CN108639329A - A kind of spiral shell with the auxiliary wing of twin screw and the attached wing pushes away combined wing aircraft - Google Patents
A kind of spiral shell with the auxiliary wing of twin screw and the attached wing pushes away combined wing aircraft Download PDFInfo
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- CN108639329A CN108639329A CN201810551560.4A CN201810551560A CN108639329A CN 108639329 A CN108639329 A CN 108639329A CN 201810551560 A CN201810551560 A CN 201810551560A CN 108639329 A CN108639329 A CN 108639329A
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- wing
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- lift
- spiral shell
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- 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
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
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- Engineering & Computer Science (AREA)
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- Aviation & Aerospace Engineering (AREA)
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Abstract
The present invention is that a kind of spiral shell with the auxiliary wing of twin screw and the attached wing pushes away combined wing aircraft, wherein rear single-screw paddle composite wing aircraft includes body, is fixedly mounted on body both sides hybrid lift wing, screw propeller；Self-enclosed ducted fan built in hybrid lift wing, hybrid lift wing outside are designed with wing hinge；The front end of the compound auxiliary wing of airscrew thrust self energizing is provided with screw propeller, the compound auxiliary wing of airscrew thrust self energizing is internally provided with self-enclosed ducted fan, the both sides of the compound auxiliary wing of airscrew thrust self energizing are provided with electro-hydraulic gas interface and wing hinge, and are flexibly connected with hybrid lift wing by the wing hinge of side；Invention not only has landing apart from short, flying speed is fast, wing structure intensity is high, wing can with energy storage, low energy consumption for flight, the hang time is long, safe the features such as, the auxiliary wing uses hybrid lift, it is ensured that the accommodation of power.
Description
Technical field
The present invention relates to a kind of aircraft, specifically a kind of spiral shell with the auxiliary wing of twin screw and the attached wing pushes away combined wing aircraft,
Belong to aircraft equipment technology field.
Background technology
Existing aircraft is broadly divided into fixed-wing and vertically taking off and landing flyer（Such as helicopter and more rotors）Two major classes.When
So also there is this product of VTOL fixed-wing.Traditional fixed-wing have the advantages that flying speed is fast, low energy consumption, but have
It is not connected to before and after main wing and tailplane, wing structure intensity is not high, is easily damaged, and landing requires high, landing distance disadvantage；
Traditional vertically taking off and landing flyer has the advantages that landing is convenient, but has that energy consumption is big, safety coefficient is low, and load capacity is poor, water
Flat flying speed is slow, is easy the shortcomings of air crash；Although current VTOL fixed-wing has the characteristics that landing is convenient, but in water
The shortcomings of controllability when flat flight is not satisfactory, and that there is flight resistances is big, and energy consumption is high, and safety coefficient is not still high.
Invention content
In view of the above-mentioned problems of the prior art, the present invention not only has landing apart from short, flying speed is fast, wing knot
Structure intensity height, wing can be with energy storage, the features such as low energy consumption, the hang time is long of flying, the hybrid lift wing of large area, hydrous waters
The flat rudder wing can play the role of aerodone under case of emergency, greatly improve the safety of aircraft, the safety of support personnel.
To achieve the goals above, the present invention includes rear single-screw paddle composite wing aircraft, is movably arranged on compound liter
The compound auxiliary wing of airscrew thrust self energizing of power aircraft both sides and shipping storehouse；Wherein, rear single-screw paddle composite wing flight
Device includes body, is fixedly mounted on body both sides hybrid lift wing, screw propeller；Wherein, it is flat to be set as deck for body
Platform；Self-enclosed ducted fan built in hybrid lift wing, hybrid lift wing outside are designed with wing hinge；Airscrew thrust is certainly
The front end for energizing the compound auxiliary wing is provided with screw propeller, and being internally provided with for the compound auxiliary wing of airscrew thrust self energizing is self-styled
Ducted fan is closed, the both sides of the compound auxiliary wing of airscrew thrust self energizing are provided with electro-hydraulic gas interface and wing hinge, and pass through one
The wing hinge of side is flexibly connected with hybrid lift wing；The side of additional fin towards body is provided with wing hinge and electro-hydraulic gas
Interface, and be mounted on the outside of the compound auxiliary wing of airscrew thrust self energizing by the way that wing hinge is folding；Electro-hydraulic gas interface carries
Lid, additional fin internal battery/fuel.
Further, propeller is a variety of dynamic structures such as electric propeller, the dynamic propeller of oil.
Further, hybrid lift wing front and back are respectively set to magnetic-type self interlocking interface male connector and magnetic-type automatic
Mutual lock interface female；Magnetic-type self interlocking interface male connector is identical as magnetic-type self interlocking interface female size.
Further, magnetic-type self interlocking interface male connector and magnetic-type self interlocking interface female are taper connection
Further, hybrid lift wing can be divided into two parts of lift main wing and balance empennage, be separately positioned on hybrid lift
The front and back of wing；It is reserved with space between lift main wing and balance empennage, the horizontal lifting rudder wing is provided in space；Wherein,
At least there are one self-enclosed ducted fans for installation inside lift main wing.
Further, further include vertical tail, the vertical tail is arranged above or below body；The vertical tail is set
It sets in wing both sides；The vertical tail may be implemented to fold；Mobilizable vertical rudder wing is installed behind the vertical tail.
Further, body is installed with cavity, and installation diagram passes, flies the modules such as control, driving in cavity..
Further, the compound auxiliary wing of airscrew thrust self energizing can be divided into the auxiliary wing of lift and auxiliary two parts of empennage of balance,
It is separately positioned on the front and back of the compound auxiliary wing of airscrew thrust self energizing；It is reserved between the auxiliary wing of lift and the auxiliary empennage of balance free
Between, the horizontal lifting rudder wing is provided in space；Wherein, at least there are one self-enclosed ducted fans for installation inside the auxiliary wing of lift.
Further, engine installation position is additionally provided on the compound auxiliary wing of airscrew thrust self energizing, in engine installation position
It is provided with power plant.
Further, the compound auxiliary wing engine installation position installation of airscrew thrust self energizing is that electric propeller or oil are dynamic
Propeller.
Further, it is provided with battery/fuel on the compound auxiliary wing of airscrew thrust self energizing.
The prior art is compared, the main feature having is invented：
1. the present invention has landing apart from short, flying speed is fast, maneuverability, avoidance ability are strong, wing structure intensity is high, machine
The wing can be with energy storage, the features such as low energy consumption of flying.Self-enclosed vertical ducted fan is relied on, aircraft can be provided in horizontal flight
Additional maneuverability, realize moment change of flight posture and track super maneuver ability.
2. the compound auxiliary wing of airscrew thrust self energizing of the present invention uses hybrid lift, i.e., by designing in aerofoil
Self-enclosed ducted fan generates the lift that lift and the auxiliary wing of lift are generated in horizontal flight, to form hybrid lift.
3. also adding additional fin on the outside of the compound auxiliary wing of airscrew thrust self energizing in the present invention, flight is improved
Lift when device horizontal flight also increases the energy of energy device.
4. the Waverider wing that the present invention is very large, can play the role of certain paraglider, gravity acceleration is substantially reduced
Degree greatly improves safety coefficient, coordinates the control function of the hydroplane wing and the vertical rudder wing and the aerofoil envelope of self-enclosed ducted fan
Function is closed, even if lift ducted fan and horizontal propeller can realize that aerodone formula is force-landed if damage simultaneously, is greatly improved
The safety of aircraft has ensured the safety of personnel and goods and materials.
5. the present invention can realize multiple functions using hardware and software platform, modularized design,
6. the present invention using both sides wing can Expanding design, wing area can be expanded when necessary, improve the standard flight when
Lift, improve load capacity.
7. the present invention also has successive magnetic-type self interlocking interface, the cluster of aircraft is facilitated to fly, into one
Step reduces power consumption when cluster flight.In front and back serial connection, the aircraft at rear only needs a small amount of energy expenditure, energy
Realize the flight of long range, the not cluster flight of only aircraft provides the low-power consumption scheme of clustering, it might even be possible to realize
Air rescue between aircraft, i.e., preceding aircraft take off faulty aircraft dragging below, realize not seen before fly
Phenomenon is rescued mutually between row device.
8. wing hinge can be passed through between the compound auxiliary wing of the airscrew thrust self energizing of invention and hybrid lift aircraft
It is attached, is controlled by hybrid lift aircraft main control unit, and can be by energy such as battery/fuel of aerofoil with electro-hydraulic gas interface
Aircraft host is passed to, the flight time is improved.The multiplication of performance may be implemented by the auxiliary wing of superimposion lift.It is modular
Design, reduces the disposable input of client, reduces buying and operation cost.
9. the compound auxiliary wing of airscrew thrust self energizing of the present invention is in parallel with the auxiliary wing of other hybrid lifts, and passes through machine
Wing hinge and electro-hydraulic gas interface are attached, synchronous to be controlled by hybrid lift aircraft main control unit, are expanded again and can be by the wing
The energy transmissions such as the battery/fuel in face give aircraft host, improve the flight time.
10. thrust device modularization can very easily realize that repair is replaced.
11. in the present invention, auxiliary wing one or both sides are provided with electro-hydraulic gas interface, realize the auxiliary wing and fly with hybrid lift
Energy intercommunication between device main plane, and action is controlled by hybrid lift aircraft, improves the flexibility of complete machine.
12. the auxiliary wing is also built-in with the horizontal lifting rudder wing, improves complete machine and manipulate agility！
13. aerofoil type energy device, efficiently uses space.
Description of the drawings
Fig. 1 is the structural schematic diagram of the present invention；
Fig. 2 is the side view of the present invention；
Fig. 3 is the rearview of the present invention；
Fig. 4 is the plan view of the present invention；
Fig. 5 is the oblique view of the present invention；
In figure：101：Body；102：Hybrid lift wing；104：Self-enclosed ducted fan；105：Vertical tail；1051. vertical
The rudder wing；106：Propeller；107：Energy Management System；1021：Lift main wing；1022：The horizontal lifting rudder wing；1023：Balance tail
The wing；1028：Wing hinge；1001：Socket；1002：Cavity；1003：Mounting hole；1006：Battery/fuel；108：Video camera；
1026：Magnetic-type self interlocking interface male connector；1027：Magnetic-type self interlocking interface female；1031, airscrew thrust self energizing
The compound auxiliary wing；10311, lift additional fin；10312, auxiliary empennage is balanced；1026, electro-hydraulic gas interface；10261, lid；111, it sends out
Motivation installation position；114, additional fin；1062, screw propeller.
Specific implementation mode
The present invention will be further described below in conjunction with the accompanying drawings.
As shown in Figures 1 to 5, a kind of spiral shell with the auxiliary wing of twin screw and the attached wing pushes away combined wing aircraft, including rear single-screw
The compound auxiliary wing of the compound rotor aircraft of paddle, the airscrew thrust self energizing for being assemblied in its wing both sides and additional fin 114；Its
In, the rear single-screw paddle composite wing aircraft includes body 101, is fixedly mounted on 101 both sides hybrid lift machine of body
The wing 102, propeller 106；Wherein, the body 101 is set as deck platform；The hybrid lift wing 102 is built-in certainly
Ducted fan 104 is closed, 102 outside of hybrid lift wing is designed with wing hinge 1028；The airscrew thrust self energizing
The front end of the compound auxiliary wing is provided with screw propeller 1062, and being internally provided with for the compound auxiliary wing of airscrew thrust self energizing is self-styled
Ducted fan 104 is closed, the both sides of the compound auxiliary wing of airscrew thrust self energizing are provided with electro-hydraulic gas interface 1036 and wing hinge
1028, and be flexibly connected with hybrid lift wing 102 by the wing hinge of side 1028；The additional fin 114 is towards machine
The side of body 101 is provided with wing hinge 1028 and electro-hydraulic gas interface 1036, and passes through 1028 folding installation of wing hinge
On the outside of the compound auxiliary wing of airscrew thrust self energizing；The electro-hydraulic gas interface 1036 carries lid 10361, in additional fin 114
Set battery/fuel 1006.
As further improvement of the invention, propeller 106 is a variety of power knots such as electric propeller, the dynamic propeller of oil
Structure.
As further improvement of the invention, 102 front and back of hybrid lift wing are respectively set to magnetic-type self interlocking
Interface male connector 1026 and magnetic-type self interlocking interface female 1027；The magnetic-type self interlocking interface male connector 1026 and magnetic
Suction self interlocking interface 1027 sizes of female are identical.
As further improvement of the invention, magnetic-type self interlocking interface male connector 1026 and magnetic-type self interlocking interface
Female 1027 is taper connection,
As further improvement of the invention, hybrid lift wing 102 can be divided into lift main wing 1021 and balance empennage 1023
Two parts, are separately positioned on the front and back of hybrid lift wing 102；It is reserved between lift main wing 1021 and balance empennage 1023
There is space, the horizontal lifting rudder wing 1022 is provided in space；Wherein, at least there are one self-enclosed for installation inside lift main wing 1021
Ducted fan 104.
Further include vertical tail 105 as further improvement of the invention, the vertical tail 105 is arranged in body 101
Above or below；The vertical tail 105 is arranged in wing both sides；The vertical tail 105 may be implemented to fold；It is described vertical
Mobilizable vertical rudder wing 1051 is installed behind empennage 105.
Improved as of the invention further, body 101 is installed with cavity 1002, in cavity 1002 installation diagram pass, fly control,
The modules such as driving.
Improved as of the invention further, the compound auxiliary wing of airscrew thrust self energizing can be divided into the auxiliary wing of lift 10311 with
And auxiliary 10,312 two parts of empennage of balance, it is separately positioned on the front and back of the compound auxiliary wing of airscrew thrust self energizing；The auxiliary wing of lift
It is reserved with space between 10311 and the auxiliary empennage of balance 10312, the horizontal lifting rudder wing 1022 is provided in space；Wherein, lift is auxiliary
At least there are one self-enclosed ducted fans 104 for installation inside the wing 10311.
As further improvement of the invention, engine installation position is additionally provided on the compound auxiliary wing of airscrew thrust self energizing
111, power plant is provided in engine installation position 111.
As further improvement of the invention, battery/fuel 1006 is provided on the compound auxiliary wing of airscrew thrust self energizing.
The prior art is compared, the main feature having is invented：
1. the present invention has landing apart from short, flying speed is fast, maneuverability, avoidance ability are strong, wing structure intensity is high, machine
The wing can be with energy storage, the features such as low energy consumption of flying.Self-enclosed vertical ducted fan is relied on, aircraft can be provided in horizontal flight
Additional maneuverability, realize moment change of flight posture and track super maneuver ability.
2. the compound auxiliary wing of airscrew thrust self energizing of the present invention uses hybrid lift, i.e., by designing in aerofoil
Self-enclosed ducted fan generates the lift that lift and the auxiliary wing of lift are generated in horizontal flight, to form hybrid lift.
3. also adding additional fin on the outside of the compound auxiliary wing of airscrew thrust self energizing in the present invention, flight is improved
Lift when device horizontal flight also increases the energy of energy device.
