GB1041116A - Helicopter - Google Patents
HelicopterInfo
- Publication number
- GB1041116A GB1041116A GB1744764A GB1744764A GB1041116A GB 1041116 A GB1041116 A GB 1041116A GB 1744764 A GB1744764 A GB 1744764A GB 1744764 A GB1744764 A GB 1744764A GB 1041116 A GB1041116 A GB 1041116A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shafts
- april
- rotor
- engine
- helicopter
- 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.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/16—Drive of rotors by means, e.g. propellers, mounted on rotor blades
- B64C27/18—Drive of rotors by means, e.g. propellers, mounted on rotor blades the means being jet-reaction apparatus
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
1,041,116. Helicopters. ROLLS-ROYCE Ltd. April 20, 1965 [April 27, 1964], No. 17447/64. Heading B7W. A helicopter rotor comprises a pair of aligned shafts 13 attached directly or indirectly to each other and to the rotor head 11 and each supporting at its outer end a gas turbine jet propulsion engine 12. When the rotor is stationary the weight of each engine and shaft is supported by a tie member 15. Sleeves 14, capable of pitch adjustment are mounted on shafts 13. The shafts 13 may be mounted on drag hinges.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1744764A GB1041116A (en) | 1964-04-27 | 1964-04-27 | Helicopter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1744764A GB1041116A (en) | 1964-04-27 | 1964-04-27 | Helicopter |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1041116A true GB1041116A (en) | 1966-09-01 |
Family
ID=10095343
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1744764A Expired GB1041116A (en) | 1964-04-27 | 1964-04-27 | Helicopter |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1041116A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2007115465A1 (en) * | 2006-04-07 | 2007-10-18 | Qin Zhao | A novel helicopter |
WO2019191240A1 (en) | 2018-03-28 | 2019-10-03 | Dewalch Diversified Lp | Aircraft propulsion and torque mitigation technologies |
-
1964
- 1964-04-27 GB GB1744764A patent/GB1041116A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2007115465A1 (en) * | 2006-04-07 | 2007-10-18 | Qin Zhao | A novel helicopter |
WO2019191240A1 (en) | 2018-03-28 | 2019-10-03 | Dewalch Diversified Lp | Aircraft propulsion and torque mitigation technologies |
CN112424065A (en) * | 2018-03-28 | 2021-02-26 | 德瓦尔奇多元化有限责任合伙公司 | Aircraft propulsion and torque mitigation techniques |
EP3774532A4 (en) * | 2018-03-28 | 2021-12-29 | Thrust Drive LLC | Aircraft propulsion and torque mitigation technologies |
US11753155B2 (en) | 2018-03-28 | 2023-09-12 | Thrust Drive Llc | Aircraft propulsion and torque mitigation technologies |
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