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AU2001280681A1 - Vibration isolation device with load dependent stiffness - Google Patents

Vibration isolation device with load dependent stiffness

Info

Publication number
AU2001280681A1
AU2001280681A1 AU2001280681A AU8068101A AU2001280681A1 AU 2001280681 A1 AU2001280681 A1 AU 2001280681A1 AU 2001280681 A AU2001280681 A AU 2001280681A AU 8068101 A AU8068101 A AU 8068101A AU 2001280681 A1 AU2001280681 A1 AU 2001280681A1
Authority
AU
Australia
Prior art keywords
vibration isolation
isolation device
load dependent
dependent stiffness
stiffness
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.)
Abandoned
Application number
AU2001280681A
Inventor
Paul J. Bachmeyer
Michael R. Blewett
Marvin D. Ohme
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.)
Lord Corp
Hamilton Sundstrand Corp
Original Assignee
Lord Corp
Hamilton Sundstrand 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 Lord Corp, Hamilton Sundstrand Corp filed Critical Lord Corp
Publication of AU2001280681A1 publication Critical patent/AU2001280681A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F3/00Spring units consisting of several springs, e.g. for obtaining a desired spring characteristic
    • F16F3/08Spring units consisting of several springs, e.g. for obtaining a desired spring characteristic with springs made of a material having high internal friction, e.g. rubber
    • F16F3/087Units comprising several springs made of plastics or the like material
    • F16F3/0873Units comprising several springs made of plastics or the like material of the same material or the material not being specified
    • F16F3/0876Units comprising several springs made of plastics or the like material of the same material or the material not being specified and of the same shape
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F3/00Spring units consisting of several springs, e.g. for obtaining a desired spring characteristic
    • F16F3/08Spring units consisting of several springs, e.g. for obtaining a desired spring characteristic with springs made of a material having high internal friction, e.g. rubber
    • F16F3/087Units comprising several springs made of plastics or the like material
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F7/00Vibration-dampers; Shock-absorbers
    • F16F7/003One-shot shock absorbers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F2228/00Functional characteristics, e.g. variability, frequency-dependence
    • F16F2228/06Stiffness
    • F16F2228/066Variable stiffness

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Vibration Prevention Devices (AREA)
  • Springs (AREA)
AU2001280681A 2000-07-21 2001-07-20 Vibration isolation device with load dependent stiffness Abandoned AU2001280681A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US21989100P 2000-07-21 2000-07-21
US60219891 2000-07-21
PCT/US2001/023015 WO2002008629A2 (en) 2000-07-21 2001-07-20 Vibration isolation device with load dependent stiffness

Publications (1)

Publication Number Publication Date
AU2001280681A1 true AU2001280681A1 (en) 2002-02-05

Family

ID=22821171

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001280681A Abandoned AU2001280681A1 (en) 2000-07-21 2001-07-20 Vibration isolation device with load dependent stiffness

Country Status (5)

Country Link
US (1) US6715746B2 (en)
EP (1) EP1301731A2 (en)
AU (1) AU2001280681A1 (en)
CA (1) CA2416832A1 (en)
WO (1) WO2002008629A2 (en)

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NL1027304C2 (en) * 2004-10-20 2006-04-24 Mecal Applied Mechanics B V Support structure, fixation member and method.
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US8104736B2 (en) * 2005-12-01 2012-01-31 Hamilton Sundstrand Corporation Gas turbine engine auxiliary component mount
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US8393601B2 (en) * 2008-10-04 2013-03-12 Applied Concepts Aircraft Solutions, Inc. Vibration isolation fastener insert
EP2184229B1 (en) * 2008-11-11 2012-10-17 AGUSTAWESTLAND S.p.A. Helicopter rotor
US7784773B1 (en) 2009-08-04 2010-08-31 Itt Manufacturing Enterprises, Inc. Isolator useful for in-line mounting with a strut
EP2366910B1 (en) * 2010-03-05 2012-11-28 The Young Engineers, Inc. Vibration isolation fastener insert
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US8770513B2 (en) * 2011-11-30 2014-07-08 Honeywell International Inc. Resilient aircraft engine mounts and aircraft engine mounting systems including the same
US9140279B2 (en) 2012-09-25 2015-09-22 The Young Engineers, Inc. Magnetic mount
EP2901067B1 (en) * 2012-09-28 2020-12-09 United Technologies Corporation Auxiliary component mounts
US9863324B2 (en) * 2013-03-21 2018-01-09 United Technologies Corporation Oil tank mount with stiffeners
US8960696B2 (en) * 2013-04-16 2015-02-24 Zhongli North America Inc. Strut top mount with MCU and integral travel limiter
EP3564511A1 (en) 2013-10-29 2019-11-06 United Technologies Corporation Oil tank mount arrangement on a geared turbofan engine
US9964042B2 (en) 2013-10-29 2018-05-08 United Technologies Corporation Bracket doubler
CN103982531B (en) * 2014-04-04 2016-08-17 浙江双金机械集团股份有限公司 Gyratory crusher pressurize cylinder shaft pin
DE102014014065B4 (en) * 2014-09-29 2016-08-04 Rheinmetall Air Defence Ag Shock bearing assembly for potentially shock-exposed equipment in military applications
US10132245B2 (en) * 2016-04-25 2018-11-20 Hamilton Sundstrand Corporation Fusible link with coulomb damping
WO2017197232A1 (en) 2016-05-13 2017-11-16 Lord Corporation Isolator devices, systems and methods for aircraft
RU175921U1 (en) * 2017-02-21 2017-12-22 федеральное государственное бюджетное образовательное учреждение высшего образования "Южно-Российский государственный политехнический университет (НПИ) имени М.И. Платова" Articulated Vibration Isolator
US10875655B2 (en) 2017-06-23 2020-12-29 Hutchinson Aerospace & Industry Inc. Vibration isolation device, especially for aircraft applications
US10967962B2 (en) * 2018-06-27 2021-04-06 Bell Helicopter Textron Inc. Removable struts for vibration isolation device mounting system
KR102135276B1 (en) 2019-02-01 2020-07-17 주식회사 만도 Apparatus for controlling power assist and method thereof
US11479104B2 (en) 2019-07-24 2022-10-25 Honeywell International Inc. System and method for gas turbine engine mount with seal
RU2754014C1 (en) * 2020-07-14 2021-08-25 Илья Юрьевич Лебединский Method for optimisation of suspension system of cabin of transport and technological machines
US12092138B2 (en) 2022-04-08 2024-09-17 Toyota Motor Engineering & Manufacturing North America, Inc. Coupling assemblies having frangible portions
CN115748834B (en) * 2022-12-13 2025-07-18 湖南大学 Multistage quasi-zero stiffness vibration isolator

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Also Published As

Publication number Publication date
WO2002008629A2 (en) 2002-01-31
WO2002008629A3 (en) 2002-04-18
US20020079630A1 (en) 2002-06-27
US6715746B2 (en) 2004-04-06
EP1301731A2 (en) 2003-04-16
CA2416832A1 (en) 2002-01-31

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