Patent ID: 8235776

Claim:
A method for controlling axial mover-system performance wherein through motor control actuation, a terminal device control damper is throttled against ducted or piped axial mover discharge flow adjusting and tuning damper control to specific damper positioning or valve constants according to the rectangular x/y coordinates of the Operating Point of the damper/valve and mover; according to the Polar Coordinates of Theta, x/y and r (distance from origin), the cutoff constant for the damper/valve position; applying specific mover constants according to the rectangular x/y coordinates for the pre-established mover characteristic curve; thus increasing BHP (Brake Horse Power) and system pressure at specific Operating Points, wherein through motor control actuation, axial mover fan blade pitch angle ( 11 ) is increased or decreased according to the Spherical Coordinates of Phi, Phase or Phasor angle from z, also as related to Power Factor in the mover driver component, and according to Rho (distance from origin), as the extendable or retractable cutoff constant for the mover blade; attaining specified mover constants ( 11 ) and flow-pressure rates ( 2 ) at a given blade angle Phi, BHP, and specific Operating Point ( 10 ).