CN106882369A - One kind combination aircraft and its landing modes - Google Patents
One kind combination aircraft and its landing modes Download PDFInfo
- Publication number
- CN106882369A CN106882369A CN201710139327.0A CN201710139327A CN106882369A CN 106882369 A CN106882369 A CN 106882369A CN 201710139327 A CN201710139327 A CN 201710139327A CN 106882369 A CN106882369 A CN 106882369A
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- CN
- China
- Prior art keywords
- wing aircraft
- fixed wing
- slot
- rotor aerocraft
- radar
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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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
One kind combination aircraft and its landing modes, belong to technical field of aerospace, more particularly to a kind of combination aircraft.Including handset and machine tool；Handset includes fixed wing aircraft, T-slot, motor and gate；Machine tool includes multi-rotor aerocraft and T-shaped axle.When fixed wing aircraft needs landing, multi-rotor aerocraft lift-off, from rear near fixed wing aircraft；After T-shaped axle is directed at T-slot, multi-rotor aerocraft accelerates flight forward, and after making T-shaped axle insertion T-slot, motor is rotated, closing gate, and fixed wing aircraft engine is stopped working, and ground is returned to fixed wing aircraft by multi-rotor aerocraft.Combination aircraft and its mode of taking off of the invention, its mode of taking off do not rely on place limitation, it is possible to achieve fixed wing aircraft takes off vertically.
Description
Technical field
One kind combination aircraft and its landing modes, belong to technical field of aerospace, more particularly to a kind of combination aircraft and
Its landing modes.
Background technology
Traditional aviation aircraft can be divided into fixed wing aircraft, helicopter and multi-rotor aerocraft.Wherein, fixed wing aircraft
Flying speed is fast, and mobility is high, and flying radius is big, and security performance coefficient is high, but due to the limitation of itself, to the bar for landing
Part requirement is harsh, and the landing of fixed wing aircraft is it is necessary to have sufficiently long runway.Helicopter can be with VTOL, but construction is multiple
It is miscellaneous, and expend larger for the culture of helicopter pilot, the driving technology requirement to driver is high.Multi-rotor aerocraft can be with
Accomplish VTOL, and it is simple to operate, it is workable, some narrow region operations can be entered, but, flying radius is small, continues
Boat ability is low, is used for taking photo by plane, monitoring field, and the scope of application is small, and more seriously, security and stability is low, due to many
Rotor craft is that many motors of multiaxis cooperate, as long as one of motor breaks down, certainly will cause to draw in the air
The accident rescued.And fixed wing aircraft is directly combined with multi-rotor aerocraft, many rotor structures can turn into solid during flight in the air
Determine the burden of the wing, or even influence is produced on the performance of fixed wing aircraft.
The content of the invention
The present invention program is that invention is a kind of can be with the combination aircraft of vertical landing in order to be directed to the deficiency of above-mentioned aircraft
And its landing modes, set up aerial runway.
One kind combination aircraft, including handset and machine tool；Handset includes fixed wing aircraft, T-slot, motor, gate and the
One radar；T-slot is placed in immediately below fixed wing aircraft, is slotted to the position of centre of gravity of fixed wing aircraft from afterbody, T-shaped, T
Type groove upper surface level；On T-slot top backward, there is a groove, groove includes motor and gate, gate one end connection motor
Rotating shaft, can rotate；Gate is divided into closing and opens two states, is closed mode when gate is laid；When gate is vertical, to beat
Open state；Gate is used to block T-shaped axle.First radar is placed in fixed wing aircraft afterbody, for launching detection signal, calibrates T-shaped
Position between groove and T-shaped axle.Machine tool includes multi-rotor aerocraft, controller, T-shaped axle and the second radar.T-shaped axle is with 3 ° ~ 10 °
Inclination angle is fixed on multi-rotor aerocraft, is rigid structure, and for being embedded into T-slot, be connected wing aircraft；Second thunder
Up to being placed on the inclined-plane that T-shaped axle is connected with multi-rotor aerocraft, it is connected with controller；Second radar is used to detect the first radar
Position；Controller is placed in inside multi-rotor aerocraft, and the positional information for being arrived according to the second detections of radar adjusts many rotors and flies
The position of row device, makes T-shaped axle alignment T-slot.
