FR2758524B1 - Rotor a pales multiples pour aeronef a voilure tournante - Google Patents
Rotor a pales multiples pour aeronef a voilure tournanteInfo
- Publication number
- FR2758524B1 FR2758524B1 FR9800447A FR9800447A FR2758524B1 FR 2758524 B1 FR2758524 B1 FR 2758524B1 FR 9800447 A FR9800447 A FR 9800447A FR 9800447 A FR9800447 A FR 9800447A FR 2758524 B1 FR2758524 B1 FR 2758524B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- rotor
- turned
- multiple blades
- blades
- 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 - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- 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)
- Turbine Rotor Nozzle Sealing (AREA)
- Moulding By Coating Moulds (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19701403A DE19701403C1 (de) | 1997-01-17 | 1997-01-17 | Mehrblattrotor für ein Drehflügelflugzeug |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2758524A1 FR2758524A1 (fr) | 1998-07-24 |
FR2758524B1 true FR2758524B1 (fr) | 2002-01-18 |
Family
ID=7817574
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9800447A Expired - Fee Related FR2758524B1 (fr) | 1997-01-17 | 1998-01-16 | Rotor a pales multiples pour aeronef a voilure tournante |
Country Status (5)
Country | Link |
---|---|
US (1) | US6039538A (fr) |
JP (1) | JPH10218098A (fr) |
DE (1) | DE19701403C1 (fr) |
FR (1) | FR2758524B1 (fr) |
IT (1) | IT1298145B1 (fr) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT1307651B1 (it) * | 1998-02-06 | 2001-11-14 | Eurocopter Deutschland | Rotore multipale |
DE19961071B4 (de) * | 1999-12-17 | 2007-04-12 | Eurocopter Deutschland Gmbh | Kupplungsmembran |
DE10316092B4 (de) | 2003-04-08 | 2014-04-30 | Eurocopter Deutschland Gmbh | Gelenkloser Rotor mit plattenförmigem Rotorkopfelement |
US9777579B2 (en) | 2012-12-10 | 2017-10-03 | General Electric Company | Attachment of composite article |
US9797257B2 (en) | 2012-12-10 | 2017-10-24 | General Electric Company | Attachment of composite article |
CN107108028B (zh) * | 2016-04-13 | 2020-05-26 | 深圳市大疆创新科技有限公司 | 桨夹、折叠桨、动力套装及无人机 |
US20170323239A1 (en) | 2016-05-06 | 2017-11-09 | General Electric Company | Constrained time computing control system to simulate and optimize aircraft operations with dynamic thermodynamic state and asset utilization attainment |
US10988244B2 (en) | 2017-05-05 | 2021-04-27 | Laflamme Aero Inc. | Helicopter rotor hub assembly and helicopter including same |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2645174C2 (de) * | 1976-10-07 | 1982-08-12 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Rotorkopf für einen schlag- und schwenkgelenklosen Rotor |
DE2903524C2 (de) * | 1979-01-31 | 1982-02-25 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Schlag- und schwenkgelenkloser Anschluß von Rotorblättern eines Drehflügelflugzeuges |
DE2917301C3 (de) * | 1979-04-28 | 1981-12-17 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Schlag-, schwenk- und blattverstellgelenkloser Rotor |
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 |
US4427340A (en) * | 1982-06-24 | 1984-01-24 | Bell Helicopter Textron Inc. | Soft inplane bearingless helicopter rotor |
US4568244A (en) * | 1983-03-22 | 1986-02-04 | United Technologies Corporation | Fiber reinforced/epoxy matrix composite helicopter rotor main hub plate |
US4708591A (en) * | 1986-01-15 | 1987-11-24 | Stephan Roman | Bladed aircraft rotor with flexible blade mountings |
US5059094A (en) * | 1989-10-13 | 1991-10-22 | Bell Helicopter Textron, Inc. | Rotor redundant force retention system for vtol and vstol aircraft |
US5263821A (en) * | 1991-01-15 | 1993-11-23 | United Technologies Corporation | Mid-beam jointed reconfigurable bearingless main rotor assembly |
EP0496695A3 (en) * | 1991-01-15 | 1993-04-21 | United Technologies Corporation | A unitary, multi-legged helicopter rotor flexbeam made solely of composite materials and the method of manufacturing same |
-
1997
- 1997-01-17 DE DE19701403A patent/DE19701403C1/de not_active Expired - Fee Related
-
1998
- 1998-01-12 US US09/005,551 patent/US6039538A/en not_active Expired - Lifetime
- 1998-01-14 JP JP10005923A patent/JPH10218098A/ja active Pending
- 1998-01-16 FR FR9800447A patent/FR2758524B1/fr not_active Expired - Fee Related
- 1998-01-16 IT IT98MI000075A patent/IT1298145B1/it active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
JPH10218098A (ja) | 1998-08-18 |
FR2758524A1 (fr) | 1998-07-24 |
ITMI980075A1 (it) | 1999-07-16 |
DE19701403C1 (de) | 1998-02-26 |
IT1298145B1 (it) | 1999-12-20 |
US6039538A (en) | 2000-03-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20091030 |