ES8103707A1 - Perfeccionamientos en monturas para estructuras del rotor de helicopteros - Google Patents

Perfeccionamientos en monturas para estructuras del rotor de helicopteros

Info

Publication number
ES8103707A1
ES8103707A1 ES489030A ES489030A ES8103707A1 ES 8103707 A1 ES8103707 A1 ES 8103707A1 ES 489030 A ES489030 A ES 489030A ES 489030 A ES489030 A ES 489030A ES 8103707 A1 ES8103707 A1 ES 8103707A1
Authority
ES
Spain
Prior art keywords
pylon
fuselage
links
resilient
pin
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
ES489030A
Other languages
English (en)
Spanish (es)
Other versions
ES489030A0 (es
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 ES489030A0 publication Critical patent/ES489030A0/es
Publication of ES8103707A1 publication Critical patent/ES8103707A1/es
Expired 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)
  • Pivots And Pivotal Connections (AREA)
  • Sliding-Contact Bearings (AREA)
  • Support Of The Bearing (AREA)
ES489030A 1979-03-01 1980-02-28 Perfeccionamientos en monturas para estructuras del rotor de helicopteros Expired ES8103707A1 (es)

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
ES489030A0 ES489030A0 (es) 1981-02-16
ES8103707A1 true ES8103707A1 (es) 1981-02-16

Family

ID=21776951

Family Applications (1)

Application Number Title Priority Date Filing Date
ES489030A Expired ES8103707A1 (es) 1979-03-01 1980-02-28 Perfeccionamientos en monturas para estructuras del rotor de helicopteros

Country Status (12)

Country Link
JP (1) JPS55160700A (enExample)
AR (1) AR226172A1 (enExample)
AU (1) AU533359B2 (enExample)
BR (1) BR8001223A (enExample)
CA (1) CA1149360A (enExample)
DE (1) DE3007200A1 (enExample)
ES (1) ES8103707A1 (enExample)
FR (1) FR2450200A1 (enExample)
GB (1) GB2043574B (enExample)
IL (1) IL59460A (enExample)
IT (1) IT1144041B (enExample)
MX (1) MX6587E (enExample)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1874600B1 (en) 2005-04-27 2012-08-15 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
JPS55160700A (en) 1980-12-13
AU533359B2 (en) 1983-11-17
IL59460A (en) 1984-02-29
GB2043574B (en) 1982-12-22
ES489030A0 (es) 1981-02-16
FR2450200B1 (enExample) 1984-08-03
IT1144041B (it) 1986-10-29
AU5593780A (en) 1980-09-04
CA1149360A (en) 1983-07-05
DE3007200C2 (enExample) 1989-01-26
GB2043574A (en) 1980-10-08
JPH0253279B2 (enExample) 1990-11-16
DE3007200A1 (de) 1980-09-11
BR8001223A (pt) 1980-11-04
AR226172A1 (es) 1982-06-15
MX6587E (es) 1985-07-26
IT8048034A0 (it) 1980-02-28
FR2450200A1 (fr) 1980-09-26

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19971001