WO2001021483A1 - Turbo rim for aircraft wheels - Google Patents
Turbo rim for aircraft wheels Download PDFInfo
- Publication number
- WO2001021483A1 WO2001021483A1 PCT/IL2000/000530 IL0000530W WO0121483A1 WO 2001021483 A1 WO2001021483 A1 WO 2001021483A1 IL 0000530 W IL0000530 W IL 0000530W WO 0121483 A1 WO0121483 A1 WO 0121483A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- wind
- turbo
- aircraft
- wheel
- landing
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/40—Alighting gear characterised by elements which contact the ground or similar surface the elements being rotated before touch-down
Definitions
- My invention relates to aircrafts that land on their wheels, while running along the runway. This is in contrast to aircraft that land vertically - e.g. helicopters. Background Art
- the wind turbo will be turned by the power of the wind that is in the opposite direction of landing, and turn the wheel that is attached, in direction and speed of the landing aircraft on the runway.
- turbo wind which I suggest above, be attached to the rim of the aircraft wheels, therefore the name of my invention is:
- Fig.6 Aircraft wheel A. Wind turbo inner side B-1 and Wind Turbo out side B-2, attached to the two sides of the wheel A. Wheel carrier arm D.
- the angle of the blades on wind turbo B-2 on the one side of the wheel will be the opposite direction of the blades on wind turbo B-1 on the other side of the wheel, in order to use the both sides of the wind power R to turn the wheel forward S-l, in the direction of landing.
- the wind turbo B-1 that will be attached on the inner side of the wheel, that is on the side of the wheel carrier arm D should be made of two parts, this will make the assembly and dismantling easier.
- the diameter of the wind turbo should not be bigger than the rim it is attached to, in order not to be damaged in case of flat tyre.
- the two wind collectors the upper one and the lower one, as one unit, for the singles or the doubles wind collectors.
- the lower wind collectors E, and G will not be lower than the rim of the wheel, not to be damaged in case of flat tyre.
- the purpose of the wind collector is to focus and direct the wind, enabling to make smaller the wind turbo and blades.
- Wind turbo will be different size and shape, with different number of blades, with vertical blades to the wheel axis, horizontal or different angles.
- the wind turbo and the wind collector will be made of materials that are used in the aircraft industry.
- the material can be metal, mixing metal or other material that are not metal.
- the material has to be strong and light, heat and corrosion resistant.
- the wind turbo and wind collector will be attached to the right place, by screws or other ways that are used in the aircraft industry. It is clear that the aircrafts producer has to be helped by air tunnel, for tasting and fitting the right wind turbo and wind collector to the different aircraft. He can use all the parts that I suggest above or just part of it, to prefer wind turbo on one side of the wheel or both sides, with wind collectors or without them, everything by the need.
- the mission is to turn the aircraft wheels, by the wind power, in the direction and speed of the running runway underneath while landing.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Wind Motors (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IL132007 | 1999-09-23 | ||
IL13200799 | 1999-09-23 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2001021483A1 true WO2001021483A1 (en) | 2001-03-29 |
WO2001021483A8 WO2001021483A8 (en) | 2001-07-12 |
Family
ID=11073267
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/IL2000/000530 WO2001021483A1 (en) | 1999-09-23 | 2000-09-05 | Turbo rim for aircraft wheels |
Country Status (1)
Country | Link |
---|---|
WO (1) | WO2001021483A1 (en) |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2370316A (en) * | 1942-11-26 | 1945-02-27 | Briggs Mfg Co | Airplane wheel |
US2404018A (en) * | 1944-03-23 | 1946-07-16 | Bernard E Yaggy | Airplane landing gear |
US2408963A (en) * | 1943-06-14 | 1946-10-08 | Leslie L Westcamp | Aircraft landing wheel rotator |
US4383665A (en) * | 1976-04-06 | 1983-05-17 | Maclean Ewen M | Wind-driven rotating aircraft landing wheels |
US4615498A (en) * | 1983-12-15 | 1986-10-07 | Tsurunosuke Ochiai | Wheel and tire for aircraft |
US4732350A (en) * | 1985-11-07 | 1988-03-22 | Lamont John S | Aircraft wheel rotation apparatus |
US5104063A (en) * | 1990-04-27 | 1992-04-14 | Hartley James M | Aircraft landing gear prerotation system |
-
2000
- 2000-09-05 WO PCT/IL2000/000530 patent/WO2001021483A1/en active Application Filing
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2370316A (en) * | 1942-11-26 | 1945-02-27 | Briggs Mfg Co | Airplane wheel |
US2408963A (en) * | 1943-06-14 | 1946-10-08 | Leslie L Westcamp | Aircraft landing wheel rotator |
US2404018A (en) * | 1944-03-23 | 1946-07-16 | Bernard E Yaggy | Airplane landing gear |
US4383665A (en) * | 1976-04-06 | 1983-05-17 | Maclean Ewen M | Wind-driven rotating aircraft landing wheels |
US4615498A (en) * | 1983-12-15 | 1986-10-07 | Tsurunosuke Ochiai | Wheel and tire for aircraft |
US4732350A (en) * | 1985-11-07 | 1988-03-22 | Lamont John S | Aircraft wheel rotation apparatus |
US5104063A (en) * | 1990-04-27 | 1992-04-14 | Hartley James M | Aircraft landing gear prerotation system |
Also Published As
Publication number | Publication date |
---|---|
WO2001021483A8 (en) | 2001-07-12 |
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