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Kamel M Al-Khalil

from Kinnelon, NJ

Also known as:
  • Kamel Mahmoud Al-Khalil
Phone and address:
11 Forge Rd, Kinnelon, NJ 07405
973 838-1794

Kamel Al-Khalil Phones & Addresses

  • 11 Forge Rd, Butler, NJ 07405 • 973 838-1794
  • Kinnelon, NJ

Work

  • Company:
    Cox & company
    Dec 1994 to Oct 2012
  • Position:
    Director of research and technology

Education

  • Degree:
    Doctorates, Doctor of Philosophy
  • School / High School:
    The University of Toledo
    1982 to 1991
  • Specialities:
    Engineering

Skills

Aircraft • Engineering • Aerospace • Engineering Management • Systems Engineering • Aerodynamics • Simulations • Flight Test • Aerospace Engineering • Testing • Aviation • Aeronautics • Avionics • R&D • Product Development • Catia • Cfd • Cross Functional Team Leadership • Composites • Airworthiness • Continuous Improvement • Electronics

Industries

Aviation & Aerospace

Us Patents

  • Energy-Efficient Electro-Thermal Ice-Protection System

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  • US Patent:
    7708227, May 4, 2010
  • Filed:
    Jan 6, 2006
  • Appl. No.:
    11/327262
  • Inventors:
    Kamel Al-Khalil - Kinnelon NJ, US
  • Assignee:
    Cox & Company, Inc. - Plainview NY
  • International Classification:
    B64D 15/12
  • US Classification:
    244134D, 244134 R, 244134 A
  • Abstract:
    A region of an airfoil to be protected from accreted ice is heated to reduce the strength of the bond between the ice and the airfoil, and is mechanically deformed to shed the accreted ice after the bond has been sufficiently weakened. Heating ceases before substantial water runback is generated. The mechanical deformation and the cessation of heating occur approximately simultaneously.
  • Energy-Efficient Electro-Thermal And Electro-Mechanical Ice-Protection Method

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  • US Patent:
    7854412, Dec 21, 2010
  • Filed:
    Nov 26, 2008
  • Appl. No.:
    12/323685
  • Inventors:
    Kamel Al-Khalil - Kinnelon NJ, US
  • Assignee:
    Cox & Company, Inc. - Plainview NY
  • International Classification:
    B64D 15/04
    B64D 15/16
    B64F 5/00
  • US Classification:
    244134R, 244134 A, 244134 D
  • Abstract:
    A region of an airfoil to be protected from accreted ice is heated to reduce the strength of the bond between the ice and the airfoil, and is mechanically deformed to shed the accreted ice after the bond has been sufficiently weakened. Heating ceases before substantial water runback is generated. The mechanical deformation and the cessation of heating occur approximately simultaneously.
  • Energy-Efficient Electro-Thermal And Electro-Mechanical Ice-Protection Method

    view source
  • US Patent:
    8430359, Apr 30, 2013
  • Filed:
    Oct 18, 2010
  • Appl. No.:
    12/906370
  • Inventors:
    Kamel Al-Khalil - Kinnelon NJ, US
  • Assignee:
    Cox & Company, Inc. - Plainview NY
  • International Classification:
    B64D 15/16
  • US Classification:
    244134A, 244134 R, 244134 D, 244134 B
  • Abstract:
    A region of an airfoil to be protected from accreted ice is heated to reduce the strength of the bond between the ice and the airfoil, and is mechanically deformed to shed the accreted ice after the bond has been sufficiently weakened. Heating ceases before substantial water runback is generated. The mechanical deformation and the cessation of heating occur approximately simultaneously.
  • Hybrid Ice-Protection System For Use On Roughness-Sensitive Airfoils

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  • US Patent:
    59215020, Jul 13, 1999
  • Filed:
    Jun 19, 1996
  • Appl. No.:
    8/665914
  • Inventors:
    Kamel M. Al-Khalil - Rutherford NJ
    Thomas F. W. Ferguson - New York NY
    Dennis M. Phillips - Pleasantville NY
  • Assignee:
    Cox & Company, Inc. - New York NY
  • International Classification:
    B64D 1500
  • US Classification:
    244134R
  • Abstract:
    An electro-thermal or hot gas anti-icer of the "running-wet" type is mounted at the leading edge of an airfoil. Mechanical de-icers are mounted on the surfaces aft of the anti-icer. The mechanical de-icers throw off ice without creating runback water, thereby eliminating runback refreeze ridges caused by a known hybrid ice-protection system. Advantageously, the de-icers are of a type in which the airfoil has a semi-rigid skin that forms an aerodynamic surface of the airfoil, and in which there is at least one mechanical actuator for flexing the skin.
  • Hybrid Ice Protection System For Use On Roughness-Sensitive Airfoils

    view source
  • US Patent:
    61965006, Mar 6, 2001
  • Filed:
    Jun 11, 1999
  • Appl. No.:
    9/330444
  • Inventors:
    Kamel M. Al-Khalil - Rutherford NJ
    Thomas F. W. Ferguson - New York NY
  • Assignee:
    Cox & Company, Inc. - New York NY
  • International Classification:
    B64D 1500
  • US Classification:
    244134R
  • Abstract:
    An electro-thermal or hot gas anti-icer of the "running-wet" type is mounted at the leading edge of an airfoil. Mechanical de-icers are mounted on the surfaces aft of the anti-icer. The mechanical de-icers throw off ice without creating runback water, thereby eliminating runback refreeze ridges caused by a known hybrid ice-protection system. Advantageously, the de-icers are of a type in which the airfoil has a semi-rigid skin that forms an aerodynamic surface of the airfoil, and in which there is at least one mechanical actuator for flexing the skin.

Resumes

Kamel Al-Khalil Photo 1

Director Of Engineering

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Location:
Butler, NJ
Industry:
Aviation & Aerospace
Work:
Cox & Company Dec 1994 - Oct 2012
Director of Research and Technology

Cox & Company Dec 1994 - Oct 2012
Director of Engineering

Nasa Glenn Research Center Jun 1991 - Dec 1994
Post Doctoral Research Associate
Education:
The University of Toledo 1982 - 1991
Doctorates, Doctor of Philosophy, Engineering
Skills:
Aircraft
Engineering
Aerospace
Engineering Management
Systems Engineering
Aerodynamics
Simulations
Flight Test
Aerospace Engineering
Testing
Aviation
Aeronautics
Avionics
R&D
Product Development
Catia
Cfd
Cross Functional Team Leadership
Composites
Airworthiness
Continuous Improvement
Electronics

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