A compressor bleed apparatus includes: a compressor comprising one or more rotors mounted for rotation about a central axis and enclosed in a compressor casing; a bleed slot passing through the compressor casing; an outer wall defining, in cooperation with the compressor casing, a plenum surrounding the compressor casing; at least one offtake pipe communicating with the plenum; and wherein at least one of the plenum and the bleed slot has a non-axisymmetric structure.
GE Aviation - Lynn, MA since Jul 2011
Engineer/Technologist
CEPIO since May 2006
Instructor
Boston University Sep 2010 - Jun 2011
Systems Engineer
Boston University May 2010 - Sep 2010
Mechanical Engineer
Education:
Boston University College of Engineering 2007 - 2011
Bachelor of Science, Aerospace Engineering