CN206345019U - Rise and fall platform and the flight control of aircraft - Google Patents
Rise and fall platform and the flight control of aircraft Download PDFInfo
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- CN206345019U CN206345019U CN201720001754.8U CN201720001754U CN206345019U CN 206345019 U CN206345019 U CN 206345019U CN 201720001754 U CN201720001754 U CN 201720001754U CN 206345019 U CN206345019 U CN 206345019U
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- 239000000758 substrate Substances 0.000 claims abstract description 33
- 238000010521 absorption reaction Methods 0.000 claims description 10
- 238000000034 method Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 230000000630 rising effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000035479 physiological effects, processes and functions Effects 0.000 description 1
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Abstract
The utility model provides the platform that rises and falls, the flight control of aircraft, belongs to aircraft field.The platform that rises and falls of the aircraft includes, substrate, to carry the aircraft；Second magnetic means, is arranged on the substrate, and the position with first magnetic means of the aircraft is corresponding, and second magnetic means is identical with the magnetic of first magnetic means, to eject first magnetic means；Power supply unit, connects second magnetic means, to provide electric energy for second magnetic means；Control unit, connects said supply unit, to control said supply unit to be powered for second magnetic means.The utility model can take off offer motive force for depopulated helicopter, it is ensured that the stationarity of depopulated helicopter takeoff and landing.
Description
Technical field
The utility model is related to aircraft field, more particularly to rise and fall platform and the aircraft of a kind of aircraft control system
System.
Background technology
Depopulated helicopter (Unmanned Aerial Vehicle, UAV) refers to that flight of the non-driver in machine is set
Standby, it can be via manipulation or automatic flight, and lands in a variety of environment, to perform the multi-task.
Now, the research of small-sized depopulated helicopter and application are more and more universal, be widely used in monitoring, investigate, early warning,
The disasters such as the military scenarios such as electronic countermeasure, communication relay and environmental monitoring, aerial survey are taken photo by plane, weather prognosis, earthquake fire search and rescue, it is defeated
The civilian occasion such as the tour of electric line and rail track.Because unmanned plane need not consider the physiology and psychological endurance of people in design
The limit, therefore can have higher mobility and flexibility.Currently in order to being easy to the takeoff and landing of depopulated helicopter, generally
In takeoff and landing, the artificial relatively flat steady region carrying depopulated helicopter of selection earth's surface, and depopulated helicopter can not be ensured
The stationarity taken off or landed.
The content of the invention
The utility model, which provides one kind and aimed at, can carry depopulated helicopter, and the offer that can be taken off for depopulated helicopter is pushed away
Rise and fall platform and the flight control of the aircraft of power.
Concrete technical scheme is as follows：
A kind of platform that rises and falls of aircraft, the first magnetic means is provided with to carry on aircraft, the aircraft；
The platform that rises and falls includes,
Substrate, to carry the aircraft；
Second magnetic means, is arranged on the substrate, the position phase with first magnetic means of the aircraft
Correspondence, second magnetic means is identical with the magnetic of first magnetic means, to eject first magnetic means；
Power supply unit, connects second magnetic means, to provide electric energy for second magnetic means；
Control unit, connects said supply unit, to control said supply unit to be powered for second magnetic means.
It is preferred that, second magnetic means is formed at the substrate surface.
It is preferred that, in addition to,
3rd magnetic means, is connected with said supply unit, is arranged on the substrate, and described with the aircraft
The position of one magnetic means is corresponding, and the magnetic of the 3rd magnetic means and first magnetic means is on the contrary, to adsorb
First magnetic means.
It is preferred that, described control unit is powered for second magnetic means to control said supply unit, or
Described control unit is to control said supply unit to be powered for the 3rd magnetic means.
It is preferred that, the 3rd magnetic means is formed at the substrate surface.
A kind of flight control, the takeoff and landing to control aircraft, the control system includes,
Aircraft, is provided with the first magnetic means；
Rise and fall platform, to carry the aircraft；
Control end, connects the aircraft and the platform that rises and falls respectively, and the control end is used in the aircraft takeoff
When, the control platform ejection aircraft that rises and falls, or
The control end is used to when the aircraft lands, and rise and fall the fixed aircraft of platform absorption described in control.
It is preferred that, the platform that rises and falls includes,
Substrate, to carry the aircraft；
Second magnetic means, is arranged on the substrate, the position phase with first magnetic means of the aircraft
Correspondence, second magnetic means is identical with the magnetic of first magnetic means, to eject first magnetic means；
Power supply unit, connects second magnetic means, to provide electric energy for second magnetic means；
3rd magnetic means, is connected with said supply unit, is arranged on the substrate, and described with the aircraft
The position of one magnetic means is corresponding, and the magnetic of the 3rd magnetic means and first magnetic means is on the contrary, to adsorb
First magnetic means；
The control end controlling the said supply unit of the platform that rises and falls to be powered for second magnetic means, or
The control end is to control the said supply unit of the platform that rises and falls to be powered for the 3rd magnetic means.
The beneficial effect of above-mentioned technical proposal, is exemplified below：
1) platform that rises and falls of aircraft can improve the stationarity of taking off of aircraft using base plate carrying aircraft；
2) flight control controls rise and fall platform ejection aircraft or absorption aircraft using control end, so as to ensure
Aircraft takeoff and the stationarity of landing.
Brief description of the drawings
Fig. 1 carries the structural representation of aircraft for the platform that rises and falls of aircraft described in the utility model.
Fig. 2 is a kind of schematic diagram of embodiment of the platform that rises and falls of aircraft described in the utility model.
Fig. 3 is a kind of module map of embodiment of flight control described in the utility model.
Fig. 4 is a kind of module map of embodiment of the inside of the platform described in the utility model that rises and falls.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the premise of creative work
Lower obtained every other embodiment, belongs to the scope of the utility model protection.
It should be noted that in the case where not conflicting, the feature in embodiment and embodiment in the utility model can
To be mutually combined.
The utility model is described in further detail with specific embodiment below in conjunction with the accompanying drawings, but not as of the present utility model
Limit.
As shown in Figure 1-2, the platform that rises and falls of a kind of aircraft, the first magnetic is provided with to carry on aircraft 1, aircraft 1
Power apparatus；
The platform 2 that rises and falls includes,
Substrate 21, to carry aircraft 1；
Second magnetic means 22, is arranged on substrate 21, and the position with the first magnetic means of aircraft 1 is corresponding, the
Two magnetic means 22 are identical with the magnetic of the first magnetic means, to eject the first magnetic means；
Power supply unit 24, connects the second magnetic means 22, to provide electric energy for the second magnetic means 22；
Control unit, connects power supply unit 24, to control power supply unit 24 to be powered for the second magnetic means 22.
Further, for example and without limitation, aircraft 1 can use depopulated helicopter, and control unit can form external
Remote control, control unit and the wireless connection of power supply unit 24, the surface of substrate 21 is provided with position block, to orientate flight as
Device 1 looks for place, in order to make the first magnetic means in aircraft 1 and the platform 2 that rises and falls in second magnetic means 22 position
It is corresponding.
In the present embodiment, the second magnetic means 22 in substrate 21 and the first magnetic means on aircraft 1 are utilized
Magnetic it is identical when energized can be aircraft 1 the offer auxiliary power that takes off, improve aircraft 1 takeoff speed, while using
The carrying aircraft 1 of substrate 21 can improve the stationarity of taking off of aircraft 1.
In a preferred embodiment, the second magnetic means 22 is formed at the surface of substrate 21, or is embedded in inside substrate 21.
In the present embodiment, for example and without limitation, the second magnetic means 22 may also be disposed on the upper surface of substrate 21
Or lower surface.
In a preferred embodiment, in addition to,
3rd magnetic means 23, is connected with power supply unit 24, is arranged on substrate 21, is filled with the first magnetic force of aircraft 1
The position put is corresponding, and the magnetic of the 3rd magnetic means 23 and the first magnetic means is on the contrary, to adsorb the first magnetic means.
Further, for example and without limitation, the 3rd magnetic means 23 may be disposed at basic upper surface or lower surface,
3rd magnetic means 23 is oppositely arranged with the second magnetic means 22.
In the present embodiment, the 3rd magnetic means 23 in substrate 21 and the first magnetic means on aircraft 1 are utilized
Magnetic conversely can provide absorption affinity for the landing of aircraft 1 when energized, be favorably improved the landing stability of aircraft 1.
In a preferred embodiment, control unit is powered for the second magnetic means 22 to control power supply unit 24, or
Control unit is to control power supply unit 24 to be powered for the 3rd magnetic means 23.
In the present embodiment, for example and without limitation, control unit can taking off or two kinds of feelings of landing according to aircraft 1
Condition, control power supply unit 24 is that the second magnetic means 22 or the 3rd magnetic means 23 are powered.
In a preferred embodiment, the 3rd magnetic means 23 is formed at the surface of substrate 21.Second magnetic means 22 is arranged at
The lower surface of substrate 21.
As shown in figure 3, a kind of flight control, the takeoff and landing to control aircraft 1, control system bag
Include,
Aircraft 1, is provided with the first magnetic means；
Rise and fall platform 2, to carry aircraft 1；
Control end 3, connects aircraft 1 and the platform 2 that rises and falls respectively, and control end 3 is used to when aircraft 1 takes off, and control is risen and fallen
Platform 2 ejects aircraft 1, or
Control end 3 is used to when aircraft 1 lands, and controls the fixed aircraft 1 of the absorption of platform 2 that rises and falls.
Further, for example and without limitation, control end 3 can use nothing with the wireless connection of platform 2 of rising and falling, aircraft 1
People's helicopter.
In the present embodiment, control system controls rise and fall the ejection aircraft 1 of platform 2 or absorption aircraft 1 using control end 3,
So as to ensure the stationarity of the takeoff and landing of aircraft 1.
As shown in figure 4, in a preferred embodiment, the platform 2 that rises and falls includes,
Substrate 21, to carry aircraft 1；
Second magnetic means 22, is arranged on substrate 21, and the position with the first magnetic means of aircraft 1 is corresponding, the
Two magnetic means 22 are identical with the magnetic of the first magnetic means, to eject the first magnetic means；
Power supply unit 24, connects the second magnetic means 22, to provide electric energy for the second magnetic means 22；
3rd magnetic means 23, is connected with power supply unit 24, is arranged on substrate 21, is filled with the first magnetic force of aircraft 1
The position put is corresponding, and the magnetic of the 3rd magnetic means 23 and the first magnetic means is on the contrary, to adsorb the first magnetic means；
Control end 3 is powered to the power supply unit 24 for the platform 2 that controls to rise and fall for the second magnetic means 22, or
Control end 3 is powered to the power supply unit 24 for the platform 2 that controls to rise and fall for the 3rd magnetic means 23.
In the present embodiment, for example and without limitation, by control end 3 power supply unit 24 can be controlled to be filled for the second magnetic force
Put 22 or the 3rd magnetic means 23 power.When aircraft 1 takes off, power supply unit 24 is that the second magnetic means 22 is powered, and is utilized
Second magnetic means 22 is identical when energized with the magnetic of the first magnetic means on aircraft 1, can make the second magnetic means 22
Active force between the first magnetic means turns into the offer auxiliary pushing power that takes off of aircraft 1, improves taking off for aircraft 1
Speed；When aircraft 1 lands, power supply unit 24 is that the 3rd magnetic means 23 is powered, and utilizes the 3rd magnetic means 23 and flight
The magnetic of the first magnetic means on device 1 is opposite when the 3rd magnetic means 23 is powered, the 3rd magnetic means 23 and the first magnetic force
Active force between device turns into absorption affinity of the platform 2 to aircraft 1 of rising and falling, and improves security when aircraft 1 lands and steady
It is qualitative.
A kind of method for controlling aircraft takeoff, applied to flight control described above, comprises the steps,
When aircraft 1 takes off, control end 3 controls the ejection aircraft 1 of platform 2 that rises and falls.In a preferred embodiment, control end
3 processes for controlling to rise and fall the ejection aircraft 1 of platform 2 are,
Control power supply unit 24 is that the second magnetic means 22 is powered, and is filled so that the second magnetic means 22 has with the first magnetic force
The magnetic identical magnetic force put, aircraft 1 is ejected from the platform 2 that rises and falls.
In the present embodiment, the second magnetic means 22 risen and fallen by control in platform 2 starts, can be when aircraft 1 takes off
For the offer auxiliary power that takes off of aircraft 1.
A kind of method for controlling aircraft landing, applied to flight control described above, comprises the steps,
When aircraft 1 lands, control end 3 controls the fixed aircraft 1 of the absorption of platform 2 that rises and falls.
In a preferred embodiment, control the to rise and fall process of the fixed aircraft 1 of the absorption of platform 2 of control end 3 is,
Control power supply unit 24 is that the 3rd magnetic means 23 is powered, and is filled so that the 3rd magnetic means 23 has with the first magnetic force
The opposite magnetic force of the magnetic put, the absorption of aircraft 1 is fixed on and risen and fallen on platform 2.
In the present embodiment, for example and without limitation, the 3rd magnetic means 23 that can be risen and fallen by control in platform 2 is opened
It is dynamic, aircraft 1 can be adsorbed in when aircraft 1 lands and risen and fallen on platform 2, improve the stability of the landing of aircraft 1.
The foregoing is only the utility model preferred embodiment, not thereby limit embodiment of the present utility model and
Protection domain, to those skilled in the art, should can appreciate that in all utilization the utility model specifications and diagram
Hold the scheme obtained by made equivalent substitution and obvious change, should be included in protection model of the present utility model
In enclosing.
Claims (7)
1. a kind of platform that rises and falls of aircraft, it is characterised in that：To carry the first magnetic force is provided with aircraft, the aircraft
Device；
The platform that rises and falls includes following structure,
Substrate, to carry the aircraft；
Second magnetic means, is arranged on the substrate, and the position with first magnetic means of the aircraft is corresponding,
Second magnetic means is identical with the magnetic of first magnetic means, to eject first magnetic means；
Power supply unit, connects second magnetic means, to provide electric energy for second magnetic means；
Control unit, connects said supply unit, to control said supply unit to be powered for second magnetic means.
2. the platform that rises and falls of aircraft according to claim 1, it is characterised in that：Second magnetic means is formed at described
Substrate surface.
3. the platform that rises and falls of aircraft according to claim 1, it is characterised in that：Also include,
3rd magnetic means, is connected with said supply unit, is arranged on the substrate, first magnetic with the aircraft
The position of power apparatus is corresponding, and the magnetic of the 3rd magnetic means and first magnetic means is on the contrary, described to adsorb
First magnetic means.
4. the platform that rises and falls of aircraft according to claim 3, it is characterised in that：Described control unit is to control the confession
Electric unit is that second magnetic means is powered, or
Described control unit is to control said supply unit to be powered for the 3rd magnetic means.
5. the platform that rises and falls of aircraft according to claim 3, it is characterised in that：3rd magnetic means is formed at described
Substrate surface.
6. a kind of flight control, it is characterised in that：Takeoff and landing to control aircraft, the control system
Including,
Aircraft, is provided with the first magnetic means；
Rise and fall platform, to carry the aircraft；
Control end, connects the aircraft and the platform that rises and falls respectively, and the control end is used in the aircraft takeoff, control
The platform that risen and fallen described in system ejects the aircraft, or
The control end is used to when the aircraft lands, and rise and fall the fixed aircraft of platform absorption described in control.
7. flight control according to claim 6, it is characterised in that：The platform that rises and falls includes,
Substrate, to carry the aircraft；
Second magnetic means, is arranged on the substrate, and the position with first magnetic means of the aircraft is corresponding,
Second magnetic means is identical with the magnetic of first magnetic means, to eject first magnetic means；
Power supply unit, connects second magnetic means, to provide electric energy for second magnetic means；
3rd magnetic means, is connected with said supply unit, is arranged on the substrate, first magnetic with the aircraft
The position of power apparatus is corresponding, and the magnetic of the 3rd magnetic means and first magnetic means is on the contrary, described to adsorb
First magnetic means；
The control end controlling the said supply unit of the platform that rises and falls to be powered for second magnetic means, or
The control end is to control the said supply unit of the platform that rises and falls to be powered for the 3rd magnetic means.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720001754.8U CN206345019U (en) | 2017-01-03 | 2017-01-03 | Rise and fall platform and the flight control of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720001754.8U CN206345019U (en) | 2017-01-03 | 2017-01-03 | Rise and fall platform and the flight control of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206345019U true CN206345019U (en) | 2017-07-21 |
Family
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720001754.8U Expired - Fee Related CN206345019U (en) | 2017-01-03 | 2017-01-03 | Rise and fall platform and the flight control of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206345019U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106853870A (en) * | 2017-01-03 | 2017-06-16 | 上海量明科技发展有限公司 | The platform that rises and falls of aircraft, control system, takeoff method and landing method |
-
2017
- 2017-01-03 CN CN201720001754.8U patent/CN206345019U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106853870A (en) * | 2017-01-03 | 2017-06-16 | 上海量明科技发展有限公司 | The platform that rises and falls of aircraft, control system, takeoff method and landing method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170721 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |