Invention Grant
- Patent Title: Diffuser pipe with axially-directed exit
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Application No.: US16440213Application Date: 2019-06-13
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Publication No.: US11435079B2Publication Date: 2022-09-06
- Inventor: Hien Duong
- 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: Norton Rose Fulbright Canada
- Main IPC: F02C3/08
- IPC: F02C3/08 ; F01D9/02 ; F04D29/44 ; F04D29/54 ; F23R3/04 ; F01D17/14 ; F04D29/22

Abstract:
A compressor diffuser for a gas turbine engine includes diffuser pipes having a tubular body including a generally radial portion, a bend portion and a generally axial portion. The generally axial portion has an exit segment extending parallel to the center axis and terminating at a pipe outlet. The bend portion is disposed radially further from the center axis than the exit segment.
Information query
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