CN106915453A - A kind of takeoff and landing mode and system - Google Patents
A kind of takeoff and landing mode and system Download PDFInfo
- Publication number
- CN106915453A CN106915453A CN201710143124.9A CN201710143124A CN106915453A CN 106915453 A CN106915453 A CN 106915453A CN 201710143124 A CN201710143124 A CN 201710143124A CN 106915453 A CN106915453 A CN 106915453A
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- China
- Prior art keywords
- aircraft
- axis
- takeoff
- bracket
- landing
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- 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
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- 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
A kind of takeoff and landing mode and system, belong to technical field of aerospace.The takeoff and landing system includes Multi-axis aircraft and aircraft；Multi-axis aircraft top is provided with bracket, and the top of bracket is U-lag, referred to as bracket slot, and the front opening of bracket slot is more than open rearward end, and the shape of the upper surface of bracket matches with the belly of aircraft, is easy to hold aircraft in consistent manner.The front end of bracket slot is higher than rear end, set the front end of bracket slot higher than the purpose of rear end be make aircraft ride over fuselage when on Multi-axis aircraft head height tail it is low, be conducive to that support is steady to be difficult to slide, and can make to ensure that aircraft main wing has positive incidence during aircraft flight in the air, be conducive to taking off.The present invention is sufficiently used the advantage of Multi-axis aircraft and aircraft.Using Multi-axis aircraft for aircraft sets up aerial runway, aircraft is set conveniently to realize VTOL, landing site occupies little space, and the construction cost on airport is low, is conducive to the popularization of aircraft.
Description
Technical field
A kind of takeoff and landing mode and system, belong to technical field of aerospace, more particularly to a kind of takeoff and landing mode and system.
Background technology
Traditional takeoff and landing mode is to accelerate to take off afterwards to a certain extent or fall-retarding on straightaway very long.
It is big not enough that traditional landing mode at least has two：First, runway is long and flatness is high, it is desirable to which the area of take-off venue is big, machine
Field construction investment is big；Second, aircraft need to install undercarriage, and preferentially using wheel undercarriage, the static load of such aircraft is negative big.At present
Though popular VTOL Fixed Wing AirVehicle can be vertically moved up or down, payload is small, less efficient, and safety coefficient is not high.
One of major reason that aircraft is not popularized is exactly inconvenient landing；Helicopter does not popularize mainly manipulation technology difficulty
Greatly, complex structure；The manned more difficult popularization of Multi-axis aircraft is because when dangerous especially people psychological dangerous and continuation of the journey
Between not grow, endurance distance is not far and efficiency is low.
The content of the invention
Above-mentioned deficiency the invention aims to overcome traditional landing mode, makes full use of aircraft and multiaxis to fly
The advantage of device, invents a kind of not high to site requirements and safely and efficiently takeoff and landing mode and system, is conducive to the general of aircraft
And.
The technical scheme is that：A kind of landing mode of aircraft is realized by following takeoff and landing system
, the takeoff and landing system includes Multi-axis aircraft and aircraft；Described Multi-axis aircraft top is provided with bracket, bracket it is upper
Portion is U-lag, referred to as bracket slot, and the front opening of bracket slot is more than open rearward end, shape and the aircraft of the upper surface of bracket
Belly matches, and is easy to hold aircraft in consistent manner.The front end of bracket slot is higher than rear end, sets the front end of bracket slot higher than rear end
Purpose be make aircraft ride over fuselage when on Multi-axis aircraft head height tail it is low, be conducive to that support is steady to be difficult to slide, and aircraft can be made
Ensure that aircraft main wing has positive incidence during flight in the air, be conducive to taking off.
Preferably, the front end of bracket slot be higher than rear end so that aircraft is ridden over when on Multi-axis aircraft, the longitudinal axis of aircraft with
The angle of the propeller Plane of rotation of Multi-axis aircraft is that the fore-and-aft direction of airframe rotates with the propeller of Multi-axis aircraft
The angle of plane is between 8 ~ 25 °.
Preferably, in order to the bracket slot of Multi-axis aircraft easily entangles the belly of aircraft, the front end of bracket slot in the air
It is smooth horn mouth.
Preferably, the right and left of bracket has been arranged symmetrically two identical support members, support member on Multi-axis aircraft
It is the main wing for supporting aircraft, rides on Multi-axis aircraft while aircraft left-right balance can be made.
Preferably, the top of support member is provided with antifriction ball, needle roller or wheel.
Preferably, described Multi-axis aircraft uses four-axle aircraft, propeller to be arranged in X-type.
