Ge Aviation
Director, Cfm Customer Programs
Ge Aviation Nov 2014 - Feb 2017
Business Operations Director, Materials and Mro Strategy
Ge Aviation Nov 2014 - Feb 2017
Regional General Manager - Mro Services
Ge Aviation Jul 2013 - Oct 2014
Executive Compliance Officer
Ge Aviation May 2011 - Jul 2013
Business Compliance Leader - Commercial
Education:
University of Glasgow
Bachelors, Aerospace Engineering
University of Strathclyde
Master of Science, Masters, Business
Skills:
Six Sigma Cross Functional Team Leadership Program Management Business Process Improvement Aviation Management Strategy
Roy L. Stone - Springboro OH, US Donna E. Gerber - Mason OH, US Kunio Masuda - West Chester OH, US David G. Blanchette - Hamersville OH, US Michael D. Fullington - West Chester OH, US
International Classification:
B08B 3/04
US Classification:
134 10
Abstract:
A method of washing a gas turbine engine, the method comprising the steps of: providing a gas turbine engine, the engine having an intake and an exhaust, the exhaust having an inner surface and an outer surface; providing a system for washing gas turbine engines, the system including a containment structure; releasably securing the containment structure to the inner surface via a retaining ring; introducing a wash liquid into the intake; and collecting the wash liquid in the containment structure.
Roy L. Stone - Springboro OH, US Donna E. Gerber - Mason OH, US Kunio Masuda - West Chester OH, US David G. Blanchette - Hamersville OH, US Michael D. Fullington - West Chester OH, US
International Classification:
B08B 3/00
US Classification:
134109
Abstract:
A system for washing a gas turbine engine, the gas turbine engine having an inlet and an exhaust, the exhaust having an inner surface and an outer surface. The system comprises: a containment structure for capturing gaseous, liquid, and solid material emerging from the engine; a filtration system for separating the gaseous, liquid, and solid material; and a retaining ring for securing the containment structure to said exhaust; wherein the retaining ring is adjustable in at least one of size and shape so as to sealingly engage the inner surface of the exhaust.