CN102085912A - Dishing magnetic suspension ring-wing aircraft - Google Patents
Dishing magnetic suspension ring-wing aircraft Download PDFInfo
- Publication number
- CN102085912A CN102085912A CN2009101135537A CN200910113553A CN102085912A CN 102085912 A CN102085912 A CN 102085912A CN 2009101135537 A CN2009101135537 A CN 2009101135537A CN 200910113553 A CN200910113553 A CN 200910113553A CN 102085912 A CN102085912 A CN 102085912A
- Authority
- CN
- China
- Prior art keywords
- wing
- ring
- magnetic suspension
- aircraft
- encircle
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Landscapes
- Toys (AREA)
Abstract
The invention relates to a dishing vertical takeoff and landing aircraft, namely a dishing magnetic suspension aircraft. The aircraft has an overall layout according to a dishing outline. An upper magnetic suspension ring-wing and a lower magnetic suspension ring-wing are suspended between an engine room 700 and a fixed ring 100 by a magnetic suspension driving device. The elevation angles of an upper ring-wing blade and a lower ring-wing blade are opposite to each other, and the driving forces of ring-wing power-drive magnetic rings (blocks) (2200 and 2600) are opposite to each other. The magnetic suspension ring-wing structure makes use of an electromotive power magnetic suspension driving principle to ensure that upper and lower magnetic suspension ring-wings are not only uprising and hovering rotor wings, but also an effective extension of fixed wings during forward flight. When the 2200 and the 2600 are loaded with electric power, a magnetic force drives the upper and lower ring-wings to rotate reversely to generate a lift force. The steering of the aircraft is also adjusted by the rotating speed of the upper and lower ring-wings. The forward flight is carried out by a driving device 800. The aircraft integrates the advantages of the fixed wing, a helicopter and a motor-less rotorcraft, can take off and land vertically, hover, cruise at a low altitude at a low speed, and can fly at a high speed. The dishing magnetic suspension aircraft overcomes the defects of the aircraft, is not provided with a mechanical device, is simple in control, and is high in safety.
Description
Affiliated technical field
The present invention relates to a kind of dish-shaped vertically taking off and landing flyer.
Background technology
In existing aircraft, vertical takeoff and landing, high-speed secure flight are the contradiction that is interweaved always.
Cyclogyro can vertical takeoff and landing, but make, the flicon complexity, poor stability.And do not overcome the flying speed and the ceiling restriction that self are brought because of rotor again; Fixed wing aircraft flying speed height, the ceiling is better than cyclogyro, but the take-off venue is required high, and can not Ultra-Low Speed, low cruise, hover.Also have partially mixed rotor aircraft to make every effort to break through, but it is not all obtained and should produce effect.
Summary of the invention
According to the demand of above prior art, the invention provides a kind of aircraft brand-new design mode, overcome the defective that existing aircraft exists to greatest extent.
One, complete machine layout structure
Dish magnetcisuspension floating ring rotor aircraft is with dish-shaped layout, and this layout was both relevant with aircraft each several part combination main points, and to possess good aerodynamic arrangement relevant with aircraft again.Take into account the two, reach perfect adaptation.
The aircraft middle part is cabin 700, is around rail assembly (constituting jointly by 2100,2200,2300,2400) in the ring wing in the magnetic suspension in cabin in turn; Magnetic suspension is the interior rail assembly (constituting jointly by 2500,2600,2700,2800) of the ring wing down; The ring wing 200 in the magnetic suspension (the ring wing number of blade can rationally be provided with because of needs); Magnetic suspension is the ring wing 300 (the ring wing number of blade can rationally be provided with because of needs) down; Set collar wing pipe link 600; Ring wing outer rail assembly (constituting jointly) in the magnetic suspension by 1300,1400,1500,1600; Magnetic suspension is the ring wing 300 outer rail assemblies (constituting jointly by 1700,1800,1900,2000) down; The set collar wing 100.
