Pratt & Whitney
Design Engineer
Piper Aircraft Mar 2011 - Nov 2011
Ecs Lead
Piper Aircraft Jun 2010 - Nov 2011
Mechanical Systems Design Engineer
United States Department of Defense May 2009 - May 2010
Intern - Responsible Engineer
Education:
Worcester Polytechnic Institute 2014 - 2017
Master of Science, Masters, Engineering
Florida Institute of Technology 2006 - 2010
Bachelors, Bachelor of Science, Aerospace Engineering
Skills:
Unigraphics Aerospace Engineering Aerospace Engineering Aircraft Design Cad Testing Aerodynamics Matlab Aircraft Finite Element Analysis Pro Engineer Fortran Manufacturing Office 2010 Heat Transfer Labview Wildfire Pro Engineer Microsoft Office 2010
2011 to 2000 Environmental Control System (ECS) LeadPiper Aircraft Vero Beach, FL May 2010 to 2011 Mechanical Systems Design EngineerUnited States Air Force Cape Canaveral, FL 2009 to 2010 InternFlorida Tech Melbourne, FL 2009 to 2010 Florida Institute of Technology Senior Design Project
Education:
Florida Institute of Technology Melbourne, FL Jan 2006 to Jan 2010 BS in Aerospace Engineering
- Hartford CT, US Michelle Diana Stearns - Lebanon CT, US Michael Luther Comeau - Manchester CT, US James P. Chasse - Wethersfield CT, US
International Classification:
F02C 7/12 F02C 3/04
Abstract:
A cooling fluid system for a gas turbine engine includes a fluid source. A turbine section includes first and second components. A fluid supply system has a primary pipe that is configured to provide a cooling supply fluid from the fluid source to a fluid fitting having a fluid junction. The fluid junction is in fluid communication with and is configured to supply a first cooling fluid to the first component. The fluid junction is in fluid communication with and is configured to supply a second cooling fluid to the second component. A flow meter is upstream from the fluid junction and is configured to receive the cooling supply fluid.
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