Invention Grant
- Patent Title: Reverse-flow gas turbine engine
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Application No.: US17077310Application Date: 2020-10-22
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Publication No.: US11408352B2Publication Date: 2022-08-09
- Inventor: Keith Morgan , Robert Peluso , Ghislain Plante , Eugene Gekht , Eric Durocher , Jean Dubreuil , Stephen Mah , Philippe Beauchesne-Martel
- 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 in fluid communication with an air inlet, the low pressure compressor section including a first plurality of variable guide vanes therein, and a low pressure turbine section drivingly engaged to the low pressure compressor section. A second spool has a high pressure compressor section in fluid communication with the low pressure compressor section to receive pressurized air therefrom, the high pressure compressor section including a second plurality of variable guide vanes at an entry thereof, and a high pressure turbine section drivingly engaged to the high pressure compressor section, the high pressure turbine section disposed upstream of the low pressure turbine section and in fluid communication therewith. An output drive shaft drivingly engages the low pressure turbine section and is adapted to drivingly engage a rotatable load of the gas turbine engine.
Public/Granted literature
- US20210270183A1 REVERSE-FLOW GAS TURBINE ENGINE Public/Granted day:2021-09-02
Information query
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