Invention Grant
- Patent Title: Reverse-flow gas turbine engine
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Application No.: US15266321Application Date: 2016-09-15
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Publication No.: US11415063B2Publication Date: 2022-08-16
- Inventor: Keith Morgan , Robert Peluso , Ghislain Plante , Eugene Gekht , Eric Durocher , Jean Dubreuil
- Applicant: PRATT & WHITNEY CANADA CORP.
- Applicant Address: CA Longueuil
- Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee Address: CA Longueuil
- Agency: Getz Balich LLC
- Main IPC: F02C7/32
- IPC: F02C7/32 ; F02C3/14 ; F02C6/20 ; F02C3/04 ; F02C3/067 ; F02C3/113 ; F02C7/36 ; F01D1/26 ; F04D25/02

Abstract:
A gas turbine engine has a first spool having a low pressure compressor section disposed forward of an air inlet along a direction of travel of the engine, and a low pressure turbine section disposed forward of the low pressure compressor section and drivingly engaged thereto. A second spool has a high pressure compressor section disposed forward of the low pressure compressor section, and a high pressure turbine section disposed forward of the high pressure compressor section and drivingly engaged thereto. The high pressure turbine section is disposed aft of the low pressure turbine section. An output drive shaft drivingly engages the low pressure turbine section and extends forwardly therefrom to drive a rotatable load. A method of operating a gas turbine engine is also discussed.
Public/Granted literature
- US20180073428A1 REVERSE-FLOW GAS TURBINE ENGINE Public/Granted day:2018-03-15
Information query
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