BRPI0622047A2 - Pilone de montagem rígida com atenuação de vibração - Google Patents

Pilone de montagem rígida com atenuação de vibração

Info

Publication number
BRPI0622047A2
BRPI0622047A2 BRPI0622047-9A2A BRPI0622047A BRPI0622047A2 BR PI0622047 A2 BRPI0622047 A2 BR PI0622047A2 BR PI0622047 A BRPI0622047 A BR PI0622047A BR PI0622047 A2 BRPI0622047 A2 BR PI0622047A2
Authority
BR
Brazil
Prior art keywords
pilone
rigid mounting
attention
vibration
vibration attention
Prior art date
Application number
BRPI0622047-9A2A
Other languages
English (en)
Inventor
Michael R Smith
Frank B Stamps
Original Assignee
Bell Helicopter Textron Inc
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 Bell Helicopter Textron Inc filed Critical Bell Helicopter Textron Inc
Publication of BRPI0622047A2 publication Critical patent/BRPI0622047A2/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/12Rotor drives
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/51Damping of blade movements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F7/00Vibration-dampers; Shock-absorbers
    • F16F7/10Vibration-dampers; Shock-absorbers using inertia effect
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/001Vibration damping devices
    • B64C2027/002Vibration damping devices mounted between the rotor drive and the fuselage
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F2230/00Purpose; Design features
    • F16F2230/16Purpose; Design features used in a strut, basically rigid

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Vibration Prevention Devices (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)
BRPI0622047-9A2A 2006-10-12 2006-10-12 Pilone de montagem rígida com atenuação de vibração BRPI0622047A2 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2006/039992 WO2008045073A2 (en) 2006-10-12 2006-10-12 Vibration-attenuating hard-mounted pylon

Publications (1)

Publication Number Publication Date
BRPI0622047A2 true BRPI0622047A2 (pt) 2014-06-10

Family

ID=39283310

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0622047-9A2A BRPI0622047A2 (pt) 2006-10-12 2006-10-12 Pilone de montagem rígida com atenuação de vibração

Country Status (8)

Country Link
US (1) US8328129B2 (pt)
EP (1) EP2071924B1 (pt)
KR (1) KR20090076903A (pt)
CN (1) CN101522521B (pt)
BR (1) BRPI0622047A2 (pt)
CA (1) CA2665700C (pt)
DE (1) DE06849841T1 (pt)
WO (1) WO2008045073A2 (pt)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8939725B2 (en) * 2007-11-07 2015-01-27 Heliscandia Aps Autonomic rotor system for an aircraft
GB2492965B (en) * 2011-07-15 2018-05-02 Agustawestland Ltd A system and method for reducing the transmission of vibration from a first vibrating body to a second body
US9777788B2 (en) * 2012-01-10 2017-10-03 Bell Helicopter Textron Inc. Rotorcraft vibration suppression system in a four corner pylon mount configuration
US8731743B2 (en) * 2012-04-11 2014-05-20 Textron Innovations Inc. Self tuning vibration isolation system
US9343890B2 (en) 2013-01-23 2016-05-17 Thomas & Betts International Llc Electrical cable restrain device using a double wedge chuck
US9365294B2 (en) * 2013-11-21 2016-06-14 Bell Helicopter Textron Inc. Helicopter transmission mount system
US9254914B2 (en) * 2013-11-21 2016-02-09 Bell Helicopter Textron Inc. Helicopter transmission mount system
FR3019522B1 (fr) * 2014-04-07 2016-05-20 Airbus Helicopters Ensemble sustentateur amovible d'un giravion et giravion
US9551393B2 (en) * 2014-04-23 2017-01-24 Bell Helicopter Textron Inc. Rotorcraft vibration isolation systems
US10745116B2 (en) * 2014-08-07 2020-08-18 Sikorsky Aircraft Corporation Anti-vibration load generating aircraft actuation system
WO2016048442A1 (en) * 2014-09-26 2016-03-31 Sikorsky Aircraft Corporation Damage adaptive vibration control
US10507920B2 (en) * 2015-05-18 2019-12-17 Sikorsky Aircraft Corp. Systems and methods for lifting body vibration control
US10550907B2 (en) * 2016-08-18 2020-02-04 Textron Innovations Inc. Liquid inertia vibration elimination system
US20180265186A1 (en) 2017-03-15 2018-09-20 Bell Helicopter Textron Inc. Vibration Isolation Systems for Advancing Blade Concept Rotorcraft
US11932380B2 (en) 2017-03-15 2024-03-19 Textron Innovations Inc. Vibration isolation systems for compound helicopters
EP3599162B1 (en) * 2018-07-27 2020-11-11 LEONARDO S.p.A. Helicopter kit
EP3599163B1 (en) * 2018-07-27 2020-11-11 LEONARDO S.p.A. Helicopter kit
US11767107B2 (en) * 2019-07-05 2023-09-26 Textron Innovations Inc. System and method for vibratory motion reduction for a pylon assembly
CN111301673B (zh) * 2020-03-04 2021-09-03 吉林工程技术师范学院 一种六翼中型无人机的旋转装置
CN114110292B (zh) * 2022-01-27 2022-04-05 智性科技南通有限公司 一种可调节混合式减振纤维增强复合材料支吊架

