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. 22, 2015

Filed:

May. 30, 2012
Applicant:

Christian Maier, Arbon, CH;

Inventor:

Christian Maier, Arbon, CH;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02B 33/44 (2006.01); F02M 25/07 (2006.01); F02B 37/00 (2006.01); F02B 37/013 (2006.01); F02B 37/10 (2006.01); F02B 37/14 (2006.01); F02B 37/16 (2006.01); F02B 39/10 (2006.01); F02B 41/10 (2006.01); F02D 28/00 (2006.01);
U.S. Cl.
CPC ...
F02M 25/0704 (2013.01); F02B 37/004 (2013.01); F02B 37/013 (2013.01); F02B 37/10 (2013.01); F02B 37/14 (2013.01); F02B 37/16 (2013.01); F02B 39/10 (2013.01); F02B 41/10 (2013.01); F02D 28/00 (2013.01); Y02T 10/144 (2013.01); Y02T 10/163 (2013.01);
Abstract

The present invention is relative to a control method of a turbo-compound engine apparatus wherein said apparatus comprises a low pressure compressor connected to the high pressure turbine and a low pressure turbine connected to a high pressure compressor by means of a coupling unit. The apparatus also comprises first bypassing means of said high pressure compressor. The method according to the invention comprises the step of deactivating said first bypassing means when at least a specific condition occurs.


Find Patent Forward Citations

Loading…