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Chad Stay Phones & Addresses

  • 8126 France Ave, Brooklyn Park, MN 55443 (763) 503-9851
  • 278 84Th St, Brooklyn Park, MN 55444 (763) 503-9851
  • 2708 84Th St, Brooklyn Center, MN 55444 (763) 503-9851
  • 6925 Humboldt Ave, Brooklyn Center, MN 55430 (763) 503-9851
  • Minneapolis, MN

Work

Company: Honeywell aerospace Jan 2013 Address: Coon Rapids, MN Position: Product line manager

Education

Degree: MBA School / High School: Keller Graduate School of Management of DeVry University 2008 to 2010

Skills

Aerospace • Six Sigma • Continuous Improvement • Avionics • Program Management • Aviation • Cross Functional Team Leadership • Design For Manufacturing • Engineering • Fmea • Engineering Management • Quality Management • Root Cause Analysis • Systems Engineering • Process Improvement • Green Belt

Industries

Aviation & Aerospace

Resumes

Resumes

Chad Stay Photo 1

Program Manager

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Location:
Minneapolis, MN
Industry:
Aviation & Aerospace
Work:
Honeywell Aerospace - Coon Rapids, MN since Jan 2013
Product Line Manager

UTC Aerospace Systems Aug 2012 - Dec 2012
Program Manager

Goodrich Sep 2010 - Aug 2012
Program Manager

Goodrich May 2011 - Nov 2011
Engineering Manager

Goodrich Apr 2006 - Aug 2010
Senior Design Engineer
Education:
Keller Graduate School of Management of DeVry University 2008 - 2010
MBA
University of Minnesota-Twin Cities 1994 - 1999
Bachelor of Science (BS), Mechanical Engineering
Skills:
Aerospace
Six Sigma
Continuous Improvement
Avionics
Program Management
Aviation
Cross Functional Team Leadership
Design For Manufacturing
Engineering
Fmea
Engineering Management
Quality Management
Root Cause Analysis
Systems Engineering
Process Improvement
Green Belt

Publications

Us Patents

Methods And Apparatus For Discrete Mirror Processing

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US Patent:
20070105483, May 10, 2007
Filed:
Nov 4, 2005
Appl. No.:
11/266984
Inventors:
David Nguyen - Savage MN, US
Chad Stay - Brooklyn Park MN, US
International Classification:
B24B 49/00
B24B 1/00
US Classification:
451008000, 451041000
Abstract:
A method is described for the processing of substrates for utilization as discrete mirrors. The method includes temporarily mounting a first end of at least one substrate onto a grinding machine plate, engaging a second end of the at least one substrate with a grinding wheel, rotating the plate and grinding wheel in opposite directions, and moving the grinding wheel and the plate toward one another at a rate.

Fill Tube-Flange Assembly For Ring Laser Gyroscope Block

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US Patent:
20080012325, Jan 17, 2008
Filed:
Sep 21, 2005
Appl. No.:
11/232350
Inventors:
Chad P. Stay - Brooklyn Park MN, US
Mark Jay Jarrett - Lake Elmo MN, US
International Classification:
F16L 19/00
US Classification:
285354
Abstract:
A fill tube and flange assembly for fabrication of ring laser gyroscope blocks is described. The assembly includes a flange assembly, a fill tube assembly, and a compression interface. The flange assembly includes a flange tube and a fluid port at a first end of the flange assembly tube. The fill tube assembly includes a fill tube and a laser block engaging portion at a first end of the fill tube. The compression interface is configured to couple second ends of the fill tube and the flange assembly tube.

Blade Tip Clearance Measurement Sensor And Method For Gas Turbine Engines

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US Patent:
20100079136, Apr 1, 2010
Filed:
Sep 29, 2008
Appl. No.:
12/286262
Inventors:
Richard W. Phillips - Eagan MN, US
Chad P. Stay - Brooklyn Park MN, US
Assignee:
ROSEMOUNT AEROSPACE INC. - Burnsville MN
International Classification:
G01B 7/00
US Classification:
32420716
Abstract:
An electromagnetic field sensor assembly for blade tip clearance measurement in a gas turbine engine is disclosed that includes a ceramic sensor body, a multi-layered wire coil wound about a distal end portion of the sensor body for producing an electromagnetic field, a ceramic well enclosing the sensor body and the coil, and a metallic housing surrounding the well and having an open distal end.

Blade Tip Clearance Measurement Sensor And Method For Gas Turbine Engines

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US Patent:
20120019237, Jan 26, 2012
Filed:
Aug 2, 2011
Appl. No.:
13/196260
Inventors:
Richard W. Phillips - Eagan MN, US
Chad P. Stay - Brooklyn Park MN, US
Martin Harrison - Northants, GB
Peter Wherritt - Oxford, GB
International Classification:
G01R 33/12
US Classification:
324239
Abstract:
An electromagnetic field sensor assembly for blade tip clearance measurement in a gas turbine engine is disclosed that includes a ceramic sensor body, a multi-layered wire coil wound about a distal end portion of the sensor body for producing an electromagnetic field, a ceramic well enclosing the sensor body and the coil, and a metallic housing surrounding the well and having an open distal end.

Blade Tip Clearance Measurement Sensor For Gas Turbine Engines

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US Patent:
20120032689, Feb 9, 2012
Filed:
Aug 26, 2011
Appl. No.:
13/199375
Inventors:
Richard W. Phillips - Eagan MN, US
Chad Phillip Stay - Brooklyn Park MN, US
Martin Harrison - Northants, GB
Peter Wherritt - Oxford, GB
International Classification:
G01R 27/04
US Classification:
324629
Abstract:
An electromagnetic field sensor assembly for blade tip clearance measurement in a gas turbine engine is disclosed that includes a ceramic sensor body, a multi-layered wire coil wound about a distal end portion of the sensor body for producing an electromagnetic field, a ceramic well enclosing the sensor body and the coil, and a metallic housing surrounding the well and having an open distal end.
Chad P Stay from Minneapolis, MN Get Report