Preferably, described Multi-axis aircraft uses six axle aircraft, propeller to be arranged in rich font.
Preferably, obtained with the bracket slot card of Multi-axis aircraft to prevent aircraft from riding over the belly of aircraft when on Multi-axis aircraft
It is too dead, stud with elastic antifriction ball in the upper surface of bracket.
Preferably, obtained with the bracket slot card of Multi-axis aircraft to prevent aircraft from riding over the belly of aircraft when on Multi-axis aircraft
It is too dead, breach is provided with the both sides of bracket, the opening of breach forward, projection, the projection is set in the relevant position of aircraft belly
It is coincide with breach, it is forward and stuck for blocking bracket transition.The setting of breach and projection can make aircraft keep left-right balance.
Preferably, the projection is the bearing pin of lateral arrangement.Indentation, there is lined with damping rubber.To make breach with projection well
It coincide, electromagnetic suction device is provided with the junction of breach and projection.
Preferably, main wing of the tailplane of aircraft higher than aircraft.
Preferably, guider is configured with aircraft, guider uses the Big Dipper or GPS navigation.
Preferably, guider is configured with Multi-axis aircraft, guider uses the Big Dipper or GPS navigation.
Preferably, aerial docking for convenience, radar installations is configured with aircraft and Multi-axis aircraft.
Preferably, aerial docking for convenience, infrared facility is configured with aircraft and Multi-axis aircraft.
Preferably, aerial docking for convenience, pattern recognition device is configured with aircraft and Multi-axis aircraft.
Preferably, aircraft does not set undercarriage or is provided with telescopic type undercarriage, sets the mesh of telescopic type undercarriage
Be convenient voluntarily there is the landing at the airport of runway, or reinstated during Multi-axis aircraft failure.
Aircraft and Multi-axis aircraft are docked by the way of artificial or automatic mode in the air.
Aircraft is manned machine or unmanned plane.
Multi-axis aircraft is unmanned plane or manned machine.
Operation principle of the invention is：When aircraft needs to take off, the belly of aircraft is first plugged into multiaxis in consistent manner and is flown
On the bracket of row device, aircraft is set to ride on Multi-axis aircraft；Start Multi-axis aircraft, aircraft vertical by Multi-axis aircraft support
Fly, after flying to certain altitude, Multi-axis aircraft support aircraft and flown windward during strong wind, and Multi-axis aircraft support when not having wind or gentle breeze
Aircraft flight forward, when flying speed takeoff speed normal close to aircraft, starts aircraft engine, drives aircraft to accelerate to fly
OK, Multi-axis aircraft reduction throttle, aircraft departs from Multi-axis aircraft, and aircraft independently flies away, and Multi-axis aircraft returns to ground.
When aircraft flies in the air needs landing, the Multi-axis aircraft on ground is connected to task to be risen fly to meet winged immediately
Machine；Multi-axis aircraft first flies to the rear of aircraft and aircraft flies in the same direction, then from the rear of aircraft slowly close to the machine of aircraft
Body belly entangles the belly of aircraft up to the bracket of Multi-axis aircraft, and following Multi-axis aircraft is combined with aircraft
Flight, then the engine misses of aircraft, next, Multi-axis aircraft carries aircraft on the back flies to ground, smoothly complete landing.
Beneficial effects of the present invention and purposes are：The advantage of the energy VTOL of Multi-axis aircraft is sufficiently used,
The advantages of cruising time for taking full advantage of aircraft is long, speed is fast, voyage is remote, safety, manipulation facilitate.It is using Multi-axis aircraft
Aircraft sets up aerial runway, aircraft is conveniently realized VTOL, and landing site occupies little space, and the construction cost on airport is low,
Be conducive to the popularization of aircraft.The invention is simple and easy to apply, with also more convenient on naval vessel；Can be widely applied to unmanned plane field,
Military field, navigation field and civil aviaton field.The invention is adapted to following job that requires special skills：Power construction, it is aerial to charge, it is fixation
Wing unmanned plane is changed battery in the air, is that military unmanned air vehicle is added ammunition etc. in the air.Aviation can militarily be taken over
The partial task of mother ship carrier.
Brief description of the drawings
Schematic diagram when Fig. 1 is aircraft and Multi-axis aircraft combination；Fig. 2 is the vertical of carriage tape Multi-axis aircraft jaggy
Body schematic diagram；Fig. 3 is the schematic diagram of Multi-axis aircraft of the bracket the right and left equipped with support member, the top dress of support member in Fig. 3
There is antifriction wheel.
