Patent ID: 8157241

Claim:
A method for regulating gas turbine engine fluid flow, comprising: providing: a flow tube having an inlet, an outlet portion, and a first bend disposed between the inlet and the outlet portion and having an axis passing through a center of the flow tube; a pair of piston rods disposed outside the flow tube at an axial location between the first bend and the outlet portion and aligned parallel to the axis; and a valve disposed within said flow tube, said valve having an axle that is perpendicular to said axis, the axle disposed between the first bend and the inlet such that the axle is offset from a plane which is parallel to said axle and to said axis, and which passes through said axis and said piston rods; flowing fluid through said flow tube; actuating a piston that is coupled to said piston rods so that said piston moves in the axial direction; rotating said axle due to the axial movement of said piston that is transmitted to the axle through the piston rods by way of crank arms; and changing the position of said valve due to the rotation of said axle.