ES2539807T3 - Montaje aislante contra vibraciones de bajo perfil, multidireccional, altamente amortiguado de forma pasiva - Google Patents

Montaje aislante contra vibraciones de bajo perfil, multidireccional, altamente amortiguado de forma pasiva Download PDF

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Publication number
ES2539807T3
ES2539807T3 ES06720770.4T ES06720770T ES2539807T3 ES 2539807 T3 ES2539807 T3 ES 2539807T3 ES 06720770 T ES06720770 T ES 06720770T ES 2539807 T3 ES2539807 T3 ES 2539807T3
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ES
Spain
Prior art keywords
section
flexible
sheet
lower flexible
attachment
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 - Lifetime
Application number
ES06720770.4T
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English (en)
Inventor
Paul S. Wilke
Conor D. Johnson
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.)
Moog Inc
Original Assignee
Moog 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 Moog Inc filed Critical Moog Inc
Application granted granted Critical
Publication of ES2539807T3 publication Critical patent/ES2539807T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F16F3/00—Spring units consisting of several springs, e.g. for obtaining a desired spring characteristic
    • F16F3/08—Spring 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
    • 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
    • F16F7/00—Vibration-dampers; Shock-absorbers
    • F16F7/10—Vibration-dampers; Shock-absorbers using inertia effect

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Vibration Prevention Devices (AREA)

Abstract

Un dispositivo aislante contra vibraciones (100) que comprende: un elemento de flexión (10) que comprende secciones flexibles superior e inferior (11,12) generalmente alineadas con un eje longitudinal común; una lámina de material viscoelástico (VEM) (71, 72, 73, 74) que tiene una primera y una segunda superficies faciales de modo tal que la primera superficie facial se fija tanto a las secciones flexibles superior como inferior; una lámina forzada rígida (81, 82, 83, 84) fijada a la segunda superficie facial de la lámina de VEM de modo tal que el movimiento de la sección flexible superior con relación a la sección flexible inferior está restringido por la lámina forzada rígida e induce allí el corte de la lámina de VEM; donde las secciones flexibles superior e inferior (11, 12) tienen cada una un medio de fijación y una porción próxima a la fijación (21, 22) de modo tal que la porción próxima a la fijación de la sección flexible superior es una distancia mínima controlada desde la porción próxima a la fijación de la sección flexible inferior, donde el elemento de flexión comprende además al menos una sección de bucle flexible (31, 32, 33, 34), donde las porciones próximas a la fijación de las secciones flexibles superior e inferior (11, 12) están conectadas entre sí dentro del elemento de flexión mediante la al menos una sección de bucle de flexión, y donde al menos una sección de bucle flexible (31, 32, 33, 34) es de forma independiente y sección transversal en relación a las porciones próximas a la fijación de las secciones flexibles superior e inferior, y es de una forma y sección transversal independientes con relación a la distancia mínima controlada entre las porciones próximas a la fijación de las secciones flexibles superior e inferior.

Description

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Claims (1)

  1. imagen1
ES06720770.4T 2006-02-01 2006-02-15 Montaje aislante contra vibraciones de bajo perfil, multidireccional, altamente amortiguado de forma pasiva Expired - Lifetime ES2539807T3 (es)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US344487 2006-02-01
US11/344,487 US7249756B1 (en) 2006-02-01 2006-02-01 Low-profile, multi-axis, highly passively damped, vibration isolation mount
PCT/US2006/005296 WO2007089248A2 (en) 2006-02-01 2006-02-15 Low profile, multi-axis, highly passively damped, vibration isolation mount

Publications (1)

Publication Number Publication Date
ES2539807T3 true ES2539807T3 (es) 2015-07-06

Family

ID=38290238

Family Applications (1)

Application Number Title Priority Date Filing Date
ES06720770.4T Expired - Lifetime ES2539807T3 (es) 2006-02-01 2006-02-15 Montaje aislante contra vibraciones de bajo perfil, multidireccional, altamente amortiguado de forma pasiva

Country Status (5)

