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:
Mar. 17, 2020

Filed:

Jan. 09, 2018
Applicant:

Perkins Engines Company Limited, Peterborough, GB;

Inventors:

Lorna Thomas, Wells, GB;

Prabhu Ramasamy, Peterborough, GB;

Kevin C. Earle, Peterborough, GB;

Steven A. Gahlings, Great Cambourne, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); F01D 25/20 (2006.01); F02C 7/06 (2006.01); F02C 7/28 (2006.01); F02C 9/20 (2006.01); F02C 6/12 (2006.01); F02B 37/007 (2006.01); F02B 37/12 (2006.01); F02B 39/14 (2006.01); F01D 25/16 (2006.01); F02B 37/00 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); F01D 25/16 (2013.01); F01D 25/20 (2013.01); F02B 37/004 (2013.01); F02B 37/007 (2013.01); F02B 37/12 (2013.01); F02B 39/14 (2013.01); F02C 6/12 (2013.01); F02C 7/06 (2013.01); F02C 7/28 (2013.01); F02C 9/20 (2013.01); F05D 2220/40 (2013.01); F05D 2240/40 (2013.01); F05D 2260/60 (2013.01); F05D 2260/98 (2013.01); F05D 2270/02 (2013.01); F05D 2270/024 (2013.01); F05D 2270/081 (2013.01); F05D 2270/304 (2013.01); F05D 2270/3015 (2013.01); F05D 2270/3062 (2013.01); Y02T 10/144 (2013.01);
Abstract

An assembly including a first turbocharger, the first turbocharger including a first turbine and a first compressor, the first turbine arranged in a turbine flowpath to be driven in rotation by an exhaust gas flowing at a variable flow rate through the turbine flowpath. The first compressor arranged in a compressor flowpath to be driven by the first turbine to urge an intake gas to flow through the compressor flowpath. The first turbine and first compressor being supported for rotation in bearings supplied via an oil flowpath at an oil pressure. The assembly further including a seal arranged between the oil flowpath and the compressor flowpath to resist leakage of the oil into the compressor flowpath and a flow control means configured to control a rotational speed of the first turbine and first compressor by controlling the flow of exhaust gas in the turbine flowpath.


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