The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Aug. 09, 2016

Filed:

Sep. 13, 2012
Applicant:

Ian Alexander Macfarlane, St. Bruno, CA;

Inventor:

Ian Alexander Macfarlane, St. Bruno, CA;

Assignee:

PRATT & WHITNEY CANADA CORP., Longueuil, Quebec, unknown;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/20 (2006.01); F01D 11/08 (2006.01); F01D 25/24 (2006.01); F02C 6/20 (2006.01);
U.S. Cl.
CPC ...
F01D 11/08 (2013.01); F01D 25/246 (2013.01); F02C 6/206 (2013.01); F05D 2230/642 (2013.01); F05D 2250/411 (2013.01); Y10T 29/49236 (2015.01);
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.


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