ATE551258T1 - Hubschrauber - Google Patents

Hubschrauber

Info

Publication number
ATE551258T1
ATE551258T1 AT08425680T AT08425680T ATE551258T1 AT E551258 T1 ATE551258 T1 AT E551258T1 AT 08425680 T AT08425680 T AT 08425680T AT 08425680 T AT08425680 T AT 08425680T AT E551258 T1 ATE551258 T1 AT E551258T1
Authority
AT
Austria
Prior art keywords
helicopter
connecting member
fuselage
rotor
transmission
Prior art date
Application number
AT08425680T
Other languages
English (en)
Inventor
Santino Pancotti
Dante Ballerio
Attilio Colombo
Original Assignee
Agustawestland Spa
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Agustawestland Spa filed Critical Agustawestland Spa
Application granted granted Critical
Publication of ATE551258T1 publication Critical patent/ATE551258T1/de

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)
AT08425680T 2008-10-21 2008-10-21 Hubschrauber ATE551258T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP08425680A EP2179922B1 (de) 2008-10-21 2008-10-21 Hubschrauber

Publications (1)

Publication Number Publication Date
ATE551258T1 true ATE551258T1 (de) 2012-04-15

Family

ID=40380696

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08425680T ATE551258T1 (de) 2008-10-21 2008-10-21 Hubschrauber

Country Status (9)

Country Link
US (1) US8141813B2 (de)
EP (1) EP2179922B1 (de)
JP (1) JP5419154B2 (de)
KR (1) KR101634184B1 (de)
CN (1) CN101723090B (de)
AT (1) ATE551258T1 (de)
PL (1) PL2179922T3 (de)
PT (1) PT2179922E (de)
RU (1) RU2499735C2 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ATE551258T1 (de) * 2008-10-21 2012-04-15 Agustawestland Spa Hubschrauber
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 (de) * 2014-07-04 2016-09-21 AGUSTAWESTLAND S.p.A. Hubschrauber mit geräusch- und schwingungsdämpfender Antriebsaufhängung
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)

* Cited by examiner, † Cited by third party
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 (de) * 1973-05-08 1976-11-12 Aerospatiale
FR2232481B1 (de) * 1973-06-08 1976-05-07 Aerospatiale
FR2270144B1 (de) * 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
FR2441902A2 (fr) * 1978-11-15 1980-06-13 Aerospatiale Dispositif de suspension multidirectionnelle pour giravion
GB2018942B (en) 1978-03-20 1982-06-03 Aerospatiale Multi-directional suspension means
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
ATE551258T1 (de) * 2008-10-21 2012-04-15 Agustawestland Spa Hubschrauber

Also Published As

Publication number Publication date
JP2010100283A (ja) 2010-05-06
KR101634184B1 (ko) 2016-07-08
RU2009138296A (ru) 2011-04-27
CN101723090B (zh) 2014-11-26
RU2499735C2 (ru) 2013-11-27
KR20100044135A (ko) 2010-04-29
PL2179922T3 (pl) 2012-08-31
EP2179922B1 (de) 2012-03-28
PT2179922E (pt) 2012-06-20
US8141813B2 (en) 2012-03-27
EP2179922A1 (de) 2010-04-28
US20100096492A1 (en) 2010-04-22
JP5419154B2 (ja) 2014-02-19
CN101723090A (zh) 2010-06-09

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