CN102862680A - Spherically dished aircraft - Google Patents
Spherically dished aircraft Download PDFInfo
- Publication number
- CN102862680A CN102862680A CN2011101844653A CN201110184465A CN102862680A CN 102862680 A CN102862680 A CN 102862680A CN 2011101844653 A CN2011101844653 A CN 2011101844653A CN 201110184465 A CN201110184465 A CN 201110184465A CN 102862680 A CN102862680 A CN 102862680A
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- CN
- China
- Prior art keywords
- aircraft
- ring
- power
- type disc
- main cabin
- 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
- 230000033001 locomotion Effects 0.000 claims description 5
- 238000000354 decomposition reaction Methods 0.000 claims description 2
- 230000003993 interaction Effects 0.000 claims description 2
- BSYNRYMUTXBXSQ-UHFFFAOYSA-N Aspirin Chemical compound CC(=O)OC1=CC=CC=C1C(O)=O BSYNRYMUTXBXSQ-UHFFFAOYSA-N 0.000 claims 2
- 238000005339 levitation Methods 0.000 abstract description 2
- 230000000630 rising effect Effects 0.000 abstract 1
- 230000010006 flight Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000009987 spinning Methods 0.000 description 1
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/001—Flying saucers
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The invention relates to a spherically dished aircraft which is different with levitation flight principles of all the spherically dished aircraft and is capable of rapidly and vertically levitating and flying. The spherically dished aircraft is composed of a vertical power system apparatus, a lateral power system apparatus, an annular dish disc, a main cabin, an upper annular track, an upper wheel, a fixed diversion apparatus, a lower annular track, a lower wheel, an undercarriage and the like. The spherically dished aircraft is capable of vertically rotating and levitating with high speed, suspending, landing, and laterally and rapidly adjusting the direction. The spherically dished aircraft has the advantages of high speed, safety, low requirements for the rising and landing place conditions and the like.
Description
Technical field
Ball dish shape aviation aircraft is a kind of aviation aircraft that is different from all aviation aircraft lift-off flight theories energy rapid vertical lift-off flights.
Background technology
Existing aviation aircraft landing conditional request is high, turns in the air slowly, several aircraft lift-off speed that can vertically go up to the air is arranged slowly and has potential safety hazard.Although there are a kind of fireworks that are plate-spinning to only have one with vertical (level) spout of certain angle to be arranged, just can the High Rotation Speed lift-off.Ball dish shape aviation aircraft has three to have with vertical (level) that the power system device of certain angle, transverse shifting power system device make the vertical High Rotation Speed lift-off of aircraft, suspend, landing, 360 ° of laterally fast tunings flights.Even aircraft security is landed.
Summary of the invention
A kind of ball dish shape aviation aircraft: can go up to the air by vertical High Rotation Speed, 360 ° of laterally fast tuning flights can be in multi-field application such as civil aviaton, military affairs, space flight.Mainly by Longitudinal system and device, lateral dynamics system and device, ring-type disc, main cabin, upper circular orbit, on take turns, decide steering hardware, lower circular orbit, lower whorl, alighting gear etc. and form (see photo).
Description of drawings
Fig. 1 is front view.Fig. 2 is birds-eye view.Fig. 3 is right elevation.Fig. 4 is the A-A cutaway view of Fig. 1.
(1) be the power system device that aircraft vertically goes up to the air, suspends, lands, power system device (1) has certain angle with vertical (level) direction, and the power decomposition of its generation is the power of vertical direction and the power of horizontal direction.Aircraft hoists, and the weight of ring-type disc (3) is supported by lower circular orbit (9) by a plurality of lower whorls (8) after the front landing.During power system device (1) initialization, horizontal force makes ring-type disc (3) around main cabin (4) rotation, when power surpasses certain numerical value, vertical power makes ring-type disc lift-off and its lift-off power is applied to by upper circular orbit (5) and takes turns (6) upper main cabins of drive (4) on a plurality of and go up to the air together, horizontal force makes ring-type disc (3) around main cabin (4) rotation, the lift-off of aircraft High Rotation Speed.Application force is zero between the rear lower whorl (8) of lift-off and lower circular orbit (9).Provide power by the power system device that is contained in top, main cabin (2) during the aircraft transverse shifting.(7) be the steering hardware of deciding of aircraft, lower circular orbit (9) interaction force on it and the ring-type disc makes main cabin
(4) hand of rotation is opposite with ring-type disc hand of rotation, and making the circular movement in main cabin (4) is that quiescence and 360 ° of tunings are determined the aircraft flight direction with respect to ground.Main cabin (4) by drive, the zone such as manned, loading forms.(10) be alighting gear.
The specific embodiment
Ball dish shape aviation aircraft is the simple a kind of aircraft of lift-off flight theory, and its target can easily be implemented and realize to present scientific and technological level.The specific embodiment is: upper circular orbit (5), on take turns (6), lower whorl (8), lower circular orbit (9) adopts the train wheel track structure, make ring-type disc (3) around main cabin (4) rotation, also can adopt magnetic levitation technology to realize its purpose.Because the power that produces when having three power system devices (1) of certain angle to work with vertical (level) direction makes ring-type disc (3) High Rotation Speed, power point is distributed on the path of motion of its circular movement incessantly, solve the difficult problem of dynamic equilibrium control, just can realize aircraft liter, the purpose that suspends, falls so the power that only need control three power system devices (1) by the spacing wireless remote control in the driving zone of main cabin (4) increases synchronously, decides, subtracts.Power system device (1) adopts also available jet engine of propeller turbine.Power system device (2) only needs burden horizontal flight power, can make aircraft easily realize supersonic flight, adopts jet engine.Decide steering hardware (7) and lower circular orbit (9) and adopt the rack-and-gear mode also can adopt friction mode, determine aircraft flight direction purpose (can make aircraft moment toward opposite sense flight) with respect to ground as quiescence and 360 ° of tunings to reach the circular movement of realizing making main cabin (4).