In figure, 1- aircrafts, 11- main wings, 12- empennages, 13- fuselages, 14- projections；2- Multi-axis aircrafts, 21- brackets, 22-
Breach, 23- Multi-axis aircraft undercarriages, 24- support members, 241- antifriction wheels.
Specific embodiment
The present invention is illustrated in conjunction with accompanying drawing.
Embodiment one：1 and 2, a kind of takeoff and landing system, including Multi-axis aircraft 2 and aircraft 1 referring to the drawings；Described
The top of Multi-axis aircraft 2 is provided with bracket 21, and the top of bracket 21 is U-lag, referred to as bracket slot, and the front opening of bracket slot is big
In open rearward end, the shape of the upper surface of bracket 21 matches with the belly of aircraft 1, is easy to hold aircraft 1 in consistent manner.Bracket slot
Front end be higher than rear end, aircraft 1 is ridden over the head of fuselage 13 when on Multi-axis aircraft 2 higher than afterbody, be conducive to support
It is steady to be difficult to slide, and can make to ensure that the main wing 11 of aircraft 1 has positive incidence during the flight in the air of aircraft 1, be conducive to aircraft 1 to take off.
For prevent aircraft 1 ride over the belly of aircraft 1 and Multi-axis aircraft 2 when on Multi-axis aircraft 2 bracket slot Ka get Tai it is dead, in bracket
21 both sides are provided with breach 22, and the opening of breach 22 forward, projection 14, the projection 14 is set in the relevant position of the belly of aircraft 1
It is coincide with breach 22, it is forward and stuck for blocking the transition of bracket 21.The setting of breach 22 and projection 14 can make aircraft 1 keep left
Right balance.
A kind of takeoff and landing system of embodiment one is so work：When aircraft 1 needs to take off, first by the machine of aircraft 1
The belly of body 13 is plugged on the bracket 21 of Multi-axis aircraft 2 in consistent manner, aircraft 1 is ridden on Multi-axis aircraft 2, Multi-axis aircraft 2
Bracket 21 on the breach 22 of left and right two block two projections 14 of the left and right sides of 1 fuselage of aircraft 13；Start Multi-axis aircraft
2, aircraft 1 by the support of Multi-axis aircraft 2 and is taken off vertically, after flying to certain altitude, the support of Multi-axis aircraft 2 flight forward of aircraft 1,
When 1 speed of flying is close to 1 normal takeoff speed of aircraft, the engine of aircraft 1 is started, drive aircraft 1 to accelerate flight, multiaxis flight
The reduction throttle of device 2, aircraft 1 departs from Multi-axis aircraft 2, and aircraft 1 independently flies away, and Multi-axis aircraft 2 returns to ground.Aerial flies
When machine 1 needs landing, the Multi-axis aircraft 2 on ground is connected to task to be risen fly to meet aircraft 1 immediately；Multi-axis aircraft 2 first flies to
The rear of aircraft 1 is flown in the same direction with aircraft 1, then from the rear of aircraft 1 belly of fuselage 13 slowly close to aircraft 1 up to multiaxis
The bracket 21 of aircraft 2 entangles the belly of fuselage 13 of aircraft 1, and the breach 22 of left and right two on the bracket 21 of Multi-axis aircraft 2 blocks
Firmly two projections 14 of the left and right sides of 1 fuselage of aircraft 13；Following Multi-axis aircraft 2 combines flight with aircraft 1, then
The engine misses of aircraft 1, next, Multi-axis aircraft 2 carries aircraft 1 on the back flies to ground, smoothly complete landing.
Embodiment two：A kind of takeoff and landing system, including Multi-axis aircraft 2 and aircraft 1；On described Multi-axis aircraft 2
Side is provided with bracket 21, and the top of bracket 21 is U-lag, referred to as bracket slot, and the front opening of bracket slot is more than open rearward end, support
The shape of the upper surface of frame 21 matches with the belly of aircraft 1, is easy to hold aircraft 1 in consistent manner.After the front end of bracket slot is higher than
End, can so make aircraft 1 ride over the head of fuselage 13 when on Multi-axis aircraft 2 higher than afterbody, be conducive to support to be surely difficult to slide, and
Can make to ensure that the main wing 11 of aircraft 1 has positive incidence during the flight in the air of aircraft 1, be conducive to aircraft 1 to take off.The right and left of bracket
Two identical support members are arranged symmetrically on Multi-axis aircraft, support member is the main wing for supporting aircraft, can make to fly
Ride on Multi-axis aircraft machine left-right balance.The top of support member 24 is provided with antifriction wheel 241, in order to avoid the top of support member
The lower surface of main wing is abraded, as shown in Figure 3.
