FR2480374B1 - Moyen de fixation supportant une charge et absorbant les chocs et les vibrations - Google Patents

Moyen de fixation supportant une charge et absorbant les chocs et les vibrations

Info

Publication number
FR2480374B1
FR2480374B1 FR8105229A FR8105229A FR2480374B1 FR 2480374 B1 FR2480374 B1 FR 2480374B1 FR 8105229 A FR8105229 A FR 8105229A FR 8105229 A FR8105229 A FR 8105229A FR 2480374 B1 FR2480374 B1 FR 2480374B1
Authority
FR
France
Prior art keywords
vibration
load
attachment means
means supporting
absorbing shock
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
FR8105229A
Other languages
English (en)
French (fr)
Other versions
FR2480374A1 (fr
Inventor
Leon L Hulett
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.)
Hutchinson Aerospace and Industry Inc
Original Assignee
Barry Wright 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 Barry Wright Corp filed Critical Barry Wright Corp
Publication of FR2480374A1 publication Critical patent/FR2480374A1/fr
Application granted granted Critical
Publication of FR2480374B1 publication Critical patent/FR2480374B1/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • F16F1/00—Springs
    • F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/362—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers made of steel wool, compressed hair, woven or non-woven textile, or like materials
    • 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
    • F16F1/00—Springs
    • F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/38—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type
    • F16F1/3835—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type characterised by the sleeve of elastic material, e.g. having indentations or made of materials of different hardness

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Textile Engineering (AREA)
  • Vibration Prevention Devices (AREA)
  • Springs (AREA)
  • Vibration Dampers (AREA)
  • Bolts, Nuts, And Washers (AREA)
FR8105229A 1980-04-11 1981-03-16 Moyen de fixation supportant une charge et absorbant les chocs et les vibrations Expired FR2480374B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13928780A 1980-04-11 1980-04-11

Publications (2)

Publication Number Publication Date
FR2480374A1 FR2480374A1 (fr) 1981-10-16
FR2480374B1 true FR2480374B1 (fr) 1986-05-16

Family

ID=22485935

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8105229A Expired FR2480374B1 (fr) 1980-04-11 1981-03-16 Moyen de fixation supportant une charge et absorbant les chocs et les vibrations

Country Status (6)

Country Link
JP (1) JPS56156535A (enrdf_load_stackoverflow)
CA (1) CA1151626A (enrdf_load_stackoverflow)
DE (1) DE3111015A1 (enrdf_load_stackoverflow)
FR (1) FR2480374B1 (enrdf_load_stackoverflow)
GB (1) GB2074289B (enrdf_load_stackoverflow)
IT (1) IT1142335B (enrdf_load_stackoverflow)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0268716A1 (en) * 1986-11-28 1988-06-01 Inabata Techno Loop Corporation Vibration damping device
US5876023A (en) * 1996-09-18 1999-03-02 Lord Corporation Vibration isolation insert for aircraft floor planels and the like
WO2009110098A1 (ja) * 2008-03-07 2009-09-11 ナブテスコ株式会社 回り止め機構付きのボルトとナット
RU2378543C1 (ru) * 2008-09-25 2010-01-10 Закрытое акционерное общество "Управляющая компания "Брянский машиностроительный завод" (ЗАО "УК "БМЗ") Цельнометаллический сайлентблок
RU2387894C1 (ru) * 2008-10-01 2010-04-27 Закрытое акционерное общество "Управляющая компания "Брянский машиностроительный завод" (ЗАО "УК "БМЗ") Цельнометаллический сайлентблок и способ его изготовления
FR2965550B1 (fr) * 2010-10-05 2012-11-02 Airbus Operations Sas Attache de type spigot pourvue d'au moins un moyen de mesure de l'effort genere par un moteur d'aeronef
US11066178B2 (en) * 2015-09-02 2021-07-20 Raytheon Technologies Corporation Link for aircraft component mounting
RU171214U1 (ru) * 2016-08-08 2017-05-24 Федеральное государственное бюджетное образовательное учреждение высшего образования "Орловский государственный университет имени И.С. Тургенева" (ФГБОУ ВО "ОГУ имени И.С. Тургенева") Сайлентблок
ES2686395B2 (es) * 2017-04-16 2019-10-18 Tejasa Tc S L L Articulación elástica.
DE102020102509A1 (de) * 2020-01-31 2021-08-05 Weber-Hydraulik Gmbh Fahrzeugkabinenlager und Kippvorrichtung mit einem Fahrzeugkabinenlager
FR3136027B1 (fr) 2022-05-24 2024-04-19 Airbus Helicopters Articulation déformable élastiquement et système muni d’une telle articulation.
US12071855B2 (en) * 2022-10-28 2024-08-27 Pratt & Whitney Canada Corp. Conduit bushing with cellular material

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE588684C (de) * 1931-09-09 1933-11-23 Thompson Prod Inc Lenkzapfenverbindung, insbesondere fuer Kraftfahrzeuge
GB434568A (en) * 1934-10-01 1935-09-04 Thompson Prod Inc Improvements in a joint
GB481974A (en) * 1936-10-06 1938-03-22 Frank Sidebotham Rippingille Improvements relating to oscillatory or pivotal joints
GB620882A (en) * 1947-01-29 1949-03-31 Wright Howard Clayton Improvements in steering gear joints
GB811668A (en) * 1956-07-16 1959-04-08 Metalastik Ltd Improvements in or relating to steering link joints for road vehicles
FR1160826A (fr) * 1956-11-12 1958-08-11 Snecma Dispositif de suspension de réacteurs
US3073557A (en) * 1961-10-10 1963-01-15 Robinson Technical Products In Shock and vibration isolating mountings for aircraft engines and the like
US3190591A (en) * 1963-02-11 1965-06-22 Cal Val Res & Dev Corp Core assembly for an engine mount
AT250188B (de) * 1963-05-10 1966-10-25 Pneumatiques Caoutchouc Mfg Elastisches Gelenk
US3259006A (en) * 1964-06-04 1966-07-05 Ford Motor Co Retaining clip
JPS5344620B2 (enrdf_load_stackoverflow) * 1973-02-06 1978-11-30
US3836100A (en) * 1973-06-13 1974-09-17 United Aircraft Corp Engine mounting arrangement

Also Published As

Publication number Publication date
IT8147893A0 (it) 1981-02-26
DE3111015C2 (enrdf_load_stackoverflow) 1991-04-11
DE3111015A1 (de) 1982-01-28
JPS56156535A (en) 1981-12-03
GB2074289B (en) 1984-10-31
JPS6112134B2 (enrdf_load_stackoverflow) 1986-04-07
CA1151626A (en) 1983-08-09
IT1142335B (it) 1986-10-08
GB2074289A (en) 1981-10-28
FR2480374A1 (fr) 1981-10-16

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Legal Events

Date Code Title Description
ST Notification of lapse