Two, the magnetcisuspension floating ring wing and structure
Magnetcisuspension floating ring wing structure is to utilize Electronmotive Force magnetic suspension driving principle, make the upper and lower ring wing of magnetic suspension be rise, hover, low speed cruises lifting rotor, stretch on effective edge of fixed-wing in flying before being again, annular layout is in nacelle exterior, guarantee the whole good aerodynamic arrangement of aircraft, overcome the purling cabin resistance problem of original cyclogyro again.
The ring wing 200 encircles the wing 300 upper and lower layouts down with magnetic suspension in the magnetic suspension, overcomes rotary torque, need not empennage, has reduced body weight, has reduced corresponding mechanical device, has improved aircraft security and effect.
The outstanding wing suspends and Electromagnetic Drive, replaces numerous and diverse mechanical device, reduces the body deadweight greatly, reduces and controls difficulty, promotes the usefulness and the safety of aircraft.
1, structure important document
The ring wing 200 in the magnetic suspension; Magnetic suspension is the ring wing 300 down; Ring rail assembly (constituting) in the magnetic suspension of the last ring wing by 2100,2200,2300,2400; Last ring wing magnetic suspension outer shroud rail assembly (constituting) by 1300,1400,1500,1600; Under encircle ring rail assembly (constituting) in the wing magnetic suspension by 2500,2600,2700,2800; Under encircle wing magnetic suspension outer shroud rail assembly (constituting) by 1700,1800,1900,2000.
The ring wing 200 is connected in ring wing magnetic suspension outer rail and connects suspended ring 1500 and be connected on the suspended ring 2300 with the interior rail of last ring wing magnetic suspension in the magnetic suspension, is suspended between the cabin 700 and the set collar wing 100.
The magnetic suspension down ring wing 300 is connected in down ring wing magnetic suspension outer rail and connects suspended ring 1900 and be connected on the suspended ring 2700 with the following wing magnetic suspension outer rail that encircles, and is suspended between the cabin 700 and the set collar wing 100.
Wherein, on encircle wing power driven magnet ring (piece) 2200 for the last ring wing 200 power driven magnet rings (piece), encircle wing power driven magnet ring (piece) 2600 down and be the ring wing 300 power driven magnet rings (piece) down, its orientation rotation of mainly playing the upper and lower ring wing drives function.Also in the upper and lower ring wing in the rail assembly outside the suspending stabilized function of magnetize,
2, turn realizes
The upper and lower ring wing is by being installed at around rail assembly, outer rail assembly in the magnetic suspension of cabin 700 and the set collar wing 100 inner rings, the upper and lower ring wing suspends, utilize Electronmotive Force magnetic suspension driving principle, the electric power that is provided by Power Drive Unit 800 upwards encircles wing power driven magnet ring (piece) 2200 and encircles wing power driven magnet ring (piece) 2600 loading electric energy down, drives upper and lower ring wing rotation with electromagnetic force.
Power Drive Unit 800; Alighting gear 900; Cabin window 1200 is arranged with reference to accompanying drawing.
This aircraft has following characteristics:
Function: can be in complex environment vertical takeoff and landing; Can hover, low speed, low cruise; Turn to freely, high-speed flight.
1, the magnetcisuspension floating ring wing is a rigid wings, has promoted the space of take-off weight.
2, interplane crack can be very little up and down for the stiffening ring wing, and counter-rotating overcomes moment of torsion up and down, does not need empennage, has alleviated the weight of body.
3, magnetic suspension design does not have mechanical device, and resistance is minimum, and Electromagnetic Drive is simple in structure.
4, realized not having strand, not having axle, No Tail Rotor.Simplified physical construction greatly, made simple.
5, machine---wing one, the set collar wing, rotor one have solved a difficult problem in the compound type aircraft flight process well and have realized that the ring wing smoothly is converted to the component part of flying wing in the aircraft high-speed flight.