4. the Waverider wing that the present invention is very large, can play the role of certain paraglider, gravity acceleration is substantially reduced
Degree greatly improves safety coefficient, coordinates the control function of the hydroplane wing and the vertical rudder wing and the aerofoil envelope of self-enclosed ducted fan
Function is closed, even if lift ducted fan and horizontal propeller can realize that aerodone formula is force-landed if damage simultaneously, is greatly improved
The safety of aircraft has ensured the safety of personnel and goods and materials.
5. the present invention can realize multiple functions using hardware and software platform, modularized design,
6. the present invention using both sides wing can Expanding design, wing area can be expanded when necessary, improve the standard flight when
Lift, improve load capacity.
7. the present invention also has successive magnetic-type self interlocking interface, the cluster of aircraft is facilitated to fly, into one
Step reduces power consumption when cluster flight.In front and back serial connection, the aircraft at rear only needs a small amount of energy expenditure, energy
Realize the flight of long range, the not cluster flight of only aircraft provides the low-power consumption scheme of clustering, it might even be possible to realize
Air rescue between aircraft, i.e., preceding aircraft take off faulty aircraft dragging below, realize not seen before fly
Phenomenon is rescued mutually between row device.
8. wing hinge can be passed through between the compound auxiliary wing of the airscrew thrust self energizing of invention and hybrid lift aircraft
It is attached, is controlled by hybrid lift aircraft main control unit, and can be by energy such as battery/fuel of aerofoil with electro-hydraulic gas interface
Aircraft host is passed to, the flight time is improved.The multiplication of performance may be implemented by the auxiliary wing of superimposion lift.It is modular
Design, reduces the disposable input of client, reduces buying and operation cost.
9. the compound auxiliary wing of airscrew thrust self energizing of the present invention is in parallel with the auxiliary wing of other hybrid lifts, and passes through machine
Wing hinge and electro-hydraulic gas interface are attached, synchronous to be controlled by hybrid lift aircraft main control unit, are expanded again and can be by the wing
The energy transmissions such as the battery/fuel in face give aircraft host, improve the flight time.
10. thrust device modularization can very easily realize that repair is replaced.
11. in the present invention, auxiliary wing one or both sides are provided with electro-hydraulic gas interface, realize the auxiliary wing and fly with hybrid lift
Energy intercommunication between device main plane, and action is controlled by hybrid lift aircraft, improves the flexibility of complete machine.
12. the auxiliary wing is also built-in with the horizontal lifting rudder wing, improves complete machine and manipulate agility！
13. aerofoil type energy device, efficiently uses space.
Schematically the present invention and embodiments thereof are described above, description is not limiting, institute in attached drawing
What is shown is also one of embodiments of the present invention, and actual structure is not limited to this.So if the common skill of this field
Art personnel are enlightened by it, without departing from the spirit of the invention, are not inventively designed and the technical solution
Similar frame mode and embodiment should all belong to the scope of the present invention.
Claims (10)
1. a kind of spiral shell with the auxiliary wing of twin screw and the attached wing pushes away combined wing aircraft, which is characterized in that multiple including rear single-screw paddle
The compound auxiliary wing of airscrew thrust self energizing and additional fin for closing rotor aircraft, being assemblied in its wing both sides（114）；
Wherein, the rear single-screw paddle composite wing aircraft includes body（101）, be fixedly mounted on body（101）Both sides
Hybrid lift wing（102）, propeller（106）；Wherein, the body（101）It is set as deck platform；The compound liter
Power wing（102）Built-in self-enclosed ducted fan（104）, hybrid lift wing（102）Outside is designed with wing hinge (1028)；
Propeller（106）For screw propeller；
The front end of the compound auxiliary wing of the airscrew thrust self energizing is provided with screw propeller（1062）, airscrew thrust is certainly
Energize the compound auxiliary wing is internally provided with self-enclosed ducted fan（104）, the both sides of the compound auxiliary wing of airscrew thrust self energizing are set
It is equipped with electro-hydraulic gas interface（1036）With wing hinge (1028), and pass through the wing hinge of side (1028) and hybrid lift wing
（102）Flexible connection；
The additional fin（114）Towards body（101）Side be provided with wing hinge (1028) and electro-hydraulic gas interface
（1036）, and be mounted on the outside of the compound auxiliary wing of airscrew thrust self energizing by the way that wing hinge (1028) is folding；Described
Electro-hydraulic gas interface（1036）With lid（10361）, additional fin（114）Internal battery/fuel（1006）.
