FR1044232A - Device for automatic variation of the general pitch for mechanical helicopter known as oscillating hub - Google Patents
Device for automatic variation of the general pitch for mechanical helicopter known as oscillating hubInfo
- Publication number
- FR1044232A FR1044232A FR1044232DA FR1044232A FR 1044232 A FR1044232 A FR 1044232A FR 1044232D A FR1044232D A FR 1044232DA FR 1044232 A FR1044232 A FR 1044232A
- Authority
- FR
- France
- Prior art keywords
- mechanical
- automatic variation
- general pitch
- oscillating hub
- 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
- B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1044232T | 1951-10-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1044232A true FR1044232A (en) | 1953-11-16 |
Family
ID=9591020
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1044232D Expired FR1044232A (en) | 1951-10-27 | 1951-10-27 | Device for automatic variation of the general pitch for mechanical helicopter known as oscillating hub |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1044232A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3999886A (en) * | 1974-10-10 | 1976-12-28 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Hingeless helicopter rotor with improved stability |
US4461611A (en) * | 1982-05-20 | 1984-07-24 | United Technologies Corporation | Helicopter rotor with blade trailing edge tabs responsive to control system loading |
-
1951
- 1951-10-27 FR FR1044232D patent/FR1044232A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3999886A (en) * | 1974-10-10 | 1976-12-28 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Hingeless helicopter rotor with improved stability |
US4461611A (en) * | 1982-05-20 | 1984-07-24 | United Technologies Corporation | Helicopter rotor with blade trailing edge tabs responsive to control system loading |
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