WO2010006354A3 - Rotor drive for autogyros, and method for vertically starting an autogyro - Google Patents
Rotor drive for autogyros, and method for vertically starting an autogyro Download PDFInfo
- Publication number
- WO2010006354A3 WO2010006354A3 PCT/AT2009/000280 AT2009000280W WO2010006354A3 WO 2010006354 A3 WO2010006354 A3 WO 2010006354A3 AT 2009000280 W AT2009000280 W AT 2009000280W WO 2010006354 A3 WO2010006354 A3 WO 2010006354A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- rotor
- autogyros
- autogyro
- masses
- rotor drive
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/02—Gyroplanes
- B64C27/021—Rotor or rotor head construction
- B64C27/025—Rotor drives, in particular for taking off; Combination of autorotation rotors and driven rotors
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
- Preparation Of Clay, And Manufacture Of Mixtures Containing Clay Or Cement (AREA)
- Toys (AREA)
Abstract
A rotor drive for autogyros comprises a rotating main rotor system encompassing rotor blades (1, 2) and identical masses (3), the distance of which from an axis of rotation (5) can be modified in a synchronously controlled manner. A device (7, 13, 14) which is mounted on the main rotor head (26) in addition to the rotor blades (1, 2) and is used for moving the masses (3) by means of a motor allows the masses (3) to be moved from an outer position into an inner position during the start such that the rotor is accelerated.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT11092008A AT506694B1 (en) | 2008-07-17 | 2008-07-17 | ROTARY DRIVE FOR BEARING SCREWDRIVER AND METHOD FOR VERTICALLY STARTING A SCREWDRIVER |
ATA1109/2008 | 2008-07-17 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2010006354A2 WO2010006354A2 (en) | 2010-01-21 |
WO2010006354A3 true WO2010006354A3 (en) | 2010-03-11 |
Family
ID=41259964
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/AT2009/000280 WO2010006354A2 (en) | 2008-07-17 | 2009-07-16 | Rotor drive for autogyros, and method for vertically starting an autogyro |
Country Status (2)
Country | Link |
---|---|
AT (1) | AT506694B1 (en) |
WO (1) | WO2010006354A2 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102016002231B4 (en) | 2016-02-25 | 2021-10-07 | Ramin Assisi | Aircraft with actively operated swiveling rotors and passively operated main rotor |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE650648C (en) * | 1935-07-20 | 1937-09-29 | E H Claude Dornier Dr Ing | Jump starting part screwdriver |
FR1404752A (en) * | 1964-06-27 | 1965-07-02 | Device intended to improve the take-off performance of propeller-lift devices | |
DE1270408B (en) * | 1958-09-30 | 1968-06-12 | Bell Helicopter Corp | Damping device for the rotor of a helicopter with a semi-rigid blade connection |
US3814351A (en) * | 1972-12-06 | 1974-06-04 | United Aircraft Corp | Coaxial rotor yaw control |
-
2008
- 2008-07-17 AT AT11092008A patent/AT506694B1/en not_active IP Right Cessation
-
2009
- 2009-07-16 WO PCT/AT2009/000280 patent/WO2010006354A2/en active Application Filing
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE650648C (en) * | 1935-07-20 | 1937-09-29 | E H Claude Dornier Dr Ing | Jump starting part screwdriver |
DE1270408B (en) * | 1958-09-30 | 1968-06-12 | Bell Helicopter Corp | Damping device for the rotor of a helicopter with a semi-rigid blade connection |
FR1404752A (en) * | 1964-06-27 | 1965-07-02 | Device intended to improve the take-off performance of propeller-lift devices | |
US3814351A (en) * | 1972-12-06 | 1974-06-04 | United Aircraft Corp | Coaxial rotor yaw control |
Also Published As
Publication number | Publication date |
---|---|
WO2010006354A2 (en) | 2010-01-21 |
AT506694B1 (en) | 2009-11-15 |
AT506694A4 (en) | 2009-11-15 |
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