ATE193942T1 - Verfahren zur herstellung von flugkörpern oder flugkörperkomponenten - Google Patents
Verfahren zur herstellung von flugkörpern oder flugkörperkomponentenInfo
- Publication number
- ATE193942T1 ATE193942T1 AT97935567T AT97935567T ATE193942T1 AT E193942 T1 ATE193942 T1 AT E193942T1 AT 97935567 T AT97935567 T AT 97935567T AT 97935567 T AT97935567 T AT 97935567T AT E193942 T1 ATE193942 T1 AT E193942T1
- Authority
- AT
- Austria
- Prior art keywords
- sic
- missile
- silicon carbide
- carbon
- components
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/34—Protection against overheating or radiation, e.g. heat shields; Additional cooling arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Ceramic Products (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Details Of Aerials (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19632893A DE19632893C2 (de) | 1996-08-16 | 1996-08-16 | Verfahren zur Herstellung von Flugkörperkomponenten aus faserverstärkter Keramik |
PCT/EP1997/004235 WO1998008044A1 (de) | 1996-08-16 | 1997-08-04 | Flugkörperkomponenten aus faserverstärkter keramik |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE193942T1 true ATE193942T1 (de) | 2000-06-15 |
Family
ID=7802697
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT97935567T ATE193942T1 (de) | 1996-08-16 | 1997-08-04 | Verfahren zur herstellung von flugkörpern oder flugkörperkomponenten |
Country Status (5)
Country | Link |
---|---|
US (1) | US6460807B1 (de) |
EP (1) | EP0918976B1 (de) |
AT (1) | ATE193942T1 (de) |
DE (2) | DE19632893C2 (de) |
WO (1) | WO1998008044A1 (de) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6935594B1 (en) | 2001-11-09 | 2005-08-30 | Advanced Ceramics Research, Inc. | Composite components with integral protective casings |
DE10157752B4 (de) * | 2001-11-27 | 2006-04-06 | Eads Space Transportation Gmbh | Düsenverlängerung |
DE10230231B4 (de) * | 2002-07-04 | 2007-07-05 | Sgl Carbon Ag | Mehrschichtiger Verbundwerkstoff |
US20040157532A1 (en) * | 2003-01-14 | 2004-08-12 | George Koutlakis | Glass-like polysaccharides |
DE102004037487A1 (de) * | 2004-07-27 | 2006-03-23 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Strahlruder und Verfahren zur Herstellung eines Strahlruders |
US7429017B2 (en) * | 2005-07-21 | 2008-09-30 | Raytheon Company | Ejectable aerodynamic stability and control |
US7681834B2 (en) * | 2006-03-31 | 2010-03-23 | Raytheon Company | Composite missile nose cone |
US7800032B1 (en) * | 2006-11-30 | 2010-09-21 | Raytheon Company | Detachable aerodynamic missile stabilizing system |
US7829829B2 (en) * | 2007-06-27 | 2010-11-09 | Kazak Composites, Incorporated | Grid fin control system for a fluid-borne object |
DE102008025355B4 (de) * | 2008-05-19 | 2013-01-24 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Rheometer und Verfahren zur rheologischen Messung an einem Probenkörper |
DE102009013150B4 (de) * | 2009-03-06 | 2011-05-05 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Bauteil zum Einsatz in Heißgasströmungen |
CN103979993B (zh) * | 2014-05-27 | 2015-07-29 | 西安超码科技有限公司 | 一种大尺寸炭/碳化硅复合材料隔热底板的制备方法 |
CN108007280B (zh) * | 2017-12-28 | 2023-08-15 | 北京威标至远科技发展有限公司 | 一种舵机防热结构 |
GB2578572B (en) * | 2018-10-30 | 2022-08-17 | Bae Systems Plc | A sabot |
EP4032144A4 (de) * | 2019-09-20 | 2022-11-16 | Aselsan Elektronik Sanayi ve Ticaret Anonim Sirketi | Verfahren zur herstellung keramischer mehrschichtstrukturen durch endlosfäden mit gleicher zusammensetzung |
CN112719804B (zh) * | 2020-12-18 | 2022-06-07 | 湖北三江航天江北机械工程有限公司 | 一种训练用空空导弹吊挂组合的加工方法 |
CN112693623B (zh) * | 2020-12-21 | 2022-05-27 | 中国空气动力研究与发展中心高速空气动力研究所 | 导弹栅格舵铰链力矩模型爪盘式自锁定位结构 |
CN112853250B (zh) * | 2020-12-28 | 2022-08-05 | 哈尔滨工业大学 | 一种组合燃气舵构件的制备方法 |
CN114235321B (zh) * | 2022-02-25 | 2022-04-26 | 中国空气动力研究与发展中心高速空气动力研究所 | 一种燃气舵和喷管一体化风洞测力实验装置 |
Family Cites Families (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1229246A (de) * | 1967-06-08 | 1971-04-21 | ||
US3676293A (en) * | 1970-04-22 | 1972-07-11 | Monsanto Co | Laminated article |
US3676623A (en) | 1970-12-17 | 1972-07-11 | Westinghouse Electric Corp | Circuit interrupter |
