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Mark Eugene Ulliman

from Cincinnati, OH
Age ~64
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Also known as:
Mark E Ulliman, Mark E Ullman, Mark N
Phone and address:
7737 Kennedy Ln, Cincinnati, OH 45242
(513) 793-7577
Related to:
Katherine L Ramirez, 38Heidi L Kar, 45Marilyn S Lary, 81Sara Lary, 47
Connected to:
Donna A Ullio, 64Craig Ulliott, 40Anne C Ullius, 57Flavia V Ullivarri, 60Flavio M Ullivarri, 85Ashley S Ullman, 36Ellen H Ullman, 97Jamie S Ullman, 60Melanie M Ullman, 72Ralph W Ullman, 85

Mark Ulliman Phones & Addresses

  • 7737 Kennedy Ln, Cincinnati, OH 45242 (513) 793-7577
  • Montgomery, OH
  • Williams Bay, WI
  • Columbus, OH

Resumes

Resumes

Mark Ulliman Photo 1

General Manager - Sales Operations

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Location:
Cincinnati, OH
Industry:
Airlines/Aviation
Work:
Ge Aviation May 1, 2004 - Sep 1, 2008
General Manager - Cfm Services
Ge Aviation May 1, 2004 - Sep 1, 2008
General Manager - Sales Operations
Education:
University of Cincinnati 1982 - 1985
Masters, Master of Science In Mechanical Engineering University of Notre Dame 1978 - 1982
Bachelor of Science In Mechanical Engineering, Bachelors, Energy, Mechanical Engineering
Skills:
Business Management
Sales Operations
Aviation
Airlines
Sales
Operations
Mark Ulliman Photo 2

Vice President Construction

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Location:
Dallas, TX
Work:

Vice President Construction
Education:
University of Cincinnati - College of Engineering and Applied Science

Business Records

Name / Title
Company / Classification
Phones & Addresses
Mark E. Ulliman
Principal
Uldin Properties LLC
Nonresidential Building Operator
7737 Kennedy Ln, Cincinnati, OH 45242

Publications

Us Patents

Gas Turbine Blade With Improved Cooling

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US Patent:
53870867, Feb 7, 1995
Filed:
Jul 19, 1993
Appl. No.:
8/093165
Inventors:
David A. Frey - West Chester OH
Mark E. Ulliman - Cincinnati OH
Assignee:
General Electric Company - Cincinnati OH
International Classification:
F01D 518
US Classification:
416 97R
Abstract:
A turbine blade is provided which includes an airfoil section having a leading edge flow region and a trailing edge flow region. The leading edge flow region includes an inner cavity having a serpentine geometry and first and second air inlets. The first air inlet is at one end of the inner cavity and is coupled to a first conduit which supplies air coolant thereto. The leading edge flow region also includes a leading edge cavity having a plurality of air film holes at the leading edge of the blade. The leading edge cavity is coupled to the inner cavity by impingement holes therebetween. The leading edge flow region further includes a refresher passageway which connects the first conduit at the base of the blade with the second inlet of the inner cavity. The refresher passageway refreshes the airflow in the inner cavity after the airflow has flowed part way through the inner cavity and has become warmed. The trailing edge flow region includes a trailing edge cavity which is isolated from the inner cavity and which is cooled by air from a second conduit at the base of the blade.
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Mark Eugene Ulliman from Cincinnati, OH, age ~64 Get Report