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PL3252339T3 - Rezonator, i statek powietrzny wyposażony w taki rezonator - Google Patents

Rezonator, i statek powietrzny wyposażony w taki rezonator

Info

Publication number
PL3252339T3
PL3252339T3 PL17171691T PL17171691T PL3252339T3 PL 3252339 T3 PL3252339 T3 PL 3252339T3 PL 17171691 T PL17171691 T PL 17171691T PL 17171691 T PL17171691 T PL 17171691T PL 3252339 T3 PL3252339 T3 PL 3252339T3
Authority
PL
Poland
Prior art keywords
resonator
aircraft fitted
aircraft
fitted
Prior art date
Application number
PL17171691T
Other languages
English (en)
Inventor
Guillaume INQUIETE
Paul Cranga
Simon CHESNE
Original Assignee
Airbus Helicopters
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 Airbus Helicopters filed Critical Airbus Helicopters
Publication of PL3252339T3 publication Critical patent/PL3252339T3/pl

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F7/00—Vibration-dampers; Shock-absorbers
    • F16F7/10—Vibration-dampers; Shock-absorbers using inertia effect
    • F16F7/1005—Vibration-dampers; Shock-absorbers using inertia effect characterised by active control of the mass
    • F16F7/1011—Vibration-dampers; Shock-absorbers using inertia effect characterised by active control of the mass by electromagnetic means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/001—Vibration damping devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/002—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion characterised by the control method or circuitry
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02—Suppression 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02—Suppression 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
    • F16F15/03—Suppression 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 using magnetic or electromagnetic means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F7/00—Vibration-dampers; Shock-absorbers
    • F16F7/10—Vibration-dampers; Shock-absorbers using inertia effect
    • F16F7/1005—Vibration-dampers; Shock-absorbers using inertia effect characterised by active control of the mass
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P1/00—Details of instruments
    • G01P1/003—Details of instruments used for damping
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
    • G01P15/02—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
    • G01P15/08—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/001—Vibration damping devices
    • B64C2027/004—Vibration damping devices using actuators, e.g. active systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/001—Vibration damping devices
    • B64C2027/005—Vibration damping devices using suspended masses

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Acoustics & Sound (AREA)
  • Electromagnetism (AREA)
  • General Physics & Mathematics (AREA)
  • Vibration Prevention Devices (AREA)
PL17171691T 2016-06-02 2017-05-18 Rezonator, i statek powietrzny wyposażony w taki rezonator PL3252339T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1600893A FR3052209B1 (fr) 2016-06-02 2016-06-02 Resonateur, et aeronef muni de ce resonateur
EP17171691.3A EP3252339B1 (fr) 2016-06-02 2017-05-18 Resonateur, et aeronef muni de ce resonateur

Publications (1)

Publication Number Publication Date
PL3252339T3 true PL3252339T3 (pl) 2019-04-30

Family

ID=56896612

Family Applications (1)

Application Number Title Priority Date Filing Date
PL17171691T PL3252339T3 (pl) 2016-06-02 2017-05-18 Rezonator, i statek powietrzny wyposażony w taki rezonator

Country Status (5)

Country Link
US (1) US10472055B2 (pl)
EP (1) EP3252339B1 (pl)
KR (1) KR101989941B1 (pl)
FR (1) FR3052209B1 (pl)
PL (1) PL3252339T3 (pl)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10345105B2 (en) * 2017-05-31 2019-07-09 The United States Of America As Represented By Secretary Of The Navy Simplified time domain switched ring/disk resonant gyroscope
US11561479B2 (en) 2019-02-04 2023-01-24 Asml Netherlands B.V. Electronic system, accelerometer, calibration method, lithographic apparatus and device manufacturing method
EP3750801B1 (en) * 2019-06-13 2021-08-04 LEONARDO S.p.A. Rotor for a hover-capable aircraft
WO2022129865A1 (en) 2020-12-15 2022-06-23 Bae Systems Plc Vibration control systems
EP4015867A1 (en) * 2020-12-15 2022-06-22 BAE SYSTEMS plc Improvements in and relating to vibration control systems
CA3205043A1 (en) * 2020-12-15 2022-06-23 Bae Systems Plc Improvements in and relating to vibration control systems
GB2602016B (en) * 2020-12-15 2025-01-08 Bae Systems Plc Improvements in and relating to vibration control systems
CN114876995B (zh) * 2022-02-08 2023-04-07 上海交通大学 多维自适应振动与噪声控制装置

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5456341A (en) 1993-04-23 1995-10-10 Moog Inc. Method and apparatus for actively adjusting and controlling a resonant mass-spring system
GB9523651D0 (en) 1995-11-18 1996-01-17 Gkn Westland Helicopters Ltd Helicopter and method for reucing vibration of a helicopter fuselage
FR2770825B1 (fr) 1997-11-13 1999-12-31 Eurocopter France Dispositif pour reduire les vibrations dans la cabine d'un aeronef a voilure tournante, notamment un helicoptere
FR2784350B1 (fr) 1998-10-12 2000-12-08 Eurocopter France Dispositif pour reduire des vibrations engendrees sur la structure d'un aeronef a voilure tournante
US6393913B1 (en) * 2000-02-08 2002-05-28 Sandia Corporation Microelectromechanical dual-mass resonator structure
US6826493B1 (en) * 2003-09-02 2004-11-30 Tao Of Systems Integration, Inc. System and method for real time determination of unsteady aerodynamic loads
US20080309910A1 (en) * 2007-05-31 2008-12-18 Nikon Corporation Vibration isolating apparatus, control method for vibration isolating apparatus, and exposure apparatus
US8973724B2 (en) * 2007-07-17 2015-03-10 Honeywell International Inc. Vibration isolators and isolation systems
US8002233B2 (en) * 2007-09-24 2011-08-23 Honeywell International Inc. Distributed network vibration isolation system and vibration isolators useful therein
FR2954273B1 (fr) * 2009-12-17 2012-02-24 Eurocopter France Structure porteuse d'un rotor, et appareil volant muni d'une telle structure porteuse
FR2954274B1 (fr) * 2009-12-17 2012-02-24 Eurocopter France Mecanisme amortisseur de vibrations, et appareil volant muni d'une structure porteuse et d'un rotor muni d'un tel mecanisme
FR2961570B1 (fr) 2010-06-17 2013-04-26 Eurocopter France Dispositif pour amortir les vibrations d'une structure.
DE102012222988B4 (de) * 2012-12-12 2021-09-23 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Mikromechanische Resonatoranordnung
FR3010386B1 (fr) * 2013-09-06 2017-01-06 Eurocopter France Dispositif de suspension antivibratoire d'un element mecanique et aeronef
EP2921842B1 (de) * 2014-03-18 2020-06-24 Russenberger Prüfmaschinen AG Resonanzprüfmaschine

Also Published As

Publication number Publication date
US20170349271A1 (en) 2017-12-07
US10472055B2 (en) 2019-11-12
KR101989941B1 (ko) 2019-09-30
KR20170137003A (ko) 2017-12-12
FR3052209B1 (fr) 2018-06-01
EP3252339B1 (fr) 2018-10-24
EP3252339A1 (fr) 2017-12-06
FR3052209A1 (fr) 2017-12-08

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