CN206476113U - A kind of fixed-wing unmanned plane takes off and landing system - Google Patents
A kind of fixed-wing unmanned plane takes off and landing system Download PDFInfo
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- CN206476113U CN206476113U CN201621015084.7U CN201621015084U CN206476113U CN 206476113 U CN206476113 U CN 206476113U CN 201621015084 U CN201621015084 U CN 201621015084U CN 206476113 U CN206476113 U CN 206476113U
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- aerial vehicle
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Abstract
The utility model is related to unmanned plane equipment technical field, more particularly to a kind of fixed-wing unmanned plane takes off and landing system.A kind of fixed-wing unmanned plane takes off and landing system, including：An at least frame fixed-wing unmanned plane and at least a frame multi-rotor unmanned aerial vehicle, are connected between the fixed-wing unmanned plane and multi-rotor unmanned aerial vehicle by removable connector, and the removable connector controls it to close or open by servomechanism.Additionally provide a kind of taking off and landing method for fixed-wing unmanned plane, multi-rotor unmanned aerial vehicle is detachably connected with fixed-wing unmanned plane by removable connector, the multi-rotor unmanned aerial vehicle drives fixed-wing unmanned plane in aerial acceleration of taking off, when wing unmanned plane to be fixed is rotated to setting speed, control removable connector to disconnect by servomechanism, realize being taken off without slideway for fixed-wing unmanned plane.The setting of ground takeoff runway is reduced, the use cost of fixed-wing unmanned plane is reduced, simple to operate, takeoff and landing is more flexible.
Description
Technical field
The utility model is related to unmanned plane equipment technical field, more particularly to a kind of fixed-wing unmanned plane takes off and landed
System.
Background technology
Common fixed-wing unmanned plane takes off is required for specific runway to be slided for it with landing, but civil area is most simultaneously
Do not possess enough spaces of taking off, therefore limit fixed-wing unmanned plane to a certain extent and pushed away in a wide range of of civil area
Extensively.
With the development of unmanned air vehicle technique, derived again take off vertically, the fixed-wing such as orbit shot is taken off, hand is thrown nobody
Machine takes off mode, but these modes also all have various defects, such as cost of manufacture is high, delivery trouble, operation are multiple
The problems such as miscellaneous, technology is immature etc., it is also industry problem that landing difficulty is reclaimed in addition.
How a kind of maneuverability suitable for fixed-wing unmanned plane, landing method simple to operate, as urgently are provided
The problem of solution.
Utility model content
The purpose of this utility model is to propose a kind of taking off and landing system for fixed-wing unmanned plane, passes through servomechanism control
System the removable connector, when fixed-wing unmanned plane takes off, multi-rotor unmanned aerial vehicle go straight up to take off drive fixed-wing nobody
Machine is to aerial so that fixed-wing unmanned plane takes off acceleration or speed reduction in landing in the air, solves the unmanned plane ground runway that takes off and builds
If input it is high, the problem of strict is required to takeoff condition.
For up to this purpose, the utility model uses following technical scheme：
A kind of fixed-wing unmanned plane takes off and landing system, including：At least a frame fixed-wing unmanned plane and at least a frame
Multi-rotor unmanned aerial vehicle, is connected between the fixed-wing unmanned plane and multi-rotor unmanned aerial vehicle by removable connector, and it is described can
Dismounting connector controls it to close or open by servomechanism.
As one of the preferred embodiments of the present invention, the removable connector include be arranged on the fixed-wing nobody
Projection on the both sides wing of machine, is arranged on handgrip corresponding with projection in the multi-rotor unmanned aerial vehicle, the handgrip is with watching
Device connection is taken, and controls it to close or open by servomechanism.
As one of the preferred embodiments of the present invention, be respectively arranged with the both sides wing of the fixed-wing unmanned plane with
The parallel outrigger shaft in fuselage axis, the projection is arranged on outrigger shaft, in order to which handgrip is grasped.
As one of the preferred embodiments of the present invention, the two ends of the outrigger shaft are respectively arranged with the projection, described
Projection is telescopic to be arranged on outrigger shaft, and the lower section of the multi-rotor unmanned aerial vehicle is evenly distributed with and projection by basic point of center of gravity
Corresponding mechanical gripper.
