Wall construction for a combustion chamber or a nozzle of a high performance propulsion plant
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United States of America Patent
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Mar 20, 2001
Grant Date -
N/A
app pub date -
Jan 19, 1999
filing date -
Jan 16, 1998
priority date (Note) -
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Abstract
A combustion chamber wall structure for a high performance propulsion plant or a wall structure for a nozzle of flying bodies has an outer pressure jacket and an inner wall member provided with a multitude of cooling channels. In operation the inner wall is in contact with hot gases. An intermediate layer made of a material having shape memory characteristics and/or superelastic characteristics is arranged between the inner wall member and the outer pressure jacket.
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