ES484029A1 - Perfeccionamientos en pendulos centrifugos de absorcion de vibraciones para rotores de helicopteros - Google Patents

Perfeccionamientos en pendulos centrifugos de absorcion de vibraciones para rotores de helicopteros

Info

Publication number
ES484029A1
ES484029A1 ES484029A ES484029A ES484029A1 ES 484029 A1 ES484029 A1 ES 484029A1 ES 484029 A ES484029 A ES 484029A ES 484029 A ES484029 A ES 484029A ES 484029 A1 ES484029 A1 ES 484029A1
Authority
ES
Spain
Prior art keywords
blade
centrifugal pendulum
rotor
plane
mounted centrifugal
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
Application number
ES484029A
Other languages
English (en)
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.)
Textron Inc
Original Assignee
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 Textron Inc filed Critical Textron Inc
Publication of ES484029A1 publication Critical patent/ES484029A1/es
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/001—Vibration damping devices
    • 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
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/50—Vibration damping features

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Apparatuses For Generation Of Mechanical Vibrations (AREA)
  • Vibration Prevention Devices (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Perfeccionamientos en péndulos centrífugos de absorción de vibraciones para rotores de helicópteros, caracterizados porque comprende en el rotor una pluralidad de palas sujetas a un conjunto de mástil-cabeza por medio de dispositivos de agarre de las palas, cuya combinación comprende: a) un par de dispositivos de pivote, cada uno de los cuales se extiende a través de cada dispositivo de agarre diametralmente opuestos y equidistantes al eje del mástil y prácticamente perpendiculares al eje cordal de la pala; y b) masas montadas en forma de péndulos simples, dos en cada pivote y simétricos al eje de orientación de la pala.
ES484029A 1978-09-11 1979-09-10 Perfeccionamientos en pendulos centrifugos de absorcion de vibraciones para rotores de helicopteros Expired ES484029A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/941,134 US4239455A (en) 1978-09-11 1978-09-11 Blade-mounted centrifugal pendulum

Publications (1)

Publication Number Publication Date
ES484029A1 true ES484029A1 (es) 1980-04-01

Family

ID=25475978

Family Applications (1)

Application Number Title Priority Date Filing Date
ES484029A Expired ES484029A1 (es) 1978-09-11 1979-09-10 Perfeccionamientos en pendulos centrifugos de absorcion de vibraciones para rotores de helicopteros

Country Status (13)

Country Link
US (1) US4239455A (es)
JP (1) JPS5555097A (es)
AR (1) AR222190A1 (es)
AU (1) AU528568B2 (es)
BR (1) BR7905806A (es)
CA (1) CA1102773A (es)
DE (1) DE2936340A1 (es)
ES (1) ES484029A1 (es)
FR (1) FR2435391A1 (es)
GB (1) GB2030949B (es)
IL (1) IL58219A (es)
IT (1) IT1162392B (es)
MX (1) MX6857E (es)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3226152C2 (de) * 1982-07-13 1984-07-19 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Pendelanordnung zur Dämpfung bzw. Tilgung niedriger Anregungsfrequenzen eines Hubschrauberrotorblattes o.dgl.
IT1205404B (it) * 1983-05-05 1989-03-15 Agusta Aeronaut Costr Rotore per elicotteri
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
US5647726A (en) * 1996-02-15 1997-07-15 Bell Helicopter Textron Inc. Rotor system vibration absorber
US5924845A (en) * 1997-04-07 1999-07-20 The United States Of America As Represented By The Secretary Of The Air Force Centrifugal pendulum absorber for engine blades
FR2768995B1 (fr) * 1997-10-01 1999-12-03 Eurocopter France Resonateur pendulaire de tete de rotor
ITMI991127A1 (it) * 1998-05-28 2000-11-21 Eurocopter Deutschland Pala per un rotore privo di supporto di un elicottero
DE10035334B4 (de) 2000-07-20 2007-11-29 Eurocopter Deutschland Gmbh Flugzeugtür und eine Außenhaut einer Flugzeugtür
FR2945788B1 (fr) * 2009-05-20 2011-05-13 Eurocopter France Dispositif a masses concentrees pour reduire les vibrations engendrees par un rotor de sustentation d'un giravion, et moyeu d'un rotor muni d'un tel dispositif
FR2945789B1 (fr) * 2009-05-20 2011-05-13 Eurocopter France Dispositif a masses reparties pour reduire les vibrations engendrees par un rotor de sustentation d'un giravion, et moyeu d'un rotor muni d'un tel dispositif
US20110085924A1 (en) * 2009-10-09 2011-04-14 Rod Shampine Pump assembly vibration absorber system
FR2959484B1 (fr) 2010-04-30 2012-11-09 Eurocopter France Dispositif pour reduire les vibrations engendrees par un rotor de sustentation d'un giravion, et moyeu d'un rotor muni d'un tel dispositif.
FR3011529B1 (fr) * 2013-10-09 2017-03-10 Snecma Pivot de pale d'helice aerienne
FR3029170B1 (fr) * 2014-11-28 2016-12-30 Airbus Helicopters Rotor arriere de giravion, giravion equipe d'un tel rotor arriere et procede d'equilibrage statique et/ou dynamique d'un rotor arriere de giravion
US10604246B2 (en) * 2016-01-21 2020-03-31 Sikorsky Aircraft Corporation Rotorcraft rotor assemblies
CN106768920A (zh) * 2016-11-29 2017-05-31 中国直升机设计研究所 一种疲劳试验装置
FR3102751A1 (fr) 2019-11-04 2021-05-07 Innostar Rotor d’aéronef mono-pale.
US20220332409A1 (en) * 2021-04-16 2022-10-20 Lockheed Martin Corporation Tunable mass damper assembly for a rotor blade

