FR2427945A1 - Agencement de montage souple pour rotor d'helicoptere a lame traversante - Google Patents
Agencement de montage souple pour rotor d'helicoptere a lame traversanteInfo
- Publication number
- FR2427945A1 FR2427945A1 FR7816730A FR7816730A FR2427945A1 FR 2427945 A1 FR2427945 A1 FR 2427945A1 FR 7816730 A FR7816730 A FR 7816730A FR 7816730 A FR7816730 A FR 7816730A FR 2427945 A1 FR2427945 A1 FR 2427945A1
- Authority
- FR
- France
- Prior art keywords
- mounting arrangement
- helicopter rotor
- flexible mounting
- blade
- blade helicopter
- 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
- B64C27/35—Rotors having elastomeric joints
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Toys (AREA)
- Tires In General (AREA)
Abstract
L'invention se rapporte à l'aéronautique. Elle a pour objet un agencement de montage souple pour rotor d'hélicoptère. Deux coques de pales 3, 4 sont portées par une lame traversante 2 flexible, reliée au moyeu par des plots lamifiés 20 élastiques. Les pieds de pales prennent appui par des articulations à rotule 26a, 27 de centre A. Application à la réalisation de rotors présentant une longue durée de vie et un démontage facile.
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7816730A FR2427945A1 (fr) | 1978-06-05 | 1978-06-05 | Agencement de montage souple pour rotor d'helicoptere a lame traversante |
DE2921421A DE2921421C2 (de) | 1978-06-05 | 1979-05-26 | Rotor für ein Drehflügelflugzeug mit mindestens zwei Nabenplatten |
GB7919130A GB2022535B (en) | 1978-06-05 | 1979-06-01 | Attaching rotor hub to blades |
US06/044,365 US4293277A (en) | 1978-06-05 | 1979-06-01 | Supple mounting arrangement for helicopter rotor with through strip |
IT23288/79A IT1121263B (it) | 1978-06-05 | 1979-06-05 | Disposizione di montaggio cedevole per rotore di elicottero a lama passante |
JP54069523A JPS6020238B2 (ja) | 1978-06-05 | 1979-06-05 | ヘリコプタ回転翼用たわみ性取付け装置 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7816730A FR2427945A1 (fr) | 1978-06-05 | 1978-06-05 | Agencement de montage souple pour rotor d'helicoptere a lame traversante |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2427945A1 true FR2427945A1 (fr) | 1980-01-04 |
FR2427945B1 FR2427945B1 (fr) | 1983-02-11 |
Family
ID=9209071
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7816730A Granted FR2427945A1 (fr) | 1978-06-05 | 1978-06-05 | Agencement de montage souple pour rotor d'helicoptere a lame traversante |
Country Status (6)
Country | Link |
---|---|
US (1) | US4293277A (fr) |
JP (1) | JPS6020238B2 (fr) |
DE (1) | DE2921421C2 (fr) |
FR (1) | FR2427945A1 (fr) |
GB (1) | GB2022535B (fr) |
IT (1) | IT1121263B (fr) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2929906C3 (de) * | 1979-07-24 | 1982-01-21 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Rotor für einen Hubschrauber mit zumindest einem Paar einander gegenüberliegender Rotorblätter |
US4349317A (en) * | 1979-11-02 | 1982-09-14 | The Boeing Company | Bearingless rotor for single and tandem helicopters |
US4381902A (en) * | 1979-12-20 | 1983-05-03 | Hughes Helicopters, Inc. | Helicopter tail rotor of the elastomerically-mounted composite flexbeam type |
DE3144099C2 (de) * | 1981-11-06 | 1983-12-01 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Rotorkopf |
US4695227A (en) * | 1985-02-27 | 1987-09-22 | Hughes Helicopters Inc. | All composite, constant speed universal joint for use in a shaft driven tiltable main rotor for a helicopter |
