FR1442684A - Rotor Head Improvements for Rotary Wing Aircraft - Google Patents
Rotor Head Improvements for Rotary Wing AircraftInfo
- Publication number
- FR1442684A FR1442684A FR22851A FR22851A FR1442684A FR 1442684 A FR1442684 A FR 1442684A FR 22851 A FR22851 A FR 22851A FR 22851 A FR22851 A FR 22851A FR 1442684 A FR1442684 A FR 1442684A
- Authority
- FR
- France
- Prior art keywords
- wing aircraft
- rotary wing
- rotor head
- head improvements
- 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
- B64C27/32—Rotors
- B64C27/33—Rotors having flexing arms
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR22851A FR1442684A (en) | 1965-06-30 | 1965-06-30 | Rotor Head Improvements for Rotary Wing Aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR22851A FR1442684A (en) | 1965-06-30 | 1965-06-30 | Rotor Head Improvements for Rotary Wing Aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1442684A true FR1442684A (en) | 1966-06-17 |
Family
ID=8583410
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR22851A Expired FR1442684A (en) | 1965-06-30 | 1965-06-30 | Rotor Head Improvements for Rotary Wing Aircraft |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1442684A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3695779A (en) * | 1970-05-18 | 1972-10-03 | Lockheed Aircraft Corp | Rotor system including a blade retention member |
US3807897A (en) * | 1970-06-11 | 1974-04-30 | Exploi De Materials Et Moteurt | Rigid hubs for variable-pitch propellers and gas turbines |
FR2402579A1 (en) * | 1977-09-07 | 1979-04-06 | Westland Aircraft Ltd | HELICOPTER ROTOR, AND HELICOPTER WITH SUCH ROTOR |
US4564336A (en) * | 1982-03-15 | 1986-01-14 | Hughes Helicopters, Inc. | Low drag, bearingless rotor head for helicopters |
US4645423A (en) * | 1985-07-29 | 1987-02-24 | United Technologies Corporation | Tension/compression rod arrangement for damping helicopter rotor blade oscillations |
US4874292A (en) * | 1988-11-18 | 1989-10-17 | The United States Of America As Represented By The Secretary Of The Army | Apparatus for damping helicopter rotor blade oscillations |
US4915585A (en) * | 1988-04-29 | 1990-04-10 | Aerospatiale Societe National Industrielle | Rotary-wing aircraft rotor head having resilient-return interblade ties with built-in damping |
-
1965
- 1965-06-30 FR FR22851A patent/FR1442684A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3695779A (en) * | 1970-05-18 | 1972-10-03 | Lockheed Aircraft Corp | Rotor system including a blade retention member |
US3807897A (en) * | 1970-06-11 | 1974-04-30 | Exploi De Materials Et Moteurt | Rigid hubs for variable-pitch propellers and gas turbines |
FR2402579A1 (en) * | 1977-09-07 | 1979-04-06 | Westland Aircraft Ltd | HELICOPTER ROTOR, AND HELICOPTER WITH SUCH ROTOR |
FR2402578A1 (en) * | 1977-09-07 | 1979-04-06 | Westland Aircraft Ltd | HELICOPTER ROTOR, AND HELICOPTER WITH SUCH ROTOR |
US4564336A (en) * | 1982-03-15 | 1986-01-14 | Hughes Helicopters, Inc. | Low drag, bearingless rotor head for helicopters |
US4645423A (en) * | 1985-07-29 | 1987-02-24 | United Technologies Corporation | Tension/compression rod arrangement for damping helicopter rotor blade oscillations |
US4915585A (en) * | 1988-04-29 | 1990-04-10 | Aerospatiale Societe National Industrielle | Rotary-wing aircraft rotor head having resilient-return interblade ties with built-in damping |
US4874292A (en) * | 1988-11-18 | 1989-10-17 | The United States Of America As Represented By The Secretary Of The Army | Apparatus for damping helicopter rotor blade oscillations |
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