6, overcome the defective of fixed-wing and cyclogyro well.
According to the present invention, with the magnetcisuspension floating ring wing solve the aircraft vertical takeoff and landing, hover, low speed low-latitude flying problem.With ring wing layout, reach body, the ring wing, the smooth and easy combination of the set collar wing, the common lift that produces in flat the flying, overcome the flat theoretical limit that flies high speed flight of cyclogyro, after running out of steam, the spin that also reliably encircles the wing overcomes the vertical decline of body, promotes the safety factor of aircraft.The upper and lower ring wing is in preceding flying, and after the speed of a ship or plane reached certain speed, aircraft lift was smoothly taken over by the lift that preceding flies to produce, and encircle wing propulsive effort and end this moment, and the preceding resistance that flies to produce makes upper and lower ring wing spin.The ring wing becomes the effective wing face of aircraft,
Description of drawings
To describe exemplary specific embodiments of the present invention with reference to the accompanying drawings in detail below, wherein:
Figure one: dish-shaped magnetcisuspension floating ring rotor aircraft front elevation
Figure two: dish-shaped magnetcisuspension floating ring rotor aircraft side birds-eye view
Figure three: dish-shaped magnetcisuspension floating ring rotor aircraft upward view
Figure four: ring rail assembly, the thin portion of outer shroud rail assembly section enlarged drawing in the magnetic suspension of dish-shaped magnetcisuspension floating ring rotor aircraft.
Among the figure token name claim, function:
100---the set collar wing: the fixing wing that rises of aircraft.
200---encircle the wing in the magnetic suspension: the aircraft landing, the wing hovers.
300---magnetic suspension is the ring wing down: the aircraft landing, the wing hovers.
2300---on encircle that rail connects suspended ring in the wing magnetic suspension: suspension coupling link wing blade.
1500---on encircle wing magnetic suspension outer rail and connect suspended ring; Suspension coupling link wing blade.
2700---rail connects suspended ring in the magnetic suspension of the ring wing down; Suspension coupling link wing blade.
1900---ring wing magnetic suspension outer rail connects suspended ring down; Suspension coupling link wing blade.
1200---cabin window; The outer form of driver and crew.
600---set collar wing connecting rod: it can place the ring wing 200 and encircle between the wing 300 down, also can place the upper and lower of the ring wing, and the ring wing is upper and lower with putting the connection cabin and the set collar wing.(this Figure of description is only listed to place and is encircled an example between the wing up and down)
700---the cabin; Drive and airborne equipment cabin body.
800---Power Drive Unit; Electric power and preceding propelling thrust are provided
900---alighting gear; Landing, slide
2200---on encircle wing power driven magnet ring (piece); The last ring wing drives, the suspending stabilized ring wing
2600---encircle wing power driven magnet ring (piece) down; Under encircle that the wing drives, the suspending stabilized ring wing
1300,1400,1600; 1700,1800,2000; 2100,2200,2400; 2500,2700,2800-ring suspending stabilized magnet ring of the wing (piece).
The specific embodiment
One, the ring wing
Among the present invention, the turn of the upper and lower ring wing be realize the aircraft landing, hover, low speed cruises, the major part that turns to.
The ring wing 200 is connected suspended ring 1500 and goes up rail connection suspended ring 2300 connections in the magnetic suspension of the ring wing in the magnetic suspension with last ring wing magnetic suspension outer rail, be suspended between 1300,1400,1600,1700,1800, the 2000 ring suspending stabilized magnet rings of the wing (piece), and, utilize magnetic suspension driving principle driven in rotation by after ring wing power driven magnet ring (piece) loads electric energy on 2200.
