Inventors:
James J. Taylor - Jensen Beach FL
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F02K 310
Abstract:
An augmentor liner 16 for a gas turbine engine is formed of thin perforated material and has pressurized cooling air surrounding it. A stiffner ring 42 is supporter from the liner with radially flexible straps 52, while relative radial displacement is limited by clips 50, 44. The liner is restrained from buckling while permitting thermal expansion.