Country Link
US (1) US7249756B1 (es)
EP (1) EP1994324B1 (es)
DK (1) DK1994324T3 (es)
ES (1) ES2539807T3 (es)
WO (1) WO2007089248A2 (es)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2872784B1 (fr) * 2004-07-09 2007-10-12 Eurocopter France Systeme de suspension d'un moteur d'aeronef a voilure tournante
FR2949250B1 (fr) * 2009-08-24 2012-01-06 Aliaxis R & D Sas Pont amortissant
GB201004473D0 (en) * 2010-03-17 2010-05-05 Trysome Ltd Lightweight engine mounting
US8875681B2 (en) 2011-10-28 2014-11-04 Robert Bosch Gmbh Fuel rail mounting arrangement
EP2773561B1 (en) 2011-11-01 2016-09-07 Moog Inc. Vibration isolation system and method
US8800534B2 (en) 2011-11-18 2014-08-12 Robert Bosch Gmbh Fuel rail mounting arrangement
US8770513B2 (en) 2011-11-30 2014-07-08 Honeywell International Inc. Resilient aircraft engine mounts and aircraft engine mounting systems including the same
EP2628682B1 (en) * 2012-02-20 2019-05-22 Airbus Defence and Space, S.A. Space shuttle damping and isolating device
US20140332632A1 (en) * 2013-05-10 2014-11-13 Space Systems/Loral, Llc Isolation of payload from launch vehicle dynamic loads
FR3012553B1 (fr) 2013-10-31 2016-06-24 Astrium Sas Module d'isolation de vibrations a effets non lineaires diminues
DE102014102330A1 (de) * 2014-02-24 2015-08-27 ThyssenKrupp Federn und Stabilisatoren GmbH Tragfedereinheit für ein Fahrzeugfahrwerk
US9273749B2 (en) 2014-03-28 2016-03-01 Honeywell International Inc. Low profile three parameter isolators and isolation systems employing the same
FR3031146B1 (fr) 2014-12-24 2017-01-13 Airbus Defence & Space Sas Dispositif de fixation amortissant entre deux elements a assembler, procede de fabrication d'un tel dispositif, ensemble de deux elements assembles a l'aide d'un tel dispositif, et procede d'assemblage
US10343374B2 (en) 2015-05-22 2019-07-09 Blue Canyon Technologies Inc. Assembly for vibration isolation of a rotatable mass
WO2016203067A1 (es) * 2015-06-16 2016-12-22 Eads Casa Espacio S.L. Atenuador pasivo ligero para naves espaciales
US10570984B1 (en) * 2017-06-28 2020-02-25 United Launch Alliance, L.L.C. Asymmetrically-shaped isolator
DE102019207826A1 (de) * 2019-05-28 2020-12-03 Zf Friedrichshafen Ag Segmentierter Schwingungstilger
FI12778Y1 (fi) * 2019-11-25 2020-09-30 Labrys Oy Jousielementti
US11802606B2 (en) 2020-05-18 2023-10-31 The Boeing Company Planate dynamic isolator
AU2021273575A1 (en) 2020-12-17 2022-07-07 The Boeing Company Satellite thermal enclosure
US12162631B2 (en) 2020-12-17 2024-12-10 Maxar Space Llc Passively damped end fittings and brackets
CA3140352A1 (en) 2020-12-17 2022-06-17 The Boeing Company Stacked satellite assemblies and related methods
CN113700943B (zh) * 2021-09-10 2023-07-21 中国航发湖南动力机械研究所 一种管路支撑结构
DE102022200760A1 (de) * 2022-01-24 2023-07-27 Christian Bauer Gmbh + Co. Kg Flachformfeder

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3692264A (en) * 1970-07-13 1972-09-19 Industrial Research Prod Inc Shock isolation mounts for fragile devices
LU80296A1 (fr) * 1978-09-28 1980-04-21 Bekaert Sa Nv Structures amortissant des vibrations mecaniques
DE3908474A1 (de) * 1988-07-22 1990-01-25 Metzeler Gmbh Ringfoermiger federkoerper aus faserverbundwerkstoffen
FR2638799B1 (fr) * 1988-11-09 1991-01-25 Hutchinson Support elastique a raideurs anisotropes, notamment pour la suspension de carrosseries
US4954377A (en) * 1988-11-22 1990-09-04 The United States Of America As Represented By The Secretary Of The Navy Load bearing connective damper
US5203435A (en) * 1990-08-31 1993-04-20 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Composite passive damping struts for large precision structures
FR2689196B1 (fr) * 1992-03-31 1995-08-04 Hutchinson Dispositif de filtrage des vibrations et systeme de fixation d'une charge sur un support comportant une pluralite de tels dispositifs.
DE4340293C2 (de) * 1993-11-26 1996-05-23 Freudenberg Carl Fa Drehschwingungstilger
US5907452A (en) * 1997-10-20 1999-05-25 International Business Machines Corporation Apparatus and method to dampen flex cable vibration to disk drive actuator
US6199801B1 (en) * 1997-12-01 2001-03-13 Csa Engineering, Inc. Whole-spacecraft passive isolation devices
US6290183B1 (en) * 1999-10-19 2001-09-18 Csa Engineering, Inc. Three-axis, six degree-of-freedom, whole-spacecraft passive vibration isolation system
US6202961B1 (en) * 2000-03-21 2001-03-20 Csa Engineering Passive, multi-axis, highly damped, shock isolation mounts for spacecraft

Also Published As

Publication number Publication date
WO2007089248A3 (en) 2007-11-01
EP1994324A4 (en) 2013-10-16
US20070176337A1 (en) 2007-08-02
EP1994324A2 (en) 2008-11-26
US7249756B1 (en) 2007-07-31
DK1994324T3 (en) 2015-06-29
EP1994324B1 (en) 2015-04-08
WO2007089248A2 (en) 2007-08-09

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