FR796870A - Moyeu d'hélice, de voilure tournante, de ventilateur, de compresseur, etc. - Google Patents
Moyeu d'hélice, de voilure tournante, de ventilateur, de compresseur, etc.Info
- Publication number
- FR796870A FR796870A FR796870DA FR796870A FR 796870 A FR796870 A FR 796870A FR 796870D A FR796870D A FR 796870DA FR 796870 A FR796870 A FR 796870A
- Authority
- FR
- France
- Prior art keywords
- propeller
- hub
- compressor
- fan
- rotary wing
- 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
- B64C27/02—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)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR796870T | 1935-01-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR796870A true FR796870A (fr) | 1936-04-16 |
Family
ID=9235386
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR796870D Expired FR796870A (fr) | 1935-01-17 | 1935-01-17 | Moyeu d'hélice, de voilure tournante, de ventilateur, de compresseur, etc. |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR796870A (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2629452A (en) * | 1947-05-20 | 1953-02-24 | United Aircraft Corp | Helicopter rotor cyclic pitch control |
US2692650A (en) * | 1946-11-19 | 1954-10-26 | Autogiro Co Of America | Pitch control mechanism for rotor blades |
-
1935
- 1935-01-17 FR FR796870D patent/FR796870A/fr not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2692650A (en) * | 1946-11-19 | 1954-10-26 | Autogiro Co Of America | Pitch control mechanism for rotor blades |
US2629452A (en) * | 1947-05-20 | 1953-02-24 | United Aircraft Corp | Helicopter rotor cyclic pitch control |
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