RU2008142851A - Способ соединения фрагментов углерод-углеродного композита и изготовленный этим способом авиационный тормозной диск - Google Patents
Способ соединения фрагментов углерод-углеродного композита и изготовленный этим способом авиационный тормозной диск Download PDFInfo
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- 239000012634 fragment Substances 0.000 title claims abstract 27
- 239000002131 composite material Substances 0.000 title claims abstract 22
- CREMABGTGYGIQB-UHFFFAOYSA-N carbon carbon Chemical compound C.C CREMABGTGYGIQB-UHFFFAOYSA-N 0.000 title claims abstract 20
- 239000011203 carbon fibre reinforced carbon Substances 0.000 title claims abstract 20
- 238000000034 method Methods 0.000 title claims abstract 16
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract 11
- 239000000843 powder Substances 0.000 claims abstract 10
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract 7
- 239000002245 particle Substances 0.000 claims abstract 4
- 239000000203 mixture Substances 0.000 claims abstract 2
- 238000003825 pressing Methods 0.000 claims abstract 2
- 238000006479 redox reaction Methods 0.000 claims abstract 2
- 239000003245 coal Substances 0.000 claims 3
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- C04B2235/38—Non-oxide ceramic constituents or additives
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- C04B2237/70—Forming laminates or joined articles comprising layers of a specific, unusual thickness
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Abstract
1. Способ соединения фрагментов углерод-углеродного композита, включающий стадии: ! получение первого фрагмента углерод-углеродного композита и второго фрагмента углерод-углеродного композита, причем второй фрагмент углерод-углеродного композита имеет поверхность, соответствующую поверхности первого фрагмента углерод-углеродного композита; ! нанесение слоя смеси порошка титана и угольного порошка на поверхность первого фрагмента; ! наложение второго фрагмента углерод-углеродного композита на слой порошка таким образом, чтобы подогнать по их поверхности с образованием конструкции из первого фрагмента углерод-углеродного композита, слоя порошка и второго фрагмента углерод-углеродного композита; ! помещение указанной конструкции в пресс и воздействие давления на конструкцию для сжатия двух фрагментов, соединенных по соответствующим друг другу поверхностям; ! пропускание электрического тока через порошок в указанной конструкции для инициирования окислительно-восстановительной реакции, в результате которой происходит связывание фрагментов углерод-углеродного композита. ! 2. Способ по п.1, включающий также дополнительно стадию удаления соединенных фрагментов композита из пресса через 30 мин после помещения в пресс несвязанных фрагментов. ! 3. Способ по п.1, в котором угольный порошок является графитовым порошком и мольное соотношение порошка титана и графитового порошка находится в интервале от 3:1 до 1:1. ! 4. Способ по п.1, в котором средний диаметр частиц порошка титана находится в интервале 25-250 мкм. ! 5. Способ по п.1, в котором углеродный порошок является графитовым порошком и средний диаметр частиц по�
Claims (9)
1. Способ соединения фрагментов углерод-углеродного композита, включающий стадии:
получение первого фрагмента углерод-углеродного композита и второго фрагмента углерод-углеродного композита, причем второй фрагмент углерод-углеродного композита имеет поверхность, соответствующую поверхности первого фрагмента углерод-углеродного композита;
нанесение слоя смеси порошка титана и угольного порошка на поверхность первого фрагмента;
наложение второго фрагмента углерод-углеродного композита на слой порошка таким образом, чтобы подогнать по их поверхности с образованием конструкции из первого фрагмента углерод-углеродного композита, слоя порошка и второго фрагмента углерод-углеродного композита;
помещение указанной конструкции в пресс и воздействие давления на конструкцию для сжатия двух фрагментов, соединенных по соответствующим друг другу поверхностям;
пропускание электрического тока через порошок в указанной конструкции для инициирования окислительно-восстановительной реакции, в результате которой происходит связывание фрагментов углерод-углеродного композита.
2. Способ по п.1, включающий также дополнительно стадию удаления соединенных фрагментов композита из пресса через 30 мин после помещения в пресс несвязанных фрагментов.
3. Способ по п.1, в котором угольный порошок является графитовым порошком и мольное соотношение порошка титана и графитового порошка находится в интервале от 3:1 до 1:1.
4. Способ по п.1, в котором средний диаметр частиц порошка титана находится в интервале 25-250 мкм.
5. Способ по п.1, в котором углеродный порошок является графитовым порошком и средний диаметр частиц порошка графита находится в интервале 1-10 мкм.
6. Способ по п.1, в котором слой порошка титана и угольного порошка имеет толщину 10-100 мкм.
7. Способ по п.1, в котором к конструкции прилагают давление в интервале 5000-10000 фунт/кв.дюйм (350-700 кг/см2).
8. Способ по п.1, в котором пропускаемый через порошок в конструкции электрический ток находится в интервале 400-1200 А.
9. Авиационный тормозной диск из углерод-углеродного композита, изготовленный способом по п.1.
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US11/391,255 | 2006-03-29 | ||
US11/391,255 US7858187B2 (en) | 2006-03-29 | 2006-03-29 | Bonding of carbon-carbon composites using titanium carbide |
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RU2008142851/03A RU2008142851A (ru) | 2006-03-29 | 2007-03-27 | Способ соединения фрагментов углерод-углеродного композита и изготовленный этим способом авиационный тормозной диск |
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US (1) | US7858187B2 (ru) |
EP (1) | EP1999089B1 (ru) |
DE (1) | DE602007003819D1 (ru) |
RU (1) | RU2008142851A (ru) |
WO (1) | WO2007115022A1 (ru) |
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US7922845B2 (en) * | 2006-03-29 | 2011-04-12 | Honeywell International Inc. | Apparatus and methods for bonding carbon-carbon composites through a reactant layer |
US9321692B2 (en) * | 2008-08-06 | 2016-04-26 | Honeywell International Inc. | Rapid synthesis of silicon carbide-carbon composites |
US20100044170A1 (en) | 2008-08-22 | 2010-02-25 | Simpson Allen H | Reactive sintering to eliminate metal inserts in carbon-carbon brake discs |
US8178212B2 (en) * | 2008-10-24 | 2012-05-15 | Honeywell International Inc. | Functionally graded high temperature bonding of fiberglass fibers to steel |
US8574470B2 (en) * | 2008-10-24 | 2013-11-05 | Honeywell International Inc. | Combustion synthesis to bond metal inserts to C-C composite surfaces |
CN103596905A (zh) * | 2011-05-27 | 2014-02-19 | 东洋炭素株式会社 | 金属材料与陶瓷-碳复合材料的接合体、其制造方法、碳材料接合体、碳材料接合体用接合材料和碳材料接合体的制造方法 |
CN112091219B (zh) * | 2019-06-17 | 2022-08-19 | 中国科学院宁波材料技术与工程研究所 | 一种石墨-钛复合材料及其制备方法和应用 |
US11125289B2 (en) | 2019-07-03 | 2021-09-21 | Honeywell International Inc. | Brake disc assembly |
US11384805B2 (en) | 2019-11-21 | 2022-07-12 | Honeywell International Inc. | Brake disc assembly |
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US5139594A (en) | 1990-06-26 | 1992-08-18 | The United States Of America As Represented By The United States Department Of Energy | Method for joining ceramic shapes |
US5340014A (en) | 1991-08-30 | 1994-08-23 | University Of Cincinnati | Combustible slurry for joining metallic or ceramic surfaces or for coating metallic, ceramic and refractory surfaces |
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US5972157A (en) * | 1995-11-20 | 1999-10-26 | Alliedsignal Inc. | Joining of rough carbon-carbon composites with high joint strength |
US6174605B1 (en) | 1996-08-20 | 2001-01-16 | Alliedsignal Inc. | Joining of rough carbon-carbon composites with high joint strength |
US7040525B2 (en) | 2002-03-20 | 2006-05-09 | Lg.Philips Lcd Co., Ltd. | Stage structure in bonding machine and method for controlling the same |
US6699427B2 (en) | 2002-07-26 | 2004-03-02 | Ucar Carbon Company Inc. | Manufacture of carbon/carbon composites by hot pressing |
JP3948377B2 (ja) | 2002-09-12 | 2007-07-25 | 株式会社豊田中央研究所 | 圧接型半導体装置 |
US6878331B2 (en) | 2002-12-03 | 2005-04-12 | Ucar Carbon Company Inc. | Manufacture of carbon composites by hot pressing |
EP1771669A2 (en) | 2004-01-21 | 2007-04-11 | Benmaxx, LLC | Disc brake rotor assembly and method for producing same |
-
2006
- 2006-03-29 US US11/391,255 patent/US7858187B2/en active Active
-
2007
- 2007-03-27 DE DE602007003819T patent/DE602007003819D1/de active Active
- 2007-03-27 EP EP07759470A patent/EP1999089B1/en not_active Expired - Fee Related
- 2007-03-27 WO PCT/US2007/065026 patent/WO2007115022A1/en active Application Filing
- 2007-03-27 RU RU2008142851/03A patent/RU2008142851A/ru not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
EP1999089A1 (en) | 2008-12-10 |
US7858187B2 (en) | 2010-12-28 |
US20070235126A1 (en) | 2007-10-11 |
DE602007003819D1 (de) | 2010-01-28 |
EP1999089B1 (en) | 2009-12-16 |
WO2007115022A1 (en) | 2007-10-11 |
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