Invention Grant
- Patent Title: Gas turbine engine inlet assembly and method of making same
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Application No.: US14036994Application Date: 2013-09-25
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Publication No.: US09784134B2Publication Date: 2017-10-10
- Inventor: Andreas Eleftheriou
- Applicant: Pratt & Whitney Canada Corp.
- Applicant Address: unknown Longueuil, Quebec
- Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee Address: unknown Longueuil, Quebec
- Agency: Norton Rose Fulbright Canada
- Main IPC: F04D29/44
- IPC: F04D29/44 ; F01D25/28 ; F02C7/04 ; F02C7/042

Abstract:
A method of fabricating an inlet assembly for a gas turbine engine, the method including defining an intake duct of the inlet assembly between first and second space apart inlet case portions, locating at least one strut across the intake duct, each strut having a proximal end made integral to the first inlet case portion and an opposed distal end engaged in a respective strut-receiving aperture defined through the second inlet case portion, while maintaining the distal end of each strut in the respective strut-receiving aperture, adjusting the relative position of the first inlet case portion and the second inlet case portion until a predetermined throat dimension of the intake duct is obtained, and locking the adjusted relative position by attaching the second inlet case portion to each strut. An inlet assembly and gas turbine engine with inlet assembly as also disclosed.
Public/Granted literature
- US20150086352A1 Gas Turbine Engine Inlet Assembly and Method of Making Same Public/Granted day:2015-03-26
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