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:
Jun. 28, 2016

Filed:

Mar. 29, 2013
Applicant:

Honeywell International Inc., Morristown, NJ (US);

Inventors:

Mark Matwey, Phoenix, AZ (US);

Mahmoud Mansour, Phoenix, AZ (US);

Yogendra Y. Sheoran, Scottsdale, AZ (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Morris Plains, NJ (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/42 (2006.01); F04D 29/68 (2006.01); F04D 27/02 (2006.01); F04D 29/44 (2006.01);
U.S. Cl.
CPC ...
F04D 29/4213 (2013.01); F04D 27/0207 (2013.01); F04D 29/441 (2013.01); F04D 29/444 (2013.01); F04D 29/682 (2013.01); F05D 2250/51 (2013.01);
Abstract

Embodiments of a turbomachine, such as a gas turbine engine, are provided. In one embodiment, the turbomachine includes an impeller, a main intake plenum in fluid communication with the inlet of the impeller, and an impeller shroud recirculation system. The impeller shroud recirculation system includes an impeller shroud extending around at least a portion of the impeller and having a shroud port therein. A shroud port cover circumscribes at least a portion of the shroud port and cooperates therewith to at least partially define an impeller recirculation flow path. The impeller recirculation flow path has an outlet positioned to discharge airflow into the main intake plenum at a location radially outboard of the shroud port when pressurized air flows from the impeller, through the shroud port, and into the impeller recirculation flow path during operation of the turbomachine.


Find Patent Forward Citations

Loading…