Recuperative impingement cooling of jet engine components

Power plants – Combustion products used as motive fluid – Combustion products generator

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165908, 415115, F02C 712

Patent

active

053636546

ABSTRACT:
Impingement cooling of a jet engine subassembly, such as a combustor. Adjacent raised corrugation portions and intervening plate portions (having impingement cooling holes) of a corrugated plate define coolant channels in fluid communication with the engine compressor. Dividers positioned transverse to the corrugation portions have a top side attached to a bottom surface of the plate portions and have a bottom side attached to the combustor liner. Corrugation portions define therewithin return channels in fluid communication with post-impingement cooling air. The dividers prevent crossflow between the impingement cooling air and the post-impingement cooling air.

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