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DE60100743D1 - Verfahren zum feststellen eines minimalen rotorblattnachstellungsatzes - Google Patents

Verfahren zum feststellen eines minimalen rotorblattnachstellungsatzes

Info

Publication number
DE60100743D1
DE60100743D1 DE60100743T DE60100743T DE60100743D1 DE 60100743 D1 DE60100743 D1 DE 60100743D1 DE 60100743 T DE60100743 T DE 60100743T DE 60100743 T DE60100743 T DE 60100743T DE 60100743 D1 DE60100743 D1 DE 60100743D1
Authority
DE
Germany
Prior art keywords
determining
rotor blade
adjustment block
blade adjustment
minimum rotor
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
Application number
DE60100743T
Other languages
English (en)
Other versions
DE60100743T2 (de
Inventor
Samuel Ventres
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Simmonds Precision Products Inc
Original Assignee
Simmonds Precision Products 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 Simmonds Precision Products Inc filed Critical Simmonds Precision Products Inc
Publication of DE60100743D1 publication Critical patent/DE60100743D1/de
Application granted granted Critical
Publication of DE60100743T2 publication Critical patent/DE60100743T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/008Rotors tracking or balancing devices
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/001Vibration damping devices
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D9/00Level control, e.g. controlling quantity of material stored in vessel
    • G05D9/12Level control, e.g. controlling quantity of material stored in vessel characterised by the use of electric means

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
  • Testing Of Balance (AREA)
DE60100743T 2000-02-24 2001-02-21 Verfahren zum feststellen eines minimalen rotorblattnachstellungsatzes Expired - Fee Related DE60100743T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US512690 1990-04-23
US09/512,690 US6415206B1 (en) 2000-02-24 2000-02-24 Method for determining a minimal set of rotor blade adjustments
PCT/US2001/005524 WO2001062590A1 (en) 2000-02-24 2001-02-21 Method for determining a minimal set of rotor blade adjustments

Publications (2)

Publication Number Publication Date
DE60100743D1 true DE60100743D1 (de) 2003-10-16
DE60100743T2 DE60100743T2 (de) 2004-07-01

Family

ID=24040131

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60100743T Expired - Fee Related DE60100743T2 (de) 2000-02-24 2001-02-21 Verfahren zum feststellen eines minimalen rotorblattnachstellungsatzes

Country Status (6)

