CN106915444A - A kind of combined type aircraft lifting gear and mode - Google Patents
A kind of combined type aircraft lifting gear and mode Download PDFInfo
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- CN106915444A CN106915444A CN201710139335.5A CN201710139335A CN106915444A CN 106915444 A CN106915444 A CN 106915444A CN 201710139335 A CN201710139335 A CN 201710139335A CN 106915444 A CN106915444 A CN 106915444A
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- 239000007787 solid Substances 0.000 claims description 2
- 238000003032 molecular docking Methods 0.000 claims 3
- 230000009286 beneficial effect Effects 0.000 abstract description 3
- 230000009187 flying Effects 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
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- 230000005622 photoelectricity Effects 0.000 description 1
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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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
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- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Transportation (AREA)
- Guiding Agricultural Machines (AREA)
Abstract
A kind of combined type aircraft lifting gear and mode, belong to technical field of aerospace.A kind of combined type aircraft lifting gear and mode, including fixed wing aircraft, many gyroplanes and Master Control Center.Fixed wing aircraft is mounted on communication module and GPS positioning system with multi-rotor aerocraft；Master Control Center uses wireless connection with fixed wing aircraft and multi-rotor aerocraft respectively, and fixed wing aircraft uses wireless connection with multi-rotor aerocraft；Fixed wing aircraft movable flap, rear activity flap, expansion link and laser range sensor before having；Plane is arcs of recesses curved surface on the body of multi-rotor aerocraft, arcs of recesses curved surface is provided with annular groove, forward recess and rearward recess, the manipulator hand of annular groove opens or closes up the annulus caught on expansion link, fixed wing aircraft is separated with multi-rotor aerocraft or is tightly locked.Combined type aircraft lifting gear of the present invention and mode, easy to operate, landing efficiency high, have saved place resource and expenditure cost, are more beneficial for the popularization of fixed wing aircraft.
Description
Technical field
A kind of combined type aircraft lifting gear and mode, belong to technical field of aerospace, more particularly to aircraft lifting gear
And mode.
Background technology
Traditional fixed wing aircraft takeoff and landing is required for ground runway more long, and required landing site's area
Greatly, build runway expenditure cost high, cause the waste of place resource, but the power consumption of fixed wing aircraft is smaller, and endurance is strong,
Security is good；And the power consumption of multi-rotor aerocraft is larger, cruising time is shorter, and security is poor, but multi-rotor aerocraft energy
Enough VTOL, required landing site's area is small.At present, some combine fixed wing aircraft with multi-rotor aerocraft
Invent some can VTOL fixed wing aircraft, although solve the problems, such as fixed wing aircraft landing, but these energy
The efficiency of the fixed wing aircraft of VTOL, stability and security are low.
The content of the invention
The purpose of the present invention is the above-mentioned deficiency for overcoming fixed wing aircraft and multi-rotor aerocraft, and is flown using fixed-wing
The respective advantage of machine and multi-rotor aerocraft, invents a kind of lifting gear docked by fixed wing aircraft and multi-rotor aerocraft
And mode.
A kind of combined type aircraft lifting gear, including fixed wing aircraft, multi-rotor aerocraft and Master Control Center.Fixed-wing
Aircraft is mounted on communication module and GPS positioning system with multi-rotor aerocraft；Master Control Center respectively with fixed wing aircraft and many
Rotor craft uses wireless connection, and fixed wing aircraft uses wireless connection with multi-rotor aerocraft.The fixed wing aircraft bag
Include fuselage, main wing, empennage, undercarriage and engine；Landing is used when undercarriage is in an emergency for fixed wing aircraft.Institute
State activity flap before fuselage bottom is provided with, rear activity flap, expansion link and laser range sensor；It is described before activity flap and
The structure of movable flap is identical afterwards, and expansion link is placed in fuselage bottom center, and laser range sensor is placed in expansion link rear side
Side, the end of the expansion link is provided with annulus, and annulus is connected through a screw thread with expansion link；The laser range sensor is used for
It is accurately positioned.The multi-rotor aerocraft includes body, horn, support meanss, propeller and motor；The upper of the body is put down
Face is arcs of recesses curved surface, and the plane has certain gradient, and inclined angle is 3 °~10 °, and body front end is higher than machine
Body tail end, arcs of recesses curved surface is mutually fitted with fixed wing aircraft fuselage bottom, and controller is provided with body；The arcs of recesses is bent
Face is provided with forward recess and rearward recess, and the forward recess is identical with the structure of rearward recess, and the center of arcs of recesses curved surface is additionally provided with
Annular groove, the inwall of the annular groove is provided with photoelectric sensor, and the inner plane of annular groove is provided with manipulator, photoelectricity
Higher than the position on manipulator top, photoelectric sensor is for detecting the presence of object, the back side edge of manipulator for sensor present position
Laser range sensor is also installed, laser range sensor is connected with manipulator, the controller respectively with manipulator and
Photoelectric sensor is connected；Higher than the position of propeller, the thickness of preceding movable flap is less than preceding recessed for the position of the arcs of recesses curved surface
The width of groove, afterwards the thickness of movable flap less than rearward recess width, it is described before activity flap and rear movable flap be respectively with
What forward recess and rearward recess connect relatively, when current active flap and rear activity flap are docked with forward recess and rearward recess respectively, ring
The location of connected in star is corresponding with the position of expansion link.
The expansion link can be withdrawn in the fuselage of fixed wing aircraft, and preceding movable flap and rear activity flap can also rotate withdrawal
In the fuselage of fixed wing aircraft.
The multi-rotor aerocraft also includes support meanss, and support meanss include spring damper and universal wheel, and spring subtracts
Shake device is used to weaken the recoil strength produced when multi-rotor aerocraft lands, and universal wheel facilitates multi-rotor aerocraft shifting on the ground
It is dynamic.
Combined type aircraft lifting gear of the present invention and mode also include energy recharge system, and the energy recharge system can
For multi-rotor aerocraft or fixed wing aircraft are powered or fuel feeding.
The mode of taking off of combined type aircraft of the present invention, is realized by lifting gear：When taking off, preceding movable flap and
Movable flap is docked completely with forward recess and rearward recess respectively afterwards, arcs of recesses curved surface is mutually affixed with fixed wing aircraft fuselage bottom
Close, the location of annular groove is corresponding with the position of expansion link, and the manipulator of the inner plane of annular groove is caught on expansion link
Annulus, fixed wing aircraft is tightly locked on the arcs of recesses curved surface of multi-rotor aerocraft；Then multi-rotor aerocraft starts electronic
Fixed wing aircraft is vertically held up machine, multi-rotor aerocraft certain altitude in the air；Multi-rotor aerocraft support fixed wing aircraft
Accelerate flight forward, fixed wing aircraft starts engine, because multi-rotor aerocraft forward flight can turn forward, so by machine
The arcs of recesses curved surface of body is set to clinoplain, and inclined angle is set to 3 °~10 °, fixed wing aircraft is also had a fixed angle of altitude, more
Be conducive to taking off for fixed wing aircraft；After fixed wing aircraft reaches the speed taken off, and the signal that will take off is transmitted to many rotors and flies
Row device, multi-rotor aerocraft unclamps annulus by controller control machinery hand, so that fixed wing aircraft is departing from many rotor flyings
Device, after fixed wing aircraft departs from many gyroplanes, preceding movable flap, rear activity flap and expansion link are automatically retracted in fuselage, many
Rotor craft is returned.
