Inventors:
John Paul Petrowicz - Rowley MA, US
Timothy Joseph Higgins - Topsfield MA, US
Walter Jackson Tingle - Danvers MA, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02G 3/00
US Classification:
60 39092, 244 53 B, 137 151, 181213, 181214, 181220, 55306, 4151212
Abstract:
A method for assembling a turbine engine including a compressor is disclosed. The method includes coupling an inlet including an inertial particle separator (IPS) and a first surface that is defined using a segment angle, to a gas turbine engine, and coupling the first surface substantially flush against a fuselage of an aircraft to reduce drag.