FR2306876A1 - Amortisseur de vibrations pour rotor d'helicoptere - Google Patents

Amortisseur de vibrations pour rotor d'helicoptere

Info

Publication number
FR2306876A1
FR2306876A1 FR7610630A FR7610630A FR2306876A1 FR 2306876 A1 FR2306876 A1 FR 2306876A1 FR 7610630 A FR7610630 A FR 7610630A FR 7610630 A FR7610630 A FR 7610630A FR 2306876 A1 FR2306876 A1 FR 2306876A1
Authority
FR
France
Prior art keywords
vibration damper
helicopter rotor
rotor vibration
helicopter
damper
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.)
Granted
Application number
FR7610630A
Other languages
English (en)
Other versions
FR2306876B1 (fr
Inventor
Larry Bruce Eastman
Irwin Jeffrey Kenigsberg
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of FR2306876A1 publication Critical patent/FR2306876A1/fr
Application granted granted Critical
Publication of FR2306876B1 publication Critical patent/FR2306876B1/fr
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/001Vibration damping devices
    • 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
    • F16F15/10Suppression of vibrations in rotating systems by making use of members moving with the system
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00Fluid reaction surfaces, i.e. impellers
    • Y10S416/50Vibration damping features

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Mechanical Operated Clutches (AREA)
  • Vibration Dampers (AREA)
  • Vibration Prevention Devices (AREA)
FR7610630A 1975-04-11 1976-04-12 Amortisseur de vibrations pour rotor d'helicoptere Granted FR2306876A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/567,158 US3988073A (en) 1975-04-11 1975-04-11 Spherical bifilar tuning pin bushing

Publications (2)

Publication Number Publication Date
FR2306876A1 true FR2306876A1 (fr) 1976-11-05
FR2306876B1 FR2306876B1 (fr) 1980-04-04

Family

ID=24265959

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7610630A Granted FR2306876A1 (fr) 1975-04-11 1976-04-12 Amortisseur de vibrations pour rotor d'helicoptere

Country Status (8)

Country Link
US (1) US3988073A (fr)
JP (1) JPS51126699A (fr)
CA (1) CA1037451A (fr)
DE (1) DE2615692A1 (fr)
FR (1) FR2306876A1 (fr)
GB (1) GB1537683A (fr)
IL (1) IL49335A0 (fr)
IT (1) IT1059707B (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4057363A (en) * 1975-11-20 1977-11-08 United Technologies Corporation Extended arm bifilar and method to eliminate second order vibration excitation
US4239455A (en) * 1978-09-11 1980-12-16 Textron, Inc. Blade-mounted centrifugal pendulum
DE3420570C1 (de) * 1984-06-01 1989-12-14 SGF Süddeutsche Gelenkscheibenfabrik GmbH & Co KG, 8264 Waldkraiburg Drehschwingungstilger
US5126641A (en) * 1991-03-08 1992-06-30 Westinghouse Electric Corp. Bidirectional variable reluctance actuator and system for active attenuation of vibration and structure borne noise utilizing same
US5495924A (en) * 1994-07-13 1996-03-05 Quiescence Engineering Corp. Half-order centrifugal pendulum vibration absorber system
FR2733483B1 (fr) * 1995-04-27 1997-07-04 Eurocopter France Dispositif d'attenuation de vibrations pour rotor d'helicoptere
AU2532999A (en) * 1998-02-13 1999-08-30 Automotive Products Plc Torsional vibration dampers
US10577089B2 (en) * 2017-05-03 2020-03-03 Sikorsky Aircraft Corporation Integrated bifilar system that absorbs vibrations in both vertical and in-plane directions

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2203951A1 (fr) * 1972-10-19 1974-05-17 Westland Aircraft Ltd

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3372758A (en) * 1967-02-15 1968-03-12 United Aircraft Corp Vibration absorber
US3540809A (en) * 1968-09-20 1970-11-17 United Aircraft Corp Vibration damped helicopter rotor
GB1445686A (en) * 1972-11-06 1976-08-11 Westland Aircraft Ltd Vibration absorbing systems

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2203951A1 (fr) * 1972-10-19 1974-05-17 Westland Aircraft Ltd

Also Published As

Publication number Publication date
GB1537683A (en) 1979-01-04
USB567158I5 (fr) 1976-03-23
US3988073A (en) 1976-10-26
DE2615692A1 (de) 1976-11-11
FR2306876B1 (fr) 1980-04-04
CA1037451A (fr) 1978-08-29
IL49335A0 (en) 1976-07-30
JPS51126699A (en) 1976-11-04
IT1059707B (it) 1982-06-21

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Legal Events

Date Code Title Description
ST Notification of lapse