The landing modes of combined type aircraft of the present invention, are realized by lifting gear：When fixed wing aircraft needs drop
When falling, falling signal is reached Master Control Center by fixed wing aircraft by communication module, and then Master Control Center instructs many rotor flyings
Device docks fixed wing aircraft in the air；When multi-rotor aerocraft detects fixed wing aircraft orientation by GPS positioning system, revolve more
Rotor aircraft carries out locating and tracking and measuring speed to fixed wing aircraft, and multi-rotor aerocraft is at leisure near fixed wing aircraft
Underface, multi-rotor aerocraft is with fixed wing aircraft with same speed horizontal flight in the same direction；Then by fixed wing aircraft and
The laser range sensor of multi-rotor aerocraft carries out precise positioning, and expansion link slowly stretches to the machinery of annular groove inner plane
Hand, when the horizontal plane residing for annulus reaches photoelectric sensor, photoelectric sensor detects object, and signal is reached into control
Device, then the annulus caught on expansion link is closed up by controller control machinery hand, so as to by fixed wing aircraft and multi-rotor aerocraft
Tight then expansion link is shunk under lock and key, and activity flap is docked completely with forward recess before making, and movable flap is completely right with rearward recess afterwards
Connect, arcs of recesses curved surface is mutually fitted with fixed wing aircraft fuselage bottom, then fixed wing aircraft stops working, multi-rotor aerocraft support
Carry fixed wing aircraft landing ground.
Combined type aircraft lifting gear of the present invention and mode, easy to operate, landing efficiency high, using fixed wing aircraft with
Multi-rotor aerocraft connection combination, allows multi-rotor aerocraft to manufacture aerial runway for fixed wing aircraft, saved place resource and
Expenditure cost, is more beneficial for the popularization of fixed wing aircraft.
Brief description of the drawings
Fig. 1 is the structural representation of a kind of combined type aircraft lifting gear of the invention and mode；Fig. 2 is of the invention a kind of
The signal connection diagram of combined type aircraft lifting gear and mode；Fig. 3 is a kind of combined type aircraft landing dress of the invention
Put and mode broken section schematic side view；Fig. 4 is the schematic cross-sectional view of expansion link and manipulator；Fig. 5 is of the invention a kind of
The schematic elevation view of combined type aircraft lifting gear and mode；Fig. 6 is the plan of fixed wing aircraft fuselage bottom；Fig. 7 is
The schematic cross-sectional view of support meanss.
In figure, 1- fixed wing aircrafts, 11- fuselages, 12- main wings, 13- empennages, 14- undercarriages, 15- engines are living before 16-
Dynamic flap, movable flap, 18- expansion links, 181- annulus, 19- laser range sensors after 17-；2- multi-rotor aerocrafts, 21-
Body, 211- controllers, 22- horns, 23- support meanss, 231- spring dampers, 232- universal wheels, 24- propellers, 25- electricity
Motivation, 26- arcs of recesses curved surfaces, 261- forward recess, 262- rearward recess, 263- annular grooves, 27- photoelectric sensors, 28- machineries
Hand；3- Master Control Centers；4- communication modules；5-GPS alignment systems.
Specific embodiment
The present invention is illustrated in conjunction with figure：A kind of combined type aircraft lifting gear, including fixed wing aircraft
1st, many gyroplanes 2 and Master Control Center 3；Fixed wing aircraft 1 is mounted on communication module 4 and GPS location with multi-rotor aerocraft 2
System 5；Master Control Center 3 uses wireless connection, fixed wing aircraft 1 and many rotations with fixed wing aircraft 1 and multi-rotor aerocraft 2 respectively
Rotor aircraft 2 uses wireless connection.The fixed wing aircraft 1 includes fuselage 11, main wing 12, empennage 13, undercarriage 14 and starts
Machine 15, landing is used when undercarriage 14 is in an emergency for fixed wing aircraft 1；The bottom of fuselage 11 movable flap before being provided with
16th, rear activity flap 17, expansion link 18 and laser range sensor 19；The knot of activity flap 16 and rear activity flap 17 before described
Structure is identical, and expansion link 18 is placed in the bottom centre position of fuselage 11, and laser range sensor 19 is placed in the back side edge of expansion link 18, described
The end of expansion link 18 is provided with annulus 181, and annulus 181 is connected through a screw thread with expansion link 18；The laser range sensor
19 are used to be accurately positioned, and the expansion link 18 can be withdrawn in the fuselage 11 of fixed wing aircraft 1, and preceding movable flap 16 and rear activity turn
Plate 17 can be also rotated in the fuselage 11 for withdrawing fixed wing aircraft 1.Multi-rotor aerocraft 2 includes body 21, horn 22, support meanss
23rd, propeller 24 and motor 25；The upper plane of body 21 is arcs of recesses curved surface 26, and the plane has certain inclination
Degree, inclined angle is 3 °~10 °, and the front end of body 21 is higher than the tail end of body 21, arcs of recesses curved surface 26 and the fuselage of fixed wing aircraft 1
11 bottoms are mutually fitted, and controller 211 is provided with body 21；The arcs of recesses curved surface 2 is provided with forward recess 261 and rearward recess
262, the forward recess 261 is identical with the structure of rearward recess 262, and the center of arcs of recesses curved surface 2 is additionally provided with annular groove
263, the inwall of the annular groove 263 is provided with photoelectric sensor 27, and the inner plane of annular groove 263 is provided with manipulator
28, higher than the position on the top of manipulator 28, photoelectric sensor 27 is for detecting the presence of object, machine for the present position of photoelectric sensor 27
The back side edge of tool hand 28 is also provided with laser range sensor 19, and laser range sensor 19 is connected with manipulator 28, described
Controller 211 is connected with manipulator 28 and photoelectric sensor 27 respectively；The support meanss 23 include spring damper 231 and ten thousand
To wheel 232, spring damper 231 is used to weaken the recoil strength produced when multi-rotor aerocraft 2 lands, and universal wheel 232 is convenient more
The movement on the ground of rotor craft 2.The position of arcs of recesses curved surface 26 is higher than the position of propeller 24, preceding movable flap 16
Thickness is less than the width of forward recess 261, afterwards the width of the thickness less than rearward recess 262 of movable flap 17, the preceding activity flap
16 and rear activity flap 17 respectively with forward recess 261 and rearward recess 262 is relative connects, current active flap 16 and rear activity turn
When plate 17 is docked with forward recess 261 and rearward recess 262 respectively, the position pair of the location of annular groove 263 and expansion link 18
Should.Combined type aircraft lifting gear also includes energy recharge system, can be that multi-rotor aerocraft 2 and fixed wing aircraft 1 are powered
Or fuel feeding.
The mode of taking off of combined type aircraft of the present invention, is realized by lifting gear：When taking off, preceding movable flap 16
Docked completely with forward recess 261 and rearward recess 262 respectively with rear movable flap 17, make arcs of recesses curved surface 26 and fixed wing aircraft 1
The bottom of fuselage 11 mutually fits, and the location of annular groove 263 is corresponding with the position of expansion link 18, is put down in annular groove 263
The manipulator 28 in face catches the annulus 181 on expansion link 18, fixed wing aircraft 1 is tightly locked in the arcs of recesses of multi-rotor aerocraft 2
On curved surface 26；Then multi-rotor aerocraft 2 starts motor 25, and multi-rotor aerocraft 2 vertically holds up in sky fixed wing aircraft 1
Middle certain altitude；The support of multi-rotor aerocraft 2 fixed wing aircraft 1 and accelerates flight forward, fixed wing aircraft 1 to start engine 15,
Because the forward flight of multi-rotor aerocraft 2 can turn forward, so the arcs of recesses curved surface 26 of body 21 is set into clinoplain, incline
Oblique angle is set to 3 °~10 °, fixed wing aircraft 1 is also had certain angle of attack, is more beneficial for taking off for fixed wing aircraft 1；When solid
Determine after wing aircraft 1 reaches the speed taken off, and the signal that will take off is transmitted to multi-rotor aerocraft 2, multi-rotor aerocraft 2 is by control
211 control machinery hand of device 28 unclamps annulus 181, so that fixed wing aircraft 1 is departing from multi-rotor aerocraft 2, fixed wing aircraft 1 takes off
After many gyroplanes 2, preceding movable flap 16, rear activity flap 17 and expansion link 18 are automatically retracted in fuselage 11, and many rotors fly
Row device 2 makes a return voyage automatically.
The landing modes of combined type aircraft of the present invention, are realized by lifting gear：When fixed wing aircraft 1 needs drop
When falling, falling signal is reached Master Control Center 3 by fixed wing aircraft 1 by communication module 4, and then Master Control Center 3 instructs many rotors
Aircraft 2 docks fixed wing aircraft 1 in the air；When multi-rotor aerocraft 2 detects the side of fixed wing aircraft 1 by GPS positioning system 5
During position, multi-rotor aerocraft 2 carries out locating and tracking and measuring speed to fixed wing aircraft 1, and multi-rotor aerocraft 2 is close at leisure
The underface of fixed wing aircraft 1, multi-rotor aerocraft 2 is with fixed wing aircraft 1 with same speed horizontal flight in the same direction；Then lead to
The laser range sensor 19 for crossing fixed wing aircraft 1 and multi-rotor aerocraft 2 carries out precise positioning, and expansion link 18 slowly stretches to ring
The manipulator 28 of the inner plane of connected in star 263, when the horizontal plane residing for annulus 181 reaches photoelectric sensor 27, photoelectric sensor
27 detect object, and signal is reached into controller 211, then are closed up by the control machinery hand 28 of controller 211 and catch expansion link 18
On annulus 181, so as to fixed wing aircraft 1 and multi-rotor aerocraft 2 is tight under lock and key, then expansion link 18 shrinks, and makes preceding work
Dynamic flap 16 is docked completely with forward recess 261, and movable flap 17 is docked completely with rearward recess 262 afterwards, make arcs of recesses curved surface 26 and
The bottom of 1 fuselage of fixed wing aircraft 11 mutually fits, and then fixed wing aircraft 1 stops working, and the support of multi-rotor aerocraft 2 carries fixed wing aircraft
Landing ground.
When fixed wing aircraft 1 need refuel or power when, fixed wing aircraft 1 after being docked with multi-rotor aerocraft 2,
Multi-rotor aerocraft 2 is refueled and is powered to fixed wing aircraft 1.
Claims (9)
1. a kind of combined type aircraft lifting gear, it is characterised in that：Including fixed wing aircraft（1）, many gyroplanes（2）And master
Control center（3）；Fixed wing aircraft（1）With multi-rotor aerocraft（2）It is mounted on communication module（4）And GPS positioning system（5）；
Master Control Center（3）Respectively with fixed wing aircraft（1）And multi-rotor aerocraft（2）Between use wireless connection, fixed wing aircraft（1）
With multi-rotor aerocraft（2）Using wireless connection；The fixed wing aircraft（1）Including fuselage（11）, main wing（12）, empennage
（13）, undercarriage（14）And engine（15）, main wing（12）Installed in fuselage（11）The left and right sides, empennage（13）Installed in fuselage
（11）Afterbody, undercarriage（14）Installed in fuselage（11）Bottom；The fuselage（11）Bottom is provided with laser range sensor
（19）, expansion link（18）, annulus（181）, preceding movable flap（16）With rear movable flap（17）, laser range sensor（19）With
In being accurately positioned；The multi-rotor aerocraft（2）Including body（21）, horn（22）, support meanss（23）, propeller（24）With
Motor（25）, body（21）Upper plane be arcs of recesses curved surface（26）, body（21）Controller is inside installed（211）；Concave arc
Shape curved surface（26）It is fixed wing aircraft（1）With multi-rotor aerocraft（2）The location of the platform of docking, annular groove 263 with
The position correspondence of expansion link 18；Body（21）Controller is inside installed（211）, arcs of recesses curved surface（26）It is provided with forward recess（261）、
Rearward recess（262）, annular groove（263）, photoelectric sensor（27）, manipulator（28）And laser range sensor（19）.
2. a kind of combined type aircraft lifting gear according to claim 1, it is characterised in that：Activity flap before described
（17）With rear movable flap（18）Structure it is identical.