The groove is an a quarter circular groove, and, perpendicular to round groove, radius is across T for a quarter circular groove
Type groove；Motor is placed in home position；Motor parallel to T-slot, perpendicular to a quarter circular groove；Gate is placed in a quarter
In circular groove.
When fixed wing aircraft needs landing, fixed wing aircraft sends request signal, and the multi-rotor aerocraft on ground is received
To landing request signal lift-off, from rear near fixed wing aircraft；Then, the first radar emission signal, the second detections of radar
The signal of one radar, is accurately positioned to the first radar, and data are sent into controller, and controller calculates solid according to data
Determine distance and the position of wing aircraft, and control the multi-rotor aerocraft to make T-shaped axle alignment T-slot, it is fully aligned after, many rotors fly
Row device accelerates, and makes T-shaped axle insertion T-slot, reaches up to groove portion top, and then motor is rotated, closing gate, fixed wing aircraft hair
Motivation is stopped working；Multi-rotor aerocraft reduction of speed, ground is returned to by multi-rotor aerocraft with fixed wing aircraft.
Combination aircraft and its landing modes of the invention, its landing modes are not limited by place, have manufactured aerial runway,
The vertical landing of fixed wing aircraft can be realized, simple structure is easy to operate.
Brief description of the drawings
Fig. 1 is handset schematic rear view；Fig. 2 is gate schematic diagram；Fig. 3 is gate left view schematic diagram；Fig. 4 is combination flight
Device schematic diagram.
In figure, 1-T type grooves, 2-T profile shafts, 3- motors, 4- gates, 5- fixed wing aircrafts, 6- multi-rotor aerocrafts, 7- first
Radar, the radars of 8- second, 9- controllers.
Specific embodiment
The present invention is illustrated in conjunction with accompanying drawing, one kind combination aircraft and its landing modes, including handset and
Machine tool；Handset includes fixed wing aircraft 5, T-slot 1, motor 3, the radar 7 of gate 4 and first；Machine tool include multi-rotor aerocraft 6,
T-shaped axle 2, the second radar 8 and controller 9.
Handset includes fixed wing aircraft 5, T-slot 1, motor 3, the radar 7 of gate 4 and first；T-slot 1 is placed in fixed-wing and flies
Immediately below machine 5, slotted to the position of centre of gravity of fixed wing aircraft 5 from afterbody, T-shaped, the upper surface level of T-slot 1；T-shaped
Backward, there is an a quarter circular groove on the top of groove 1, and, perpendicular to T-slot 1, radius is across T-slot for a quarter circular groove
1, home position has a motor 3, motor 3 parallel to T-slot 1, perpendicular to a quarter circular groove；Gate 4 is placed in groove,
One end connects the rotating shaft of motor 3, can rotate, and is divided into closing and opens two states, is closed mode when gate 4 is laid；Work as lock
Door 4 is open mode vertically；First radar 7 is placed in the afterbody of fixed wing aircraft 5, for launching detection signal, calibrates the He of T-slot 1
Position between T-shaped axle 2.
Machine tool includes multi-rotor aerocraft 6, controller 9, the radar 8 of T-shaped axle 2 and second；T-shaped axle 2 is with 3 ° ~ 10 ° inclinations angle
It is fixed on multi-rotor aerocraft 6, is rigid structure, for being embedded into T-slot 1, is connected wing aircraft 5；Second radar 8
It is placed in T-shaped axle 2 to be connected on inclined-plane with multi-rotor aerocraft 6, is connected with controller 9, the position for detecting the first radar 7；Control
Device processed 9 is placed in inside multi-rotor aerocraft 6, and the positional information for being detected according to the second radar 8 adjusts multi-rotor aerocraft 6
Position, make T-shaped axle 2 be aligned T-slot 1.
When fixed wing aircraft 5 needs landing, fixed wing aircraft 5 sends request signal, and the multi-rotor aerocraft 6 on ground connects
Landing request signal lift-off is received, from rear near fixed wing aircraft 5；The transmission signal of first radar 7, the detection of the second radar 8 the
The signal of one radar 7, is accurately positioned to the first radar 7, and data are sent into controller 9, and controller 9 is according to data meter
Calculate fixed wing aircraft 5 distance and position, and control multi-rotor aerocraft 6 make T-shaped axle 2 be aligned T-slot 1, it is fully aligned after,
Multi-rotor aerocraft 6 accelerates, and T-shaped axle 2 is inserted T-slot 1, reaches up to groove portion top, and then motor 3 is rotated, and gate 4 is closed
Close, fixed wing aircraft 5 stops working；The reduction of speed of multi-rotor aerocraft 6, ground is returned to by multi-rotor aerocraft 6 with fixed wing aircraft 5.
