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. 26, 2014

Filed:

Sep. 07, 2011
Applicants:

Douglas C. Hofer, Niskayuna, NY (US);

Anthony Furman, Niskayuna, NY (US);

Thomas Lavertu, Niskayuna, NY (US);

Inventors:

Douglas C. Hofer, Niskayuna, NY (US);

Anthony Furman, Niskayuna, NY (US);

Thomas Lavertu, Niskayuna, NY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02B 33/44 (2006.01); F02B 41/10 (2006.01); F02B 37/00 (2006.01); F02B 37/013 (2006.01); F02B 37/18 (2006.01);
U.S. Cl.
CPC ...
F02B 37/005 (2013.01); F02B 37/013 (2013.01); F02B 37/004 (2013.01); F02B 41/10 (2013.01); F02B 37/18 (2013.01); Y02T 10/144 (2013.01); Y02T 10/163 (2013.01);
Abstract

Methods and systems are provided for operating a turbocharged engine. An engine system comprises a turbocharger, a bypass path, and a turbo-compound unit. The turbocharger may include a turbine mechanically coupled to a compressor. The turbo-compound unit may include a turbine mechanically coupled to a load, such as a generator. The turbo-compound unit may be coupled in a bypass path around the turbocharger turbine. In this manner, thermodynamic energy flowing through the bypass path may be harvested to increase the engine-operating efficiency. Further, gas flow through the bypass path may be adjusted to potentially improve the transient response of the turbocharger.


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