FR2353439A1 - Dispositif pour absorber les vibrations produites par le rotor d'un aeronef - Google Patents

Dispositif pour absorber les vibrations produites par le rotor d'un aeronef

Info

Publication number
FR2353439A1
FR2353439A1 FR7616969A FR7616969A FR2353439A1 FR 2353439 A1 FR2353439 A1 FR 2353439A1 FR 7616969 A FR7616969 A FR 7616969A FR 7616969 A FR7616969 A FR 7616969A FR 2353439 A1 FR2353439 A1 FR 2353439A1
Authority
FR
France
Prior art keywords
hub
high density
vibration absorber
metal ball
sides forming
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
FR7616969A
Other languages
English (en)
Other versions
FR2353439B1 (fr
Inventor
Rene Louis Mouille
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Group SAS filed Critical Airbus Group SAS
Priority to FR7616969A priority Critical patent/FR2353439A1/fr
Publication of FR2353439A1 publication Critical patent/FR2353439A1/fr
Application granted granted Critical
Publication of FR2353439B1 publication Critical patent/FR2353439B1/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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/001Vibration damping devices
    • B64C2027/003Vibration damping devices mounted on rotor hub, e.g. a rotary force generator

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Prevention Devices (AREA)
FR7616969A 1976-06-04 1976-06-04 Dispositif pour absorber les vibrations produites par le rotor d'un aeronef Granted FR2353439A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7616969A FR2353439A1 (fr) 1976-06-04 1976-06-04 Dispositif pour absorber les vibrations produites par le rotor d'un aeronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7616969A FR2353439A1 (fr) 1976-06-04 1976-06-04 Dispositif pour absorber les vibrations produites par le rotor d'un aeronef

Publications (2)

Publication Number Publication Date
FR2353439A1 true FR2353439A1 (fr) 1977-12-30
FR2353439B1 FR2353439B1 (fr) 1981-08-28

Family

ID=9174019

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7616969A Granted FR2353439A1 (fr) 1976-06-04 1976-06-04 Dispositif pour absorber les vibrations produites par le rotor d'un aeronef

Country Status (1)

Country Link
FR (1) FR2353439A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2435391A1 (fr) * 1978-09-11 1980-04-04 Textron Inc Pendule centrifuge monte sur une pale de rotor d'helicoptere
WO1999014114A1 (fr) * 1997-09-15 1999-03-25 Sikorsky Aircraft Corporation Masse inertielle pour isolateurs de vibrations

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2435391A1 (fr) * 1978-09-11 1980-04-04 Textron Inc Pendule centrifuge monte sur une pale de rotor d'helicoptere
WO1999014114A1 (fr) * 1997-09-15 1999-03-25 Sikorsky Aircraft Corporation Masse inertielle pour isolateurs de vibrations

Also Published As

Publication number Publication date
FR2353439B1 (fr) 1981-08-28

Similar Documents

Publication Publication Date Title
JP3034951B2 (ja) 振動制動器
GB2133152B (en) Accelerometer with beam resonator force transducer
GB2123371B (en) Pendulum for damping low excitation frequencies of helicopter rotor blade of the like
IL58219A (en) Apparatus for reducing vibration at the hub of a helicopter rotor assembly
FR2353439A1 (fr) Dispositif pour absorber les vibrations produites par le rotor d'un aeronef
JPS5347147A (en) Heat source device
US3075619A (en) Vibration suppressor
FR2362311A1 (fr) Amortisseur de vibrations pour vilebrequin
JPS52127606A (en) Compressor
JPS56138541A (en) Vibration absorbing structure
JPS57106451A (en) Ultrasonic vibration mold for continuous casting
FR2449593A1 (fr) Dispositif de suspension du fuselage a la transmission d'un helicoptere
GEORGE Research on helicopter rotor noise[Final Report, 2 Oct. 1973- 31 Dec. 1974]
SU418642A1 (fr)
JPS5684156A (en) Continuous casting method of molten metal
JPS57140501A (en) Rotary blade
JPS52109215A (en) Vibration damper wheel for railway
Laura et al. Vibrations of beams and plates with edges elastically restrained against rotation carrying elastically mounted masses
SU1608020A1 (ru) Установка дл выбивки литейных форм
SU740404A1 (ru) Устройство дл выбивки форм
JPS5795236A (en) Vibration preventing device for wiper
ADELMAN et al. Vibration analysis of a 1/40-scale dynamic model of Saturn 5 launch platform-umbilical tower configuration(Direct stiffness method of computing vibrational characteristics of dynamic model of Apollo- Saturn 5 vehicle- umbilical tower configuration)
JPS5611137A (en) Combined mold for continuous casting of metal
SU835632A1 (ru) Инерционна решетка
PRIKHODKO Sound diffraction by prolate thin-walled elastic shells of revolution(Difraktsiia zvuka na vytianutykh tonkostennykh uprugikh obolochkakh vrashcheniia)

Legal Events

Date Code Title Description
ST Notification of lapse