CPC F02C 9/18 (2013.01) [F01D 9/02 (2013.01); F01D 25/12 (2013.01); F01D 25/24 (2013.01); F02C 7/18 (2013.01); F05D 2220/32 (2013.01)] | 18 Claims |
1. An assembly for a turbine engine, comprising:
a case structure extending circumferentially about and axially along an axis; and
an air conduit having a conduit centerline, a conduit first end and a conduit second end, the air conduit extending longitudinally along the conduit centerline between the conduit first end and the conduit second end, the conduit first end connected to the case structure at a first location, the conduit second end connected to the case structure at a second location, the air conduit displaced from the case structure longitudinally between the conduit first end and the conduit second end, and at least a majority of the conduit centerline following a non-straight trajectory;
wherein the case structure and the air conduit are formed together as a monolithic body.
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