Claims (3)
- It is 1. a kind of to combine aircraft, it is characterised in that：Including handset and machine tool, handset includes fixed wing aircraft（5）, T-slot （1）, motor（3）, gate（4）With the first radar（7）；Machine tool includes multi-rotor aerocraft（6）, T-shaped axle（2）, the second radar（8） And controller（9）；The T-slot of handset（1）It is placed in fixed wing aircraft（5）Underface, slots to fixed wing aircraft from afterbody （5）Position of centre of gravity, T-shaped, T-slot（1）Upper surface level；In T-slot（1）Backward, there is the semicircle of an a quarter on top, Disc is perpendicular to T-slot（1）, radius is across T-slot（1）, home position has a motor（3）, motor（3）Parallel to T-slot （1）, perpendicular to disc；Gate 4 is placed in a quarter disc, one end connection motor（3）Rotating shaft；First radar（7）It is placed in solid Determine wing aircraft（5）Afterbody；The T-shaped axle of machine tool（2）Multi-rotor aerocraft is fixed on certain inclination angle（6）On；Second radar（8） It is placed in T-shaped axle（2）With multi-rotor aerocraft（6）On joint face, controller is connected（9）；Controller（9）It is placed in multi-rotor aerocraft （6）It is internal.
- 2. one kind according to claim 1 combines aircraft, it is characterised in that：T-shaped axle（2）Fixed with 3 ° ~ 10 ° inclinations angle In multi-rotor aerocraft（6）On.
- 3. one kind according to claim 1 and 2 combines aircraft, and its landing modes is characterised by：Work as fixed wing aircraft （5）When needing landing, fixed wing aircraft（5）Send request signal, the multi-rotor aerocraft on ground（6）Receive landing request letter Number lift-off, from rear near fixed wing aircraft（5）；First radar（7）Transmission signal, the second radar（8）Detect the first radar（7） Signal, to the first radar（7）Accurately positioned, and data are sent to controller（9）, controller（9）According to data meter Calculate fixed wing aircraft（5）Distance and position, and control multi-rotor aerocraft（6）Make T-shaped axle（2）Alignment T-slot（1）, it is complete After full alignment, multi-rotor aerocraft（6）Accelerate, make T-shaped axle（2）Insertion T-slot（1）, until up to groove portion top, then motor （3）Rotate, gate（4）Close, fixed wing aircraft（5）It is flame-out；Multi-rotor aerocraft（6）Reduction of speed, by multi-rotor aerocraft（6）Band Fixed wing aircraft（5）Return to ground.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710139327.0A CN106882369A (en) | 2017-03-10 | 2017-03-10 | One kind combination aircraft and its landing modes |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710139327.0A CN106882369A (en) | 2017-03-10 | 2017-03-10 | One kind combination aircraft and its landing modes |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106882369A true CN106882369A (en) | 2017-06-23 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710139327.0A Withdrawn CN106882369A (en) | 2017-03-10 | 2017-03-10 | One kind combination aircraft and its landing modes |
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| CN (1) | CN106882369A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104875885A (en) * | 2015-06-17 | 2015-09-02 | 沈阳飞机工业（集团）有限公司 | Composite aircraft |
| 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 |
| US20170036762A1 (en) * | 2015-08-03 | 2017-02-09 | Dustin Gamble | Release and Capture of a Fixed-Wing Aircraft |
| 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 |
| CN206537502U (en) * | 2017-03-10 | 2017-10-03 | 佛山市神风航空科技有限公司 | One kind combination aircraft |
-
2017
- 2017-03-10 CN CN201710139327.0A patent/CN106882369A/en not_active Withdrawn
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104875885A (en) * | 2015-06-17 | 2015-09-02 | 沈阳飞机工业（集团）有限公司 | Composite aircraft |
| US20170036762A1 (en) * | 2015-08-03 | 2017-02-09 | Dustin Gamble | Release and Capture of a Fixed-Wing Aircraft |
| 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 |
| 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 |
| CN206537502U (en) * | 2017-03-10 | 2017-10-03 | 佛山市神风航空科技有限公司 | One kind combination aircraft |
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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: 20170623 |