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:
Apr. 12, 2016

Filed:

Jul. 06, 2012
Applicants:

William Byron Roberts, Ii, Wellington, NV (US);

Shawn P. Lawlor, Bellevue, WA (US);

Robert E. Breidenthal, Seattle, WA (US);

Inventors:

William Byron Roberts, II, Wellington, NV (US);

Shawn P. Lawlor, Bellevue, WA (US);

Robert E. Breidenthal, Seattle, WA (US);

Assignee:

Dresser-Rand Company, Olean, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 21/00 (2006.01); F04D 27/02 (2006.01); F04D 29/56 (2006.01); F04D 29/68 (2006.01); F04D 29/54 (2006.01);
U.S. Cl.
CPC ...
F04D 21/00 (2013.01); F04D 27/0207 (2013.01); F04D 27/0215 (2013.01); F04D 29/547 (2013.01); F04D 29/563 (2013.01); F04D 29/682 (2013.01); Y02E 10/721 (2013.01); Y10T 137/85938 (2015.04);
Abstract

A supersonic compressor including a rotor to deliver a gas at supersonic conditions to a diffuser. The diffuser includes a plurality of aerodynamic ducts that have converging and diverging portions, for deceleration of gas to subsonic conditions and then for expansion of subsonic gas, to change kinetic energy of the gas to static pressure. The aerodynamic ducts include vortex generating structures for controlling boundary layer, and structures for changing the effective contraction ratio to enable starting even when the aerodynamic ducts are designed for high pressure ratios, and structures for boundary layer control. In an embodiment, aerodynamic ducts are provided having an aspect ratio of in excess of two to one, when viewed in cross-section orthogonal to flow direction at an entrance to the aerodynamic duct.


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