UA79259U - Helicopter rotor - Google Patents
Helicopter rotorInfo
- Publication number
- UA79259U UA79259U UAU201302092U UAU201302092U UA79259U UA 79259 U UA79259 U UA 79259U UA U201302092 U UAU201302092 U UA U201302092U UA U201302092 U UAU201302092 U UA U201302092U UA 79259 U UA79259 U UA 79259U
- Authority
- UA
- Ukraine
- Prior art keywords
- helicopter rotor
- blades
- blade
- possibility
- axis
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
-
- 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
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/467—Aerodynamic features
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Toys (AREA)
Abstract
A helicopter rotor comprises a vertical shaft for connecting with an engine, on which at least two blades are horizontally fastened and directed to opposite sides relative to the axis of shaft with possibility of their synchronous rotation relative to the horizontal plane as well as a screw tilting control mechanism, furthermore each blade is equipped with at least one adjustable wing mounted from the side of lower surface of the blade and perpendicularly thereto with possibility of its turning in vertical plane and a control mechanism of their synchronous rotation, and the adjustable wings are mounted on the blades at the same distance from the axis of vertical shaft of the helicopter rotor.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
UAU201302092U UA79259U (en) | 2013-02-19 | 2013-02-19 | Helicopter rotor |
PCT/UA2013/000045 WO2014129997A1 (en) | 2013-02-19 | 2013-04-29 | Helicopter rotor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
UAU201302092U UA79259U (en) | 2013-02-19 | 2013-02-19 | Helicopter rotor |
Publications (1)
Publication Number | Publication Date |
---|---|
UA79259U true UA79259U (en) | 2013-04-10 |
Family
ID=51391639
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UAU201302092U UA79259U (en) | 2013-02-19 | 2013-02-19 | Helicopter rotor |
Country Status (2)
Country | Link |
---|---|
UA (1) | UA79259U (en) |
WO (1) | WO2014129997A1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB201409424D0 (en) * | 2014-05-28 | 2014-07-09 | Agustawestland Ltd | Device which is subject to fluid flow |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10347802B3 (en) * | 2003-10-10 | 2005-05-19 | Repower Systems Ag | Rotor blade for a wind turbine |
RU2265554C1 (en) * | 2004-04-01 | 2005-12-10 | Открытое акционерное общество "Камов" | Helicopter with coaxial main rotors |
RU2277498C1 (en) * | 2005-01-24 | 2006-06-10 | Государственное образовательное учреждение высшего профессионального образования "Орловский государственный технический университет" (ОрелГТУ) | Helicopter main rotor |
RU2369525C2 (en) * | 2008-01-15 | 2009-10-10 | Андрей Леонидович Шпади | Convertiplane |
-
2013
- 2013-02-19 UA UAU201302092U patent/UA79259U/en unknown
- 2013-04-29 WO PCT/UA2013/000045 patent/WO2014129997A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2014129997A1 (en) | 2014-08-28 |
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