FR2523071B1 - Rotor d'helicoptere - Google Patents
Rotor d'helicoptereInfo
- Publication number
- FR2523071B1 FR2523071B1 FR8303900A FR8303900A FR2523071B1 FR 2523071 B1 FR2523071 B1 FR 2523071B1 FR 8303900 A FR8303900 A FR 8303900A FR 8303900 A FR8303900 A FR 8303900A FR 2523071 B1 FR2523071 B1 FR 2523071B1
- Authority
- FR
- France
- Prior art keywords
- helicopter rotor
- 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
- B64C27/32—Rotors
- B64C27/322—Blade travel limiting devices, e.g. droop stops
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT67304/82A IT1155133B (it) | 1982-03-11 | 1982-03-11 | Rotore per elicotteri |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2523071A1 FR2523071A1 (fr) | 1983-09-16 |
FR2523071B1 true FR2523071B1 (fr) | 1985-12-06 |
Family
ID=11301296
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8303900A Expired FR2523071B1 (fr) | 1982-03-11 | 1983-03-09 | Rotor d'helicoptere |
Country Status (5)
Country | Link |
---|---|
US (1) | US4551067A (fr) |
DE (1) | DE3308073A1 (fr) |
FR (1) | FR2523071B1 (fr) |
GB (1) | GB2116507B (fr) |
IT (1) | IT1155133B (fr) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT1159375B (it) * | 1983-03-15 | 1987-02-25 | Agusta Aeronaut Costr | Rotore per elicotteri |
FR2551723B1 (fr) * | 1983-09-08 | 1985-12-13 | Aerospatiale | Dispositif a butees escamotables pour limiter les battements des pales d'un rotor principal de giravion |
IT1182447B (it) * | 1985-02-19 | 1987-10-05 | Agusta Aeronaut Costr | Rotore per elicotteri |
IT1196801B (it) * | 1986-11-25 | 1988-11-25 | Agusta Aeronaut Costr | Rotore per elicotteri |
FR2648106B1 (fr) * | 1989-06-08 | 1991-09-27 | Aerospatiale | Dispositif de butees escamotables pour pales de rotors de giravions, et tete de rotor le comportant |
FR2750948B1 (fr) * | 1996-07-12 | 1998-10-30 | Eurocopter France | Dispositif de blocage, au moins en pas, des pales d'un rotor |
WO2010068194A1 (fr) | 2008-12-09 | 2010-06-17 | Sikorsky Aircraft Corporation | Butée d'avance pour système de rotor comprenant un amortisseur d'avance/de retard fluide élastomère |
FR3017855B1 (fr) * | 2014-02-21 | 2016-04-29 | Airbus Helicopters | Rotor pour giravion comportant un mecanisme de butee en battement, et giravion |
FR3020341B1 (fr) | 2014-04-24 | 2016-04-29 | Airbus Helicopters | Rotor comportant un mecanisme de butee en trainee, et aeronef |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH212105A (de) * | 1938-02-12 | 1940-10-31 | Flettner Anton | Hubschrauber mit paarweise ineinander kämmenden Rotoren. |
GB673113A (en) * | 1949-10-03 | 1952-06-04 | John Brown & Company Ltd | Improvements in or relating to mountings for blades of wind motors or of propellers or of helicopter rotors |
US2614640A (en) * | 1951-02-01 | 1952-10-21 | United Aircraft Corp | Rotor blade support |
US2719593A (en) * | 1953-03-05 | 1955-10-04 | United Aircraft Corp | Combined anti-flapping and droop stop |
US3533713A (en) * | 1968-04-01 | 1970-10-13 | Lockheed Aircraft Corp | Rotor locking device |
US3853426A (en) * | 1972-09-05 | 1974-12-10 | United Aircraft Corp | Elastomeric helicopter rotor head with dynamic and static blade coning and droop stops |
DE2452974C3 (de) * | 1974-11-08 | 1978-03-09 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Hubschrauberrotorblatt |
US3932059A (en) * | 1975-01-10 | 1976-01-13 | United Technologies Corporation | Droop stops for helicopter rotor having elastomeric bearings |
US4203708A (en) * | 1978-06-26 | 1980-05-20 | United Technologies Corporation | Elastomeric rotor load reaction system |
US4235570A (en) * | 1978-06-26 | 1980-11-25 | United Technologies Corporation | Elastomeric helicopter rotor load reaction system |
FR2434079A1 (fr) * | 1978-08-23 | 1980-03-21 | Aerospatiale | Dispositif pour limiter les battements des pales d'un rotor principal de giravion |
IT1129070B (it) * | 1980-04-03 | 1986-06-04 | Agusta Aeronaut Costr | Rotore a giunti elastomerici per elicotteri |
US4297079A (en) * | 1980-07-14 | 1981-10-27 | Goodall Semimetallic Hose & Mfg. Co. | Variable pitch marine propeller |
US4368006A (en) * | 1980-08-07 | 1983-01-11 | The United States Of America As Represented By The Secretary Of The Navy | Droop stop for fully articulated rotor |
-
1982
- 1982-03-11 IT IT67304/82A patent/IT1155133B/it active
-
1983
- 1983-03-02 US US06/471,342 patent/US4551067A/en not_active Expired - Fee Related
- 1983-03-08 GB GB08306344A patent/GB2116507B/en not_active Expired
- 1983-03-08 DE DE19833308073 patent/DE3308073A1/de not_active Withdrawn
- 1983-03-09 FR FR8303900A patent/FR2523071B1/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR2523071A1 (fr) | 1983-09-16 |
GB8306344D0 (en) | 1983-04-13 |
GB2116507A (en) | 1983-09-28 |
US4551067A (en) | 1985-11-05 |
IT1155133B (it) | 1987-01-21 |
IT8267304A0 (it) | 1982-03-11 |
DE3308073A1 (de) | 1983-09-29 |
GB2116507B (en) | 1985-07-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TP | Transmission of property | ||
ST | Notification of lapse |