Claims (5)
1. ball dish shape aviation aircraft is characterized as: a large section globoid (1) and around the ring-type disc (3) of its rotation.
2. (1) on the ring-type disc is the power system device that aircraft vertically goes up to the air, suspends, lands, be characterized as: power system device (1) has certain angle with vertical (level) direction, and the power decomposition of its generation is the power of vertical direction and the power of horizontal direction.Vertical power makes the lift-off of ring-type disc and its lift-off power is applied to by upper circular orbit (5) takes turns (6) upper main cabins of drive (4) lift-off.Horizontal force makes ring-type disc (3) around main cabin (4) rotation.
3. (2) are the power system devices of aircraft transverse shifting.
4. (7) are the steering hardwares of deciding of aircraft, be characterized as: device (7) makes main cabin (4) hand of rotation opposite with ring-type disc hand of rotation with lower circular orbit (9) interaction force on the ring-type disc, and making the circular movement in main cabin (4) is that quiescence and 360 ° of tunings of energy be determined the aircraft flight direction with respect to ground.
5. after aircraft hoisted front landing, the ring-type disc was supported by lower circular orbit (9) by the lower whorl (8) on main cabin (4).
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011101844653A CN102862680A (en) | 2011-07-04 | 2011-07-04 | Spherically dished aircraft |
| PCT/CN2012/000353 WO2013004070A1 (en) | 2011-07-04 | 2012-03-21 | Spherical saucer-shaped aviation aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011101844653A CN102862680A (en) | 2011-07-04 | 2011-07-04 | Spherically dished aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102862680A true CN102862680A (en) | 2013-01-09 |
Family
ID=47436475
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011101844653A Pending CN102862680A (en) | 2011-07-04 | 2011-07-04 | Spherically dished aircraft |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN102862680A (en) |
| WO (1) | WO2013004070A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105109686A (en) * | 2015-09-15 | 2015-12-02 | 长沙冠创控制科技有限公司 | Saucer-shaped aircraft and autonomous flight system |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2547156C1 (en) * | 2014-03-08 | 2015-04-10 | Эдуард Иванович Соловьев | Aircraft named after eduard solovyov |
| CN113581475A (en) * | 2021-08-31 | 2021-11-02 | 王智强 | Circular disc wing solar electric airplane |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN85103564A (en) * | 1985-05-08 | 1986-11-05 | 韩冬青 | Plate-like craft |
| US4807830A (en) * | 1986-12-15 | 1989-02-28 | Horton Paul F | Aircraft with magnetically coupled annulus |
| US5072892A (en) * | 1989-12-01 | 1991-12-17 | Carrington Alfred C | Aerodynamic device |
| CN1231978A (en) * | 1998-08-03 | 1999-10-20 | 刘辉 | Dish shaped aircraft |
| CN2734621Y (en) * | 2004-04-18 | 2005-10-19 | 张志坚 | Dish type flight device |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3946970A (en) * | 1974-12-16 | 1976-03-30 | Blankenship Ben F | Gyroscopically stabilized, vertical takeoff and landing aircraft |
| CN2210151Y (en) * | 1994-05-19 | 1995-10-18 | 张梦说 | Flying disc for aviation |
| CN1433930A (en) * | 2003-01-13 | 2003-08-06 | 于明华 | Disk shape aerobat |
| CN1830724A (en) * | 2006-04-20 | 2006-09-13 | 赵根 | Self-rotating stable type aircraft |
| CN101323375A (en) * | 2007-06-11 | 2008-12-17 | 李本现 | Safe green aerocraft 'flying saucer' |
| CN101927826A (en) * | 2010-05-10 | 2010-12-29 | 李文奇 | Rotor wing disk-shaped aviation aircraft |
-
2011
- 2011-07-04 CN CN2011101844653A patent/CN102862680A/en active Pending
-
2012
- 2012-03-21 WO PCT/CN2012/000353 patent/WO2013004070A1/en active Application Filing
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN85103564A (en) * | 1985-05-08 | 1986-11-05 | 韩冬青 | Plate-like craft |
| US4807830A (en) * | 1986-12-15 | 1989-02-28 | Horton Paul F | Aircraft with magnetically coupled annulus |
| US5072892A (en) * | 1989-12-01 | 1991-12-17 | Carrington Alfred C | Aerodynamic device |
| CN1231978A (en) * | 1998-08-03 | 1999-10-20 | 刘辉 | Dish shaped aircraft |
| CN2734621Y (en) * | 2004-04-18 | 2005-10-19 | 张志坚 | Dish type flight device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105109686A (en) * | 2015-09-15 | 2015-12-02 | 长沙冠创控制科技有限公司 | Saucer-shaped aircraft and autonomous flight system |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2013004070A1 (en) | 2013-01-10 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20130109 |