Gearless/oilless gas turbine engine

Rotary kinetic fluid motors or pumps – With shaft connected fluid force subjected thrust balancing...

Reexamination Certificate

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C415S229000, C415S230000

Reexamination Certificate

active

06881027

ABSTRACT:
The complex mechanical gear trains and lubrication systems of conventional engine configurations are eliminated by using combinations of hydrodynamic air foil bearings, hydrodynamic solid geometry carbon seals/bearings, magnetic bearings, and electrical starter/generators that can also act as bearings to support the high speed shafts of gas turbine engines. The various bearing types and the starter/generators are arranged in such a way as to share peak loads experienced by the engine shaft during maximum aircraft maneuvers. This results in a minimal bearing and engine size.

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patent: 6524005 (2003-02-01), Bridges
R. Nims, Development of an Oilless, Gearless and Bleedable Under Armor Auxiliary Unit, ASME 95-GT-444, 12 pgs, Jun. 1995.

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