US 11,732,656 B2
Turbine engine with soaring air conduit
Lawrence A. Binek, Glastonbury, CT (US); and Matthew E. Lynch, Canton, CT (US)
Assigned to Raytheon Technologies Corporation, Farmington, CT (US)
Filed by Raytheon Technologies Corporation, Farmington, CT (US)
Filed on Mar. 31, 2021, as Appl. No. 17/219,207.
Prior Publication US 2022/0316408 A1, Oct. 6, 2022
Int. Cl. F01D 9/02 (2006.01); F02C 9/18 (2006.01); F01D 25/12 (2006.01); F01D 25/24 (2006.01); F02C 7/18 (2006.01)
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
OG exemplary drawing
 
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.