3. a kind of combined type aircraft lifting gear according to claim 1 and 2, it is characterised in that：Preceding movable flap
（17）Thickness be less than forward recess（261）Width, movable flap afterwards（18）Thickness be less than rearward recess（262）Width, it is preceding
Movable flap（17）With rear movable flap（18）Respectively with forward recess（261）And rearward recess（262）It is relative to connect, the preceding movable transverse
Bar（285）Diameter be less than front through hole（171）Diameter, movable cross bar afterwards（286）Diameter be less than rear through hole（181）It is straight
Footpath；Current active flap（17）With rear movable flap（18）Respectively with forward recess（261）And rearward recess（262）When docking completely,
Preceding movable cross bar（285）And front through hole（171）Location level is concentric, afterwards movable cross bar（286）With rear through hole（181）Institute
The position level at place is concentric.
4. a kind of combined type aircraft lifting gear according to claim 1 and 2, it is characterised in that：The arcs of recesses is bent
Face（26）Inclined surface angle for 3 °~10 °, body（21）Front end is higher than body（21）Tail end；The arcs of recesses curved surface
（26）Position be higher than propeller（24）Position.
5. a kind of combined type aircraft lifting gear according to claim 1 and 2, it is characterised in that：The support meanss
（23）Including spring damper（231）And universal wheel（232）.
6. a kind of combined type aircraft lifting gear according to claim 1 and 2, it is characterised in that：Expansion link（18）Energy
Withdraw fixed wing aircraft（1）Fuselage（11）It is interior, preceding movable flap（16）With rear movable flap（17）Also withdrawal can be rotated to fix
Wing aircraft（1）Fuselage（11）It is interior.
7. a kind of combined type aircraft lifting gear according to claim 1, it is characterised in that：Expansion link（18）End
Annulus is installed（181）, annulus（181）With expansion link（18）It is connected through a screw thread.
8. a kind of mode of taking off of combined type aircraft lifting gear, it is characterised in that：Preceding movable flap（16）Turn with rear activity
Plate（17）Respectively with forward recess（261）And rearward recess（262）Dock completely, make arcs of recesses curved surface（26）With fixed wing aircraft（1）
Fuselage（11）Bottom mutually fits, annular groove（263）Location and expansion link（18）Position correspondence, annular groove
（263）The manipulator of inner plane（28）Catch expansion link（18）On annulus（181）, make fixed wing aircraft（1）It is tight to be locked in many rotations
Rotor aircraft（2）Arcs of recesses curved surface（26）On；Then multi-rotor aerocraft（2）Start motor（25）, multi-rotor aerocraft
（2）By fixed wing aircraft（1）It is vertical to hold up certain altitude in the air；Multi-rotor aerocraft（2）Hold in the palm fixed wing aircraft（1）Accelerate
Flight forward, fixed wing aircraft（1）Start engine（15）；Work as fixed wing aircraft（1）After reaching the speed taken off, and by signal
It is transmitted to multi-rotor aerocraft（2）, multi-rotor aerocraft（2）By controller（211）Control machinery hand（28）Unclamp annulus
（181）, so that fixed wing aircraft（1）Departing from multi-rotor aerocraft（2）, fixed wing aircraft（1）Depart from many gyroplanes（2）
Afterwards, preceding movable flap（16）, rear activity flap（17）And expansion link（18）Automatically retract fuselage（11）It is interior, multi-rotor aerocraft
（2）Make a return voyage.
9. a kind of landing modes of combined type aircraft lifting gear, it is characterised in that：Work as fixed wing aircraft（1）Need landing
When, fixed wing aircraft（1）By communication module（4）Falling signal is reached into Master Control Center（3）, then Master Control Center（3）Instruction
Multi-rotor aerocraft（2）Aerial docking fixed wing aircraft（1）；Work as multi-rotor aerocraft（2 pass through GPS positioning system（5）Detect
Fixed wing aircraft（1）During orientation, multi-rotor aerocraft（2）To fixed wing aircraft（1）Locating and tracking and measuring speed are carried out, is revolved more
Rotor aircraft（2）At leisure near fixed wing aircraft（1）Underface, multi-rotor aerocraft（2）With fixed wing aircraft（1）With phase
Same speed horizontal flight in the same direction；Then fixed wing aircraft is passed through（1）And multi-rotor aerocraft（2）Laser range sensor
（19）Carry out precise positioning, expansion link（18）Slowly stretch to annular groove（263）The manipulator of inner plane（28）, work as annulus
（181）Reach photoelectric sensor（27）During residing horizontal plane, photoelectric sensor（27）Object is detected, and signal is reached into control
Device processed（211）, then by controller（211）Control machinery hand（28）Close up and catch expansion link（18）On annulus（181）, so that will
Fixed wing aircraft（1）With multi-rotor aerocraft（2）It is tight under lock and key, then expansion link（18）Shrink, activity flap before making（16）With
Forward recess（261）Dock completely, afterwards movable flap（17）With rearward recess（262）Dock completely, make arcs of recesses curved surface（26）With it is solid
Determine wing aircraft（1）Fuselage（11）Bottom mutually fits, then fixed wing aircraft（1）It is flame-out, multi-rotor aerocraft（2）Support is carried fixes
Wing aircraft landing ground.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710139335.5A CN106915444A (en) | 2017-03-10 | 2017-03-10 | A kind of combined type aircraft lifting gear and mode |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710139335.5A CN106915444A (en) | 2017-03-10 | 2017-03-10 | A kind of combined type aircraft lifting gear and mode |
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| CN106915444A true CN106915444A (en) | 2017-07-04 |
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Cited By (10)
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| WO2018107278A1 (en) * | 2016-12-13 | 2018-06-21 | Ryan Evaristo Pinto | System and method for capturing and releasing fixed-wing aircraft |
| CN108820221A (en) * | 2018-08-16 | 2018-11-16 | 上海重塑能源科技有限公司 | Take-off system |
| CN110104199A (en) * | 2019-04-28 | 2019-08-09 | 南京航空航天大学 | A kind of lifting gear for unmanned plane Air Launched Platform |
| CN110231641A (en) * | 2019-07-05 | 2019-09-13 | 上海埃依斯航天科技有限公司 | A kind of rocket one sub grade remains accurate positioning device and localization method |
| CN110937111A (en) * | 2019-11-29 | 2020-03-31 | 西北工业大学 | Small-size cluster unmanned aerial vehicle dispensing system of gliding style |
| CN112224417A (en) * | 2020-09-22 | 2021-01-15 | 南京航空航天大学 | Aircraft provided with modular embedded landing gear and application method thereof |
| CN112722284A (en) * | 2021-01-15 | 2021-04-30 | 南京航空航天大学 | Auxiliary vertical take-off and landing method and device for fixed-wing aircraft |
| CN113371196A (en) * | 2021-07-15 | 2021-09-10 | 吉林建筑大学 | High remote sensing survey and drawing unmanned aerial vehicle of security |
| US20210316861A1 (en) * | 2017-09-06 | 2021-10-14 | Hood Technology Corporation | Rotorcraft-assisted system for launching and retrieving a fixed-wing aircraft into and from free flight |
| 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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| CN108820221A (en) * | 2018-08-16 | 2018-11-16 | 上海重塑能源科技有限公司 | Take-off system |
| CN110104199A (en) * | 2019-04-28 | 2019-08-09 | 南京航空航天大学 | A kind of lifting gear for unmanned plane Air Launched Platform |
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| CN110937111A (en) * | 2019-11-29 | 2020-03-31 | 西北工业大学 | Small-size cluster unmanned aerial vehicle dispensing system of gliding style |
| CN112224417A (en) * | 2020-09-22 | 2021-01-15 | 南京航空航天大学 | Aircraft provided with modular embedded landing gear and application method thereof |
| CN112722284A (en) * | 2021-01-15 | 2021-04-30 | 南京航空航天大学 | Auxiliary vertical take-off and landing method and device for fixed-wing aircraft |
| CN112722284B (en) * | 2021-01-15 | 2021-12-14 | 南京航空航天大学 | Auxiliary vertical take-off and landing method and device for fixed-wing aircraft |
| CN113371196A (en) * | 2021-07-15 | 2021-09-10 | 吉林建筑大学 | High remote sensing survey and drawing unmanned aerial vehicle of security |
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