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:
Sep. 15, 2020

Filed:

Apr. 29, 2016
Applicant:

Concepts Nrec, Llc, White River Junction, VT (US);

Inventor:

David Japikse, Woolwich, ME (US);

Assignee:

Concepts NREC, LLC, White River Junction, VT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/44 (2006.01); F04D 29/42 (2006.01); F02C 6/12 (2006.01); F04D 17/10 (2006.01); F04D 29/46 (2006.01);
U.S. Cl.
CPC ...
F04D 29/444 (2013.01); F02C 6/12 (2013.01); F04D 17/10 (2013.01); F04D 29/4206 (2013.01); F04D 29/462 (2013.01); F05D 2250/52 (2013.01); F05D 2260/961 (2013.01);
Abstract

Turbomachines having one or more flow guiding features designed to increase the performance of the turbomachine (). In some examples, flow guiding features are designed and configured to bias a circumferential pressure distribution at a diffuser inlet () toward circumferential uniformity, otherwise account for such low-frequency spatial pressure variations, increase the controllability of spatial flow field variations, or modifying flow field variations, etc. In some examples, a diffuser () having a row () of vanes () that include a plurality of first vanes () and at least one second vane (A,B,A,B,) having a different characteristic than the first vanes () are disclosed. In some examples, diffusers () having an aperiodic section () including one or more biased passages (A,A,B,A,A,) for biasing a flow field are disclosed. And in some examples, turbomachines having flowwise elongate recesses () in one or both of a hub () and shroud () surface are disclosed.


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