IL50685A - Bifilar vibration absorber for a helicopter - Google Patents

Bifilar vibration absorber for a helicopter

Info

Publication number
IL50685A
IL50685A IL50685A IL5068576A IL50685A IL 50685 A IL50685 A IL 50685A IL 50685 A IL50685 A IL 50685A IL 5068576 A IL5068576 A IL 5068576A IL 50685 A IL50685 A IL 50685A
Authority
IL
Israel
Prior art keywords
helicopter
vibration absorber
bifilar vibration
bifilar
absorber
Prior art date
Application number
IL50685A
Other languages
English (en)
Other versions
IL50685A0 (en
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 IL50685A0 publication Critical patent/IL50685A0/xx
Publication of IL50685A publication Critical patent/IL50685A/xx

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/001—Vibration damping devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10—Suppression of vibrations in rotating systems by making use of members moving with the system
    • F16F15/14—Suppression 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
    • F16F15/1407—Suppression 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 the rotation being limited with respect to the driving means
    • F16F15/145—Masses mounted with play with respect to driving means thus enabling free movement over a limited range
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Vibration Prevention Devices (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
IL50685A 1975-11-20 1976-10-15 Bifilar vibration absorber for a helicopter IL50685A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/633,886 US4057363A (en) 1975-11-20 1975-11-20 Extended arm bifilar and method to eliminate second order vibration excitation

Publications (2)

Publication Number Publication Date
IL50685A0 IL50685A0 (en) 1976-12-31
IL50685A true IL50685A (en) 1979-11-30

Family

ID=24541529

Family Applications (1)

Application Number Title Priority Date Filing Date
IL50685A IL50685A (en) 1975-11-20 1976-10-15 Bifilar vibration absorber for a helicopter

Country Status (11)

Country Link
US (2) US4057363A (xx)
JP (2) JPS5264798A (xx)
BR (1) BR7607360A (xx)
CA (1) CA1062226A (xx)
CH (1) CH605252A5 (xx)
DE (1) DE2645980C2 (xx)
FR (1) FR2332176A1 (xx)
GB (1) GB1516567A (xx)
IL (1) IL50685A (xx)
IT (1) IT1064390B (xx)
NL (1) NL7611834A (xx)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
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
US5954480A (en) * 1997-08-28 1999-09-21 Sikorsky Aircraft Corporation Vibration isolator for rotorcraft
US5901616A (en) * 1997-09-15 1999-05-11 Sikorsky Aircraft Corporation Inertial mass for vibration isolators
US8162606B2 (en) 2004-08-30 2012-04-24 Lord Corporation Helicopter hub mounted vibration control and circular force generation systems for canceling vibrations
CN101022994B (zh) 2004-08-30 2012-07-04 洛德公司 直升飞机振动控制系统和消除振动的旋转力发生器
US8267652B2 (en) * 2004-08-30 2012-09-18 Lord Corporation Helicopter hub mounted vibration control and circular force generation systems for canceling vibrations
US7722322B2 (en) * 2004-08-30 2010-05-25 Lord Corporation Computer system and program product for controlling vibrations
US8435002B2 (en) * 2004-08-30 2013-05-07 Lord Corporation Helicopter vibration control system and rotating assembly rotary forces generators for canceling vibrations
WO2009055007A2 (en) 2007-10-25 2009-04-30 Lord Corporation Distributed active vibration control systems and rotary wing aircraft with suppressed vibrations

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2552739A (en) * 1951-05-15 Method of tracking kotor blades
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
US3488998A (en) * 1967-08-24 1970-01-13 Charles A Bonsor Balancing device
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
US3952601A (en) * 1974-12-18 1976-04-27 United Technologies Corporation Helicopter rotor blade balancing method
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

Also Published As

Publication number Publication date
CH605252A5 (xx) 1978-09-29
US4057363A (en) 1977-11-08
NL7611834A (nl) 1977-05-24
BR7607360A (pt) 1977-09-20
GB1516567A (en) 1978-07-05
IL50685A0 (en) 1976-12-31
US4083654A (en) 1978-04-11
JPS6235680Y2 (xx) 1987-09-10
JPS61163799U (xx) 1986-10-11
CA1062226A (en) 1979-09-11
DE2645980C2 (de) 1986-07-31
FR2332176A1 (fr) 1977-06-17
FR2332176B1 (xx) 1981-05-29
DE2645980A1 (de) 1977-06-08
IT1064390B (it) 1985-02-18
JPS5264798A (en) 1977-05-28

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