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Cody Renshaw Phones & Addresses

  • 1609 Kensington Dr, Washington, IL 61571
  • Peoria, IL
  • Springfield, IL

Work

Company: Caterpillar inc. Mar 2020 Position: Hydraulics strategy and commercial manager

Education

Degree: Master of Business Administration, Masters School / High School: Bradley University 2007 to 2009 Specialities: Business Administration, Management, Business Administration and Management, International Business

Skills

Engineering • Lean Manufacturing • Six Sigma • Continuous Improvement • Dmaic • Product Development • Fmea • Manufacturing • Process Improvement • Value Stream Mapping • Project Management • Management • Black Belt • Product Management • Powertrain • Kaizen • Start Ups • Engineering Management • Supply Chain Management • Business Process Improvement • Strategy • Toyota Production System • Manufacturing Engineering • Root Cause Analysis • Leadership • Vision Development • Failure Mode and Effects Analysis • Cross Functional Team Leadership

Languages

English • Mandarin

Industries

Machinery

Resumes

Resumes

Cody Renshaw Photo 1

Hydraulics Strategy And Commercial Manager

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Location:
1776 Kingsbury Rd, Washington, IL 61571
Industry:
Machinery
Work:
Caterpillar Inc.
Hydraulics Strategy and Commercial Manager
Education:
Bradley University 2007 - 2009
Master of Business Administration, Masters, Business Administration, Management, Business Administration and Management, International Business
University of Illinois at Urbana - Champaign 1997 - 2001
Bachelors, Bachelor of Science, Mechanical Engineering
Skills:
Engineering
Lean Manufacturing
Six Sigma
Continuous Improvement
Dmaic
Product Development
Fmea
Manufacturing
Process Improvement
Value Stream Mapping
Project Management
Management
Black Belt
Product Management
Powertrain
Kaizen
Start Ups
Engineering Management
Supply Chain Management
Business Process Improvement
Strategy
Toyota Production System
Manufacturing Engineering
Root Cause Analysis
Leadership
Vision Development
Failure Mode and Effects Analysis
Cross Functional Team Leadership
Languages:
English
Mandarin

Publications

Us Patents

Retarding And Filter Cleaning Method And System

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US Patent:
20070119146, May 31, 2007
Filed:
Nov 30, 2005
Appl. No.:
11/289321
Inventors:
James Callas - Peoria IL, US
Kevin Martin - Washburn IL, US
Cody Renshaw - Peoria IL, US
Thomas Sopko - East Peoria IL, US
Andrew Tonsor - East Peoria IL, US
International Classification:
F02C 7/052
US Classification:
060039092
Abstract:
A filter cleaning system is provided for a gas turbine engine including a compressor section and a combustor section. A mechanism is operatively connected to the gas turbine engine and is configured to be driven by the gas turbine engine in a first mode and configured to drive the gas turbine engine in a second mode. A first flow path is for delivering compressed air to the compressor section. At least one air filter is configured to filter air entering the first flow path. A second flow path is for delivering compressed air from the compressor section to the combustor section in the first mode. A third flow path is for delivering compressed air from the compressor section to the at least one air filter during the second mode.

Multiple Turbine System With A Single Recuperator

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US Patent:
20070137211, Jun 21, 2007
Filed:
Dec 19, 2005
Appl. No.:
11/305112
Inventors:
James Callas - Peoria IL, US
Kevin Martin - Washburn IL, US
Cody Renshaw - Peoria IL, US
Thomas Sopko - East Peoria IL, US
Andrew Tonsor - East Peoria IL, US
International Classification:
F02C 7/10
US Classification:
060772000, 060039511
Abstract:
A turbine system is provided including a plurality of gas turbine engines, each having a compressor section for producing compressed air, a combustor section, and a turbine section yielding hot exhaust gas. A single, common recuperator section is shared by and operatively associated with the plurality of gas turbine engines. A first flow path within the single, common recuperator section is configured to receive compressed air produced by the compressor section of each gas turbine engine. A second flow path, separated from the first flow path and within the single, common recuperator section is configured to receive hot exhaust gases yielded by the turbine section of each gas turbine engine.

Power System

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US Patent:
20070175201, Aug 2, 2007
Filed:
Jan 31, 2006
Appl. No.:
11/342618
Inventors:
James Callas - Peoria IL, US
Cody Renshaw - Peoria IL, US
Brian Howson - Peoria IL, US
Kevin Martin - Washbum IL, US
International Classification:
F02C 3/14
US Classification:
060039350
Abstract:
A power system includes a rotary compressor. The power system may also include one or more power sources drivingly connected to the rotary compressor, the one or more power sources not including a turbine. Additionally, the power system may include a turbine, the turbine being free to rotate independently of the rotary compressor. The power system may also include power-system controls operable to cause the rotary compressor to generate a gas flow by causing the one or more power sources to rotate the rotary compressor. Additionally, the power system may be operable to direct at least a portion of the gas flow generated by the rotary compressor through the turbine to rotate the turbine.
Cody P Renshaw from Washington, IL, age ~46 Get Report