A kind of takeoff and landing system of embodiment two is so work：When aircraft 1 needs to take off, first by the machine of aircraft 1
The belly of body 13 is plugged on the bracket 21 of Multi-axis aircraft 2 in consistent manner, aircraft 1 is ridden on Multi-axis aircraft 2, Multi-axis aircraft 2
Two support members 24 support the main wing 11 of aircraft 1, antifriction wheel 241 withstands the lower surface of main wing 11；Start Multi-axis aircraft
2, aircraft 1 by the support of Multi-axis aircraft 2 and is taken off vertically, after flying to certain altitude, the support of Multi-axis aircraft 2 flight forward of aircraft 1,
When 1 speed of flying is close to 1 normal takeoff speed of aircraft, the engine of aircraft 1 is started, drive aircraft 1 to accelerate flight, multiaxis flight
The reduction throttle of device 2, aircraft 1 departs from Multi-axis aircraft 2, and aircraft 1 independently flies away, and Multi-axis aircraft 2 returns to ground.Aerial flies
When machine 1 needs landing, the Multi-axis aircraft 2 on ground is connected to task to be risen fly to meet aircraft 1 immediately；Multi-axis aircraft 2 first flies to
The rear of aircraft 1 is flown in the same direction with aircraft 1, then from the rear of aircraft 1 belly of fuselage 13 slowly close to aircraft 1 up to multiaxis
The bracket 21 of aircraft 2 entangles the belly of fuselage 13 of aircraft 1, and two support members 24 of Multi-axis aircraft 2 support the master of aircraft 1
The wing 11, antifriction wheel 241 withstands the lower surface of main wing 11；Following Multi-axis aircraft 2 combines flight with aircraft 1, then
The engine misses of aircraft 1, next, Multi-axis aircraft 2 carries aircraft 1 on the back flies to ground, smoothly complete landing.
Claims (14)
1. a kind of takeoff and landing system, it is characterised in that：Including Multi-axis aircraft and aircraft；Described Multi-axis aircraft top sets
Bracket is put, the shape of the upper surface of bracket matches with the belly of aircraft；The front end of bracket slot is higher than rear end.
2. a kind of takeoff and landing system according to claim 1, it is characterised in that：The fore-and-aft direction and multiaxis of airframe
The angle of the propeller Plane of rotation of aircraft is between 8 ~ 25 °.
3. a kind of takeoff and landing system according to claim 1, it is characterised in that：The front end of bracket slot is smooth loudspeaker
Mouthful.
4. a kind of takeoff and landing system according to claim 1 or 2 or 3, it is characterised in that：The right and left of bracket is more
Two identical support members are arranged symmetrically on axle aircraft, the top of support member is provided with antifriction ball, needle roller or wheel；Or
Person：Be provided with breach in the both sides of bracket, the opening of breach forward, projection is set in the relevant position of aircraft belly, the projection with
Breach coincide.
5. a kind of takeoff and landing system according to claim 1 or 2 or 3, it is characterised in that：Described Multi-axis aircraft is adopted
With four-axle aircraft, propeller is in X-type arrangement；Or：Described Multi-axis aircraft uses six axle aircraft, and propeller is in rich word
Type is arranged.
6. a kind of takeoff and landing system according to claim 1 or 2 or 3, it is characterised in that：The upper surface of bracket studs with bullet
Property antifriction ball.
7. a kind of takeoff and landing system according to claim 1, it is characterised in that：The projection is the pin of lateral arrangement
Axle；Indentation, there is lined with damping rubber；To make breach be coincide well with projection, it is provided with electromagnetism in the junction of breach and projection and inhales
Attach together and put.
8. a kind of takeoff and landing system according to claim 1 or 2 or 3, it is characterised in that：The tailplane of aircraft is higher than
The main wing of aircraft.
9. a kind of takeoff and landing system according to claim 1 or 2 or 3, it is characterised in that：Navigation dress is configured with aircraft
Put, guider uses the Big Dipper or GPS navigation；Guider is configured with Multi-axis aircraft, guider uses the Big Dipper or GPS
Navigation.
10. a kind of takeoff and landing system according to claim 1 or 2 or 3, it is characterised in that：Aerial docking for convenience,
Radar installations is configured with aircraft and Multi-axis aircraft；Aerial docking, is configured with red on aircraft and Multi-axis aircraft for convenience
Outer line apparatus.
