FR2331480A1 - Amortisseur de vibrations bifilaire pour rotor d'helicoptere - Google Patents

Amortisseur de vibrations bifilaire pour rotor d'helicoptere

Info

Publication number
FR2331480A1
FR2331480A1 FR7629524A FR7629524A FR2331480A1 FR 2331480 A1 FR2331480 A1 FR 2331480A1 FR 7629524 A FR7629524 A FR 7629524A FR 7629524 A FR7629524 A FR 7629524A FR 2331480 A1 FR2331480 A1 FR 2331480A1
Authority
FR
France
Prior art keywords
vibration damper
helicopter rotor
bifilar vibration
bifilar
helicopter
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
FR7629524A
Other languages
English (en)
Other versions
FR2331480B1 (fr
Inventor
Irwin Jeffrey Kenigsberg
Edward Sterling Carter
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 FR2331480A1 publication Critical patent/FR2331480A1/fr
Application granted granted Critical
Publication of FR2331480B1 publication Critical patent/FR2331480B1/fr
Granted 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
    • 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)
  • Vibration Prevention Devices (AREA)
  • Mechanical Operated Clutches (AREA)
FR7629524A 1975-11-13 1976-10-01 Amortisseur de vibrations bifilaire pour rotor d'helicoptere Granted FR2331480A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/631,577 US3988074A (en) 1975-11-13 1975-11-13 Anhedral bifilar

Publications (2)

Publication Number Publication Date
FR2331480A1 true FR2331480A1 (fr) 1977-06-10
FR2331480B1 FR2331480B1 (fr) 1981-05-29

Family

ID=24531814

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7629524A Granted FR2331480A1 (fr) 1975-11-13 1976-10-01 Amortisseur de vibrations bifilaire pour rotor d'helicoptere

Country Status (11)

Country Link
US (1) US3988074A (fr)
JP (1) JPS5925719B2 (fr)
BR (1) BR7607361A (fr)
CA (1) CA1064455A (fr)
CH (1) CH605251A5 (fr)
DE (1) DE2645981C2 (fr)
FR (1) FR2331480A1 (fr)
GB (1) GB1522058A (fr)
IL (1) IL50684A (fr)
IT (1) IT1064381B (fr)
NL (1) NL7611833A (fr)

Families Citing this family (4)

* 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
FR2733483B1 (fr) * 1995-04-27 1997-07-04 Eurocopter France Dispositif d'attenuation de vibrations pour rotor d'helicoptere
DE19961071B4 (de) * 1999-12-17 2007-04-12 Eurocopter Deutschland Gmbh Kupplungsmembran
GB2482545B (en) * 2010-08-06 2017-05-03 Ge Aviat Systems Ltd Aircraft propellers with composite blades mounted to a single propeller hub

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2519762A (en) * 1945-07-09 1950-08-22 United Aircraft Corp Gyrodynamic damper
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
GB1465266A (en) * 1973-04-26 1977-02-23 Westland Aircraft Ltd Rotors for rotary wing aircraft
GB1468359A (en) * 1973-10-09 1977-03-23 Westland Aircraft Ltd Bifilar vibration dampers

Also Published As

Publication number Publication date
US3988074A (en) 1976-10-26
IL50684A (en) 1980-12-31
BR7607361A (pt) 1977-09-20
CA1064455A (fr) 1979-10-16
IT1064381B (it) 1985-02-18
NL7611833A (nl) 1977-05-17
DE2645981A1 (de) 1977-05-26
JPS5262897A (en) 1977-05-24
GB1522058A (en) 1978-08-23
DE2645981C2 (de) 1986-02-06
JPS5925719B2 (ja) 1984-06-20
FR2331480B1 (fr) 1981-05-29
IL50684A0 (en) 1976-12-31
CH605251A5 (fr) 1978-09-29

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