FR2369158A1 - Rotor d'helicoptere sans articulations de battement et de trainee - Google Patents
Rotor d'helicoptere sans articulations de battement et de traineeInfo
- Publication number
- FR2369158A1 FR2369158A1 FR7732151A FR7732151A FR2369158A1 FR 2369158 A1 FR2369158 A1 FR 2369158A1 FR 7732151 A FR7732151 A FR 7732151A FR 7732151 A FR7732151 A FR 7732151A FR 2369158 A1 FR2369158 A1 FR 2369158A1
- Authority
- FR
- France
- Prior art keywords
- helicopter rotor
- trail
- beat
- joints
- hub
- 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.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/37—Rotors having articulated joints
- B64C27/45—Rotors having articulated joints with a feathering hinge only
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Wind Motors (AREA)
Abstract
Rotor d'hélicoptère non articulé dont chaque pale est solidaire d'un longeron résistant à la flexion monté tournant sur un moyeu essentiellement rigide par l'intermédiaire de paliers d'angles de pale, des éléments de liaison résistants à la traction étant prévus entre lesdits longerons pour compenser les forces centrifuges. Le moyeu 8 comporte deux plaques de support 4, 6 faites d'un matériau composite fibreux, avec direction radiale des fibres, qui sont maintenues écartées par des renforts de cisaillement 46, 58, 60 et soutiennent entre elles les paliers d'angle de pale 10, 12. Avantages de construction légère et de fiabilité en service.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2648343A DE2648343C3 (de) | 1976-10-26 | 1976-10-26 | Schlag- und schwenkgelenkloser Rotor für Drehflügelflugzeuge |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2369158A1 true FR2369158A1 (fr) | 1978-05-26 |
FR2369158B1 FR2369158B1 (fr) | 1984-06-01 |
Family
ID=5991376
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7732151A Granted FR2369158A1 (fr) | 1976-10-26 | 1977-10-25 | Rotor d'helicoptere sans articulations de battement et de trainee |
Country Status (6)
Country | Link |
---|---|
US (1) | US4195967A (fr) |
JP (1) | JPS5353898A (fr) |
DE (1) | DE2648343C3 (fr) |
FR (1) | FR2369158A1 (fr) |
GB (1) | GB1545712A (fr) |
IT (1) | IT1086932B (fr) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2447856A1 (fr) * | 1979-02-02 | 1980-08-29 | Agusta Aeronaut Costr | Rotor articule pour helicoptere |
EP0085127A1 (fr) * | 1982-02-02 | 1983-08-10 | Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung | Rotor, en particulier pour aéronef à aile tournante, avec moyeu en matière plastique renforcé par des fibres |
FR2529860A1 (fr) * | 1982-07-08 | 1984-01-13 | Aerospatiale | Plateau de moyeu, procede de fabrication et moyeu de rotor de giravion equipe de tels plateaux |
FR2582283A1 (fr) * | 1985-05-16 | 1986-11-28 | United Technologies Corp | Structure a enroulement de filaments destinee a etre utilisee comme moyen de transmission de couple |
FR2587938A1 (fr) * | 1985-09-30 | 1987-04-03 | United Technologies Corp | Structure enroulee de filaments comportant des anneaux de renforcement enroules de filaments, utilisable comme transmission de couple |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2722250A1 (de) * | 1977-03-23 | 1978-11-23 | Messerschmitt Boelkow Blohm | Rotor eines drehfluegelflugzeugs |
US4306836A (en) * | 1978-05-25 | 1981-12-22 | Kaman Aerospace Corporation | Hub assembly |
DE3006088A1 (de) * | 1980-02-19 | 1981-08-20 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Rotor eines drehfluegelflugzeugs |
IT1155132B (it) * | 1982-03-11 | 1987-01-21 | Agusta Aeronaut Costr | Rotore per elicotteri |
IT1155131B (it) * | 1982-03-11 | 1987-01-21 | Agusta Aeronaut Costr | Mozzo di rotore di elicotteri |
US4466774A (en) * | 1982-08-30 | 1984-08-21 | United Technologies Corporation | Composite flexbeam joint |
US4543040A (en) * | 1982-09-30 | 1985-09-24 | The Boeing Company | Helicopter rotor system |
IT1159375B (it) * | 1983-03-15 | 1987-02-25 | Agusta Aeronaut Costr | Rotore per elicotteri |
US4568244A (en) * | 1983-03-22 | 1986-02-04 | United Technologies Corporation | Fiber reinforced/epoxy matrix composite helicopter rotor main hub plate |
US4585393A (en) * | 1983-03-22 | 1986-04-29 | United Technologies Corporation | Fiber reinforced/epoxy matrix composite helicopter rotor yoke |
US4568245A (en) * | 1983-03-22 | 1986-02-04 | United Technologies Corporation | Composite helicopter rotor hub |
GB2165026A (en) * | 1984-09-26 | 1986-04-03 | Jose A Avila | Composite torsion link |
IT1182448B (it) * | 1985-02-19 | 1987-10-05 | Agusta Aeronaut Costr | Mozzo metallico per un rotore di elicottero |
US4797064A (en) * | 1987-07-30 | 1989-01-10 | United Technologies Corporation | Composite helicopter rotor hub |
US5980206A (en) * | 1996-05-31 | 1999-11-09 | Sikorsky Aircraft Corporation | Monolithic structure having improved flaw tolerance |
CA3004054C (fr) | 2017-05-05 | 2024-02-13 | Laflamme Aero Inc. | Assemblage de moyeu de rotor d'helicoptere et helicoptere comportant ledit assemblage |
US10988243B2 (en) * | 2019-03-15 | 2021-04-27 | Bell Textron Inc. | Tension-torsion strap |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2156182A1 (fr) * | 1971-10-12 | 1973-05-25 | Messerschmitt Boelkow Blohm | |
FR2192942A1 (fr) * | 1972-07-14 | 1974-02-15 | United Aircraft Corp | |
FR2324512A1 (fr) * | 1975-09-20 | 1977-04-15 | Messerschmitt Boelkow Blohm | Dispositif de raccordement d'une pale au moyeu d'un rotor rigide d'helicoptere |
FR2362754A1 (fr) * | 1976-08-25 | 1978-03-24 | Messerschmitt Boelkow Blohm | Rotor pour aeronef a voiture tournante |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1205757A (en) * | 1967-02-07 | 1970-09-16 | Westland Aircraft Ltd | Improvements in or relating to rotor heads for rotary wing aircraft |
US3384185A (en) * | 1967-06-02 | 1968-05-21 | Aerojet General Co | Rotor hubs |
DE1531355B1 (de) * | 1967-07-01 | 1970-07-23 | Bolkow Gmbh | schlag-und schwenkgelenklose aufhangung der roterblatter eines drehflugelflgzeuges am roterkopf. |
US3549444A (en) * | 1967-12-28 | 1970-12-22 | Harry S Katz | Filament wound blade and compressor |
FR2041747A1 (fr) * | 1969-05-20 | 1971-02-05 | Sud Aviation | |
US4012169A (en) * | 1973-05-10 | 1977-03-15 | Societe Nationale Industrielle Aerospatiale | Rotor for rotating wing type aircraft |
GB1432117A (en) * | 1973-05-10 | 1976-04-14 | Aerospatiale | Rotor for rotating wing type aircraft |
IT1011053B (it) * | 1974-03-07 | 1977-01-20 | Agusta Aeronaut Costr | Mozzo di rotore per elicottero dota do ti elementi flessibili quali ar ticolazioni virtuali |
-
1976
- 1976-10-26 DE DE2648343A patent/DE2648343C3/de not_active Expired
-
1977
- 1977-10-21 US US05/844,317 patent/US4195967A/en not_active Expired - Lifetime
- 1977-10-21 GB GB43992/77A patent/GB1545712A/en not_active Expired
- 1977-10-25 FR FR7732151A patent/FR2369158A1/fr active Granted
- 1977-10-25 IT IT28940/77A patent/IT1086932B/it active
- 1977-10-26 JP JP12768377A patent/JPS5353898A/ja active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2156182A1 (fr) * | 1971-10-12 | 1973-05-25 | Messerschmitt Boelkow Blohm | |
FR2192942A1 (fr) * | 1972-07-14 | 1974-02-15 | United Aircraft Corp | |
FR2324512A1 (fr) * | 1975-09-20 | 1977-04-15 | Messerschmitt Boelkow Blohm | Dispositif de raccordement d'une pale au moyeu d'un rotor rigide d'helicoptere |
FR2362754A1 (fr) * | 1976-08-25 | 1978-03-24 | Messerschmitt Boelkow Blohm | Rotor pour aeronef a voiture tournante |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2447856A1 (fr) * | 1979-02-02 | 1980-08-29 | Agusta Aeronaut Costr | Rotor articule pour helicoptere |
EP0085127A1 (fr) * | 1982-02-02 | 1983-08-10 | Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung | Rotor, en particulier pour aéronef à aile tournante, avec moyeu en matière plastique renforcé par des fibres |
FR2529860A1 (fr) * | 1982-07-08 | 1984-01-13 | Aerospatiale | Plateau de moyeu, procede de fabrication et moyeu de rotor de giravion equipe de tels plateaux |
EP0099294A2 (fr) * | 1982-07-08 | 1984-01-25 | AEROSPATIALE Société Nationale Industrielle | Plateau de moyeu, procédé de fabrication et moyeu de rotor de giravion équipé de tels plateaux |
EP0099294A3 (en) * | 1982-07-08 | 1984-05-02 | Societe Nationale Industrielle Aerospatiale Societe Dite: | Rotor hub plates, manufacturing process and rotor craft hub embodying them |
US4556365A (en) * | 1982-07-08 | 1985-12-03 | Societe Nationale Industrielle Et Aerospatiale | Hub plate for a helicopter rotor, method of manufacturing it, and a helicopter rotor hub equipped with plates |
FR2582283A1 (fr) * | 1985-05-16 | 1986-11-28 | United Technologies Corp | Structure a enroulement de filaments destinee a etre utilisee comme moyen de transmission de couple |
FR2587938A1 (fr) * | 1985-09-30 | 1987-04-03 | United Technologies Corp | Structure enroulee de filaments comportant des anneaux de renforcement enroules de filaments, utilisable comme transmission de couple |
Also Published As
Publication number | Publication date |
---|---|
DE2648343B2 (de) | 1980-10-16 |
DE2648343C3 (de) | 1981-06-19 |
GB1545712A (en) | 1979-05-16 |
JPS5353898A (en) | 1978-05-16 |
IT1086932B (it) | 1985-05-31 |
DE2648343A1 (de) | 1978-04-27 |
US4195967A (en) | 1980-04-01 |
FR2369158B1 (fr) | 1984-06-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |