installed vertical L-type installing plate 8, and the vertical L-type installing plate 8 connects anteversion and retroversion
The power transmission shaft of skew adjustment motor.
Tilt forward and back the power transmission shaft of adjustment motor 5 and the power transmission shaft for the adjustment motor 4 that tilts forms and is mutually perpendicular to structure.
The elevating mechanism is pressure liftable bar 2, and the drive mechanism of pressure liftable bar 2 connects control system.
When mobile platform 1 is with wave or when environmentally descending floating, the height induction device of landing platform 6 can allow pressure liftable
The height of the adjust automatically landing platform of bar 2, landing platform is set to remain fixed height above sea level movement；When platform because of wave or
During environment run-off the straight, the gyroscope automatic control module of landing platform 6 will send signal and drive the adjustment motor 4 that tilts
Suitable operating is done with adjustment motor 5 is tilted forward and back, so as to adjust landing platform, landing platform 6 is remained horizontality.
The utility model is described in detail above, it is described above, only the preferred embodiment of the utility model and
, it is when the utility model practical range can not be limited, i.e., all to make equivalent changes and modifications according to the application scope, it all should still belong to this
In utility model covering scope.
Claims (4)
1. a kind of can the aircraft landing platform of keep level and adjustment height, including mobile platform, landing platform and control automatically
System processed, landing stage+module have on mobile platform, having at least one landing platform on mobile platform in control system
Gyroscope automatic control module, it is characterised in that：The landing stage+module is tilted forward and back on adjustment motor in one, is tilted forward and back
Adjustment motor is installed on one and tilted on adjustment motor, tilts forward and back adjustment motor and the adjustment motor that tilts collectively forms
The horizontal adjusting mechanism of landing platform；The adjustment motor that tilts is installed on a hoistable platform, and hoistable platform passes through lift
Structure is installed on mobile platform, and elevating mechanism and hoistable platform form the height regulating mechanism of landing platform together；Tilt forward and back
Adjustment motor, the adjustment motor that tilts connect control system with elevating mechanism；Height sensing dress is installed on landing platform
Put, gyroscope automatic control module is also installed on landing platform.
2. it is according to claim 1 can automatically keep level and adjust height aircraft landing platform, it is characterised in that：
The adjustment motor that tilts is installed on hoistable platform by a support, and the adjustment motor that tilts forward and back is installed on a water
On the horizontal L-type installing plate for putting down edge-on installation, the horizontal L-type installing plate connection, which tilts, adjusts the power transmission shaft of motor；It is described
For landing stage+module on a vertically installed vertical L-type installing plate, the vertical L-type installing plate connection tilts forward and back adjustment motor
Power transmission shaft.
3. it is according to claim 2 can automatically keep level and adjust height aircraft landing platform, it is characterised in that：
The power transmission shaft for tilting forward and back adjustment motor forms with the power transmission shaft for tilting adjustment motor and is mutually perpendicular to structure.
4. it is according to claim 1 can automatically keep level and adjust height aircraft landing platform, it is characterised in that：
The elevating mechanism is pressure liftable bar, and the drive mechanism of pressure liftable bar connects control system.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720459061.3U CN207173991U (en) | 2017-04-27 | 2017-04-27 | Can automatically keep level and adjust height aircraft landing platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720459061.3U CN207173991U (en) | 2017-04-27 | 2017-04-27 | Can automatically keep level and adjust height aircraft landing platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207173991U true CN207173991U (en) | 2018-04-03 |
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ID=61733650
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720459061.3U Active CN207173991U (en) | 2017-04-27 | 2017-04-27 | Can automatically keep level and adjust height aircraft landing platform |
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| CN (1) | CN207173991U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106976566A (en) * | 2017-04-27 | 2017-07-25 | 东莞市丸红电子有限公司 | Level can be kept automatically and adjusts the aircraft landing platform of height |
| TWI770716B (en) * | 2020-12-11 | 2022-07-11 | 財團法人金屬工業研究發展中心 | Drone take-off and landing operation system and drone take-off and landing operation method |
-
2017
- 2017-04-27 CN CN201720459061.3U patent/CN207173991U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106976566A (en) * | 2017-04-27 | 2017-07-25 | 东莞市丸红电子有限公司 | Level can be kept automatically and adjusts the aircraft landing platform of height |
| TWI770716B (en) * | 2020-12-11 | 2022-07-11 | 財團法人金屬工業研究發展中心 | Drone take-off and landing operation system and drone take-off and landing operation method |
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