JPS56156535A - Vibration and shock absorbing type fixing device - Google Patents

Vibration and shock absorbing type fixing device

Info

Publication number
JPS56156535A
JPS56156535A JP5308881A JP5308881A JPS56156535A JP S56156535 A JPS56156535 A JP S56156535A JP 5308881 A JP5308881 A JP 5308881A JP 5308881 A JP5308881 A JP 5308881A JP S56156535 A JPS56156535 A JP S56156535A
Authority
JP
Japan
Prior art keywords
vibration
fixing device
shock absorbing
type fixing
absorbing type
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
JP5308881A
Other languages
English (en)
Japanese (ja)
Other versions
JPS6112134B2 (fr
Inventor
Eru Haretsuto Reon
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 JPS56156535A publication Critical patent/JPS56156535A/ja
Publication of JPS6112134B2 publication Critical patent/JPS6112134B2/ja
Granted 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Textile Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Prevention Devices (AREA)
  • Springs (AREA)
  • Vibration Dampers (AREA)
  • Bolts, Nuts, And Washers (AREA)
JP5308881A 1980-04-11 1981-04-10 Vibration and shock absorbing type fixing device Granted JPS56156535A (en)

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
JPS56156535A true JPS56156535A (en) 1981-12-03
JPS6112134B2 JPS6112134B2 (fr) 1986-04-07

Family

ID=22485935

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5308881A Granted JPS56156535A (en) 1980-04-11 1981-04-10 Vibration and shock absorbing type fixing device

Country Status (6)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009110098A1 (fr) * 2008-03-07 2009-09-11 ナブテスコ株式会社 Boulon à mécanisme anti-desserrage

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0268716A1 (fr) * 1986-11-28 1988-06-01 Inabata Techno Loop Corporation Amortisseur de vibrations
US5876023A (en) * 1996-09-18 1999-03-02 Lord Corporation Vibration isolation insert for aircraft floor planels and the like
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.
US20240141802A1 (en) * 2022-10-28 2024-05-02 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 (fr) * 1973-02-06 1978-11-30
US3836100A (en) * 1973-06-13 1974-09-17 United Aircraft Corp Engine mounting arrangement

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009110098A1 (fr) * 2008-03-07 2009-09-11 ナブテスコ株式会社 Boulon à mécanisme anti-desserrage
JP5193282B2 (ja) * 2008-03-07 2013-05-08 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
US8747039B2 (en) 2008-03-07 2014-06-10 Nabtesco Corporation Bolt and nut with rotation prohibiting mechanism

Also Published As

Publication number Publication date
IT1142335B (it) 1986-10-08
IT8147893A0 (it) 1981-02-26
GB2074289A (en) 1981-10-28
FR2480374A1 (fr) 1981-10-16
GB2074289B (en) 1984-10-31
CA1151626A (fr) 1983-08-09
DE3111015A1 (de) 1982-01-28
JPS6112134B2 (fr) 1986-04-07
FR2480374B1 (fr) 1986-05-16
DE3111015C2 (fr) 1991-04-11

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