The magnetic suspension down ring wing 300 is connected suspended ring 1900 and rail connection suspended ring 2600 connections in the magnetic suspension of the ring wing down with ring wing magnetic suspension outer rail down, be suspended in 2100,2200,2400; 2500, between 2700, the 2800 ring suspending stabilized magnet rings of the wing (piece), and encircle wing power driven magnet rings (piece) by 2700 times and utilize Electronmotive Force magnetic suspension driving principle driven in rotation.
The last ring wing 200 and the following ring wing 300, the elevation angle is opposite, contrarotation.
Two, landing, hover, low speed cruises, turn to, the implementation of each motion morphology of high-speed flight
The aircraft vertical takeoff and landing, hover by magnetcisuspension float in the magnetic suspension in ring rail assembly and the magnetic suspension outer rail assembly suspension magnetic suspension ring wing 200 and magnetic suspension down 300 contrarotations of the ring wing produce lift and finish.Also mainly by the last ring wing 200 and the ring wing 300 high speed revolutions generation down, the preceding generating unit that flies is divided lift to lift when low speed, low cruise, and the preceding propelling thrust that flies is provided by Power Drive Unit 800.
During the aircraft low-speed operations, lift is mainly produced by the upper and lower magnetcisuspension floating ring wing.During the aircraft high-speed flight, the preceding power of flying provides the high speed propelling thrust by Power Drive Unit 800.The lift that lift flies to produce before by aircraft and go up the ring wing 200, to encircle the lift of the wing 300 contrarotations down synthetic.
1, low speed is in the high-speed transitions process, and lift is synthetic by move ahead lift and upper and lower rotor lift.
2, after forward flight speed acquires a certain degree, unload upper and lower ring wing additionaling power, the ring wing is preceding flying to change the hand of rotation spin under the drag effect, also make it convert the effective component part of wing to, cabin, the ring wing, the set collar wing are because of its pneumatic structure, in preceding the flying common lift that produces has realized that lift is seamlessly transitting of the main lift that moves ahead that produces to whole machine body by rotor.Because having overcome traditional cyclogyro moves ahead to the dependence of rotor, has solved the velocity limit problem of rotor dependent form aircraft high-speed flight.
In flight course, lift is made a concerted effort big or small distribution by aircraft operators and aircraft operatorless device adjusting configuration, guarantees to seamlessly transit.
Because the alternative that lift produces, aircraft can be in complex environment vertical takeoff and landing; Can hover, low speed, low cruise; But high-speed flight.To the flying field no dependence.
Dogled is realized by the rotating speed of regulating the upper and lower ring wing.By regulating the rotating speed size of the upper and lower ring wing, change upper and lower ring wing moment of torsion and realize the adjusting of aircraft direction.Also can change thrust regulation, or install auxilliary wing adjusting additional by Power Drive Unit 800.
Fixed-wing connecting rod 600 performance lift are to the conduction of fuselage and the solidating effect of the body and the set collar wing.
Claims (2)
1. layout: cross-arranging type cabin 700---on encircle the wing 200, the encircle the wing 300 down---layout structure of the set collar wing 100.
2. magnetcisuspension floating ring wing suspension drive pattern: on encircle ring rail assembly (constituting) in the wing 200 magnetic suspension by 2100,2200,2300,2400; The last ring wing 200 magnetic suspension outer shroud rail assemblies (constituting) by 1300,1400,1500,1600; Under encircle ring rail assembly (constituting) in the wing 300 magnetic suspension by 2500,2600,2700,2800; Under encircle the wing 300 magnetic suspension outer shroud rail assemblies (constituting) by 1700,1800,1900,2000.
The last ring wing 200 connects on suspended ring 1500 and the suspended ring 2300, is suspended between the cabin 700 and the set collar wing 100.
