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Kevin M Wiedenmann

age ~40

from Wichita, KS

Also known as:
  • Kevin M Widenmann
  • Kevin N
Phone and address:
15915 E Boxthorn St, Wichita, KS 67228
9134618371

Kevin Wiedenmann Phones & Addresses

  • 15915 E Boxthorn St, Wichita, KS 67228 • 9134618371
  • Andover, KS
  • Lawrence, KS
  • 13950 130Th St, Olathe, KS 66062 • 9137801631 • 9137802528

Work

  • Company:
    Bombardier aerospace
    Aug 2012
  • Address:
    Wichita, Kansas Area
  • Position:
    Senior flight test engineer - learjet 70/75

Education

  • Degree:
    Aerospace Engineering
  • School / High School:
    University of Kansas
    2002 to 2007

Skills

Aerospace • Flight Test • Aircraft • Aircraft Systems • Avionics • Systems Engineering • Cfd • Aerospace Engineering • System Testing • Aeronautics • Testing • Aircraft Design • Engineering Management • Aviation • Wind Tunnel Testing • Aerodynamics • Aircraft Maintenance • Airworthiness • Composites • Analysis • Propulsion • Stress Analysis • As9100 • Helicopters • Nastran • Catia • Fortran • Test Planning • Program Management • Leadership • Engineering • Management

Languages

English • Spanish

Industries

Aviation & Aerospace

Us Patents

  • Electrothermal And Electro Expulsive Hybrid Ice Protection System For Engine Inlet

    view source
  • US Patent:
    20130228653, Sep 5, 2013
  • Filed:
    Nov 16, 2012
  • Appl. No.:
    13/678906
  • Inventors:
    Brandon C. Clarke - West Chester OH, US
    Kevin Michael Wiedenmann - Andover KS, US
    Roger E. Kornfeld - Whitewater KS, US
    Kevin L. Obrachta - Wichita KS, US
    Neal G. Rolfes - Wichita KS, US
  • Assignee:
    SPIRIT AEROSYSTEMS, INC. - Wichita KS
  • International Classification:
    B64D 15/12
    B64D 15/16
  • US Classification:
    244134 D
  • Abstract:
    A hybrid ice protection system (HIPS) including both an electro-expulsive de-icing system (EEDS) and electrothermal heaters to first break ice away from an outer surface of an engine nacelle inlet lip and then melt remaining residual ice from the outer surface of the inlet lip. The EEDS may have a plurality of EEDS actuators positioned to provide striking force to inner surfaces of both outer and inner walls of the inlet lip. The electrothermal heaters may be positioned to heat the inlet lip at areas between locations where the EEDS actuators provide striking force. The HIPS may also include a control system for actuating the EEDS actuators to strike the inner surface of the inlet lip when the inlet lip is at or below a predetermined temperature and then activating the electrothermal heaters to remove residual ice left on the inlet lip after actuation of the EEDS actuators.

Resumes

Kevin Wiedenmann Photo 1

Lead Flight Test Engineer

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Location:
Wichita, KS
Industry:
Aviation & Aerospace
Work:
Bombardier Aerospace - Wichita, Kansas Area since Aug 2012
Senior Flight Test Engineer - Learjet 70/75

Bombardier Aerospace May 2011 - Aug 2012
Flight Test Team Mechanical Systems Lead - Learjet 85

Spirit AeroSystems Dec 2007 - May 2011
Environmental Control & Thermal Analysis Engineer II

Spirit Aerosystems Jun 2007 - Dec 2007
Design Engineer

DARcorporation Jul 2005 - May 2007
Aerospace Engineer (Co-op)
Education:
University of Kansas 2002 - 2007
Aerospace Engineering
Skills:
Aerospace
Flight Test
Aircraft
Aircraft Systems
Avionics
Systems Engineering
Cfd
Aerospace Engineering
System Testing
Aeronautics
Testing
Aircraft Design
Engineering Management
Aviation
Wind Tunnel Testing
Aerodynamics
Aircraft Maintenance
Airworthiness
Composites
Analysis
Propulsion
Stress Analysis
As9100
Helicopters
Nastran
Catia
Fortran
Test Planning
Program Management
Leadership
Engineering
Management
Languages:
English
Spanish

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