FR2205640A1 - - Google Patents

Info

Publication number
FR2205640A1
FR2205640A1 FR7339164A FR7339164A FR2205640A1 FR 2205640 A1 FR2205640 A1 FR 2205640A1 FR 7339164 A FR7339164 A FR 7339164A FR 7339164 A FR7339164 A FR 7339164A FR 2205640 A1 FR2205640 A1 FR 2205640A1
Authority
FR
France
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.)
Withdrawn
Application number
FR7339164A
Other languages
French (fr)
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.)
Westland Group PLC
Original Assignee
Westland Aircraft Ltd
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 Westland Aircraft Ltd filed Critical Westland Aircraft Ltd
Publication of FR2205640A1 publication Critical patent/FR2205640A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • 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
    • F16F15/14Suppression of vibrations in rotating systems by making use of members moving with the system using masses freely rotating with the system, i.e. uninvolved in transmitting driveline torque, e.g. rotative dynamic dampers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/001Vibration damping devices
    • 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)
  • Vibration Prevention Devices (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Vibration Dampers (AREA)
FR7339164A 1972-11-06 1973-11-05 Withdrawn FR2205640A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5108872A GB1445686A (en) 1972-11-06 1972-11-06 Vibration absorbing systems

Publications (1)

Publication Number Publication Date
FR2205640A1 true FR2205640A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1974-05-31

Family

ID=10458613

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7339164A Withdrawn FR2205640A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1972-11-06 1973-11-05

Country Status (7)

Country Link
US (1) US3887296A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
CA (1) CA972738A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE2354973A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
FR (1) FR2205640A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
GB (1) GB1445686A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
IN (1) IN138438B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
IT (1) IT996371B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2530216A1 (fr) * 1982-07-13 1984-01-20 Messerschmitt Boelkow Blohm Pendule pour l'amortissement ou la suppression des basses frequences d'excitation d'une pale de rotor d'helicoptere ou analogue
EP0147694A3 (de) * 1983-12-10 1985-11-27 Johann Klug Schwungrad

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3988073A (en) * 1975-04-11 1976-10-26 United Technologies Corporation Spherical bifilar tuning pin bushing
US3988074A (en) * 1975-11-13 1976-10-26 United Technologies Corporation Anhedral bifilar
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
NL1005000C2 (nl) * 1997-01-14 1998-07-15 Aerpac Special Products B V Windturbine.
PT1101034E (pt) * 1998-07-28 2005-08-31 Neg Micon As Pa de turbina eolica com um meio de amortecimento de oscilacoes em forma de u
US6493689B2 (en) * 2000-12-29 2002-12-10 General Dynamics Advanced Technology Systems, Inc. Neural net controller for noise and vibration reduction
FR2894040B1 (fr) * 2005-11-28 2011-10-21 Eurocopter France Dispositif d'asservissement pour un vibrateur a rotors desequilibres.
CN107148383B (zh) * 2016-05-31 2019-03-08 深圳市大疆创新科技有限公司 无人飞行器的机架及无人飞行器

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2353681A (en) * 1939-11-03 1944-07-18 United Aircraft Corp Propeller hub damper
US2349187A (en) * 1941-03-08 1944-05-16 Westinghouse Electric & Mfg Co Vibration dampener
US2462961A (en) * 1945-01-24 1949-03-01 United Aircraft Corp Propeller blade vibration absorber
US2462962A (en) * 1945-09-26 1949-03-01 United Aircraft Corp Blade vibration absorber
US3540809A (en) * 1968-09-20 1970-11-17 United Aircraft Corp Vibration damped helicopter rotor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2530216A1 (fr) * 1982-07-13 1984-01-20 Messerschmitt Boelkow Blohm Pendule pour l'amortissement ou la suppression des basses frequences d'excitation d'une pale de rotor d'helicoptere ou analogue
EP0147694A3 (de) * 1983-12-10 1985-11-27 Johann Klug Schwungrad

Also Published As

Publication number Publication date
IT996371B (it) 1975-12-10
DE2354973A1 (de) 1974-07-18
CA972738A (en) 1975-08-12
US3887296A (en) 1975-06-03
IN138438B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1976-01-31
GB1445686A (en) 1976-08-11

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Legal Events

Date Code Title Description
ST Notification of lapse