ES2160402T3 - Dispositivo de suspension de una carga util en un lanzador espacial. - Google Patents

Dispositivo de suspension de una carga util en un lanzador espacial.

Info

Publication number
ES2160402T3
ES2160402T3 ES98905458T ES98905458T ES2160402T3 ES 2160402 T3 ES2160402 T3 ES 2160402T3 ES 98905458 T ES98905458 T ES 98905458T ES 98905458 T ES98905458 T ES 98905458T ES 2160402 T3 ES2160402 T3 ES 2160402T3
Authority
ES
Spain
Prior art keywords
launcher
useful load
fluid
suspension device
cameras
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
ES98905458T
Other languages
English (en)
Inventor
Pascal Marie-Dominique Hubert
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.)
Centre National dEtudes Spatiales CNES
Original Assignee
Centre National dEtudes Spatiales CNES
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 Centre National dEtudes Spatiales CNES filed Critical Centre National dEtudes Spatiales CNES
Application granted granted Critical
Publication of ES2160402T3 publication Critical patent/ES2160402T3/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
    • F16F1/00—Springs
    • F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/42—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by the mode of stressing
    • F16F1/52—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by the mode of stressing loaded in combined stresses
    • F16F1/54—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by the mode of stressing loaded in combined stresses loaded in compression and shear
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/641—Interstage or payload connectors
    • 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
    • F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
    • F16F9/02—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using gas only or vacuum
    • F16F9/04—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using gas only or vacuum in a chamber with a flexible wall
    • F16F9/0418—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using gas only or vacuum in a chamber with a flexible wall having a particular shape, e.g. annular, spherical, tube-like
    • 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
    • F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
    • F16F9/10—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using liquid only; using a fluid of which the nature is immaterial
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/641—Interstage or payload connectors
    • B64G1/6425—Interstage or payload connectors arrangements for damping vibrations

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • Child & Adolescent Psychology (AREA)
  • Vehicle Body Suspensions (AREA)
  • Vibration Prevention Devices (AREA)
  • Toys (AREA)
  • Fluid-Damping Devices (AREA)
  • Gas Burners (AREA)

Abstract

.ESTE COMPRENDE CAMARAS ANULARES CON FLUIDO DE GEOMETRIA VARIABLE (12 I ) INSTALADAS ENTRE DICHA LANZADERA Y DICHA CARGA UTIL Y UN PRIMER (10") Y UN SEGUNDO (11") DISPOSITIVO RIGIDO FIJADOS, POR AMBAS PARTES DE DICHAS CAMARAS (12 I ), A DICHA CARGA UTIL Y A LA LANZADERA, RESPECTIVAMENTE PARA TRANSMITIR ESFUERZOS ENTRE ELLOS A TRAVES DE DICHAS CAMARAS. LAS CAMARAS CON FLUIDO (12 I ) Y EL PRIMER (10") Y EL SEGUNDO ( 11") ORGANO RIGIDO DE ACOPLAMIENTO SON COEXTENSIVOS, DE FORMA ANULAR Y COAXIALES A UN EJE LONGITUDINAL COMUN A LA LANZADERA Y A LA CARGA UTILES. EL PRIMER (10") Y EL SEGUNDO (11") ELEMENTO RIGIDO ANULAR DE ACOPLAMIENTO COMPRENDEN CADA UNO NERVADURAS EXTERNAS (10A", 10B") E INTERNAS (11A", 11B") RESPECTIVAMENTE, SEPARADAS AXIALMENTE POR UNA DE LAS CAMARAS CON FLUIDO ANULAR (12 I ).
ES98905458T 1997-01-29 1998-01-29 Dispositivo de suspension de una carga util en un lanzador espacial. Expired - Lifetime ES2160402T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9700949A FR2758791B1 (fr) 1997-01-29 1997-01-29 Dispositif de suspension d'une charge utile dans un lanceur spatial

Publications (1)

Publication Number Publication Date
ES2160402T3 true ES2160402T3 (es) 2001-11-01

Family

ID=9503082

Family Applications (1)

Application Number Title Priority Date Filing Date
ES98905458T Expired - Lifetime ES2160402T3 (es) 1997-01-29 1998-01-29 Dispositivo de suspension de una carga util en un lanzador espacial.

Country Status (8)

