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. 04, 2015

Filed:

Jun. 25, 2009
Applicants:

Douglas Carl Hofer, Clifton Park, NY (US);

Zachary William Nagel, Ballston Lake, NY (US);

David Graham Holmes, Schenectady, NY (US);

Inventors:

Douglas Carl Hofer, Clifton Park, NY (US);

Zachary William Nagel, Ballston Lake, NY (US);

David Graham Holmes, Schenectady, NY (US);

Assignee:

General Electric Company, Niskayuna, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 21/00 (2006.01); F04D 17/12 (2006.01); F04D 29/44 (2006.01); F04D 29/28 (2006.01);
U.S. Cl.
CPC ...
F04D 21/00 (2013.01); F04D 17/127 (2013.01); F04D 29/284 (2013.01); F04D 29/44 (2013.01);
Abstract

The present invention provides novel supersonic compressors comprising novel supersonic compressor rotors. The supersonic compressor rotors are designed to operate at very high rotational speed wherein the velocity of the gas entering the supersonic compressor rotor is greater than the local speed of sound in the gas, hence the descriptor 'supersonic'. The new supersonic compressors comprise at least one supersonic compressor rotor defining an inner cylindrical cavity and an outer rotor rim and at least one radial flow channel allowing fluid communication between the inner cylindrical cavity and the outer rotor rim, said radial flow channel comprising a supersonic compression ramp. The novel supersonic compressor rotors are expected to enhance the performance of supersonic compressors comprising them, and to provide for greater design versatility in systems comprising such novel supersonic compressors.


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