Family Cites Families (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1506385A (fr) * 1966-09-16 1967-12-22 Sud Aviation Procédé d'atténuation et atténuateur électro-hydraulique de vibrations pour aérodyne à voilure tournante
US3514054A (en) * 1967-06-05 1970-05-26 United Aircraft Corp Vibration isolation system
US3638885A (en) * 1970-03-09 1972-02-01 Boeing Co Lag frequency selective damper
US4236607A (en) * 1979-02-26 1980-12-02 Textron, Inc. Vibration suppression system
FR2629545B1 (fr) * 1988-03-30 1993-02-19 Aerospatiale Contre-fiche elastique a resonateur hydro-mecanique integre notamment pour la suspension d'une boite de transmission sur un giravion et dispositif de suspension en comportant application
FR2678032B1 (fr) * 1991-06-18 1993-10-01 Aerospatiale Ste Nationale Indle Dispositif de liaison elastique entre deux pieces, et aeronef a voilure tournante comportant ledit dispositif.
FR2680848B1 (fr) * 1991-08-29 1995-03-17 Aerospatiale Ste Nat Indle Procede et dispositif pour filtrer les excitations vibratoires transmises entre deux pieces, notamment entre le rotor et le fuselage d'un helicoptere.
US5231336A (en) * 1992-01-03 1993-07-27 Harman International Industries, Inc. Actuator for active vibration control
US5538373A (en) * 1992-02-20 1996-07-23 Giddings & Lewis, Inc. Machine tool vibration isolation system
US5456341A (en) * 1993-04-23 1995-10-10 Moog Inc. Method and apparatus for actively adjusting and controlling a resonant mass-spring system
JP2772410B2 (ja) 1993-09-17 1998-07-02 防衛庁技術研究本部長 ヘリコプタの能動防振装置
US5439082A (en) * 1994-04-01 1995-08-08 Bell Helicopter Textron Inc. Hydraulic inertial vibration isolator
US5551650A (en) * 1994-06-16 1996-09-03 Lord Corporation Active mounts for aircraft engines
US5456427A (en) * 1994-07-25 1995-10-10 The United States Of America As Represented By The Secretary Of The Navy Air-launchable gliding sonobuoy
US5682069A (en) * 1994-08-30 1997-10-28 Harris Corporation Concentrically mounted vibration attenuator and method
EP0786057B1 (en) * 1994-10-12 1999-12-29 Lord Corporation ACTIVE SYSTEMS AND DEVICES INCLUDING ACTIVE VIBRATION ABSORBERS (AVAs)
FR2731405B1 (fr) * 1995-03-10 1997-05-09 Eurocopter France Systeme pour minimiser l'excitation dynamique d'un helicoptere
US5806803A (en) * 1995-11-30 1998-09-15 Hughes Electronics Corporation Spacecraft radiator cooling system
DE19621700C2 (de) * 1996-05-30 2001-09-27 Eurocopter Deutschland Aktiver Schwingungsminderer
FR2749901B1 (fr) * 1996-06-12 2000-12-08 Eurocopter France Dispositif pour reduire les vibrations engendrees par un rotor de sustentation d'un aeronef a voilure tournante
US6073887A (en) * 1997-07-16 2000-06-13 Space Systems/Loral, Inc. High power spacecraft with full utilization of all spacecraft surfaces
US6073888A (en) * 1998-12-02 2000-06-13 Loral Space & Communications, Ltd. Sequenced heat rejection for body stabilized geosynchronous satellites
GB0004649D0 (en) * 2000-02-29 2000-04-19 Gkn Westland Helicopters Ltd Vibration damping apparatus
WO2002027210A1 (en) * 2000-09-26 2002-04-04 Bell Helicopter Textron Inc. Method and apparatus for improved vibration isolation
US6851529B2 (en) * 2002-04-18 2005-02-08 Honeywell International Inc. Multifunction vibration isolation strut
US6769644B2 (en) * 2002-12-23 2004-08-03 The Boeing Company Tail boom saddle for maintaining helicoptor main rotor blades in a stowed configuration for helicopter stowage and transport
US7370829B2 (en) * 2004-06-10 2008-05-13 Lord Corporation Method and system for controlling helicopter vibrations
US7490792B1 (en) * 2004-11-16 2009-02-17 Cartercopters, L.L.C. Aircraft with rotor vibration isolation
DE602005008019D1 (de) 2005-05-16 2008-08-21 Agusta Spa Hubschrauber mit verbesserter Schwingungskontrollvorrichtung
US7717368B2 (en) * 2005-06-07 2010-05-18 Urban Aeronautics Ltd. Apparatus for generating horizontal forces in aerial vehicles and related method
FR2889687B1 (fr) * 2005-08-10 2007-11-30 Eurocopter France Procede de decouplage solidien selectif de bruit, rotule lamifie, liaison mecanique et aeronef.

