公开(公告)号：US12092025B2

公开(公告)日：2024-09-17

申请号：US17837102

申请日：2022-06-10

Applicant: Unison Industries, LLC

Inventor： John P. Parsons

IPC: F01D17/02 ,  F02C7/00 ,  G01K1/08 ,  G01K13/024

CPC classification number: F02C7/00 ,  F01D17/02 ,  G01K1/08 ,  G01K13/024 ,  F05D2220/32 ,  F05D2260/80

Abstract: A gas turbine engine can include a compressor section, a combustion section, and a turbine section in serial flow arrangement. At least one of the combustion section or turbine section can have an exhaust gas passage. The turbine engine can also include an exhaust gas temperature sensor with a housing having an elongated probe portion. The elongated probe portion can have an outer wall bounding an interior. A temperature probe can be provided within the housing.

公开(公告)号：US20230193821A1

公开(公告)日：2023-06-22

申请号：US17837102

申请日：2022-06-10

Applicant: Unison Industries, LLC

Inventor： John P. Parsons

IPC: F02C7/00 ,  F01D17/02 ,  G01K13/024 ,  G01K1/08

CPC classification number: F02C7/00 ,  F01D17/02 ,  G01K13/024 ,  G01K1/08 ,  F05D2220/32 ,  F05D2260/80

Abstract: A gas turbine engine can include a compressor section, a combustion section, and a turbine section in serial flow arrangement. At least one of the combustion section or turbine section can have an exhaust gas passage. The turbine engine can also include an exhaust gas temperature sensor with a housing having an elongated probe portion. The elongated probe portion can have an outer wall bounding an interior. A temperature probe can be provided within the housing.