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. 01, 2015

Filed:

Mar. 15, 2013
Applicant:

GM Global Technology Operations Llc, Detroit, MI (US);

Inventor:

Robert D. Straub, Lowell, MI (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02B 25/00 (2006.01); F02B 33/00 (2006.01); F02B 25/14 (2006.01); F02B 33/44 (2006.01); F01N 13/10 (2010.01); F02B 37/18 (2006.01); F02B 25/02 (2006.01); F02B 75/02 (2006.01);
U.S. Cl.
CPC ...
F01N 13/107 (2013.01); F02B 25/02 (2013.01); F02B 33/44 (2013.01); F02B 37/18 (2013.01); F01N 2240/36 (2013.01); F01N 2260/06 (2013.01); F01N 2260/08 (2013.01); F02B 25/14 (2013.01); F02B 2075/025 (2013.01); Y02T 10/144 (2013.01);
Abstract

A porting system for a turbo-charged loop scavenged two-stroke engine includes a cylinder including a cylinder wall and a cylinder head. At least one inlet port is provided in the cylinder wall. The at least one inlet port is arranged a first distance from the cylinder head and fluidically connected to a compressor portion of a turbo-charger. A first exhaust port is provided in the cylinder wall. The first exhaust port is arranged a second distance from the cylinder head and is fluidically connected to a turbine portion of the turbo-charger through first exhaust passage. A second exhaust port is provided in the cylinder wall. The second exhaust port is arranged a third distance from the cylinder head that is greater than the second distance and the second exhaust passage is fluidically connected to a second exhaust passage bypassing the turbine portion.


Find Patent Forward Citations

Loading…