Wherein, on encircle wing power driven magnet ring (piece) 2200, encircle the wing 300 power driven magnet rings (piece) 2600 down, in rail assembly in the upper and lower ring wing, rise the magnetic suspension function, its radical function is that the orientation rotation of the upper and lower ring wing drives function.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009101135537A CN102085912A (en) | 2009-12-03 | 2009-12-03 | Dishing magnetic suspension ring-wing aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009101135537A CN102085912A (en) | 2009-12-03 | 2009-12-03 | Dishing magnetic suspension ring-wing aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102085912A true CN102085912A (en) | 2011-06-08 |
Family
ID=44097953
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009101135537A Pending CN102085912A (en) | 2009-12-03 | 2009-12-03 | Dishing magnetic suspension ring-wing aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102085912A (en) |
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102358424A (en) * | 2011-08-17 | 2012-02-22 | 梁锡球 | Flying saucer aircraft |
| CN102602538A (en) * | 2012-04-12 | 2012-07-25 | 北京工业大学 | Magnetic levitation self-driven double-spiral-wing flying saucer |
| WO2013056275A2 (en) * | 2011-10-12 | 2013-04-18 | Groenewald Felix Errol | Aircraft |
| CN103085975A (en) * | 2011-11-08 | 2013-05-08 | 王力丰 | Rotary transport flywheel of goods and control method thereof |
| CN104724287A (en) * | 2015-02-04 | 2015-06-24 | 李广成 | Saucer-shaped aircraft |
| CN105752330A (en) * | 2016-02-19 | 2016-07-13 | 张红艳 | Disk-like aircraft capable of adjusting flying attitude |
| CN106005412A (en) * | 2016-07-08 | 2016-10-12 | 夏建国 | Flying saucer type vertical take-off and landing high-speed electromagnetic airplane |
| CN106516127A (en) * | 2016-11-30 | 2017-03-22 | 中国直升机设计研究所 | Magnetic levitation rotor wing system and helicopter with same |
| CN106892106A (en) * | 2017-04-06 | 2017-06-27 | 重庆鸿动翼科技有限公司 | Electromagnetic Drive tandem wing aerodynamic vehicle |
| CN106892115A (en) * | 2017-04-01 | 2017-06-27 | 李宣南 | A kind of dish-shaped manned craft |
| CN107539480A (en) * | 2016-06-24 | 2018-01-05 | 丁广帅 | A kind of New Ring-like Type rotor |
| CN107985555A (en) * | 2017-11-13 | 2018-05-04 | 上海顺砾智能科技有限公司 | One kind is without the mute unmanned plane of wing formula |
| WO2019204493A1 (en) | 2018-04-17 | 2019-10-24 | The Maglev Aero Co. | Systems and methods for vertical takeoff and landing using magnetic levitation |
| CN111907732A (en) * | 2020-04-30 | 2020-11-10 | 蓝箭航天空间科技股份有限公司 | Space verification aircraft |
| CN112319812A (en) * | 2019-08-05 | 2021-02-05 | 李越标 | Magnetic suspension disk-shaped aircraft |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3997131A (en) * | 1973-12-12 | 1976-12-14 | Alberto Kling | Rotor means for an aircraft |
| EP0861777A1 (en) * | 1992-06-22 | 1998-09-02 | United Technologies Corporation | An integrated spline/cone seat subassembly |
| WO2001087707A1 (en) * | 2000-05-15 | 2001-11-22 | Sunlase, Inc. | Aircraft and hybrid with magnetic airfoil suspension and drive |
| US20030122033A1 (en) * | 2000-05-17 | 2003-07-03 | Hengwei Gao | Ring-shaped wing helicopter |
| CN1647998A (en) * | 2003-07-30 | 2005-08-03 | C.R.F.阿西安尼顾问公司 | Flying machine |
| CN101323375A (en) * | 2007-06-11 | 2008-12-17 | 李本现 | Safe green aerocraft 'flying saucer' |
