DE60026896D1 - Strukturbauteil aus einem Verbundwerkstoff mit eingebauter Dämpfung - Google Patents

Strukturbauteil aus einem Verbundwerkstoff mit eingebauter Dämpfung

Info

Publication number
DE60026896D1
DE60026896D1 DE60026896T DE60026896T DE60026896D1 DE 60026896 D1 DE60026896 D1 DE 60026896D1 DE 60026896 T DE60026896 T DE 60026896T DE 60026896 T DE60026896 T DE 60026896T DE 60026896 D1 DE60026896 D1 DE 60026896D1
Authority
DE
Germany
Prior art keywords
damping
built
composite material
structural component
component made
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
DE60026896T
Other languages
English (en)
Other versions
DE60026896T2 (de
Inventor
Emil M Shtarkman
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.)
Northrop Grumman Systems Corp
Original Assignee
Northrop Grumman 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 Northrop Grumman Corp filed Critical Northrop Grumman Corp
Publication of DE60026896D1 publication Critical patent/DE60026896D1/de
Application granted granted Critical
Publication of DE60026896T2 publication Critical patent/DE60026896T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/02—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers
    • B29C70/021—Combinations of fibrous reinforcement and non-fibrous material
    • B29C70/025—Combinations of fibrous reinforcement and non-fibrous material with particular filler
    • 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
    • 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
    • B64G1/648—Tethers
    • 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
    • F16F1/366—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers made of fibre-reinforced plastics, i.e. characterised by their special construction from such 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
    • F16F1/371—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by inserts or auxiliary extension or exterior elements, e.g. for rigidification
    • 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
    • F16F9/30—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium with solid or semi-solid material, e.g. pasty masses, as damping medium
    • 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
    • F16F2226/00—Manufacturing; Treatments
DE60026896T 1999-05-27 2000-05-18 Strukturbauteil aus einem Verbundwerkstoff mit eingebauter Dämpfung Expired - Lifetime DE60026896T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US321502 1999-05-27
US09/321,502 US6345788B1 (en) 1999-05-27 1999-05-27 Composite structure element with built-in damping

Publications (2)

Publication Number Publication Date
DE60026896D1 true DE60026896D1 (de) 2006-05-18
DE60026896T2 DE60026896T2 (de) 2006-08-24

Family

ID=23250870

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60026896T Expired - Lifetime DE60026896T2 (de) 1999-05-27 2000-05-18 Strukturbauteil aus einem Verbundwerkstoff mit eingebauter Dämpfung

Country Status (4)

Country Link
US (1) US6345788B1 (de)
EP (1) EP1055600B1 (de)
JP (1) JP3367936B2 (de)
DE (1) DE60026896T2 (de)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2787764B1 (fr) * 1998-12-29 2001-02-16 Centre Nat Etd Spatiales Dispositif de suspension d'une charge utile dans un lanceur spatial
SE515850C2 (sv) * 2000-09-18 2001-10-15 Saab Ericsson Space Ab Anordning och metod vid en rymdfarkost
US20050064165A1 (en) * 2003-09-22 2005-03-24 Cleveland Mark A. Acoustically damped composite construction for the forward portion of a rocket or missile
US7222823B2 (en) * 2004-07-06 2007-05-29 Ata Engineering, Inc. Payload adapter
DE102009054458A1 (de) 2009-12-10 2011-06-16 Zf Friedrichshafen Ag Anordnungsstruktur in Sandwichbauweise und deren Anwendung
RU2478532C1 (ru) * 2011-08-04 2013-04-10 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Космическая головная часть и способ ее сборки
RU2478531C1 (ru) * 2011-08-04 2013-04-10 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Космическая головная часть
ES2597706T3 (es) * 2012-05-09 2017-01-20 Ruag Space Ab Anillo de interfaz de soporte de carga para una nave espacial
US20140332632A1 (en) * 2013-05-10 2014-11-13 Space Systems/Loral, Llc Isolation of payload from launch vehicle dynamic loads
RU2564458C1 (ru) * 2014-06-26 2015-10-10 Российская Федерация, от имени которой выступает Федеральное космическое агентство Космическая головная часть
KR101854140B1 (ko) 2016-11-01 2018-05-03 한국항공우주연구원 위성 구조체
US10562650B2 (en) * 2017-06-28 2020-02-18 The Boeing Company Corrugated payload adaptor structure
KR102007185B1 (ko) * 2017-12-08 2019-08-05 연세대학교 산학협력단 탄성메타물질을 이용한 인공위성 우주 테더 장치
RU183999U1 (ru) * 2018-04-18 2018-10-11 Федеральное государственное автономное образовательное учреждение высшего образования "Национальный исследовательский Томский государственный университет" (НИ ТГУ) Адаптер в виде конической оболочки вращения из композиционных материалов
CN111619831B (zh) * 2020-04-29 2021-11-16 航天东方红卫星有限公司 一种连杆式星箭分离机构

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4310132A (en) * 1978-02-16 1982-01-12 Nasa Fuselage structure using advanced technology fiber reinforced composites
US4411380A (en) * 1981-06-30 1983-10-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Metal matrix composite structural panel construction
US4682744A (en) * 1985-04-08 1987-07-28 Rca Corporation Spacecraft structure
JPS6360743A (ja) * 1986-09-02 1988-03-16 東レ株式会社 軽量複合材料
US4898783A (en) * 1986-10-14 1990-02-06 The Dow Chemical Company Sound and thermal insulation
US4812854A (en) * 1987-05-05 1989-03-14 Harris Corp. Mesh-configured rf antenna formed of knit graphite fibers
US4983451A (en) 1987-08-05 1991-01-08 Kabushiki Kaisha Kobe Seiko Sho Carbon fiber-reinforced carbon composite material and process for producing the same
CA1332129C (en) * 1987-11-21 1994-09-27 Tadao Inabata Light filler material having damping function and composite material thereof
DD278990A1 (de) * 1988-12-30 1990-05-23 Oschatz Glasseide Veb Leitfaehiges textiles flaechengebilde aus glasseidenelementarfaeden
US5171630A (en) * 1989-04-17 1992-12-15 Georgia Tech Research Corporation Flexible multiply towpreg
FR2655036B1 (fr) * 1989-11-27 1993-07-09 Pradom Ltd Materiaux composites complexes a matrice organique-metallique, leur procede de fabrication et leur utilisation pour la fabrication de produits de haute technologie destines notamment a l'aerospatial ou aux vehicules a grande vitesse, tels que tgv.
CA2042417A1 (en) * 1990-05-29 1991-11-30 Peter G. Donecker Process to manufacture conductive composite articles
FR2667616B1 (fr) * 1990-10-05 1993-01-15 Aerospatiale Procede et installation de metallisation en continu d'une meche de fibres etalee.
US5494634A (en) * 1993-01-15 1996-02-27 The United States Of America As Represented By The Secretary Of The Navy Modified carbon for improved corrosion resistance
US5474262A (en) * 1994-02-08 1995-12-12 Fairchild Space And Defense Corporation Spacecraft structure and method
GB9408567D0 (en) * 1994-04-29 1994-06-22 Mediquest Products Ltd A valve for urine drainage applications
US5655757A (en) 1995-02-17 1997-08-12 Trw Inc. Actively controlled damper
GB9504372D0 (en) * 1995-03-04 1995-04-26 British Aerospace A composite laminate
US6045680A (en) * 1996-05-30 2000-04-04 E. I. Du Pont De Nemours And Company Process for making thermally stable metal coated polymeric monofilament or yarn
US5848767A (en) * 1996-08-05 1998-12-15 The Boeing Company One piece spacecraft frame
AU5584898A (en) * 1996-11-15 1998-06-03 Brigham Young University Damped composite structures with fiber wave patterns and method and apparatus for making same
US5961078A (en) * 1997-06-27 1999-10-05 Mcdonnell Douglas Corporation Passive axial vibration isolation system for a spacecraft launch vehicle
US6098926A (en) * 1998-08-06 2000-08-08 Lockheed Martin Corporation Composite fairing with integral damping and internal helmholz resonators

Also Published As

Publication number Publication date
JP3367936B2 (ja) 2003-01-20
EP1055600A3 (de) 2001-08-29
JP2001129917A (ja) 2001-05-15
US6345788B1 (en) 2002-02-12
DE60026896T2 (de) 2006-08-24
EP1055600A2 (de) 2000-11-29
EP1055600B1 (de) 2006-03-29

Similar Documents

Publication Publication Date Title
DE60026896D1 (de) Strukturbauteil aus einem Verbundwerkstoff mit eingebauter Dämpfung
DE69921477D1 (de) Katheter mit einer versteifung aus verbundmaterial
DE69823353D1 (de) Verbundgegenstände mit einem fluorpolymergemisch
DE59901643D1 (de) Verbundmaterial mit einem verstärkten verbindungsbereich
ATE489514T1 (de) Verbundbaustoff
DE10085065T1 (de) Aufsaugeartikel mit einem entfaltbaren Dichtungselement
ID26777A (id) Pelapis susunan suatu komposit
DE60022871D1 (de) Superabsorbierende polymere enthaltende kompositmaterialien
ATA130298A (de) Verbundwerkstoff aus zumindest zwei schichten
DE69527212T2 (de) Absorbierender artikel mit einem verbundabsorptionskern
DE69911507D1 (de) Flügelstruktur aus Faserverbundstoff
DE60012330D1 (de) Verbundvliesmaterial
DE69420963T2 (de) Absorbierendes verbundmaterial mit starken dochteigenschaften
DE69914974D1 (de) Ausleger aus Verbundwerkstoff
DE602004010401D1 (de) Cellulosegefüllte thermoplastische verbundwerkstoffe
DE60005097D1 (de) Kombinationsbehälter
DE50007631D1 (de) Kunststoffbauelement mit Einlegeteilen
ID28374A (id) Bahan penyerap
DE60130545D1 (de) Beschichtungskabine mit pulverrückgewinnung
DK1173134T3 (da) Termoplastisk flerlagsstruktur
DE19983822T1 (de) Dehnbares Verbundmaterial mit kontinuierlichen Kräuseln
DE69515338D1 (de) Anzug aus einem Verbundvliesstoff
DE69916471D1 (de) Thermoplastische copolyester-zusammensetzungen die mit epoxidverbindungen modifiziert sind
DE60121247D1 (de) Empfänger mit einem Synthesizer
DE69913886D1 (de) Stossabsorbierendes Material

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
R082 Change of representative

Ref document number: 1055600

Country of ref document: EP

Representative=s name: WUESTHOFF & WUESTHOFF PATENT- UND RECHTSANWAEL, DE

R081 Change of applicant/patentee

Ref document number: 1055600

Country of ref document: EP

Owner name: NORTHROP GRUMMAN SYSTEMS CORPORATION, US

Free format text: FORMER OWNER: NORTHROP GRUMMAN CORP., LOS ANGELES, US

Effective date: 20120814

R082 Change of representative

Ref document number: 1055600

Country of ref document: EP

Representative=s name: WUESTHOFF & WUESTHOFF PATENT- UND RECHTSANWAEL, DE

Effective date: 20120814