公开(公告)号：US20160069210A1

公开(公告)日：2016-03-10

申请号：US14787320

申请日：2014-05-30

Applicant: United Technologies Corporation

Inventor： Philip Robert Rioux ,  Nicholas R. Leslie ,  Neil L. Tatman

IPC: F01D25/14 ,  F01D17/10 ,  F04D19/00 ,  F01D25/24

CPC classification number: F01D25/145 ,  F01D17/105 ,  F01D25/24 ,  F02C6/08 ,  F02C7/24 ,  F04D19/002 ,  F05D2220/32 ,  F05D2250/36 ,  F05D2260/231

Abstract: 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.

Abstract translation: 隔热罩包括构造成在内部连接点处连接到内部发动机壳体的第一端和构造成在外部连接点处连接到外部发动机壳体的第二端。 隔热罩还包括从径向上游部分沿向后方向延伸的凸起。 还公开了一种包括隔热罩的压缩机部分和燃气涡轮发动机。

公开(公告)号：US20140366613A1

公开(公告)日：2014-12-18

申请号：US14107771

申请日：2013-12-16

Applicant: United Technologies Corporation

Inventor： Eli Cole Warren ,  Nicholas R. Leslie

IPC: F01D25/24 ,  G01M15/14 ,  F16B5/06

CPC classification number: G01M15/14 ,  F01D11/20 ,  F01D17/02 ,  F01D21/003 ,  F01D25/24 ,  F01D25/285 ,  F05D2220/32 ,  Y10T29/4932 ,  Y10T403/3993

Abstract: A probe assembly for a gas turbine engine is disclosed. The probe assembly may include a probe, and a fastener to retain the probe within a case of the gas turbine engine, the fastener including a sealing arrangement with a heat shield of the gas turbine engine.

Abstract translation: 公开了一种用于燃气涡轮发动机的探针组件。 探针组件可以包括探针和将探针保持在燃气涡轮发动机的壳体内的紧固件，该紧固件包括具有燃气涡轮发动机的隔热罩的密封装置。