CPC F01D 25/24 (2013.01) [F01D 9/02 (2013.01); F02C 7/222 (2013.01); F23R 3/002 (2013.01); F05D 2220/32 (2013.01); F05D 2230/60 (2013.01); F05D 2240/12 (2013.01); F05D 2240/128 (2013.01); F05D 2240/14 (2013.01); F05D 2240/35 (2013.01)] | 16 Claims |
1. An assembly for a gas turbine engine, comprising:
a stationary engine structure including a diffuser, a combustor, an engine case and a plenum, the combustor disposed within the plenum, the engine case forming a peripheral boundary of the plenum, and a gas path extending sequentially through the diffuser, the plenum and the combustor;
a first section of the stationary engine structure formed as a first monolithic body, the first section including the diffuser and the combustor; and
a second section of the stationary structure formed as a second monolithic body, the second section comprising the engine case;
wherein the second section circumscribes the first section.
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