A heat shield includes a first end configured to connect to an inner engine case at an inner connecting point, and a second end configured to connect to an outer engine case at an outer connecting point. The heat shield also includes a bulge extending in an aft direction from a radially upstream portion. A compressor section and a gas turbine engine including the heat shield are also disclosed.
申请公布号
WO2014204629(A1)
申请公布日期
2014.12.24
申请号
WO2014US40116
申请日期
2014.05.30
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
RIOUX, PHILIP ROBERT;LESLIE, NICHOLAS R.;TATMAN, NEIL L.