As one of the preferred embodiments of the present invention, the removable connector include be separately positioned on fixed-wing nobody
The the first electromagnetism part and the second electromagnetism part of machine and multi-rotor unmanned aerial vehicle, the first electromagnetism part and the second electromagnetism part are mutually adsorbed, and
First electromagnetism part and/or the second electromagnetism part control its magnetic by servomechanism.
As one of the preferred embodiments of the present invention, the guiding of bell mouth shape is provided with the outside of the first electromagnetism part
Cylinder, the second electromagnetism part is the frustum cone structure being adapted with guide cylinder inner structure.
As one of the preferred embodiments of the present invention, in addition to net is intercepted, the interception net is arranged on more than at least two
Between rotor wing unmanned aerial vehicle, and the edge for intercepting net is provided with and can receive the draw-string netted by servomechanism progress pull.
Additionally provide a kind of taking off and landing method for fixed-wing unmanned plane, by removable connector by many rotors nobody
Machine is detachably connected with fixed-wing unmanned plane, and the multi-rotor unmanned aerial vehicle drives fixed-wing unmanned plane in aerial acceleration of taking off, and treats
When the propeller of fixed-wing unmanned plane is rotated to setting speed, control removable connector to disconnect by servomechanism, realize
Fixed-wing unmanned plane takes off vertically without runway.
As one of the preferred embodiments of the present invention, when fixed-wing unmanned plane needs landing, controlled by servomechanism many
Rotor wing unmanned aerial vehicle close to fixed-wing unmanned plane and by close removable connector so that fixed-wing unmanned plane and many rotors nobody
Machine is connected, and the motor of fixed-wing unmanned plane is closed at least before landing, after fixed-wing unmanned plane drops down onto ground, passes through servo
Device control removable connector is disconnected, to separate multi-rotor unmanned aerial vehicle and fixed-wing unmanned plane.
As one of the preferred embodiments of the present invention, when fixed-wing unmanned plane needs landing, at least two are connected to
Interception net between multi-rotor unmanned aerial vehicle, setting height hovering in the air is kept by multi-rotor unmanned aerial vehicle, will be solid by servomechanism
The speed for determining wing unmanned plane is reduced to after certain numerical value and closes its engine, and the fixed-wing unmanned plane falls to the net for intercepting net
Face, and being played fixed-wing unmanned plane pocket by draw-string, takes back ground by multi-rotor unmanned aerial vehicle by intercepting net by fixed-wing unmanned plane
Face.
Beneficial effect：The removable connector controlled by servomechanism, when fixed-wing unmanned plane takes off, by many
Rotor wing unmanned aerial vehicle goes straight up to the drive fixed-wing unmanned plane that takes off to aerial, accelerates or drops to cause fixed-wing unmanned plane to take off in the air
Fall slow down, reduce the setting of ground takeoff runway, reduce the use cost of fixed-wing unmanned plane 1, it is simple to operate, take off and
Landing is more flexible.
Brief description of the drawings
Fig. 1 is the structural representation taken off with landing system for the fixed-wing unmanned plane that the utility model embodiment 1 is provided
One；
Fig. 2 is the structural representation taken off with landing system for the fixed-wing unmanned plane that the utility model embodiment 1 is provided
Two.
Fig. 3 is the structural representation taken off with landing system for the fixed-wing unmanned plane that the utility model embodiment 3 is supplied.
In figure：
1st, fixed-wing unmanned plane；2nd, multi-rotor unmanned aerial vehicle；3rd, net is intercepted；11st, outrigger shaft.
Embodiment
Further illustrate the technical solution of the utility model below in conjunction with the accompanying drawings and by embodiment.
Embodiment 1
The utility model provides a kind of taking off and landing system for fixed-wing unmanned plane, as shown in Figure 1-2, including：One
Frame fixed-wing unmanned plane 1 and two frame multi-rotor unmanned aerial vehicles 2, by can between the fixed-wing unmanned plane 1 and multi-rotor unmanned aerial vehicle 2
Dismantle and be respectively arranged with the extension parallel with fuselage axis on connector connection, the both sides wing of the fixed-wing unmanned plane
Axle 11, the removable connector includes the projection being arranged on outrigger shaft 11, and the two ends of the outrigger shaft 11 are respectively arranged with
The projection, the lower section of the multi-rotor unmanned aerial vehicle 2 is evenly distributed with the mechanical gripper corresponding with projection by basic point of center of gravity,
In order to which handgrip is grasped.The handgrip is connected with servomechanism, and controls it to close or open by servomechanism.