Country Link
US (1) US6244541B1 (es)
EP (1) EP0956236B1 (es)
JP (1) JP2001509751A (es)
DE (2) DE69801309D1 (es)
ES (1) ES2160402T3 (es)
FR (1) FR2758791B1 (es)
RU (1) RU2203839C2 (es)
WO (1) WO1998032658A1 (es)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2166234B1 (es) * 1998-11-18 2003-02-16 Eads Constr Aeronauticas Sa Un sistema de modificacion de las propiedades de rigidez/amortiguacion de uniones estructurales.
FR2787765B1 (fr) 1998-12-29 2001-02-16 Centre Nat Etd Spatiales Dispositif de support d'une charge utile dans un lanceur de ladite charge utile
FR2787764B1 (fr) 1998-12-29 2001-02-16 Centre Nat Etd Spatiales Dispositif de suspension d'une charge utile dans un lanceur spatial
US6202961B1 (en) * 2000-03-21 2001-03-20 Csa Engineering Passive, multi-axis, highly damped, shock isolation mounts for spacecraft
SE515850C2 (sv) * 2000-09-18 2001-10-15 Saab Ericsson Space Ab Anordning och metod vid en rymdfarkost
US6609681B2 (en) * 2001-07-05 2003-08-26 The Boeing Company Method and apparatus for damping vibration
US6695261B2 (en) * 2002-02-11 2004-02-24 The Boeing Company Shock isolation system for spacecraft fairing
US20050109878A1 (en) * 2002-03-28 2005-05-26 Dutch Space B.V. Spacecraft and method for building such a spacecraft and an adapter to be used in such a spacecraft
US20050056509A1 (en) * 2003-09-16 2005-03-17 The Boeing Company Shock isolation system
US7222823B2 (en) * 2004-07-06 2007-05-29 Ata Engineering, Inc. Payload adapter
US7819221B1 (en) * 2005-09-27 2010-10-26 The United States Of America As Represented By The Secretary Of The Air Force Lightweight acoustic damping treatment
FR2895775B1 (fr) * 2006-01-03 2008-02-29 Alcatel Sa Dispositif d'amortissement actif des vibrations subies par un element fragile d'un equipement en mouvement, a auto-alimentation
US7866607B2 (en) * 2006-12-21 2011-01-11 Intelsat Piggyback satellite payload arrangement, a device for and method of attaching a piggyback satellite payload and adapter to be used for a piggyback satellite payload arrangement for launching the piggyback satellite
US7905453B2 (en) * 2006-12-21 2011-03-15 Intelsat Piggyback equipment panel payload arrangement, a device for and method of attaching a hosted secondary piggyback payload and adapter to be used for a piggyback secondary payload arrangement for launching the piggyback equipment panel secondary
FR2951792B1 (fr) * 2009-10-28 2017-02-03 Airbus Operations Sas Dispositif de liaison a amortissement antivibratoire
FR2965876B1 (fr) * 2010-10-11 2013-10-18 Airbus Operations Sas Dispositif de filtrage fluide de vibrations mecaniques
JP2012131410A (ja) * 2010-12-22 2012-07-12 Mitsubishi Heavy Ind Ltd アダプタおよびペイロード打ち上げ用ロケット
JP5888671B2 (ja) * 2011-11-24 2016-03-22 株式会社Ｉｈｉエアロスペース 振動緩和装置
FR3012553B1 (fr) * 2013-10-31 2016-06-24 Astrium Sas Module d'isolation de vibrations a effets non lineaires diminues
US10214303B1 (en) * 2016-09-27 2019-02-26 Space Systems/Loral, Llc Low cost launch vehicle fairing
US10562650B2 (en) * 2017-06-28 2020-02-18 The Boeing Company Corrugated payload adaptor structure
CN109264029A (zh) * 2018-09-27 2019-01-25 宁波天擎航天科技有限公司 一种运载火箭
US20250026497A1 (en) * 2023-07-17 2025-01-23 Maxar Space Llc Linked spacecraft dispensing
US12214909B1 (en) * 2023-07-17 2025-02-04 Maxar Space Llc Dispensing hinge assembly

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB252843A (en) * 1925-04-14 1926-06-10 George Sydney Dominy Improvements relating to the supporting of road & rail vehicles and all apparatus needing isolation from vibration, by means of air under pressure
US2047963A (en) * 1933-04-25 1936-07-21 Edward L Hoffman Aircraft engine mount
US2999707A (en) * 1956-11-28 1961-09-12 Mobay Chemical Corp Flexible joint
US3222017A (en) * 1964-03-30 1965-12-07 Gen Electric Engine mounting
GB1079281A (en) * 1964-10-06 1967-08-16 Metalastik Ltd Resilient mountings and supports
JPS5447075A (en) * 1977-09-20 1979-04-13 Toshiba Corp Vibration-proof equipment
FR2426830A1 (fr) * 1978-05-22 1979-12-21 Org Europeene De Rech Dispositif a moment d'inertie a suspension magnetique
DE2838737A1 (de) * 1978-09-06 1980-03-20 Messerschmitt Boelkow Blohm Daemmelement zur schwingungsisolierung
US4361296A (en) * 1980-03-10 1982-11-30 The Boeing Company Uniflange coupling assembly
US4765382A (en) * 1987-07-20 1988-08-23 Sahagian Edward H Reinforced resilient wheel
US4811919A (en) * 1987-08-06 1989-03-14 Lord Corporation Volume compensated fluid mount
US4848525A (en) * 1987-11-02 1989-07-18 The Boeing Company Dual mode vibration isolator
US5244170A (en) * 1991-10-15 1993-09-14 General Dynamics Corporation, Space Systems Division Passive nonlinear interface strut (PNIS)
US5219051A (en) * 1991-10-25 1993-06-15 Honeywell Inc. Folded viscous damper
RU2066799C1 (ru) * 1992-07-02 1996-09-20 Дмитрий Юганесович Аллик Виброизолирующая опора
RU2044661C1 (ru) * 1994-08-29 1995-09-27 Волжское муниципальное производственно-техническое предприятие "АВТОПРОМ" Пневматическая подвеска
US5655757A (en) * 1995-02-17 1997-08-12 Trw Inc. Actively controlled damper
US5878980A (en) * 1997-02-05 1999-03-09 Hughes Electronics Corporation Attenuation ring
US6012680A (en) * 1997-06-27 2000-01-11 Mcdonnell Douglas Corporation Passive lateral vibration isolation system for a spacecraft launch vehicle

Also Published As

Publication number Publication date
JP2001509751A (ja) 2001-07-24
EP0956236B1 (fr) 2001-08-08
WO1998032658A1 (fr) 1998-07-30
DE69801309T2 (de) 2002-04-25
DE69801309T4 (de) 2003-11-20
DE69801309D1 (de) 2001-09-13
FR2758791A1 (fr) 1998-07-31
US6244541B1 (en) 2001-06-12
RU2203839C2 (ru) 2003-05-10
FR2758791B1 (fr) 1999-03-26
EP0956236A1 (fr) 1999-11-17

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