Cantilevered tip turbine engine

Power plants – Reaction motor – Interrelated reaction motors

Reexamination Certificate

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Details

C060S796000

Reexamination Certificate

active

08033094

ABSTRACT:
A tip turbine engine (10) according to the present invention includes an engine support structure (12) for cantilevering a load bearing shaft from an engine support plane (P). An engine support structure (12) defines the engine support plane (P), which is perpendicular to an engine centerline (A). The shaft (60) is rotationally fixed, coaxial with the engine centerline (A), and structurally supported by the engine support structure (12) such that a load borne by the shaft (60) is transferred along the engine support plane.

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