PL2179922T3 - Helikopter - Google Patents
HelikopterInfo
- Publication number
- PL2179922T3 PL2179922T3 PL08425680T PL08425680T PL2179922T3 PL 2179922 T3 PL2179922 T3 PL 2179922T3 PL 08425680 T PL08425680 T PL 08425680T PL 08425680 T PL08425680 T PL 08425680T PL 2179922 T3 PL2179922 T3 PL 2179922T3
- Authority
- PL
- Poland
- Prior art keywords
- helicopter
- connecting member
- fuselage
- rotor
- transmission
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/001—Vibration damping devices
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S416/00—Fluid reaction surfaces, i.e. impellers
- Y10S416/50—Vibration damping features
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Prevention Devices (AREA)
- Toys (AREA)
- Medicines Containing Material From Animals Or Micro-Organisms (AREA)
- Inorganic Insulating Materials (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP08425680A EP2179922B1 (en) | 2008-10-21 | 2008-10-21 | Helicopter |
Publications (1)
Publication Number | Publication Date |
---|---|
PL2179922T3 true PL2179922T3 (pl) | 2012-08-31 |
Family
ID=40380696
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL08425680T PL2179922T3 (pl) | 2008-10-21 | 2008-10-21 | Helikopter |
Country Status (9)
Country | Link |
---|---|
US (1) | US8141813B2 (pl) |
EP (1) | EP2179922B1 (pl) |
JP (1) | JP5419154B2 (pl) |
KR (1) | KR101634184B1 (pl) |
CN (1) | CN101723090B (pl) |
AT (1) | ATE551258T1 (pl) |
PL (1) | PL2179922T3 (pl) |
PT (1) | PT2179922E (pl) |
RU (1) | RU2499735C2 (pl) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
PT2179922E (pt) * | 2008-10-21 | 2012-06-20 | Agustawestland Spa | Helicóptero |
US9033301B1 (en) * | 2011-04-26 | 2015-05-19 | The Boeing Company | Vibration reduction system using an extended washer |
FR3006022B1 (fr) * | 2013-05-21 | 2015-06-05 | Eurocopter France | Architecture de montage d'une boite de transmission de puissance d'un giravion, comprenant un dispositif amortisseur de vibrations mettant en oeuvre des amortisseurs lamifies |
EP2962935B1 (en) * | 2014-07-04 | 2016-09-21 | AGUSTAWESTLAND S.p.A. | Helicopter with noise and vibration damping transmission mounting |
FR3050437B1 (fr) * | 2016-04-25 | 2019-07-19 | Safran Aircraft Engines | Dispositif de suspension pour un systeme propulsif d'aeronef |
CN107031831B (zh) * | 2016-11-21 | 2019-10-29 | 芜湖万户航空航天科技有限公司 | 无人直升机电机固定装置 |
US11167842B2 (en) | 2017-10-10 | 2021-11-09 | Bell Helicopter Textron Inc. | Mount for supporting a component and attenuating noise |
US11584521B2 (en) | 2019-09-26 | 2023-02-21 | Textron Innovations Inc. | Pylon restraint system |
FR3136027B1 (fr) * | 2022-05-24 | 2024-04-19 | Airbus Helicopters | Articulation déformable élastiquement et système muni d’une telle articulation. |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2615657A (en) * | 1946-08-28 | 1952-10-28 | Bell Aircraft Corp | Helicopter engine-rotor support |
FR1507306A (fr) * | 1966-11-17 | 1967-12-29 | Sud Aviation | Dispositif de liaison filtrant les vibrations entre un organe vibrant et un support,notamment un rotor et une structure d'hélicoptère |
US3565386A (en) * | 1969-02-19 | 1971-02-23 | Gen Motors Corp | Mount for a body and coupling unit therefor |
US3698663A (en) * | 1970-12-07 | 1972-10-17 | Textron Inc | Rotary wing pylon mounting system |