A kind of 11. takeoff and landing system according to claim 1 or 2 or 3, it is characterised in that：Aircraft does not set undercarriage.
A kind of 12. takeoff and landing systems according to claim 1, it is characterised in that：Aircraft and Multi-axis aircraft are in the air
Dock by the way of artificial or automatic mode.
A kind of 13. takeoff and landing systems, it is characterised in that：When aircraft needs to take off, first the belly of aircraft is inserted in consistent manner
On the bracket of upper Multi-axis aircraft, aircraft is set to ride on Multi-axis aircraft；Start Multi-axis aircraft, by Multi-axis aircraft support winged
Machine takes off vertically, and after flying to certain altitude, Multi-axis aircraft support aircraft and flown windward during strong wind, and multiaxis flies when not having wind or gentle breeze
Row device support aircraft flight forward, when flying speed takeoff speed normal close to aircraft, starts aircraft engine, drives aircraft
Accelerate flight, Multi-axis aircraft reduction throttle, aircraft departs from Multi-axis aircraft, and aircraft is independently flown away, and Multi-axis aircraft is returned
Ground.
A kind of 14. takeoff and landing systems, it is characterised in that：When aircraft needs landing, the Multi-axis aircraft on ground is connected to task
Rise immediately and fly to meet aircraft；Multi-axis aircraft first flies to the rear of aircraft and aircraft flies in the same direction, then from the rear of aircraft
Slowly the belly close to aircraft is until the bracket of Multi-axis aircraft entangles the belly of aircraft, following Multi-axis aircraft
Flight is combined with aircraft, then the engine misses of aircraft, next, Multi-axis aircraft carries aircraft on the back flies to ground,
Smoothly complete landing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710143124.9A CN106915453A (en) | 2017-03-10 | 2017-03-10 | A kind of takeoff and landing mode and system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710143124.9A CN106915453A (en) | 2017-03-10 | 2017-03-10 | A kind of takeoff and landing mode and system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106915453A true CN106915453A (en) | 2017-07-04 |
Family
ID=59460383
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710143124.9A Pending CN106915453A (en) | 2017-03-10 | 2017-03-10 | A kind of takeoff and landing mode and system |
Country Status (1)
| Country | Link |
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| CN (1) | CN106915453A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110239726A (en) * | 2019-05-14 | 2019-09-17 | 中国空气动力研究与发展中心计算空气动力研究所 | A method of for internally burying the oiling of magazine Aircraft Air plus bullet |
| JP2019163041A (en) * | 2017-11-06 | 2019-09-26 | 株式会社エアロネクスト | Flying body and method for controlling flying body |
| CN111498132A (en) * | 2020-04-27 | 2020-08-07 | 南京工程学院 | Servo tracking robot for intelligent safe landing of aircraft landing gear fault |
| CN113716048A (en) * | 2021-07-22 | 2021-11-30 | 北京航空航天大学 | Taking-off and landing method for floating type air mobile airport platform carrying fixed-wing aircraft |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005400A (en) * | 2016-07-13 | 2016-10-12 | 绵阳空天科技有限公司 | Vertical-takeoff auxiliary system for fixed-wing aircraft |
| CN106043689A (en) * | 2016-07-22 | 2016-10-26 | 绵阳空天科技有限公司 | Vertical take-off auxiliary system for top-mounted fixed-wing aircraft |
-
2017
- 2017-03-10 CN CN201710143124.9A patent/CN106915453A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005400A (en) * | 2016-07-13 | 2016-10-12 | 绵阳空天科技有限公司 | Vertical-takeoff auxiliary system for fixed-wing aircraft |
| CN106043689A (en) * | 2016-07-22 | 2016-10-26 | 绵阳空天科技有限公司 | Vertical take-off auxiliary system for top-mounted fixed-wing aircraft |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2019163041A (en) * | 2017-11-06 | 2019-09-26 | 株式会社エアロネクスト | Flying body and method for controlling flying body |
| CN110239726A (en) * | 2019-05-14 | 2019-09-17 | 中国空气动力研究与发展中心计算空气动力研究所 | A method of for internally burying the oiling of magazine Aircraft Air plus bullet |
| CN111498132A (en) * | 2020-04-27 | 2020-08-07 | 南京工程学院 | Servo tracking robot for intelligent safe landing of aircraft landing gear fault |
| CN113716048A (en) * | 2021-07-22 | 2021-11-30 | 北京航空航天大学 | Taking-off and landing method for floating type air mobile airport platform carrying fixed-wing aircraft |
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Application publication date: 20170704 |