FR2449593B1 - - Google Patents

Info

Publication number
FR2449593B1
FR2449593B1 FR8004158A FR8004158A FR2449593B1 FR 2449593 B1 FR2449593 B1 FR 2449593B1 FR 8004158 A FR8004158 A FR 8004158A FR 8004158 A FR8004158 A FR 8004158A FR 2449593 B1 FR2449593 B1 FR 2449593B1
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.)
Expired
Application number
FR8004158A
Other versions
FR2449593A1 (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.)
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 FR2449593A1 publication Critical patent/FR2449593A1/fr
Application granted granted Critical
Publication of FR2449593B1 publication Critical patent/FR2449593B1/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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/001—Vibration damping devices
    • B64C2027/002—Vibration damping devices mounted between the rotor drive and the fuselage

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Prevention Devices (AREA)
FR8004158A 1979-02-26 1980-02-26 Dispositif de suspension du fuselage a la transmission d'un helicoptere Granted FR2449593A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US1522979A 1979-02-26 1979-02-26

Publications (2)

Publication Number Publication Date
FR2449593A1 FR2449593A1 (fr) 1980-09-19
FR2449593B1 true FR2449593B1 (fr) 1983-07-18

Family

ID=21770216

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8004158A Granted FR2449593A1 (fr) 1979-02-26 1980-02-26 Dispositif de suspension du fuselage a la transmission d'un helicoptere

Country Status (12)

Country Link
JP (1) JPS55156798A (fr)
AR (1) AR226171A1 (fr)
AU (1) AU534537B2 (fr)
BR (1) BR8001117A (fr)
CA (1) CA1142155A (fr)
DE (1) DE3006762A1 (fr)
ES (1) ES488948A1 (fr)
FR (1) FR2449593A1 (fr)
GB (1) GB2043573B (fr)
IL (1) IL59458A (fr)
IT (1) IT1126962B (fr)
MX (1) MX6586E (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19711845C2 (de) * 1997-03-21 1999-01-14 Eurocopter Deutschland Mechanischer Schwingungstilger
US6328293B1 (en) 1998-09-18 2001-12-11 Lord Corporation Multi-linkage suspension system including outboard isolators
CN102770347B (zh) * 2010-02-16 2015-07-15 贝尔直升机泰克斯特龙公司 变刚度液体惯性隔振器

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2615657A (en) * 1946-08-28 1952-10-28 Bell Aircraft Corp Helicopter engine-rotor support
US3698663A (en) * 1970-12-07 1972-10-17 Textron Inc Rotary wing pylon mounting system
GB1380710A (en) * 1970-12-29 1975-01-15 Kawasaki Heavy Ind Ltd Rotary wing aircraft
US3845917A (en) * 1971-10-18 1974-11-05 Textron Inc Helicopter vibration isolation
US3857534A (en) * 1972-02-04 1974-12-31 Textron Inc Multi-frequency helicopter vibration isolation
FR2232481B1 (fr) * 1973-06-08 1976-05-07 Aerospatiale
US3858831A (en) * 1973-12-26 1975-01-07 Textron Inc Nodal beam inertial flexure
US3945628A (en) * 1973-12-26 1976-03-23 Textron Inc. Nodal beam inertial flexure
US4088042A (en) * 1976-09-07 1978-05-09 The Boeing Company Vibration isolation system
US4111386A (en) * 1976-12-09 1978-09-05 United Technologies Corporation Helicopter rotor and transmission mounting and vibration isolation system

Also Published As

Publication number Publication date
AU534537B2 (en) 1984-02-02
JPH0214240B2 (fr) 1990-04-06
AU5585280A (en) 1980-09-04
AR226171A1 (es) 1982-06-15
JPS55156798A (en) 1980-12-06
IT8047998A0 (it) 1980-02-25
ES488948A1 (es) 1980-09-16
DE3006762C2 (fr) 1988-10-13
CA1142155A (fr) 1983-03-01
MX6586E (es) 1985-07-26
FR2449593A1 (fr) 1980-09-19
IT1126962B (it) 1986-05-21
BR8001117A (pt) 1980-10-29
DE3006762A1 (de) 1980-09-11
IL59458A (en) 1984-11-30
GB2043573B (en) 1983-03-23
GB2043573A (en) 1980-10-08

Similar Documents

Publication Publication Date Title
BR8002583A (fr)
BR8006808A (fr)
FR2450200B1 (fr)
FR2446901B3 (fr)
AT364253B (fr)
AU78569S (fr)
AU79557S (fr)
AU78385S (fr)
AU78386S (fr)
AU78389S (fr)
AU78390S (fr)
AU78391S (fr)
AU78270S (fr)
AU79200S (fr)
AU78271S (fr)
AU79558S (fr)
AU79559S (fr)
AU79826S (fr)
AU79918S (fr)
AU79950S (fr)
AU80228S (fr)
BR5901094U (fr)
AU77763S (fr)
AU77669S (fr)
BE878260A (fr)

Legal Events

Date Code Title Description
ST Notification of lapse