US 11,852,031 B2
Conduit bracket for a gas turbine engine
Mateusz Pelc, Rzeszow (PL); and Julien Girard, Saint-Julie (CA)
Assigned to Pratt & Whitney Canada Corp., Longueuil (CA)
Filed by Pratt & Whitney Canada Corp., Longueuil (CA)
Filed on Aug. 3, 2021, as Appl. No. 17/392,710.
Prior Publication US 2023/0043298 A1, Feb. 9, 2023
Int. Cl. F01D 25/28 (2006.01)
CPC F01D 25/28 (2013.01) 13 Claims
OG exemplary drawing
 
1. An assembly for a turbine engine, comprising:
a static structure of the turbine engine comprising a port;
a conduit extending longitudinally through the port; and
a bracket coupling the conduit to the static structure, the bracket comprising:
a first base mount attached to the static structure;
a second base mount attached to the static structure;
a conduit mount mechanically coupled with the conduit;
a first damper between the first base mount and the conduit mount; and
a second damper between the second base mount and the conduit mount;
wherein the first damper includes a lateral leg and a longitudinal leg;
wherein the lateral leg extends laterally between and is connected to the first base mount and the longitudinal leg;
wherein the longitudinal leg extends longitudinally between and is connected to the lateral leg and the conduit mount;
wherein the lateral leg includes a first segment and a second segment;
wherein the first segment is connected between the first base mount and the second segment;
wherein the first segment is angularly offset from the first base mount by a first obtuse angle; and
wherein the second segment is angularly offset from the first segment by a second obtuse angle.