The removable connector controlled by servomechanism, when fixed-wing unmanned plane 1 takes off, passes through many rotors of two framves
Unmanned plane 2 goes straight up to the drive fixed-wing unmanned plane 1 that takes off to aerial, accelerates or drops to cause fixed-wing unmanned plane 1 to take off in the air
Fall slow down, reduce the setting of ground takeoff runway, reduce the use cost of fixed-wing unmanned plane 1, it is simple to operate, take off and
Landing is more flexible.The setting of the outrigger shaft causes the raised top for being higher than fixed-wing unmanned plane 1, the mating connection with handgrip
It is more easy and accurate, improve the joint efficiency of raised and handgrip.
When it is implemented, outrigger shaft 11 can also be not provided with the fixed-wing unmanned plane 1, undercarriage can also be not provided with
And pulley.When fixed-wing unmanned plane is one, the multi-rotor unmanned aerial vehicle can also be 2N, and wherein N is natural number,
To reach the vertical and landing takeoff without takeoff runway of fixed-wing unmanned plane 1.It is described many when fixed-wing unmanned plane is one
Rotor wing unmanned aerial vehicle can also be one, and the outrigger shaft 11 is arranged on the top of fixed-wing unmanned plane 1, and correspondence fixed-wing nobody
The center of gravity of machine 1, the multi-rotor unmanned aerial vehicle 2 can also be multiple, then the quantity of the outrigger shaft 11 is counted with multi-rotor unmanned aerial vehicle 2
Amount is identical, and the outrigger shaft 11 is uniformly arranged on around the center of gravity of fixed-wing unmanned plane 1.It is additionally provided with the projection anti-skidding
Fin or groove, in favor of the crawl and positioning of handgrip.
The utility model additionally provides a kind of taking off and landing method for fixed-wing unmanned plane, passes through matching somebody with somebody for raised and handgrip
Multi-rotor unmanned aerial vehicle 2 is detachably connected by conjunction with fixed-wing unmanned plane 1, and the multi-rotor unmanned aerial vehicle 2 drives fixed-wing unmanned plane 1
In aerial acceleration of taking off, when the propeller of wing unmanned plane 1 to be fixed is rotated to setting speed, detachably connected by servomechanism control
Fitting is disconnected, and realizes being taken off vertically without runway for fixed-wing unmanned plane 1.Described raised is set to setting inclination angle
The projection of degree, firmly grasps with it under servomechanism control in order to handgrip and is connected.
When fixed-wing unmanned plane 1 needs landing, multi-rotor unmanned aerial vehicle 2 is controlled close to fixed-wing unmanned plane 1 by servomechanism,
When handgrip is close to projection, handgrip is closed by servomechanism so that fixed-wing unmanned plane 1 is connected with multi-rotor unmanned aerial vehicle 2, can
To close the motor of fixed-wing unmanned plane 1 immediately, the motor of fixed-wing unmanned plane 1 can also be closed before landing, in fixed-wing
Unmanned plane 1 is dropped down onto behind ground, controls removable connector to disconnect by servomechanism, to separate multi-rotor unmanned aerial vehicle 2 and consolidate
Determine wing unmanned plane 1.
Pass through handgrip and the raised structure being engaged so that fixed-wing unmanned plane 1 is in takeoff and landing, by many rotors
Unmanned plane 2 provide it is hovered in aerial power, be not required to build ground takeoff runway on the basis of, complete fixed-wing nobody
The skyborne takeoff and landing of machine 1, and separated in time with multi-rotor unmanned aerial vehicle 2 after takeoff and landing, it is simple to operate.
Embodiment 2
As different from Example 1, the removable connector includes being separately positioned on fixed-wing unmanned plane and many rotors
The the first electromagnetism part and the second electromagnetism part of unmanned plane, the first electromagnetism part and the second electromagnetism part are mutually adsorbed, and the first electromagnetism part
And/or second electromagnetism part its magnetic is controlled by servomechanism.The first electromagnetism part and the second electromagnetism part at least one of which are
Electromagnet, another can be electromagnet or the metal that can be adsorbed by electromagnet.
