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.

Patent No.:

US 9046111 B1

PDF
Full Text
Expired
Date of Patent:
Jun. 02, 2015

Filed:

Feb. 18, 2011
Applicants:

Neil W. Harvey, Derby, GB;

John J. Bolger, Derby, GB;

Inventors:

Neil W. Harvey, Derby, GB;

John J. Bolger, Derby, GB;

Assignee:

ROLLS-ROYCE PLC, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F04D 29/32 (2006.01); F04D 29/66 (2006.01); F04D 29/54 (2006.01); F04D 29/68 (2006.01);
U.S. Cl.
CPC ...
F04D 29/324 (2013.01); F01D 5/141 (2013.01); F04D 29/666 (2013.01); F04D 29/544 (2013.01); F04D 29/681 (2013.01);
Abstract

An aerofoil for a compressor comprising a suction surface and a pressure surface with a thickness distribution defined therebetween, the aerofoil further comprising a first local maximum in the thickness distribution and a second local maximum in the thickness distribution, the second local maximum being downstream of the first local maximum and the second local maxima being formed by a first region of concave curvature in the suction surface between the first and second local maxima, wherein the second local maximum is disposed such that in use a boundary layer upstream of the second local maximum on the suction surface is thinned by the second local maximum, and in addition the boundary layer may be sufficiently thinned so that an interaction of an upstream flow feature with the thinned boundary layer is capable of generating a turbulent spot with a calmed region downstream of the turbulent spot.


Find Patent Forward Citations

Harvey, Neil. (2015). Compressor aerofoil (U.S. Patent No. 9046111). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9046111

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