| CN201284014Y (en) * | 2008-08-25 | 2009-08-05 | 王人庆 | Discs type helicopters |
-
2009
- 2009-12-03 CN CN2009101135537A patent/CN102085912A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3997131A (en) * | 1973-12-12 | 1976-12-14 | Alberto Kling | Rotor means for an aircraft |
| EP0861777A1 (en) * | 1992-06-22 | 1998-09-02 | United Technologies Corporation | An integrated spline/cone seat subassembly |
| WO2001087707A1 (en) * | 2000-05-15 | 2001-11-22 | Sunlase, Inc. | Aircraft and hybrid with magnetic airfoil suspension and drive |
| US20030122033A1 (en) * | 2000-05-17 | 2003-07-03 | Hengwei Gao | Ring-shaped wing helicopter |
| CN1647998A (en) * | 2003-07-30 | 2005-08-03 | C.R.F.阿西安尼顾问公司 | Flying machine |
| CN101323375A (en) * | 2007-06-11 | 2008-12-17 | 李本现 | Safe green aerocraft 'flying saucer' |
| CN201284014Y (en) * | 2008-08-25 | 2009-08-05 | 王人庆 | Discs type helicopters |
Cited By (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102358424A (en) * | 2011-08-17 | 2012-02-22 | 梁锡球 | Flying saucer aircraft |
| US9272779B2 (en) | 2011-10-12 | 2016-03-01 | Felix Errol Groenewald | Aircraft with pivoting rotor mast |
| WO2013056275A2 (en) * | 2011-10-12 | 2013-04-18 | Groenewald Felix Errol | Aircraft |
| WO2013056275A3 (en) * | 2011-10-12 | 2013-05-16 | Groenewald Felix Errol | Aircraft |
| CN103085975A (en) * | 2011-11-08 | 2013-05-08 | 王力丰 | Rotary transport flywheel of goods and control method thereof |
| CN102602538A (en) * | 2012-04-12 | 2012-07-25 | 北京工业大学 | Magnetic levitation self-driven double-spiral-wing flying saucer |
| CN102602538B (en) * | 2012-04-12 | 2014-12-31 | 北京工业大学 | Magnetic levitation self-driven double-spiral-wing flying saucer |
| CN104724287A (en) * | 2015-02-04 | 2015-06-24 | 李广成 | Saucer-shaped aircraft |
| CN105752330A (en) * | 2016-02-19 | 2016-07-13 | 张红艳 | Disk-like aircraft capable of adjusting flying attitude |
| CN107539480A (en) * | 2016-06-24 | 2018-01-05 | 丁广帅 | A kind of New Ring-like Type rotor |
| CN106005412A (en) * | 2016-07-08 | 2016-10-12 | 夏建国 | Flying saucer type vertical take-off and landing high-speed electromagnetic airplane |
| CN106516127A (en) * | 2016-11-30 | 2017-03-22 | 中国直升机设计研究所 | Magnetic levitation rotor wing system and helicopter with same |
| CN106516127B (en) * | 2016-11-30 | 2019-01-22 | 中国直升机设计研究所 | A kind of magnetic suspension rotor system and the helicopter with it |
| CN106892115A (en) * | 2017-04-01 | 2017-06-27 | 李宣南 | A kind of dish-shaped manned craft |
| CN106892106A (en) * | 2017-04-06 | 2017-06-27 | 重庆鸿动翼科技有限公司 | Electromagnetic Drive tandem wing aerodynamic vehicle |
| CN107985555A (en) * | 2017-11-13 | 2018-05-04 | 上海顺砾智能科技有限公司 | One kind is without the mute unmanned plane of wing formula |
| WO2019204493A1 (en) | 2018-04-17 | 2019-10-24 | The Maglev Aero Co. | Systems and methods for vertical takeoff and landing using magnetic levitation |
| EP3781790A4 (en) * | 2018-04-17 | 2022-01-19 | The Maglev Aero Co. | VERTICAL TAKE-OFF AND LANDING SYSTEMS AND METHODS USING MAGNETIC LEVITATION |
| US11292592B2 (en) | 2018-04-17 | 2022-04-05 | Maglev Aero Inc. | Systems and methods for independent pitch control of rotor blades of rotor assembly to achieve directional control |
| US11541998B2 (en) | 2018-04-17 | 2023-01-03 | Maglev Aero Inc. | Systems and methods for controlling lift using contra-rotating rotors |
