Invention Grant
- Patent Title: Turboprop engine with compressor turbine shroud
- Patent Title (中): 涡轮螺旋桨发动机带压缩机涡轮罩
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Application No.: US13613904Application Date: 2012-09-13
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Publication No.: US09410441B2Publication Date: 2016-08-09
- Inventor: Ian Alexander Macfarlane
- Applicant: Ian Alexander Macfarlane
- 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: F02C7/20
- IPC: F02C7/20 ; F01D11/08 ; F01D25/24 ; F02C6/20

Abstract:
A turboprop engine including an annular outer case including a mount ring for attachment to an aircraft along a plane to transfer loads from a propeller and having an annular flange extending radially inwardly therefrom within the plane, an annular turbine support case received within the outer case and connected to the outer case only through a direct connection with the annular flange allowing a limited relative pivoting motion between the turbine support case and the mount ring, and a turbine section including a rotor closely surrounded by a shroud with an annular tip clearance being defined therebetween, the shroud being directly connected to and located by the turbine support case. A method of isolating a turbine shroud from propeller loads in a propeller engine is also disclosed.
Public/Granted literature
- US20140069107A1 TURBOPROP ENGINE WITH COMPRESSOR TURBINE SHROUD Public/Granted day:2014-03-13
Information query
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