发明名称 |
Düsenerweiterung für ein Triebwerk und Verfahren zur Herstellung und Kühlung einer Düsenerweiterung |
摘要 |
<p>The extension (10) has a nozzle cover (18) limiting a flow cross-section (24), which is extended from a nozzle extension inlet (14) to a nozzle extension outlet (16). The nozzle extension inlet is connected with a combustion chamber outlet of a combustion chamber of an engine. The nozzle cover comprises two shell elements (26, 28) made of a ceramic fiber reinforced composite material, where the shell elements are fixed relative to each other. The shell element (26) limits an interior space (22), and the composite material is carbon/silicon carbide material. An independent claim is also included for a method for producing a nozzle extension for an engine.</p> |
申请公布号 |
DE102008020198(B8) |
申请公布日期 |
2015.05.13 |
申请号 |
DE20081020198 |
申请日期 |
2008.04.15 |
申请人 |
ASTRIUM GMBH;DEUTSCHES ZENTRUM FÜR LUFT- UND RAUMFAHRT E.V. |
发明人 |
ORTELT, MARKUS;HEIDENREICH, BERNHARD;BEYER, STEFFEN;GREUEL, DIRK;HALD, HERMANN;STARK, RALF |
分类号 |
F02K1/82 |
主分类号 |
F02K1/82 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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