FR2228662B1 (pl) * | 1973-05-08 | 1976-11-12 | Aerospatiale | |
FR2232481B1 (pl) * | 1973-06-08 | 1976-05-07 | Aerospatiale | |
FR2270144B1 (pl) * | 1974-05-09 | 1976-10-15 | Aerospatiale | |
US4111386A (en) * | 1976-12-09 | 1978-09-05 | United Technologies Corporation | Helicopter rotor and transmission mounting and vibration isolation system |
US4274510A (en) * | 1978-03-20 | 1981-06-23 | Societe Nationale Industrielle Aerospatiale | Multi-directional suspension means for rotor aircraft |
FR2441902A2 (fr) * | 1978-11-15 | 1980-06-13 | Aerospatiale | Dispositif de suspension multidirectionnelle pour giravion |
DE2825177A1 (de) * | 1978-06-08 | 1979-12-13 | Hatz Motoren | Brennkraftmaschine |
FR2474996A1 (fr) * | 1980-02-05 | 1981-08-07 | Aerospatiale | Dispositif de suspension antiresonnante pour helicoptere |
FR2584373B1 (fr) * | 1985-07-03 | 1990-07-06 | Aerospatiale | Dispositif de suspension antiresonnante a six degres de liberte pour helicoptere |
FR2669982B1 (fr) * | 1990-11-30 | 1993-02-19 | Aerospatiale | Dispositif de suspension anti-resonnante pour helicoptere. |
RU2065381C1 (ru) * | 1993-01-19 | 1996-08-20 | Вертолетный научно-технический комплекс им.Н.И.Камова | Главный редуктор вертолета |
CN1161024A (zh) * | 1994-10-18 | 1997-10-01 | 联合工艺公司 | 用于无轴承转子的减振支承安装组件 |
FR2728539A1 (fr) * | 1994-12-23 | 1996-06-28 | Eurocopter France | Dispositif de suspension anti-vibratoire bidirectionnelle pour rotor d'helicoptere |
FR2787762B1 (fr) * | 1998-12-29 | 2001-03-09 | Eurocopter France | Dispositif de suspension antivibratoire avec ressort en torsion, pour helicoptere |
FR2795386B1 (fr) * | 1999-06-22 | 2001-11-09 | Eurocopter France | Dispositif de suspension antivibratoire avec ressorts en torsion entre batteurs et structure, pour helicoptere |
RU2263608C1 (ru) * | 2004-04-01 | 2005-11-10 | Открытое акционерное общество "Камов" | Редуктор легкого вертолета |
FR2889687B1 (fr) * | 2005-08-10 | 2007-11-30 | Eurocopter France | Procede de decouplage solidien selectif de bruit, rotule lamifie, liaison mecanique et aeronef. |
CN1880170A (zh) * | 2006-04-28 | 2006-12-20 | 刘世英 | 直升飞机机身自转的主动控制技术 |
PT2179922E (pt) * | 2008-10-21 | 2012-06-20 | Agustawestland Spa | Helicóptero |
-
2008
- 2008-10-21 PT PT08425680T patent/PT2179922E/pt unknown
- 2008-10-21 AT AT08425680T patent/ATE551258T1/de active
- 2008-10-21 PL PL08425680T patent/PL2179922T3/pl unknown
- 2008-10-21 EP EP08425680A patent/EP2179922B1/en active Active
-
2009
- 2009-10-19 US US12/581,560 patent/US8141813B2/en active Active
- 2009-10-19 RU RU2009138296/11A patent/RU2499735C2/ru active
- 2009-10-21 KR KR1020090100352A patent/KR101634184B1/ko active IP Right Grant
- 2009-10-21 CN CN200910206601.7A patent/CN101723090B/zh active Active
- 2009-10-21 JP JP2009258386A patent/JP5419154B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
JP2010100283A (ja) | 2010-05-06 |
KR20100044135A (ko) | 2010-04-29 |
ATE551258T1 (de) | 2012-04-15 |
CN101723090A (zh) | 2010-06-09 |
CN101723090B (zh) | 2014-11-26 |
RU2499735C2 (ru) | 2013-11-27 |
KR101634184B1 (ko) | 2016-07-08 |
RU2009138296A (ru) | 2011-04-27 |
EP2179922A1 (en) | 2010-04-28 |
EP2179922B1 (en) | 2012-03-28 |
PT2179922E (pt) | 2012-06-20 |
US8141813B2 (en) | 2012-03-27 |
US20100096492A1 (en) | 2010-04-22 |
JP5419154B2 (ja) | 2014-02-19 |
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