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE672424C (de) * 1936-03-14 1939-03-02 Paul Konrad Drehschwingungsdaempfer fuer Spanndraehte, Trag- und Leitwerksflaechen und Einstellvorrichtung fuer Luftschrauben
US2426130A (en) * 1944-12-12 1947-08-19 United Aircraft Corp Rotor blade
US2519762A (en) * 1945-07-09 1950-08-22 United Aircraft Corp Gyrodynamic damper
US2638170A (en) * 1947-06-28 1953-05-12 Richard H Prewitt Aircraft propeller or rotor
GB754033A (en) * 1953-06-11 1956-08-01 Sncaso Rotor and stabilising mechanism, especially for helicopters
US2934151A (en) * 1958-02-24 1960-04-26 United Aircraft Corp Helicopter rotor
US3035643A (en) * 1959-10-13 1962-05-22 Bell Aerospace Corp Device to alter dynamic characteristics of rotor systems
DE1176489B (de) * 1962-02-15 1964-08-20 Dornier Werke Gmbh Drehfluegelsystem mit gelenkigem oder ela-stischem Anschluss der Fluegelblaetter
US3289770A (en) * 1963-08-14 1966-12-06 Bolkow Gmbh Helicopter rotor system
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
GB1443148A (en) * 1972-10-19 1976-07-21 Westland Aircraft Ltd Bifilar vibration dampers
GB1445686A (en) * 1972-11-06 1976-08-11 Westland Aircraft Ltd Vibration absorbing systems
GB1468359A (en) * 1973-10-09 1977-03-23 Westland Aircraft Ltd Bifilar vibration dampers
US3988073A (en) * 1975-04-11 1976-10-26 United Technologies Corporation Spherical bifilar tuning pin bushing
FR2353439A1 (fr) * 1976-06-04 1977-12-30 Aerospatiale Dispositif pour absorber les vibrations produites par le rotor d'un aeronef

Also Published As

Publication number Publication date
US4239455A (en) 1980-12-16
JPH0159158B2 (es) 1989-12-15
GB2030949A (en) 1980-04-16
AU528568B2 (en) 1983-05-05
FR2435391B1 (es) 1983-11-18
JPS5555097A (en) 1980-04-22
FR2435391A1 (fr) 1980-04-04
AR222190A1 (es) 1981-04-30
CA1102773A (en) 1981-06-09
IT7950204A0 (it) 1979-09-07
IT1162392B (it) 1987-03-25
DE2936340A1 (de) 1980-04-03
BR7905806A (pt) 1980-05-20
IL58219A (en) 1981-12-31
AU5061779A (en) 1980-03-20
GB2030949B (en) 1982-07-28
MX6857E (es) 1986-09-08
DE2936340C2 (es) 1988-10-13

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19990301