The detachable member being made up of the first magnetic part and the second magnetic part, in wing unmanned plane and many rotations of being connected
During wing unmanned plane, it is more accurate to align, and connects more convenient, reduces the difficulty of servomechanism operation；Separation fixed-wing nobody
When machine 1 and multi-rotor unmanned aerial vehicle, more rapid, safety is separated.
When it is implemented, the guide cylinder of bell mouth shape is provided with the outside of the first electromagnetism part, the second electromagnetism part
For the frustum cone structure being adapted with guide cylinder inner structure.The design of the guide cylinder and frustum cone structure so that the first electromagnet and
Second electromagnet aligned when magnetic is connected it is more convenient and accurate, it is more convenient during separation.
The utility model additionally provides a kind of taking off and landing method for fixed-wing unmanned plane, passes through the first electromagnetism part and
Multi-rotor unmanned aerial vehicle is detachably connected by the cooperation of two electromagnetism parts with fixed-wing unmanned plane, and the multi-rotor unmanned aerial vehicle, which drives, fixes
Wing unmanned plane is in aerial acceleration of taking off, when wing unmanned plane to be fixed is rotated to setting speed, is detachably connected by servomechanism control
Fitting is disconnected, and realizes being taken off without runway for fixed-wing unmanned plane.Described raised is set to setting angle of inclination
Projection, firmly grasps with it under servomechanism control in order to handgrip and is connected.
When fixed-wing unmanned plane needs landing, multi-rotor unmanned aerial vehicle is controlled close to fixed-wing unmanned plane by servomechanism, when
When first electromagnetism part is close to the second electromagnetism part, the first electromagnetism part and/or the second electromagnetism part are closed by servomechanism so that fixed-wing
Unmanned plane is connected with multi-rotor unmanned aerial vehicle, and the motor of fixed-wing unmanned plane can be closed immediately, can also be closed before landing
The motor of fixed-wing unmanned plane, after fixed-wing unmanned plane drops down onto ground, controls removable connector to disconnect and connects by servomechanism
Connect, to separate multi-rotor unmanned aerial vehicle and fixed-wing unmanned plane.
Embodiment 3
From unlike embodiment 1 and embodiment 2, the fixed-wing unmanned plane take off with landing system also include intercept
Net 3, as Figure 1-3, the interception net 3 are arranged between at least two multi-rotor unmanned aerial vehicles 2, and the side for intercepting net 3
Edge is provided with can carry out the draw-string that pull receives net by servomechanism.The setting for intercepting net 3, when solving landing, by can
Dismounting component connection is between the fixed-wing unmanned plane 1 of state of flight and multi-rotor unmanned aerial vehicle 2 connection difficulty is higher to ask
Topic, by the setting for intercepting net 3 so that fixed-wing unmanned plane 1 is in landing, and the mode of landing is more simple, more easy to operate.
Additionally provide a kind of taking off and landing method for fixed-wing unmanned plane, by removable connector by many rotors nobody
Machine 2 is detachably connected with fixed-wing unmanned plane 1, and the multi-rotor unmanned aerial vehicle 2 drives fixed-wing unmanned plane 1 to add in aerial take off
Speed, when wing unmanned plane 1 to be fixed is rotated to setting speed, controls removable connector to disconnect by servomechanism, realizes solid
Determine being taken off without runway for wing unmanned plane 1.
When fixed-wing unmanned plane 1 needs landing, the interception net between at least two multi-rotor unmanned aerial vehicles is connected to, is passed through
Multi-rotor unmanned aerial vehicle 2 keeps setting height hovering in the air, and the speed of fixed-wing unmanned plane 1 is reduced into a fixed number by servomechanism
Close its engine after value, the fixed-wing unmanned plane falls to the wire side for intercepting net 3, and by draw-string by fixed-wing unmanned plane 1
Pocket is risen, and ground is taken back by intercepting net 3 by fixed-wing unmanned plane 1 by multi-rotor unmanned aerial vehicle 2.
Technical principle of the present utility model is described above in association with specific embodiment.These descriptions are intended merely to explain this reality
With new principle, and the limitation to the utility model protection domain can not be construed in any way.Based on explanation herein,
Those skilled in the art, which would not require any inventive effort, can associate other embodiments of the present utility model,
These modes are fallen within protection domain of the present utility model.
