CN108945422A - A kind of spiral shell with the auxiliary wing of twin screw and the attached wing pushes away composite wing airfreighter - Google Patents
A kind of spiral shell with the auxiliary wing of twin screw and the attached wing pushes away composite wing airfreighter Download PDFInfo
- Publication number
- CN108945422A CN108945422A CN201810550532.0A CN201810550532A CN108945422A CN 108945422 A CN108945422 A CN 108945422A CN 201810550532 A CN201810550532 A CN 201810550532A CN 108945422 A CN108945422 A CN 108945422A
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- China
- Prior art keywords
- wing
- auxiliary
- lift
- airfreighter
- spiral shell
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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
- B64C27/22—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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
Abstract
The present invention is that a kind of spiral shell with the auxiliary wing of twin screw and the attached wing pushes away composite wing airfreighter, wherein rear single-screw paddle composite wing aircraft includes body, is fixedly mounted on body two sides hybrid lift wing, screw propeller；Wherein, self-enclosed ducted fan built in hybrid lift wing, the outside design of hybrid lift wing have 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 two 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 by the wing hinge of side with hybrid lift wing；The side of additional fin towards body is provided with wing hinge and electro-hydraulic gas interface, and is mounted on the outside of the compound auxiliary wing of airscrew thrust self energizing by the way that wing hinge is folding.The auxiliary wing of the present invention uses hybrid lift, it is ensured that the adaptation range 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 composite wing shipping and flies
Machine belongs to aircraft equipment technology field.
Background technique
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 high, safety coefficient is low, and load capacity is poor, water
Flat flying speed is slow, is easy the disadvantages of air crash；Although current VTOL fixed-wing has the characteristics that landing is convenient, but in water
The disadvantages 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.
Summary of the invention
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 the airscrew thrust self energizing of power aircraft two sides and shipping storehouse；Wherein, rear single-screw paddle composite wing flight
Device includes body, is fixedly mounted on body two 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, the outside design of hybrid lift wing have 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 two 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 has
Lid, additional fin internal battery/fuel.Shipping storehouse is mounted on the lower section of body.
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 lift main wing and balance two parts of 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,
One self-enclosed ducted fan is at least installed inside lift main wing.
It further, further include vertical tail, the vertical tail is arranged above or below body；The vertical tail is set
It sets in wing two 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, a self-enclosed ducted fan is at least installed 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 device.
Further, battery/fuel 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, obstacle 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 modularization auxiliary wing of ducted fan drive-in hybrid lift of the invention uses hybrid lift, i.e., existed by design
Self-enclosed ducted fan in aerofoil generates the lift that lift and the auxiliary wing of lift are generated in horizontal flight, to be formed compound
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, cooperates 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 damage simultaneously, the forced landing of aerodone formula is also able to achieve, greatly improves
The safety of aircraft has ensured the safety of personnel and goods and materials.
5. the present invention uses hardware and software platform, modularized design, multiple functions are able to achieve,
6. the present invention using two 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 socket, the cluster of aircraft is facilitated to fly, further decreases cluster flight
When power consumption.When front and back is connected in series, the aircraft at rear only needs a small amount of energy consumption, can be achieved with flying for long range
Row, the cluster flight of only aircraft does not provide the low-power consumption scheme of clustering, it might even be possible to realize the sky between aircraft
Faulty aircraft dragging below is taken off, realizes and mutually come to sb.'s rescue between aircraft not seen before by middle rescue, i.e., preceding aircraft
Help phenomenon.
8. can pass through between the auxiliary wing of modularization ducted fan drive-in hybrid lift and hybrid lift aircraft of invention
Wing hinge and electro-hydraulic gas interface are attached, and are controlled by hybrid lift aircraft main control unit, and can be by battery/combustion of aerofoil
The energy transmissions such as material give aircraft host, improve the flight time.The multiplication of performance may be implemented by the auxiliary wing of superimposion lift.
Modular design reduces the disposable investment of client, reduces buying and operation cost.
9. the modularization auxiliary wing of ducted fan drive-in hybrid lift of the invention is in parallel with the auxiliary wing of other hybrid lifts,
And be attached by wing hinge and electro-hydraulic gas interface, synchronization is controlled by hybrid lift aircraft main control unit, is expanded again
And the energy transmissions such as battery/fuel of aerofoil can be given to aircraft host, improve the flight time.
10. thrust device modularization can very easily realize maintenance replacement.
11. in the present invention, auxiliary wing one or both sides are provided with electro-hydraulic gas interface, realize the auxiliary wing and hybrid lift flies
Energy intercommunication between device main plane, and the control by hybrid lift aircraft is acted, improve 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.
Detailed description of the invention
Fig. 1 is structural schematic diagram of the invention；
Fig. 2 is side view of the invention；
Fig. 3 is rearview of the invention；
Fig. 4 is plan view of the invention；
Fig. 5 is oblique view of the 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: fixation 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；113, shipping storehouse.
Specific embodiment
The present invention will be further described with reference to the accompanying drawing.