2. a kind of spiral shell with the auxiliary wing of twin screw and the attached wing according to claim 1 pushes away combined wing aircraft, which is characterized in that
The propeller（106）For a variety of dynamic structures such as electric propeller, the dynamic propellers of oil.
3. a kind of spiral shell with the auxiliary wing of twin screw and the attached wing according to claim 1 pushes away combined wing aircraft, which is characterized in that
The hybrid lift wing（102）Front and back are respectively set to magnetic-type self interlocking interface male connector（1026）With it is magnetic-type from
Move mutual lock interface female（1027）；The magnetic-type self interlocking interface male connector（1026）With magnetic-type self interlocking interface mother
Head（1027）Size is identical.
4. a kind of spiral shell with the auxiliary wing of twin screw and the attached wing according to claim 3 pushes away combined wing aircraft, which is characterized in that
The magnetic-type self interlocking interface male connector（1026）With magnetic-type self interlocking interface female（1027）For taper connection.
5. a kind of spiral shell with the auxiliary wing of twin screw and the attached wing according to claim 1 pushes away combined wing aircraft, which is characterized in that
The hybrid lift wing（102）Lift main wing can be divided into（1021）And balance empennage（1023）Two parts, set respectively
It sets in hybrid lift wing（102）Front and back；Lift main wing（1021）With balance empennage（1023）Between be reserved with space, it is empty
It is interior to be provided with the horizontal lifting rudder wing（1022）；Wherein, lift main wing（1021）There are one self-enclosed ducts for internal at least installation
Fan（104）.
6. a kind of spiral shell with the auxiliary wing of twin screw and the attached wing according to claim 1 pushes away combined wing aircraft, which is characterized in that
It further include vertical tail（105）, the vertical tail（105）It is arranged in body（101）Above or below；The vertical tail
（105）It is arranged in wing both sides；The vertical tail（105）It may be implemented to fold；The vertical tail（105）It is equipped with below
Mobilizable vertical rudder wing（1051）.
7. a kind of spiral shell with the auxiliary wing of twin screw and the attached wing according to claim 1 pushes away combined wing aircraft, which is characterized in that
The body（101）It is installed with cavity（1002）, cavity（1002）Interior installation diagram passes, flies the modules such as control, driving.
8. a kind of spiral shell with the auxiliary wing of twin screw and the attached wing according to claim 1 pushes away combined wing aircraft, which is characterized in that
The compound auxiliary wing of the airscrew thrust self energizing can be divided into the auxiliary wing of lift（10311）And the auxiliary empennage of balance（10312）Two
Part is separately positioned on the front and back of the compound auxiliary wing of airscrew thrust self energizing；The auxiliary wing of lift（10311）With the auxiliary empennage of balance
（10312）Between be reserved with space, the horizontal lifting rudder wing is provided in space（1022）；Wherein, the auxiliary wing of lift（10311）It is internal
At least there are one self-enclosed ducted fans for installation（104）.
9. a kind of spiral shell with the auxiliary wing of twin screw and the attached wing according to claim 1 pushes away combined wing aircraft, which is characterized in that
It is additionally provided with engine installation position on the compound auxiliary wing of the airscrew thrust self energizing（111）, engine installation position（111）Peace
Dress is electric propeller or the dynamic propeller of oil.
10. a kind of spiral shell with the auxiliary wing of twin screw and the attached wing according to claim 1 pushes away combined wing aircraft, feature exists
In being provided with battery/fuel on the compound auxiliary wing of the airscrew thrust self energizing（1006）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810551560.4A CN108639329A (en) | 2018-05-31 | 2018-05-31 | A kind of spiral shell with the auxiliary wing of twin screw and the attached wing pushes away combined wing aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810551560.4A CN108639329A (en) | 2018-05-31 | 2018-05-31 | A kind of spiral shell with the auxiliary wing of twin screw and the attached wing pushes away combined wing aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108639329A true CN108639329A (en) | 2018-10-12 |
Family
ID=63759003
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810551560.4A Pending CN108639329A (en) | 2018-05-31 | 2018-05-31 | A kind of spiral shell with the auxiliary wing of twin screw and the attached wing pushes away combined wing aircraft |
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Citations (9)
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|---|---|---|---|---|
| US6561456B1 (en) * | 2001-12-06 | 2003-05-13 | Michael Thomas Devine | Vertical/short take-off and landing aircraft |
| US6843447B2 (en) * | 2003-01-06 | 2005-01-18 | Brian H. Morgan | Vertical take-off and landing aircraft |
| US20100051741A1 (en) * | 2008-09-03 | 2010-03-04 | Anvar Ismailov | Unmanned air vehicle |
| CN102530248A (en) * | 2011-12-12 | 2012-07-04 | 周景荣 | Design method for multifunctional helicopter |
| CN102658866A (en) * | 2012-05-25 | 2012-09-12 | 辽宁通用航空研究院 | Conjoined aircraft with straight layout |
| CN105235891A (en) * | 2015-01-04 | 2016-01-13 | 北京零零无限科技有限公司 | Foldable unmanned aerial vehicle |
| CN107089316A (en) * | 2016-02-18 | 2017-08-25 | 张飞 | Flying wing type dual-culvert vertical take-off and landing aircraft |
| CN107651168A (en) * | 2017-09-30 | 2018-02-02 | 肇庆高新区国专科技有限公司 | A kind of unmanned plane wingfold mechanism and method for folding |
| WO2018078388A1 (en) * | 2016-10-27 | 2018-05-03 | Mono Aerospace Ip Ltd | Vertical take-off and landing aircraft and control method |
-
2018
- 2018-05-31 CN CN201810551560.4A patent/CN108639329A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6561456B1 (en) * | 2001-12-06 | 2003-05-13 | Michael Thomas Devine | Vertical/short take-off and landing aircraft |
| US6843447B2 (en) * | 2003-01-06 | 2005-01-18 | Brian H. Morgan | Vertical take-off and landing aircraft |
| US20100051741A1 (en) * | 2008-09-03 | 2010-03-04 | Anvar Ismailov | Unmanned air vehicle |
| CN102530248A (en) * | 2011-12-12 | 2012-07-04 | 周景荣 | Design method for multifunctional helicopter |
| CN102658866A (en) * | 2012-05-25 | 2012-09-12 | 辽宁通用航空研究院 | Conjoined aircraft with straight layout |
| CN105235891A (en) * | 2015-01-04 | 2016-01-13 | 北京零零无限科技有限公司 | Foldable unmanned aerial vehicle |
| CN107089316A (en) * | 2016-02-18 | 2017-08-25 | 张飞 | Flying wing type dual-culvert vertical take-off and landing aircraft |
| WO2018078388A1 (en) * | 2016-10-27 | 2018-05-03 | Mono Aerospace Ip Ltd | Vertical take-off and landing aircraft and control method |
| CN107651168A (en) * | 2017-09-30 | 2018-02-02 | 肇庆高新区国专科技有限公司 | A kind of unmanned plane wingfold mechanism and method for folding |
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Application publication date: 20181012 |