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:
May. 10, 2016

Filed:

Jul. 13, 2011
Applicant:

Thomas Povey, Oxford, GB;

Inventor:

Thomas Povey, Oxford, GB;

Assignee:

ISIS INNOVATION LTD, Summertown, Oxford, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/02 (2006.01); F01D 5/14 (2006.01); F01D 9/04 (2006.01);
U.S. Cl.
CPC ...
F01D 9/02 (2013.01); F01D 5/143 (2013.01); F01D 5/145 (2013.01); F01D 9/023 (2013.01); F01D 9/041 (2013.01); F05D 2220/321 (2013.01); F05D 2240/12 (2013.01); F05D 2250/71 (2013.01); F05D 2250/713 (2013.01); Y02T 50/673 (2013.01); Y02T 50/675 (2013.01);
Abstract

A vane assembly () for an axial flow turbine engine provides a plurality of nozzles () arranged symmetrically around a turbine axis formed by an inner hub (), an outer casing () and vanes () intermediate pairs of adjacent nozzles. The nozzles have a cross-section normal to the turbine axis that changes smoothly with the position of the cross-section along the turbine axis from a first shape having a minimum radius of curvature of a first value that is no less than a limit L, providing the cross-section with no highly curved corners, to a second shape having a minimum radius of curvature of a second value less than the first value, providing corners. This allows the secondary flow structure to be designed to improve aerodynamic loss and cooling performance.


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