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 composite wing airfreighter, including rear list
The compound auxiliary wing of the compound rotor aircraft of propeller type, the airscrew thrust self energizing for being assemblied in its wing two sides and additional fin 114；
Wherein, the rear single-screw paddle composite wing aircraft includes body 101, is fixedly mounted on 101 two sides hybrid lift of body
Wing 102, propeller 106；Wherein, the body 101 is set as deck platform；Built in the hybrid lift wing 102
Self-enclosed ducted fan 104, design has wing hinge 1028 on the outside of hybrid lift wing 102；The airscrew thrust confession
The front end of the compound auxiliary wing of energy is provided with screw propeller 1062, and the compound auxiliary wing of airscrew thrust self energizing is internally provided with certainly
Ducted fan 104 is closed, the two 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 by the wing hinge 1028 of side with hybrid lift wing 102；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 the folding installation of wing hinge 1028
On the outside of the compound auxiliary wing of airscrew thrust self energizing；The electro-hydraulic gas interface 1036 has lid 10361, in additional fin 114
Set battery/fuel 1006.Shipping storehouse 113 is mounted on the lower section of body 101
As further improvement of the invention, propeller 106 is a variety of dynamic structures such as electric propeller, the dynamic propeller of oil.
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, be at least equipped with inside lift main wing 1,021 one it is self-enclosed
Ducted fan 104.
It further include vertical tail 105, the vertical tail 105 is arranged in body 101 as further improvement of the invention
Above or below；The vertical tail 105 is arranged in wing two 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 10311 of lift 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 10312 of balance, the horizontal lifting rudder wing 1022 is provided in space；Wherein, lift is auxiliary
One self-enclosed ducted fan 104 is at least installed 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 device 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, obstacle 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 modularization auxiliary wing of ducted fan drive-in hybrid lift of the invention uses hybrid lift, i.e., existed by design
Self-enclosed ducted fan in aerofoil generates the lift that lift and the auxiliary wing of lift are generated in horizontal flight, to be formed compound
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, cooperates 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 damage simultaneously, the forced landing of aerodone formula is also able to achieve, greatly improves
The safety of aircraft has ensured the safety of personnel and goods and materials.
5. the present invention uses hardware and software platform, modularized design, multiple functions are able to achieve,
6. the present invention using two 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 socket, the cluster of aircraft is facilitated to fly, further decreases cluster flight
When power consumption.When front and back is connected in series, the aircraft at rear only needs a small amount of energy consumption, can be achieved with flying for long range
Row, the cluster flight of only aircraft does not provide the low-power consumption scheme of clustering, it might even be possible to realize the sky between aircraft
Faulty aircraft dragging below is taken off, realizes and mutually come to sb.'s rescue between aircraft not seen before by middle rescue, i.e., preceding aircraft
Help phenomenon.
8. can pass through between the auxiliary wing of modularization ducted fan drive-in hybrid lift and hybrid lift aircraft of invention
Wing hinge and electro-hydraulic gas interface are attached, and are controlled by hybrid lift aircraft main control unit, and can be by battery/combustion of aerofoil
The energy transmissions such as material give aircraft host, improve the flight time.The multiplication of performance may be implemented by the auxiliary wing of superimposion lift.
Modular design reduces the disposable investment of client, reduces buying and operation cost.
9. the modularization auxiliary wing of ducted fan drive-in hybrid lift of the invention is in parallel with the auxiliary wing of other hybrid lifts,
And be attached by wing hinge and electro-hydraulic gas interface, synchronization is controlled by hybrid lift aircraft main control unit, is expanded again
And the energy transmissions such as battery/fuel of aerofoil can be given to aircraft host, improve the flight time.
10. thrust device modularization can very easily realize maintenance replacement.
11. in the present invention, auxiliary wing one or both sides are provided with electro-hydraulic gas interface, realize the auxiliary wing and hybrid lift flies
Energy intercommunication between device main plane, and the control by hybrid lift aircraft is acted, improve 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 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 composite wing airfreighter, which is characterized in that including rear single screw
The compound auxiliary wing of the compound rotor aircraft of formula, the airscrew thrust self energizing for being assemblied in its wing two sides and additional fin (114)；
Wherein, the rear single-screw paddle composite wing aircraft includes body (101), is fixedly mounted on body (101) two sides
Hybrid lift wing (102), propeller (106)；Wherein, the body (101) is set as deck platform；The compound liter
Self-enclosed ducted fan (104) built in power wing (102), the design of hybrid lift wing (102) outside have wing hinge (1028)；
Propeller (106) is screw propeller；
The front end of the compound auxiliary wing of the airscrew thrust self energizing is provided with screw propeller (1062), and airscrew thrust is certainly
Being internally provided with self-enclosed ducted fan (104) for the compound auxiliary wing is energized, the two sides of the compound auxiliary wing of airscrew thrust self energizing are set
It is equipped with electro-hydraulic gas interface (1036) and wing hinge (1028), and passes through the wing hinge of side (1028) and hybrid lift wing
(102) it is flexibly connected；
The side of additional fin (114) towards the body (101) is provided with wing hinge (1028) and electro-hydraulic gas interface
(1036), it and by the way that wing hinge (1028) are folding is mounted on the outside of the compound auxiliary wing of airscrew thrust self energizing；Described
Electro-hydraulic gas interface (1036) has lid (10361), additional fin (114) internal battery/fuel (1006)；
The shipping storehouse (113) is mounted on the lower section of body (101).
