United Technologies Corporation

Arun Kumar Jayasingh

Herbert L Walker

Jonathan D Little

David Maliniak

Daniel J Monahan

Anthony T Lindsey

Veerachari J Mayachari

Rakesh Sharma N Dumavath

A gas turbine engine includes a nosecone assembly attached to a gas turbine engine. The nosecone assembly includes a support structure and a nosecone attached to the support structure. The nosecone includes at least a first tool hole extending through the nosecone. The first tool hole is structurally reinforced.

Removable nosecone for a gas turbine engine

An assembly for a gas turbine engine includes a rotor formed by a drum and a hub. The drum has a generally conically shaped inner surface that defines a flow path along a first cavity. The hub is connected to the drum and has a conically shaped inner surface that defines a flow path along a second cavity.

Gas turbine engine rotor drain feature

A gas turbine engine includes a compressor section and a nosecone assembly. The compressor section includes an inlet guide vane assembly including an inner shroud, an outer shroud, and an inlet guide vane extending from the inner shroud to the outer shroud. The nosecone assembly is attached to the inner shroud.

Gas turbine engine with attached nosecone

Growing community of inventors

East Hartford, CT, United States of America

Arun Kumar Jayasingh