Country Link
US (1) US6415206B1 (de)
EP (1) EP1257463B1 (de)
AT (1) ATE249358T1 (de)
AU (1) AU2001241619A1 (de)
DE (1) DE60100743T2 (de)
WO (1) WO2001062590A1 (de)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6687572B2 (en) * 2001-11-15 2004-02-03 Honeywell International Inc. Supervisory method and system for improved control model updates applied to dynamic balancing
AU2002313053A1 (en) * 2002-03-18 2003-10-20 Eurocopter Method and device for detecting defects of at least one rotary wing aircraft rotor
US6950763B1 (en) 2002-11-27 2005-09-27 Simmonds Precision Products, Inc. Optimal shaft balance using integer programming to handle discrete adjustment
US6814543B2 (en) 2002-12-30 2004-11-09 General Electric Company Method and apparatus for bucket natural frequency tuning
FR2871438B1 (fr) * 2004-06-10 2006-08-04 Eurocopter France Procede pour regler au moins un rotor deficient d'un giravion
FR2871435B1 (fr) * 2004-06-10 2006-08-18 Eurocopter France Dispositif d'indication d'un niveau de battement
US7512463B1 (en) 2005-02-16 2009-03-31 Simmonds Precision Products, Inc. Reducing vibration using QR decomposition and unconstrained optimization for a multi-rotor aircraft
US8041520B2 (en) * 2007-09-26 2011-10-18 Gilbert Ronald Mesec Method to detect mechanical faults and dynamic instability in rotor systems of helicopters, tilt rotor aircraft, and whirl towers
US8496434B2 (en) * 2009-05-21 2013-07-30 Textron Innovations Inc. Differential pitch-control to optimize co-rotating stacked rotor performance
US8639458B2 (en) * 2010-02-02 2014-01-28 Simmonds Precision Products, Inc. Techniques for use with rotor track and balance to reduce vibration
EP2576344A2 (de) 2010-05-26 2013-04-10 Lord Corporation Aktive echtzeitvibrationskontrolle für hubschrauber sowie rotorverfolgungs- und -balancesysteme
US8812255B2 (en) 2010-09-28 2014-08-19 Simmonds Precision Products, Inc. Wireless rotor track and balance system for rotorcraft
US20130092786A1 (en) * 2011-10-13 2013-04-18 Sikorsky Aircraft Corporation Interferometric strain field sensor system for measuring rotor state
US8766578B2 (en) * 2012-02-27 2014-07-01 Canadian Space Agency Method and apparatus for high velocity ripple suppression of brushless DC motors having limited drive/amplifier bandwidth
US10065732B2 (en) * 2012-08-21 2018-09-04 Technology For Energy Corporation Systems and methods of tracking rotor blades
US9758258B2 (en) * 2012-11-29 2017-09-12 Sirkorsky Aircraft Corporation Rotary wing aircraft blade tracking
US9758243B1 (en) 2013-03-06 2017-09-12 RMCI, Inc. Calculation of helicopter rotor balance adjustments and coefficients using mobile devices or custom coefficients
US9026277B2 (en) * 2013-09-12 2015-05-05 Sikorsky Aircraft Corporation Rotor track and balance with improved linear optimization
EP3055207B1 (de) * 2013-10-10 2018-10-03 UMS Skeldar Sweden AB System und verfahren zur messung des winkels eines hubschrauberschlaggelenks
US9243979B2 (en) * 2014-01-14 2016-01-26 Simmonds Precision Products, Inc. System and method for adjustment response analysis
EP3239039B1 (de) * 2016-04-29 2019-07-24 Ratier-Figeac SAS Blattstruktur-gesundheitsüberwachungssystem

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3945256A (en) 1975-04-21 1976-03-23 Chadwick-Helmuth Company, Inc. Helicopter rotor balancing apparatus and method
GB2159484A (en) 1984-05-22 1985-12-04 Micro Control Tech Ltd Method and apparatus for tracking a helicopter rotor or other rotating mass
US4937758A (en) 1987-09-04 1990-06-26 Technology Integration And Development Group, Inc. Method and apparatus for reducing vibration over the full operating range of a rotor and a host device
US4999534A (en) * 1990-01-19 1991-03-12 Contraves Goerz Corporation Active vibration reduction in apparatus with cross-coupling between control axes
US5049795A (en) * 1990-07-02 1991-09-17 Westinghouse Electric Corp. Multivariable adaptive vibration canceller
US5206816A (en) * 1991-01-30 1993-04-27 Westinghouse Electric Corp. System and method for monitoring synchronous blade vibration
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.
US5471880A (en) * 1994-04-28 1995-12-05 Electric Power Research Institute Method and apparatus for isolating and identifying periodic Doppler signals in a turbine
DE19627869A1 (de) * 1996-07-11 1998-01-15 Zf Luftfahrttechnik Gmbh Hubschrauber
US5815307A (en) * 1997-03-26 1998-09-29 The Board Of Trustees Of The Leland Stanford Junior University Aperiodic quasi-phasematching gratings for chirp adjustments and frequency conversion of ultra-short pulses
US5990712A (en) * 1997-10-03 1999-11-23 Motorola, Inc. Harmonic generator
US6208949B1 (en) * 1998-07-01 2001-03-27 Adaptive Audio, Inc. Method and apparatus for dynamical system analysis
US6094989A (en) * 1998-08-21 2000-08-01 Siemens Westinghouse Power Corporation Method and apparatus for analyzing non-synchronous blade vibrations using unevenly spaced probes

Also Published As

Publication number Publication date
US6415206B1 (en) 2002-07-02
AU2001241619A1 (en) 2001-09-03
EP1257463B1 (de) 2003-09-10
ATE249358T1 (de) 2003-09-15
EP1257463A1 (de) 2002-11-20
WO2001062590A1 (en) 2001-08-30
DE60100743T2 (de) 2004-07-01

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee