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Matthew S Oakes, 471931 Matzen Ranch Cir, Petaluma, CA 94954

Matthew Oakes Phones & Addresses

1931 Matzen Ranch Cir, Petaluma, CA 94954    707-9818711   

5 Persimmon Ct, Petaluma, CA 94954    707-7627008   

2607 Nelson Ave, Redondo Beach, CA 90278   

Harbor City, CA   

Los Angeles, CA   

5 Persimmon Ct, Petaluma, CA 94954   

Ranks

Licence: Dist. of Columbia - Active Date: 2004

Mentions for Matthew S Oakes

Career records & work history

Lawyers & Attorneys

Matthew Oakes Photo 1

Matthew RO Oakes - Lawyer

Address:
Dept. of Justice
202-5142686 (Office)
Licenses:
Dist. of Columbia - Active 2004

License Records

Matthew Robert Oakes

Licenses:
License #: TJ-0000087 - Expired
Category: Electrical Examiners
Type: Journeyperson Electrician

Matthew Oakes resumes & CV records

Resumes

Matthew Oakes Photo 45

Engineering Manager At Honeywell

Location:
245 Railroad St, Woonsocket, RI 02895
Industry:
Automotive
Work:
Honeywell
Engineering Manager at Honeywell
Education:
California Polytechnic State University - San Luis Obispo 1995 - 2000
Bachelors, Bachelor of Science, Mechanical Engineering
Matthew Oakes Photo 46

Matthew Oakes

Location:
United States

Publications & IP owners

Us Patents

Variable Geometry Turbocharger With Guide Pins

US Patent:
2011011, May 12, 2011
Filed:
Nov 9, 2009
Appl. No.:
12/614618
Inventors:
Kolja Nikolic - Yorba Linda CA, US
Michael Moyer - Redondo Beach CA, US
George Adeff - Westchester CA, US
Kevin Slupski - Redondo Beach CA, US
Matthew Oakes - Redondo Beach CA, US
Dennis L. Brookshire - Novi MI, US
International Classification:
F01D 17/16
F02B 37/22
US Classification:
415163
Abstract:
A variable geometry turbocharger assembly comprises a unison ring which rotates about a longitudinal axis defined by a shaft on which a turbine wheel and compressor wheel are attached in order to pivot a plurality of vanes and thereby control a flow of exhaust gas to the turbine wheel. The unison ring rotates on at least one guide pin which is secured to the turbocharger. The guide pins may be press-fit into apertures in a center housing at an outer pilot surface. In other embodiments the guide pins may be press-fit into a different part of the turbocharger such as a nozzle ring. The guide pins may each have a wear surface which defines a circumferential radius of curvature which is substantially equal to a circumferential radius of curvature of a radially inner surface of the unison ring.

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