Also Published As

Publication number Publication date
EP2071924A2 (en) 2009-06-24
KR20090076903A (ko) 2009-07-13
WO2008045073A3 (en) 2008-11-27
DE06849841T1 (de) 2009-10-08
CN101522521A (zh) 2009-09-02
CA2665700C (en) 2013-11-19
CN101522521B (zh) 2013-06-12
CA2665700A1 (en) 2008-04-17
EP2071924B1 (en) 2013-09-18
EP2071924A4 (en) 2012-12-19
US8328129B2 (en) 2012-12-11
US20100090055A1 (en) 2010-04-15
WO2008045073A2 (en) 2008-04-17

Similar Documents

Publication Publication Date Title
BRPI0622047A2 (pt) Pilone de montagem rígida com atenuação de vibração
EP2095986A4 (en) ENGINE STORAGE STRUCTURE
DK2155138T3 (da) Vibrationsindretning
DE602008004003D1 (de) Elastische Triebwerksbefestigung
DE112008002758A5 (de) Befestigungsbeschlag
BRPI0712078A2 (pt) suporte de montagem ajustÁvel
DE502005008248D1 (de) Befestigungselement
BRPI0817276A2 (pt) Montagem restringidora
BRPI0817249A2 (pt) Montagem restringidora
FR2904389B1 (fr) Palier de montage elastique
DE602007003901D1 (de) Anbringungsstruktur
DE602007001179D1 (de) Vibrationsdämpfendes Element
BRPI0907549A2 (pt) unidade de montagem
DE502007006739D1 (de) Befestigungsclip
ATE459770T1 (de) Montageelement
DE602007005079D1 (de) Tintenbefestigungsanordnung
DE502007002527D1 (de) Befestigungsclip
DE502007000874D1 (de) Befestigungsanordnung mit lösbarer Verrastung
FI20065364A0 (fi) Värähtelyn vaimennusjärjestelmä
BRPI0821527A2 (pt) Montagem de alcaraviz
BRPI0915035A2 (pt) montagem de motor
FI20085203A0 (fi) Värähtelyn vaimennusjärjestely
DE112008003789A5 (de) Schwingungsdämpfer
DE602007006818D1 (de) Montageanordnung
RU55310U8 (ru) Виброизолятор

Legal Events

Date Code Title Description
B11A Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing
B11Y Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette]