CN106915440A - The landing method and its device of a kind of fixed wing aircraft - Google Patents
The landing method and its device of a kind of fixed wing aircraft Download PDFInfo
- Publication number
- CN106915440A CN106915440A CN201710139310.5A CN201710139310A CN106915440A CN 106915440 A CN106915440 A CN 106915440A CN 201710139310 A CN201710139310 A CN 201710139310A CN 106915440 A CN106915440 A CN 106915440A
- Authority
- CN
- China
- Prior art keywords
- wing aircraft
- fixed wing
- rotor aerocraft
- landing
- cross
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
Abstract
The landing method and its device of the landing method and its device of a kind of fixed wing aircraft, category vehicle technology field, more particularly to a kind of fixed wing aircraft；Including fixed wing aircraft and multi-rotor aerocraft, fixed wing aircraft is equipped with d GPS locating module and infrarede emitting diode and criss-cross groove is provided with directly over position of centre of gravity, groove center is equipped with crash sensor, the four direction of groove respectively has a spacer, and spacer is driven using electronic or hydraulic way；Multi-rotor aerocraft has a cross, and equipped with individual infrared camera；Infrared camera and infrarede emitting diode realize accurate alignment by image recognition, and when cross touches crash sensor, four spacer automatic locking crosses, cross is engaged with groove.The present invention allows fixed wing aircraft and multi-rotor aerocraft connection to combine, and multi-rotor aerocraft provides the aerial runway of landing for fixed wing aircraft, reduces runway construction, is conducive to the popularization of fixed wing aircraft.
Description
Technical field
The present invention relates to vehicle technology field, more particularly to a kind of fixed wing aircraft landing method and its device.
Background technology
Traditional fixed wing aircraft advantage is fast flying speed, and voyage and cruise time are long, have the disadvantage landing distance,
Seek high-quality runway.The advantage of multi-rotor aerocraft is smaller place VTOL, and hovering has the disadvantage that power consumption is big, fast
Degree is slow, cruising time is short.
The content of the invention
The present invention provides a kind of landing method and its device of fixed wing aircraft, the race the purpose is to reduce fixed wing aircraft
Road is built, and is conducive to the popularization of fixed-wing.
To achieve the above object, the technical scheme taken of the present invention is：
A kind of landing-gear of fixed wing aircraft of the present invention, including fixed wing aircraft and multi-rotor aerocraft；The fixed-wing flies
Criss-cross groove is provided with directly over machine position of centre of gravity, described groove center is provided with a crash sensor, described
The four direction of groove respectively has a spacer, and spacer is driven using electronic or hydraulic way；Described multi-rotor aerocraft
It is arranged right below a cross.
The fixed wing aircraft and multi-rotor aerocraft are separately installed with damping device.
The fixed wing aircraft is provided with d GPS locating module, and the multi-rotor aerocraft is arranged on fixed-wing by receiving
The location information of the d GPS locating module acquisition of information fixed wing aircraft on aircraft.
The multi-rotor aerocraft is provided with infrared camera, and the fixed wing aircraft is provided with infrarede emitting diode,
Accurate alignment is realized by image recognition.
A kind of landing method of fixed wing aircraft：When fixed wing aircraft prepares to land, d GPS locating module is positioned,
Multi-rotor aerocraft on ground obtains surface and the fixed-wing of the fixed wing aircraft that flies to after the location information of fixed wing aircraft
The equidirectional flight of aircraft, the infrared camera on infrarede emitting diode and multi-rotor aerocraft on fixed wing aircraft is by figure
As identification technology is accurately aligned, the cross of multi-rotor aerocraft flies gradually to be aligned from directly over fixed wing aircraft and is close to
The criss-cross groove of the surface of fixed-wing, the cross on the fully-inserted fixed wing aircraft of the cross of multi-rotor aerocraft
Connected in star and when touching crash sensor, four spacers of groove are pinned under the driving of hydraulic means or electric device
Cross, now fixed wing aircraft power set be stopped, multi-rotor aerocraft with fixed wing aircraft fly back ground land.
Therefore, it is that fixed wing aircraft is carried the invention provides the landing method and its device of a kind of fixed wing aircraft
For aerial runway, runway construction is reduced, be conducive to the popularization of fixed wing aircraft.
Brief description of the drawings
Fig. 1 is the schematic top plan view of fixed wing aircraft.
Fig. 2 is the left view schematic diagram of multi-rotor aerocraft.
Fig. 3 is the left view schematic diagram of fixed wing aircraft and multi-rotor aerocraft docking.
In figure, 1- fixed wing aircrafts, 2- spacers, 3- crash sensors, 4- grooves, 5- multi-rotor aerocrafts, 6- crosses
Frame, 8- infrared cameras, 9- infrarede emitting diodes.
Specific embodiment
In conjunction with accompanying drawing, 1 ~ 3 couple of present invention is illustrated：A kind of landing-gear of fixed wing aircraft, including fixed-wing
Aircraft 1 and multi-rotor aerocraft 5；Criss-cross groove 4 is provided with directly over the position of centre of gravity of the fixed wing aircraft 1, described is recessed
The center of groove 4 is provided with a crash sensor 3, and the four direction of described groove 4 respectively has a spacer 2, and spacer 2 is adopted
Driven with electronic or hydraulic way；Described multi-rotor aerocraft 5 is arranged right below a cross 6.
The fixed wing aircraft 1 and multi-rotor aerocraft 5 are separately installed with damping device.
The fixed wing aircraft 1 is provided with d GPS locating module, and the multi-rotor aerocraft 5 is fixed by receiving to be arranged on
The location information of the d GPS locating module acquisition of information fixed wing aircraft 1 on wing aircraft 1.
The multi-rotor aerocraft 5 is provided with infrared camera 8 and is located on cross 6, and the fixed wing aircraft 1 is installed
There is infrarede emitting diode 9, accurate alignment is realized by image recognition.
A kind of landing method of fixed wing aircraft：When fixed wing aircraft 1 prepares to land, d GPS locating module is positioned,
Multi-rotor aerocraft 5 on ground obtains surface and the fixation of the aircraft of fixed-wing 1 that flies to after the location information of fixed wing aircraft 1
Wing aircraft 1 flies in the same direction, the infrared camera 8 on infrarede emitting diode 9 and multi-rotor aerocraft 5 on fixed wing aircraft 1
Accurately it is aligned by image recognition technology, the flight from directly over fixed wing aircraft 1 of multi-rotor aerocraft 5 is gradually aligned and is close to
The cross groove 4 of the surface of fixed wing aircraft 1, when the fully-inserted fixed wing aircraft 1 of the cross 6 of multi-rotor aerocraft 5
On groove 4 and when touching crash sensor 3, four spacers 2 of groove 4 pin cross under the driving of hydraulic means
Frame 6, now the power set of fixed wing aircraft 1 be stopped, multi-rotor aerocraft 5 with fixed wing aircraft 1 fly back ground land,
Fixed wing aircraft 1 puts down the undercarriage of itself before landing, and steadily after landing, hydraulic means drives spacer 2 to wing aircraft to be fixed 1
Cross 6 is decontroled, multi-rotor aerocraft 5 flies back ground, now 6 one-tenth of the cross undercarriage of multi-rotor aerocraft 5.
Claims (7)
1. a kind of landing-gear of fixed wing aircraft, it is characterised in that：Including fixed wing aircraft（1）And multi-rotor aerocraft（5）；
The fixed wing aircraft（1）Criss-cross groove is provided with directly over position of centre of gravity（4）, described groove（4）Four direction it is each
There is a spacer（2）, spacer（2）Driven using electronic or hydraulic way；Described multi-rotor aerocraft（5）Underface sets
There is a cross（6）.
2. the landing-gear of a kind of fixed wing aircraft according to claim 1, it is characterised in that：Fixed wing aircraft（1）With
Multi-rotor aerocraft（5）It is separately installed with damping device.
3. the landing-gear of a kind of fixed wing aircraft according to claim 1, it is characterised in that：Groove（4）Feel at ease center
Equipped with a crash sensor（3）.
4. the landing-gear of a kind of fixed wing aircraft according to claim 1, it is characterised in that：Fixed wing aircraft（1）Peace
Equipped with d GPS locating module；Multi-rotor aerocraft（5）Fixed wing aircraft is arranged on by receiving（1）On d GPS locating module information
Obtain fixed wing aircraft（1）Location information.
5. the landing-gear of a kind of fixed wing aircraft according to claim 1, it is characterised in that：Multi-rotor aerocraft（5）
Infrared camera is installed（8）And positioned at cross（6）On；Fixed wing aircraft（1）Infrarede emitting diode is installed（9）.
6. a kind of landing method of fixed wing aircraft, it is characterised in that：Work as fixed wing aircraft（1）When preparing landing, on ground
Multi-rotor aerocraft（5）Obtain fixed wing aircraft（1）Location information after fly to fixed-wing（1）The surface of aircraft and fixed-wing
Aircraft（1）Flight, fixed wing aircraft in the same direction（1）On infrarede emitting diode（9）And multi-rotor aerocraft（5）On infrared take the photograph
As head（8）Accurately it is aligned by image recognition technology, multi-rotor aerocraft（5）From fixed wing aircraft（1）Surface is gradually
Alignment is near fixed wing aircraft（1）Surface cross groove（4）, work as multi-rotor aerocraft（5）Cross（6）Completely
Insertion fixed wing aircraft（1）On groove（4）And touch crash sensor（3）When, groove（4）Four spacers（2）
Cross is pinned under the driving of hydraulic means or electric device（6）, now fixed wing aircraft（1）Power set are stopped,
Multi-rotor aerocraft（5）With fixed wing aircraft（1）Fly back ground landing.
7. the landing method of a kind of fixed wing aircraft according to claim 6, it is characterised in that：Fixed wing aircraft before landing
（1）Put down the undercarriage of itself, wing aircraft to be fixed（1）After steady landing, hydraulic means drives spacer（2）Decontrol cross
（6）, multi-rotor aerocraft（5）Fly back ground, now cross（6）Into multi-rotor aerocraft（5）Undercarriage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710139310.5A CN106915440A (en) | 2017-03-10 | 2017-03-10 | The landing method and its device of a kind of fixed wing aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710139310.5A CN106915440A (en) | 2017-03-10 | 2017-03-10 | The landing method and its device of a kind of fixed wing aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106915440A true CN106915440A (en) | 2017-07-04 |
Family
ID=59460416
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710139310.5A Withdrawn CN106915440A (en) | 2017-03-10 | 2017-03-10 | The landing method and its device of a kind of fixed wing aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106915440A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107618665A (en) * | 2017-09-18 | 2018-01-23 | 佛山市神风航空科技有限公司 | A kind of method and device for increasing multi-rotor aerocraft flying distance |
| CN107640315A (en) * | 2017-09-18 | 2018-01-30 | 佛山市神风航空科技有限公司 | A kind of device for increasing multi-rotor aerocraft flying distance |
| US11912435B2 (en) | 2019-07-10 | 2024-02-27 | Israel Aerospace Industries Ltd. | Air vehicle system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202328551U (en) * | 2011-12-05 | 2012-07-11 | Tcl空调器(中山)有限公司 | Installing structure for middle separation plate |
| CN105059550A (en) * | 2015-08-31 | 2015-11-18 | 深圳市飞研智能科技有限公司 | Double unmanned aerial vehicle with improved endurance |
| CN105867409A (en) * | 2016-03-30 | 2016-08-17 | 深圳市高巨创新科技开发有限公司 | Unmanned aerial vehicle air docking method and system |
| 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 |
| CN206537501U (en) * | 2017-03-10 | 2017-10-03 | 佛山市神风航空科技有限公司 | A kind of landing-gear of fixed wing aircraft |
-
2017
- 2017-03-10 CN CN201710139310.5A patent/CN106915440A/en not_active Withdrawn
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202328551U (en) * | 2011-12-05 | 2012-07-11 | Tcl空调器(中山)有限公司 | Installing structure for middle separation plate |
| CN105059550A (en) * | 2015-08-31 | 2015-11-18 | 深圳市飞研智能科技有限公司 | Double unmanned aerial vehicle with improved endurance |
| CN105867409A (en) * | 2016-03-30 | 2016-08-17 | 深圳市高巨创新科技开发有限公司 | Unmanned aerial vehicle air docking method and system |
| 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 |
| CN206537501U (en) * | 2017-03-10 | 2017-10-03 | 佛山市神风航空科技有限公司 | A kind of landing-gear of fixed wing aircraft |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107618665A (en) * | 2017-09-18 | 2018-01-23 | 佛山市神风航空科技有限公司 | A kind of method and device for increasing multi-rotor aerocraft flying distance |
| CN107640315A (en) * | 2017-09-18 | 2018-01-30 | 佛山市神风航空科技有限公司 | A kind of device for increasing multi-rotor aerocraft flying distance |
| US11912435B2 (en) | 2019-07-10 | 2024-02-27 | Israel Aerospace Industries Ltd. | Air vehicle system |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20170704 |