Variable camber and stagger airfoil and method

Rotary kinetic fluid motors or pumps – Method of operation

Reexamination Certificate

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C415S160000

Reexamination Certificate

active

07114911

ABSTRACT:
Aerodynamically efficient air flow management in axial flow-turbines is provided by utilizing a variable stagger and camber airfoil. In an exemplary embodiment of the invention, this is accomplished by providing a two-piece airfoil including a strut and a flap, each of which is mounted to articulate about a common, radially oriented axis. The strut and flap are respectively positioned by a strut gear and a flap gear, located at the radial end of the airfoil and, in an exemplary embodiment, are driven by a stepped synchronizing ring.

REFERENCES:
patent: 3318574 (1967-05-01), Tyler
patent: 4579507 (1986-04-01), Corrigan et al.
patent: 4995786 (1991-02-01), Wheeler et al.
patent: 5314301 (1994-05-01), Knight
patent: 5620301 (1997-04-01), Lawer

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