FR1335388A - Monture pour moteur, notamment pour réacteur d'aéronef - Google Patents

Monture pour moteur, notamment pour réacteur d'aéronef

Info

Publication number
FR1335388A
FR1335388A FR911188A FR911188A FR1335388A FR 1335388 A FR1335388 A FR 1335388A FR 911188 A FR911188 A FR 911188A FR 911188 A FR911188 A FR 911188A FR 1335388 A FR1335388 A FR 1335388A
Authority
FR
France
Prior art keywords
engine
mount
aircraft
aircraft engine
engine mount
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
FR911188A
Other languages
English (en)
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.)
Robinson Technical Products Inc
Original Assignee
Robinson Technical Products 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 Robinson Technical Products Inc filed Critical Robinson Technical Products Inc
Application granted granted Critical
Publication of FR1335388A publication Critical patent/FR1335388A/fr
Expired legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/04—Aircraft characterised by the type or position of power plants of piston type

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Springs (AREA)
  • Vibration Prevention Devices (AREA)
FR911188A 1961-10-10 1962-10-03 Monture pour moteur, notamment pour réacteur d'aéronef Expired FR1335388A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US144185A US3073557A (en) 1961-10-10 1961-10-10 Shock and vibration isolating mountings for aircraft engines and the like

Publications (1)

Publication Number Publication Date
FR1335388A true FR1335388A (fr) 1963-08-16

Family

ID=22507463

Family Applications (1)

Application Number Title Priority Date Filing Date
FR911188A Expired FR1335388A (fr) 1961-10-10 1962-10-03 Monture pour moteur, notamment pour réacteur d'aéronef

Country Status (3)

Country Link
US (1) US3073557A (fr)
FR (1) FR1335388A (fr)
GB (1) GB1009788A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1267106B (de) * 1964-08-06 1968-04-25 Wtz Automobilbau Hohenstein Er Fusshebelgelenk fuer Kraftfahrzeuge
EP0250659A2 (fr) * 1986-05-19 1988-01-07 The Boeing Company Dispositif de support de turbine avec amortisseurs de vibrations

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3250502A (en) * 1963-03-14 1966-05-10 Robinson Technical Products In Shock and vibration isolating support
US3442479A (en) * 1968-01-24 1969-05-06 North American Rockwell Mounting means
FR2228662B1 (fr) * 1973-05-08 1976-11-12 Aerospatiale
US4214738A (en) * 1977-05-02 1980-07-29 General Electric Company Three-dimensional isolation mount
CA1151626A (fr) * 1980-04-11 1983-08-09 Leon L. Hulett Support antivibration
US4514458A (en) * 1983-11-09 1985-04-30 Lord Corporation Spring-like material formed of compressed metallic wire
US4748806A (en) * 1985-07-03 1988-06-07 United Technologies Corporation Attachment means
US5230407A (en) * 1990-06-22 1993-07-27 Applied Power Inc. Linkage rod with shock absorbing
US20020063368A1 (en) * 2000-11-29 2002-05-30 Kabir Omar M. Mesh bearing damper for an energy storage rotor
WO2006108028A2 (fr) * 2005-04-04 2006-10-12 Lord Corporation Systeme de suspension d'un groupe auxiliaire l'isolant de la structure de l'aeronef
CA2992243C (fr) * 2007-10-19 2021-01-12 Lord Corporation Systeme de suspension pour groupe auxiliaire d'energie d'avion muni d'un element elastomere
US20090166506A1 (en) * 2008-01-02 2009-07-02 Freudenberg-Nok General Partnership Engine Mount With Two Piece Core
ES2686395B2 (es) * 2017-04-16 2019-10-18 Tejasa Tc S L L Articulación elástica.
US11702891B2 (en) 2020-11-21 2023-07-18 Cnpc Usa Corporation Force modulation system with an elastic force member for downhole conditions

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE462389A (fr) * 1943-07-22
US2420452A (en) * 1944-10-02 1947-05-13 Lord Mfg Co Resilient mounting
US2638303A (en) * 1946-03-12 1953-05-12 Us Navy Shock mount
GB740519A (en) * 1953-11-06 1955-11-16 Wells & Company Ltd A Improvements in or relating to anti-vibration mounting devices
US2869858A (en) * 1956-08-01 1959-01-20 Metal Textile Corp Vibration and shock absorptive cushion element

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1267106B (de) * 1964-08-06 1968-04-25 Wtz Automobilbau Hohenstein Er Fusshebelgelenk fuer Kraftfahrzeuge
EP0250659A2 (fr) * 1986-05-19 1988-01-07 The Boeing Company Dispositif de support de turbine avec amortisseurs de vibrations
EP0250659A3 (en) * 1986-05-19 1989-05-31 The Boeing Company Aircraft engine mount system with vibration isolators

Also Published As

Publication number Publication date
GB1009788A (en) 1965-11-10
US3073557A (en) 1963-01-15

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