Claims (7)
1. a kind of fixed-wing unmanned plane takes off and landing system, it is characterised in that including：An at least frame fixed-wing unmanned plane
(1) and an at least frame multi-rotor unmanned aerial vehicle (2), by removable between the fixed-wing unmanned plane (1) and multi-rotor unmanned aerial vehicle (2)
Connector connection is unloaded, and the removable connector controls it to close or open by servomechanism.
2. fixed-wing unmanned plane according to claim 1 takes off and landing system, it is characterised in that described detachably to connect
Fitting includes the projection being arranged on the both sides wing of the fixed-wing unmanned plane (1), is arranged on the multi-rotor unmanned aerial vehicle (2)
The upper handgrip corresponding with projection, the handgrip is connected with servomechanism, and controls it to close or open by servomechanism.
3. fixed-wing unmanned plane according to claim 2 takes off and landing system, it is characterised in that the fixed-wing without
The outrigger shaft (11) parallel with fuselage axis is respectively arranged with man-machine both sides wing, the projection is arranged on outrigger shaft
(11) on, in order to which handgrip is grasped.
4. fixed-wing unmanned plane according to claim 3 takes off and landing system, it is characterised in that the outrigger shaft
(11) two ends are respectively arranged with the projection, and the projection is telescopic to be arranged on outrigger shaft (11), many rotors without
The lower section of man-machine (2) is evenly distributed with and raised corresponding mechanical gripper by basic point of center of gravity.
5. fixed-wing unmanned plane according to claim 1 takes off and landing system, it is characterised in that described detachably to connect
Fitting includes being separately positioned on fixed-wing unmanned plane (1) and the first electromagnetism part and the second electromagnetism part of multi-rotor unmanned aerial vehicle (2), institute
State the first electromagnetism part and the second electromagnetism part is mutually adsorbed, and the first electromagnetism part and/or the second electromagnetism part control its magnetic by servomechanism
Property.
6. fixed-wing unmanned plane according to claim 5 takes off and landing system, it is characterised in that first electromagnetism
The guide cylinder of bell mouth shape is provided with the outside of part, the second electromagnetism part is the round platform knot being adapted with guide cylinder inner structure
Structure.
7. fixed-wing unmanned plane according to claim any one of 1-6 takes off and landing system, it is characterised in that also wrap
Interception net (3) is included, the interception net (3) is arranged between at least two multi-rotor unmanned aerial vehicles (2), and the interception net (3)
Edge is provided with can carry out the draw-string that pull receives net by servomechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621015084.7U CN206476113U (en) | 2016-08-31 | 2016-08-31 | A kind of fixed-wing unmanned plane takes off and landing system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621015084.7U CN206476113U (en) | 2016-08-31 | 2016-08-31 | A kind of fixed-wing unmanned plane takes off and landing system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206476113U true CN206476113U (en) | 2017-09-08 |
Family
ID=59756129
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621015084.7U Withdrawn - After Issue CN206476113U (en) | 2016-08-31 | 2016-08-31 | A kind of fixed-wing unmanned plane takes off and landing system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206476113U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106428554A (en) * | 2016-08-31 | 2017-02-22 | 天津曙光天成科技有限公司 | Takeoff and landing system and method for fixed-wing unmanned aerial vehicle |
| CN109956043A (en) * | 2017-12-26 | 2019-07-02 | 广州亿航智能技术有限公司 | Flight instruments |
| CN110816846A (en) * | 2019-11-29 | 2020-02-21 | 集美大学 | Can realize fixed wing unmanned aerial vehicle of vertical take-off |
-
2016
- 2016-08-31 CN CN201621015084.7U patent/CN206476113U/en not_active Withdrawn - After Issue
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106428554A (en) * | 2016-08-31 | 2017-02-22 | 天津曙光天成科技有限公司 | Takeoff and landing system and method for fixed-wing unmanned aerial vehicle |
| CN109956043A (en) * | 2017-12-26 | 2019-07-02 | 广州亿航智能技术有限公司 | Flight instruments |
| CN110816846A (en) * | 2019-11-29 | 2020-02-21 | 集美大学 | Can realize fixed wing unmanned aerial vehicle of vertical take-off |
| CN110816846B (en) * | 2019-11-29 | 2021-05-04 | 集美大学 | Can realize fixed wing unmanned aerial vehicle of vertical take-off |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20170908 Effective date of abandoning: 20181012 |
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| AV01 | Patent right actively abandoned |