2. a kind of spiral shell with the auxiliary wing of twin screw and the attached wing according to claim 1 pushes away composite wing airfreighter, feature
It is, the propeller (106) is a variety of dynamic structures such as electric propeller, the dynamic propeller 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 composite wing airfreighter, feature
It is, described hybrid lift wing (102) front and back are respectively set to magnetic-type self interlocking interface male connector (1026) and magnetic
Suction self interlocking interface female (1027)；The magnetic-type self interlocking interface male connector (1026) and magnetic-type self interlocking
Interface female (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 composite wing airfreighter, feature
It is, the magnetic-type self interlocking interface male connector (1026) and magnetic-type self interlocking interface female (1027) are taper company
It connects.
5. a kind of spiral shell with the auxiliary wing of twin screw and the attached wing according to claim 1 pushes away composite wing airfreighter, feature
It is, the hybrid lift wing (102) can be divided into lift main wing (1021) and balance (1023) two parts of empennage, point
It She Zhi not be in the front and back of hybrid lift wing (102)；It is reserved between lift main wing (1021) and balance empennage (1023) free
Between, the horizontal lifting rudder wing (1022) is provided in space；Wherein, be at least equipped with inside lift main wing (1021) one it is self-enclosed
Ducted 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 composite wing airfreighter, feature
It is, further includes vertical tail (105), the vertical tail (105) is arranged above or below body (101)；It is described vertical
Empennage (105) is arranged in wing two sides；The vertical tail (105) may be implemented to fold；The vertical tail (105) is pacified below
Equipped with 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 composite wing airfreighter, feature
It is, the body (101) is installed with cavity (1002), and the interior installation diagram of cavity (1002) 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 composite wing airfreighter, feature
It is, the compound auxiliary wing of the airscrew thrust self energizing can be divided into the auxiliary wing of lift (10311) and the auxiliary empennage (10312) of balance
Two parts are separately positioned on the front and back of the compound auxiliary wing of airscrew thrust self energizing；The auxiliary wing of lift (10311) and the auxiliary tail of balance
It is reserved with space between the wing (10312), the horizontal lifting rudder wing (1022) is provided in space；Wherein, in the auxiliary wing of lift (10311)
Portion is at least equipped with a self-enclosed ducted fan (104).
9. a kind of spiral shell with the auxiliary wing of twin screw and the attached wing according to claim 1 pushes away composite wing airfreighter, feature
It is, is additionally provided with engine installation position (111), engine installation position on the compound auxiliary wing of the airscrew thrust self energizing
(111) power device is provided in.
10. a kind of spiral shell with the auxiliary wing of twin screw and the attached wing according to claim 1 pushes away composite wing airfreighter, feature
It is, is provided with battery/fuel (1006) on the compound auxiliary wing of the airscrew thrust self energizing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810550532.0A CN108945422A (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 composite wing airfreighter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810550532.0A CN108945422A (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 composite wing airfreighter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108945422A true CN108945422A (en) | 2018-12-07 |
Family
ID=64492713
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810550532.0A Pending CN108945422A (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 composite wing airfreighter |
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| CN (1) | CN108945422A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205131649U (en) * | 2015-10-30 | 2016-04-06 | 佛山市神风航空科技有限公司 | Multi -axis aircraft |
| CN206012959U (en) * | 2016-09-08 | 2017-03-15 | 朗星无人机系统有限公司 | A kind of how culvert vertical take-off and landing unmanned machine |
| CN107089316A (en) * | 2016-02-18 | 2017-08-25 | 张飞 | Flying wing type dual-culvert vertical take-off and landing aircraft |
| CN107813929A (en) * | 2016-09-11 | 2018-03-20 | 郎风 | Combined type dalta wing duct aircraft |
| CN107856838A (en) * | 2017-11-10 | 2018-03-30 | 肇庆市高新区晓靖科技有限公司 | A kind of unmanned plane wingfold mechanism |
-
2018
- 2018-05-31 CN CN201810550532.0A patent/CN108945422A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205131649U (en) * | 2015-10-30 | 2016-04-06 | 佛山市神风航空科技有限公司 | Multi -axis aircraft |
| CN107089316A (en) * | 2016-02-18 | 2017-08-25 | 张飞 | Flying wing type dual-culvert vertical take-off and landing aircraft |
| CN206012959U (en) * | 2016-09-08 | 2017-03-15 | 朗星无人机系统有限公司 | A kind of how culvert vertical take-off and landing unmanned machine |
| CN107813929A (en) * | 2016-09-11 | 2018-03-20 | 郎风 | Combined type dalta wing duct aircraft |
| CN107856838A (en) * | 2017-11-10 | 2018-03-30 | 肇庆市高新区晓靖科技有限公司 | A kind of unmanned plane wingfold mechanism |
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Application publication date: 20181207 |