US3796616A (en) * | 1972-05-23 | 1974-03-12 | Haveg Industries Inc | Porous substrate for fibrous graphite structure produced by addition of degradable material |
US4476178A (en) | 1982-06-24 | 1984-10-09 | United Technologies Corporation | Composite silicon carbide coatings for carbon-carbon materials |
US4425407A (en) | 1982-06-24 | 1984-01-10 | United Technologies Corporation | CVD SiC pretreatment for carbon-carbon composites |
US4477024A (en) | 1983-04-05 | 1984-10-16 | The United States Of America As Represented By The Secretary Of The Air Force | Carbon/carbon rocket motor exit cone reinforcement |
NO153190C (no) * | 1983-10-20 | 1986-01-29 | Raufoss Ammunisjonsfabrikker | Anordning ved raketter. |
JPS61122162A (ja) * | 1984-11-14 | 1986-06-10 | 日立化成工業株式会社 | 炭素繊維強化炭素材料の製造法 |
JPS61247663A (ja) * | 1985-04-22 | 1986-11-04 | 工業技術院長 | 炭素連続繊維強化SiC複合体の製造方法 |
US4706912A (en) * | 1985-12-16 | 1987-11-17 | The United States Of America As Represented By The Secretary Of The Army | Structural external insulation for hypersonic missiles |
US4961384A (en) * | 1986-02-18 | 1990-10-09 | The United States Of America As Represented By The Secretary Of The Army | Hypervelocity penetrator for an electromagnetic accelerator |
FR2611198B1 (fr) * | 1987-02-25 | 1991-12-06 | Aerospatiale | Materiau composite a matrice et fibres de renforcement carbonees et son procede de fabrication |
DE3927917A1 (de) * | 1989-08-24 | 1991-02-28 | Rheinmetall Gmbh | Fluegelstabilisiertes geschoss |
FR2667591B1 (fr) * | 1990-10-04 | 1993-11-05 | Ceramiques Composites | Procede d'assemblage d'objets en carbure de silicium et assemblages ainsi obtenus. |
JPH0813713B2 (ja) * | 1990-10-11 | 1996-02-14 | 東芝セラミックス株式会社 | SiC被覆C/C複合材 |
JPH07119079B2 (ja) * | 1991-03-15 | 1995-12-20 | 三井造船株式会社 | 高温耐熱強度部材 |
JP2704332B2 (ja) * | 1991-10-11 | 1998-01-26 | 株式会社ノリタケカンパニーリミテド | 炭素繊維強化窒化珪素質ナノ複合材及びその製造方法 |
DE4136880C2 (de) * | 1991-11-09 | 1994-02-17 | Sintec Keramik Gmbh | Verfahren zur Herstellung eines oxidationsbeständigen Bauteils auf CFC-Basis und dessen Anwendung |
US5525372A (en) * | 1992-09-08 | 1996-06-11 | The United States Of America As Represented By The Secretary Of The Army | Method of manufacturing hybrid fiber-reinforced composite nozzle material |
US5291830A (en) * | 1992-10-30 | 1994-03-08 | Lockheed Corporation | Dual-mode semi-passive nosetip for a hypersonic weapon |
US5411763A (en) * | 1993-01-11 | 1995-05-02 | Martin Marietta Energy Systems, Inc. | Method of making a modified ceramic-ceramic composite |
JPH06305863A (ja) * | 1993-04-28 | 1994-11-01 | Mitsubishi Kasei Corp | 炭化珪素質被覆炭素繊維強化炭素複合材の製造法 |
US6037023A (en) * | 1994-07-08 | 2000-03-14 | Raytheon Company | Broadband composite structure fabricated from inorganic polymer matrix reinforced with glass or ceramic woven cloth |
DE19513508A1 (de) * | 1995-04-10 | 1996-10-17 | Abb Research Ltd | Verdichter |
US5806791A (en) * | 1995-05-26 | 1998-09-15 | Raytheon Company | Missile jet vane control system and method |
DE19730674A1 (de) * | 1997-07-17 | 1999-01-21 | Deutsch Zentr Luft & Raumfahrt | Brennkammer und Verfahren zur Herstellung einer Brennkammer |
DE19746598C2 (de) * | 1997-10-22 | 2000-12-07 | Dornier Gmbh | Keramikverbundwerkstoff und seine Verwendung |
DE19804232C2 (de) * | 1998-02-04 | 2000-06-29 | Daimler Chrysler Ag | Brennkammer für Hochleistungstriebwerke und Düsen |
-
1996
- 1996-08-16 DE DE19632893A patent/DE19632893C2/de not_active Revoked
-
1997
- 1997-08-04 AT AT97935567T patent/ATE193942T1/de not_active IP Right Cessation
- 1997-08-04 EP EP97935567A patent/EP0918976B1/de not_active Expired - Lifetime
- 1997-08-04 WO PCT/EP1997/004235 patent/WO1998008044A1/de active IP Right Grant
- 1997-08-04 US US09/242,372 patent/US6460807B1/en not_active Expired - Fee Related
- 1997-08-04 DE DE59701892T patent/DE59701892D1/de not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
WO1998008044A1 (de) | 1998-02-26 |
US6460807B1 (en) | 2002-10-08 |
DE59701892D1 (de) | 2000-07-20 |
EP0918976A1 (de) | 1999-06-02 |
DE19632893A1 (de) | 1998-02-19 |
EP0918976B1 (de) | 2000-06-14 |
DE19632893C2 (de) | 2001-02-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
REN | Ceased due to non-payment of the annual fee |