COMPRESSOR CASE SNAP ASSEMBLY

摘要

A turbine engine case spacer includes an air seal and a flange. The air seal is snap fit to the flange, and each flange includes at least two distinct material layers.

主权项

1. A turbine engine comprising:
a compressor section including a compressor case; a combustor in fluid communication with the compressor section; a turbine section including a turbine case, said turbine section in fluid communication with the combustor; wherein at least one of said compressor case and said turbine case includes a plurality of case spacers, each of said case spacers having at least one flange; at least one air seal, wherein each of said flanges is separated from an adjacent component by one of said at least one air seals; wherein said at least one seal is snap fit to said flange; and wherein at least one of said flanges includes at least two distinct material layers.