FR1213809A - Moyeu pour rotor d'hélicoptère rapide - Google Patents
Moyeu pour rotor d'hélicoptère rapideInfo
- Publication number
- FR1213809A FR1213809A FR1213809DA FR1213809A FR 1213809 A FR1213809 A FR 1213809A FR 1213809D A FR1213809D A FR 1213809DA FR 1213809 A FR1213809 A FR 1213809A
- Authority
- FR
- France
- Prior art keywords
- hub
- helicopter rotor
- fast
- fast helicopter
- rotor
- 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
- B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
- B64C27/59—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical
- B64C27/615—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including flaps mounted on blades
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/30—Wing lift efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1213809T | 1958-10-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1213809A true FR1213809A (fr) | 1960-04-04 |
Family
ID=9676702
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1213809D Expired FR1213809A (fr) | 1958-10-29 | 1958-10-29 | Moyeu pour rotor d'hélicoptère rapide |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1213809A (fr) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3077934A (en) * | 1960-07-19 | 1963-02-19 | Kaman Aircraft Corp | Rotor control system for a helicopter |
US3129769A (en) * | 1962-09-21 | 1964-04-21 | Kaman Aircraft Corp | Fail safe device for servo flap controlled rotor blades |
US3134444A (en) * | 1961-08-23 | 1964-05-26 | Kaman Aircraft Corp | Aircraft rotor-propeller |
US4461611A (en) * | 1982-05-20 | 1984-07-24 | United Technologies Corporation | Helicopter rotor with blade trailing edge tabs responsive to control system loading |
-
1958
- 1958-10-29 FR FR1213809D patent/FR1213809A/fr not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3077934A (en) * | 1960-07-19 | 1963-02-19 | Kaman Aircraft Corp | Rotor control system for a helicopter |
US3134444A (en) * | 1961-08-23 | 1964-05-26 | Kaman Aircraft Corp | Aircraft rotor-propeller |
US3129769A (en) * | 1962-09-21 | 1964-04-21 | Kaman Aircraft Corp | Fail safe device for servo flap controlled rotor blades |
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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