GB606305A - Improvements in or relating to rotary wing aircraft - Google Patents
Improvements in or relating to rotary wing aircraftInfo
- Publication number
- GB606305A GB606305A GB109346A GB109346A GB606305A GB 606305 A GB606305 A GB 606305A GB 109346 A GB109346 A GB 109346A GB 109346 A GB109346 A GB 109346A GB 606305 A GB606305 A GB 606305A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing aircraft
- blade
- flapping
- rotary wing
- relating
- 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
- B64C27/32—Rotors
- B64C27/37—Rotors having articulated joints
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Transmission Devices (AREA)
Abstract
606,305. Rotary wing aircraft. FAIREY AVIATION CO., Ltd., and BENNETT, J. A. J. Jan. 11, 1946, No. 1093. [Class 4] The dynamic stability of a rotating wing aircraft is improved at the expense of the static stability by disposing the flapping hinge 5 of each blade 3 on the opposite side of a plane through the rotor hub axis and parallel to the flapping axis from the blade 3. As shown, the flapping hinges 5 are formed in lugs 11 secured to the triangular rotor head 1, the usual drag pivot 4 being provided between the drag link 2 and the blade 3.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB109346A GB606305A (en) | 1946-01-11 | 1946-01-11 | Improvements in or relating to rotary wing aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB109346A GB606305A (en) | 1946-01-11 | 1946-01-11 | Improvements in or relating to rotary wing aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB606305A true GB606305A (en) | 1948-08-11 |
Family
ID=9716028
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB109346A Expired GB606305A (en) | 1946-01-11 | 1946-01-11 | Improvements in or relating to rotary wing aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB606305A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2678785A (en) * | 1952-04-17 | 1954-05-18 | Northrop Aircraft Inc | Rotating blade speed brake |
EP0039138A2 (en) * | 1980-04-14 | 1981-11-04 | WESTLAND plc | Improvements in or relating to aerodynamic rotors |
CN107140202A (en) * | 2017-05-12 | 2017-09-08 | 上海寅翅智能科技有限公司 | A kind of centrifugal flapping hinge rotor head |
-
1946
- 1946-01-11 GB GB109346A patent/GB606305A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2678785A (en) * | 1952-04-17 | 1954-05-18 | Northrop Aircraft Inc | Rotating blade speed brake |
EP0039138A2 (en) * | 1980-04-14 | 1981-11-04 | WESTLAND plc | Improvements in or relating to aerodynamic rotors |
EP0039138A3 (en) * | 1980-04-14 | 1982-11-10 | WESTLAND plc | Improvements in or relating to aerodynamic rotors |
CN107140202A (en) * | 2017-05-12 | 2017-09-08 | 上海寅翅智能科技有限公司 | A kind of centrifugal flapping hinge rotor head |
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