DE3526470C1 (de) * | 1985-07-24 | 1987-01-02 | Messerschmitt Boelkow Blohm | Rotor,insbesondere eines Drehfluegelflugzeugs |
US4729753A (en) * | 1985-11-04 | 1988-03-08 | Bell Helicopter Textron Inc. | Constant velocity elastomeric bearing joint |
FR2613319B1 (fr) * | 1987-03-30 | 1989-06-30 | Aerospatiale | Dispositif de palier combine pour rotor de giravion, et rotor equipe d'un tel dispositif de palier |
FR2653405B1 (fr) * | 1989-10-20 | 1992-02-07 | Aerospatiale | Dispositif visco-elastique rotatif de rappel elastique et d'amortissement en trainee pour pale de rotor de giravion, et tete de rotor le comportant. |
US6024325A (en) * | 1997-01-09 | 2000-02-15 | Cartercopters, Llc | Rotor for rotary wing aircraft |
US7097169B2 (en) * | 2004-08-04 | 2006-08-29 | Skf Usa Inc. | Elastomeric bearing with modified cylindrical core |
US9394937B2 (en) * | 2011-05-10 | 2016-07-19 | Silvestro Caruso | Elastomeric teetering hinge |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3484174A (en) * | 1968-04-08 | 1969-12-16 | Kaman Corp | Rotary wing system |
FR2310920A1 (fr) * | 1975-05-14 | 1976-12-10 | Aerospatiale | Agencement de rotor pour aeronef a voilure tournante |
US4047839A (en) * | 1976-05-28 | 1977-09-13 | United Technologies Corporation | Torque reacting means for the hubs of cross beam rotors |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2012703A1 (fr) * | 1968-07-11 | 1970-03-20 | Acero Andres Francisco | |
US3874815A (en) * | 1973-11-15 | 1975-04-01 | Boeing Co | Rotary head assembly for rotary wing aircraft |
US3880551A (en) * | 1973-11-15 | 1975-04-29 | Boeing Co | Rotary head assembly for rotary wing aircraft |
FR2285298A1 (fr) * | 1974-09-19 | 1976-04-16 | Aerospatiale | Agencement de rotor de queue pour giravions |
US4008980A (en) * | 1975-06-26 | 1977-02-22 | United Technologies Corporation | Composite helicopter spar and means to alleviate stress concentration |
US3999887A (en) * | 1975-07-09 | 1976-12-28 | Lord Corporation | Propeller assembly |
-
1978
- 1978-06-05 FR FR7816730A patent/FR2427945A1/fr active Granted
-
1979
- 1979-05-26 DE DE2921421A patent/DE2921421C2/de not_active Expired
- 1979-06-01 US US06/044,365 patent/US4293277A/en not_active Expired - Lifetime
- 1979-06-01 GB GB7919130A patent/GB2022535B/en not_active Expired
- 1979-06-05 JP JP54069523A patent/JPS6020238B2/ja not_active Expired
- 1979-06-05 IT IT23288/79A patent/IT1121263B/it active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3484174A (en) * | 1968-04-08 | 1969-12-16 | Kaman Corp | Rotary wing system |
FR2310920A1 (fr) * | 1975-05-14 | 1976-12-10 | Aerospatiale | Agencement de rotor pour aeronef a voilure tournante |
US4047839A (en) * | 1976-05-28 | 1977-09-13 | United Technologies Corporation | Torque reacting means for the hubs of cross beam rotors |
Also Published As
Publication number | Publication date |
---|---|
GB2022535A (en) | 1979-12-19 |
DE2921421A1 (de) | 1979-12-06 |
IT7923288A0 (it) | 1979-06-05 |
GB2022535B (en) | 1982-08-18 |
US4293277A (en) | 1981-10-06 |
JPS54159999A (en) | 1979-12-18 |
FR2427945B1 (fr) | 1983-02-11 |
DE2921421C2 (de) | 1982-08-12 |
IT1121263B (it) | 1986-04-02 |
JPS6020238B2 (ja) | 1985-05-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
TP | Transmission of property | ||
ST | Notification of lapse | ||
ST | Notification of lapse |