JPH0253279B2 - - Google Patents

Info

Publication number
JPH0253279B2
JPH0253279B2 JP55024663A JP2466380A JPH0253279B2 JP H0253279 B2 JPH0253279 B2 JP H0253279B2 JP 55024663 A JP55024663 A JP 55024663A JP 2466380 A JP2466380 A JP 2466380A JP H0253279 B2 JPH0253279 B2 JP H0253279B2
Authority
JP
Japan
Prior art keywords
pylon
fuselage
rotor
mount
transmission
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.)
Expired
Application number
JP55024663A
Other languages
English (en)
Japanese (ja)
Other versions
JPS55160700A (en
Inventor
Ruisu Kuresatsupu Uezuri
Uein Maiazu Aran
Padomanaban Uisuwanasuan Sasui
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 JPS55160700A publication Critical patent/JPS55160700A/ja
Publication of JPH0253279B2 publication Critical patent/JPH0253279B2/ja
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
    • B64C2027/002Vibration 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)
  • Pivots And Pivotal Connections (AREA)
  • Sliding-Contact Bearings (AREA)
  • Support Of The Bearing (AREA)
JP2466380A 1979-03-01 1980-03-01 Mount for helicopter pylon Granted JPS55160700A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US1640379A 1979-03-01 1979-03-01

Publications (2)

Publication Number Publication Date
JPS55160700A JPS55160700A (en) 1980-12-13
JPH0253279B2 true JPH0253279B2 (enrdf_load_stackoverflow) 1990-11-16

Family

ID=21776951

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2466380A Granted JPS55160700A (en) 1979-03-01 1980-03-01 Mount for helicopter pylon

Country Status (12)

Country Link
JP (1) JPS55160700A (enrdf_load_stackoverflow)
AR (1) AR226172A1 (enrdf_load_stackoverflow)
AU (1) AU533359B2 (enrdf_load_stackoverflow)
BR (1) BR8001223A (enrdf_load_stackoverflow)
CA (1) CA1149360A (enrdf_load_stackoverflow)
DE (1) DE3007200A1 (enrdf_load_stackoverflow)
ES (1) ES489030A0 (enrdf_load_stackoverflow)
FR (1) FR2450200A1 (enrdf_load_stackoverflow)
GB (1) GB2043574B (enrdf_load_stackoverflow)
IL (1) IL59460A (enrdf_load_stackoverflow)
IT (1) IT1144041B (enrdf_load_stackoverflow)
MX (1) MX6587E (enrdf_load_stackoverflow)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2605448C (en) 2005-04-27 2011-07-12 Bell Helicopter Textron Inc. Elastomeric spring-damper with integral stops
DE102009015806B4 (de) * 2009-04-01 2013-04-04 Otmar Birkner Tragschrauber
CN109522636B (zh) * 2018-11-09 2022-12-30 中国直升机设计研究所 一种用于直升机抗坠毁分析的轮式起落架简化方法

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US322379A (en) * 1885-07-14 Axel jorgensen
FR1334044A (fr) * 1961-09-01 1963-08-02 Maschf Augsburg Nuernberg Ag Dispositif de suspension d'un moteur dans le châssis d'un véhicule routier ou ferroviaire
DE1269890B (de) * 1963-09-26 1968-06-06 Dornier Gmbh Stabilisierungseinrichtung fuer Drehfluegelflugzeuge
US3690607A (en) * 1970-02-16 1972-09-12 Kenneth C Mard 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
IT8048034A0 (it) 1980-02-28
GB2043574B (en) 1982-12-22
FR2450200B1 (enrdf_load_stackoverflow) 1984-08-03
AU533359B2 (en) 1983-11-17
AR226172A1 (es) 1982-06-15
BR8001223A (pt) 1980-11-04
DE3007200A1 (de) 1980-09-11
IT1144041B (it) 1986-10-29
CA1149360A (en) 1983-07-05
AU5593780A (en) 1980-09-04
FR2450200A1 (fr) 1980-09-26
ES8103707A1 (es) 1981-02-16
MX6587E (es) 1985-07-26
JPS55160700A (en) 1980-12-13
DE3007200C2 (enrdf_load_stackoverflow) 1989-01-26
ES489030A0 (es) 1981-02-16
IL59460A (en) 1984-02-29
GB2043574A (en) 1980-10-08

Similar Documents

Publication Publication Date Title
US4362281A (en) Pylon mounting system for reducing helicopter vibration
US4619349A (en) Vibration isolator
CA2793576C (en) Landing gear vibration absorber and method of operating said landing gear vibration absorber
US7726602B2 (en) Arrangement for mounting an engine on the airframe of an aircraft
CN103195852B (zh) 一种机械最优化的液体惯性减振器和飞行器塔式系统
US3727862A (en) Aircraft power-unit suspension system
US3540809A (en) Vibration damped helicopter rotor
US7607892B2 (en) Rotorcraft rotor with blades hinged in flap and in lag
US3698663A (en) Rotary wing pylon mounting system
JPH0159959B2 (enrdf_load_stackoverflow)
CA2802152C (en) Rotorcraft vibration suppression system in a four corner pylon mount configuration
US20110155841A1 (en) Vibration damper mechanism, and a flying machine including a carrier structure and a rotor provided with such a mechanism
US4140028A (en) Vibration isolation system
US6494680B2 (en) Rotor with rotor head vibration suppressor comprising vertical pendulums
US3035643A (en) Device to alter dynamic characteristics of rotor systems
US4247061A (en) Helicopter with stabilator detuned in antisymmetric vibration modes from main rotor wake excitation frequency
US4311213A (en) Vibration isolation system
EP0008303A1 (en) Constant frequency bifilar vibration absorber
JPS5825898B2 (ja) ばね・質量共振形吸振器
US4766984A (en) Nonlinear vibration absorber
US4365771A (en) Inplane nodalization system
JP3257691B2 (ja) 2つの部材間の静的力の伝達と振動励起を減衰する連結装置
JPH0253279B2 (enrdf_load_stackoverflow)
US4428550A (en) Vibration-insulating stability improving torque force device
US2487646A (en) Rubber mounted tail rotor