General Electric Company

Avco Corporation

Alan John Charlton

Peter W Mueller

Richard M Norris

John Dawson

Clifford Edward Allen, Jr

Peter Kent

A method facilitates assembling a gas turbine engine. The method comprises providing an engine frame including an integrally formed outer band, an inner band, and a plurality of circumferentially-spaced apart struts extending radially therebetween, and providing at least one fairing that is formed as an integral single piece casting and includes a first sidewall and a second sidewall connected at a leading edge and a trailing edge such that at least one cooling chamber is defined therebetween. The method also comprises coupling the at least one fairing around at least one strut such that the strut extends through the fairing at least one cooling chamber and such that during the coupling process the fairing is only transitioned axially around the strut rather being slid radially along the strut.

Methods and apparatus for assembling gas turbine engines

A turbine frame includes first and second coaxially disposed rings having a plurality of circumferentially spaced apart struts extending therebetween. A plurality of clevises join respective first ends of the struts to the first ring for removably joining the struts thereto. Each of the clevises includes a base removably fixedly joined to the first ring, and a pair of legs extending away from the base and spaced apart to define a U-shaped clevis slot receiving the strut first end. The strut first end is removably fixedly joined to the clevis legs by a pair of expansion bolts. The clevis base includes a central aperture aligned with a first port in the first ring for providing access therethrough.

Turbine frame

A multichannel particle separator for use in cleaning engine inlet air is disclosed. The separator uses a plurality of channel assemblies arranged in parallel side-by-side fashion within a substantially rectangular housing. Separation of undesired particles is achieved by accelerating the incoming airstream to a high velocity and turning it such that inertia carries the dirt particles into a particle collection chamber. A small percentage of the incoming air is used to induce particulate matter to proceed into the particle collection chambers. Heated air from a source within the adjacent engine is passed along passages within the interior of each channel assembly to heat the surface thereof and prevent ice formation thereon when operating under adverse meteorological conditions. The small percentage of diverted incoming air and the spent hot air are combined in the particle collection chambers to form a turbulence generator which maintains the separated particulates and collected moisture in suspension for exhaustion overboard through a common scavenge manifold.

Growing community of inventors

Boxford, MA, United States of America

Alan John Charlton