| US11541997B2 (en) | 2018-04-17 | 2023-01-03 | Maglev Aero Inc. | Systems and methods for improved rotor assembly for use with a stator |
| US11591080B2 (en) | 2018-04-17 | 2023-02-28 | Maglev Aero Inc. | Systems and methods for drive control of a magnetically levitated rotor |
| US11958596B2 (en) | 2018-04-17 | 2024-04-16 | Maglev Aero Inc. | Systems and methods for reducing noise based on effective rotor area relative to a center of rotation |
| EP4434894A3 (en) * | 2018-04-17 | 2025-01-15 | The Maglev Aero Co. | Systems and methods for vertical takeoff and landing using magnetic levitation |
| CN112319812A (en) * | 2019-08-05 | 2021-02-05 | 李越标 | Magnetic suspension disk-shaped aircraft |
| CN111907732A (en) * | 2020-04-30 | 2020-11-10 | 蓝箭航天空间科技股份有限公司 | Space verification aircraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102085912A (en) | Dishing magnetic suspension ring-wing aircraft | |
| CA2979607C (en) | Wing extension winglets for tiltrotor aircraft | |
| RU180474U1 (en) | Vertical takeoff and landing airplane | |
| CN202728574U (en) | Composite aircraft with fixed wing and electric multiple propellers combined and with helicopter function | |
| CN103587683A (en) | Small-sized aircraft with tiltable rotor wings | |
| CN106628162A (en) | Composite unmanned aerial vehicle | |
| CN110001949A (en) | A kind of compound rotation unmanned helicopter of close coupled type | |
| CN206704537U (en) | A kind of fixed-wing unmanned plane | |
| CN113044212B (en) | Medium-sized tilt rotor unmanned aerial vehicle | |
| CN202728571U (en) | Private aircraft | |
| CN204197290U (en) | A kind of novel tiltrotor aircraft | |
| CN205469821U (en) | Perpendicular or short take off and landing fixed wing aircraft | |
| CN107878747A (en) | A kind of Fixed Wing AirVehicle of VTOL | |
| CN108382578B (en) | High-speed hybrid layout vertical take-off and landing aircraft | |
| CN112027073A (en) | Combined type tilting wing longitudinal rotation double-rotor aircraft | |
| CN212951108U (en) | Variable-diameter unmanned tilt rotorcraft | |
| CN206288230U (en) | Full electricity autogyro | |
| CN211281472U (en) | Duct tail sitting posture VTOL unmanned aerial vehicle | |
| CN211253017U (en) | Unmanned aerial vehicle with tandem wings capable of vertically taking off and landing | |
| CN111532426A (en) | Aircraft with V-shaped empennage and multiple rotors in vertical take-off and landing layout | |
| CN207523932U (en) | Tandem wing tilting rotor wing unmanned aerial vehicle | |
| CN110861770A (en) | Unmanned rotation gyroplane | |
| CN213083496U (en) | Aircraft with wings capable of vertically taking off and landing | |
| CN109263922A (en) | A kind of rotatable aircraft of motor | |
| CN109263903A (en) | A kind of multifunction aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| DD01 | Delivery of document by public notice |
Addressee: Fan Lei Document name: Notification of Publication of the Application for Invention |
|
| DD01 | Delivery of document by public notice |
Addressee: Fan Lei Document name: Notification of before Expiration of Request of Examination as to Substance |
|
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| DD01 | Delivery of document by public notice |
Addressee: Fan Lei Document name: Notification of Passing Examination on Formalities |
|
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20110608 |
|
| RJ01 | Rejection of invention patent application after publication |