The Garrett Corporation

Alliedsignal Inc.

Geoffrey D Woodhouse

George B Mattson

Robert A Hatch

Harvey B Jansen

Frederic E Bolliger

Leon D Lewis

Robert B Sumegi

Wilfried Wiher

Bruce S Anson

An aircraft subsystem provides the aircraft with all its electrical and conditioned air requirements without requiring the extraction of either shaft power and/or pressurized air from the aircraft's main engines. At the core of this subsystem are two rotating assemblies journaled on non-oil lubricated bearings to a housing. One assembly includes a cooling turbine, a starter/generator, a core compressor, and a high pressure stage of a two stage axial turbine, all mounted on a single shaft. A combustor is disposed between the core compressor and the turbine. The other assembly is comprised of the low pressure stage of the axial turbine coupled to a load compressor via a second shaft. The high pressure turbine stage and cooling turbine are sized to drive the core compressor and starter/generator which provides all the aircraft's electrical needs both on the ground and inflight. The low pressure turbine stage drives the load compressor, which produces pressurized air that is conditioned through heat exchange components and then expanded and cooled across the cooling turbine before being delivered to the aircraft cabin.

Fully integrated environmental and secondary power system

A system for automatically controlling the buoyancy of a lighter-than-air craft by condensing water ballast from engine exhaust gases.

Ballast management system for lighter than air craft

A recuperated gas turbine engine control and method which provides improved idling and limits both turbine inlet temperature and recuperator inlet temperature to different, preselected maximum levels.

Control for turbine and recuperator inlet temperatures

A free turbine gas turbine engine with an automatic idle reset control and method which anticipates requirement for engine acceleration and increases idle speed before request for acceleration is received.

Gas turbine engine idle control and method

A control system for a gas turbine engine includes provisions for adjusting fuel flow in relation to gas generator speed, and for adjusting guide vane position in relation to power turbine speed.

Gas turbine engine fuel control

A recuperated gas turbine engine fuel and guide vane control which controls fuel flow and guide vane position during engine idling and acceleration to minimize fuel consumption while providing fast acceleration for a ground vehicle.

Variable geometry gas turbine engine fuel and guide vane control

A free turbine engine for driving ground vehicles with various deceleration or braking actions including power feedback braking wherein the turbine compressor is selectively interconnected with the power output shaft only in such a manner whereby compressor inertia assists in decelerating the vehicle.

Growing community of inventors

Phoenix, AZ, United States of America

Geoffrey D Woodhouse