JPS55156798A - Mounting structure for transmission of helicopter - Google Patents

Mounting structure for transmission of helicopter

Info

Publication number
JPS55156798A
JPS55156798A JP2235280A JP2235280A JPS55156798A JP S55156798 A JPS55156798 A JP S55156798A JP 2235280 A JP2235280 A JP 2235280A JP 2235280 A JP2235280 A JP 2235280A JP S55156798 A JPS55156798 A JP S55156798A
Authority
JP
Japan
Prior art keywords
helicopter
transmission
mounting structure
mounting
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
JP2235280A
Other languages
English (en)
Other versions
JPH0214240B2 (ja
Inventor
Rei Haruuesu Denisu
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 JPS55156798A publication Critical patent/JPS55156798A/ja
Publication of JPH0214240B2 publication Critical patent/JPH0214240B2/ja
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)
JP2235280A 1979-02-26 1980-02-26 Mounting structure for transmission of helicopter Granted JPS55156798A (en)

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
JPS55156798A true JPS55156798A (en) 1980-12-06
JPH0214240B2 JPH0214240B2 (ja) 1990-04-06

Family

ID=21770216

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2235280A Granted JPS55156798A (en) 1979-02-26 1980-02-26 Mounting structure for transmission of helicopter

Country Status (12)

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

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
WO2011103078A1 (en) * 2010-02-16 2011-08-25 Bell Helicopter Textron Inc. Variabale stiffness liquid inertia vibration eliminator

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 (ja) * 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
DE3006762A1 (de) 1980-09-11
AU534537B2 (en) 1984-02-02
ES488948A1 (es) 1980-09-16
AU5585280A (en) 1980-09-04
IT1126962B (it) 1986-05-21
GB2043573A (en) 1980-10-08
FR2449593A1 (fr) 1980-09-19
GB2043573B (en) 1983-03-23
FR2449593B1 (ja) 1983-07-18
BR8001117A (pt) 1980-10-29
IT8047998A0 (it) 1980-02-25
IL59458A (en) 1984-11-30
CA1142155A (en) 1983-03-01
JPH0214240B2 (ja) 1990-04-06
DE3006762C2 (ja) 1988-10-13
MX6586E (es) 1985-07-26
AR226171A1 (es) 1982-06-15

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