DE60026896D1 - Strukturbauteil aus einem Verbundwerkstoff mit eingebauter Dämpfung - Google Patents
Strukturbauteil aus einem Verbundwerkstoff mit eingebauter DämpfungInfo
- 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
Links
- 239000002131 composite material Substances 0.000 title 1
- 238000013016 damping Methods 0.000 title 1
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
- B64G1/641—Interstage or payload connectors
- B64G1/6425—Interstage or payload connectors arrangements for damping vibrations
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Laminated Bodies (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Details Of Aerials (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/321,502 US6345788B1 (en) | 1999-05-27 | 1999-05-27 | Composite structure element with built-in damping |
US321502 | 1999-05-27 |
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 (16)
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 |
SE0003315L (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 |
EP2662289B1 (de) * | 2012-05-09 | 2016-07-13 | RUAG Space AB | Verbindungsring mit Lastlager für ein Raumschiff |
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 |
US20230211901A1 (en) * | 2022-01-03 | 2023-07-06 | Northrop Grumman Systems Corporation | Latticed structure for vibration control in dynamic environments |
Family Cites Families (23)
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 |
WO1998021034A1 (en) * | 1996-11-15 | 1998-05-22 | 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 |
-
1999
- 1999-05-27 US US09/321,502 patent/US6345788B1/en not_active Expired - Lifetime
-
2000
- 2000-05-18 EP EP00110232A patent/EP1055600B1/de not_active Expired - Lifetime
- 2000-05-18 DE DE60026896T patent/DE60026896T2/de not_active Expired - Lifetime
- 2000-05-26 JP JP2000156164A patent/JP3367936B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP1055600B1 (de) | 2006-03-29 |
EP1055600A2 (de) | 2000-11-29 |
US6345788B1 (en) | 2002-02-12 |
EP1055600A3 (de) | 2001-08-29 |
JP3367936B2 (ja) | 2003-01-20 |
DE60026896T2 (de) | 2006-08-24 |
JP2001129917A (ja) | 2001-05-15 |
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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 |
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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 |