Fluid reaction surfaces (i.e. – impellers) – With control means responsive to non-cyclic condition... – Impeller rotation speed responsive
Patent
1990-09-04
1993-05-25
Look, Edward K.
Fluid reaction surfaces (i.e., impellers)
With control means responsive to non-cyclic condition...
Impeller rotation speed responsive
416129, 416154, 416156, 416162, B65H 300
Patent
active
052134717
ABSTRACT:
The invention concerns a system for controlling an aircraft propeller. A hydraulic motor controls pitch of the propeller blades. The propeller blades are characterized by the absence of feather-inducing counterweights. An overspeed governor senses when propeller speed exceeds a limit, and, in response, assumes control of the hydraulic motor and drives the blades toward a coarsened pitch position, which reduces the propeller speed. In another form of the invention, a mechanical brake can override the hydraulic motor and mechanically retard a rotating gear, which causes the propeller blades to move toward a coarsened pitch.
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patent: 4936746 (1990-06-01), Mayo
patent: 5019006 (1991-05-01), Schneider
patent: 5100729 (1991-04-01), Adamson
Hora Petr
Joyce David L.
Mears John S.
Miller Edwin K.
Roberts Robert L.
General Electric Company
Look Edward K.
Newholm Therese M.
Rafter John R.
Squillaro Jerome C.
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