Engine arrangement

Rotary kinetic fluid motors or pumps – Plural runners supported for relative motion or on separate... – Interdigitated – oppositely extending – coaxial – axially...

Reexamination Certificate

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Details

C415S068000, C416S128000, C416S160000, C416S1700HM

Reexamination Certificate

active

07850417

ABSTRACT:
In a contra rotating propeller engine propeller blade assemblies are provided which rotate in opposite directions as a result of association with an epicyclic gear assembly acting as a differential gearbox. A carrier is provided to drive one propeller blade assembly. Actuators are provided to cause pitch angle adjustment of the respective propeller blades of the assemblies. These actuators, are secured upon a stationary structure and act through actuator rods and appropriate mechanisms to cause such angular pitch adjustment. Rotational de-couplers are provided to rotationally isolate the actuators while an actuator rod part acts across the assemblies and a rotational de-coupler to de-couple contra rotation between the assemblies while still allowing axial displacement for adjustment of the other propeller blade assembly.

REFERENCES:
patent: 3904315 (1975-09-01), Schwartz
patent: 4738589 (1988-04-01), Wright
patent: 4842484 (1989-06-01), Johnson
patent: 4936746 (1990-06-01), Mayo et al.
patent: 5152668 (1992-10-01), Bulman et al.
patent: 5213471 (1993-05-01), Miller et al.
patent: 5242265 (1993-09-01), Hora et al.
patent: A 2002-349700 (2002-12-01), None

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