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Pressure regulation valve with integrated downstream pressure tap

  • US 5,664,760 A
  • Filed: 04/06/1995
  • Issued: 09/09/1997
  • Est. Priority Date: 04/06/1995
  • Status: Expired due to Term
First Claim
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1. In a pressure regulation valve, for an aircraft environmental control system, of the type having a butterfly valve with a pivotable disk that controls fluid flow through a main body, a pressure tap downstream of the disk to sense fluid pressure, an actuator to move the disk, and a controller that positions the actuator and thus the disk, the improvement comprising:

  • a. a baffle insert sleeve which is adapted in size and shape to fit within a discharge channel of the butterfly valve, downstream from the disk, wherein the insert has an inlet end adjacent the disk and an outlet end adjacent an outlet of the discharge channel;

    b. a flow baffle, within the insert, having a grid of throughbores for segmenting turbulent flow caused by the disk and making the turbulent flow more laminar within the valve body, wherein;

    i. a plurality of the throughbores are generally parallel to a central axis of the discharge channel;

    ii. a plurality of the throughbores are canted to direct the flow through them toward an inner wall of the baffle sleeve insert, downstream of the flow baffle;

    c. a ring of pressure-tap holes in the insert, downstream of the flow baffle;

    d. lip means for converting dynamic fluid pressure to static pressure at the pressure-tap holes, said lip means comprising an annular lip on the outlet end of the insert, adjacent the pressure-tap holes and downstream thereof, that acts as a dam to block the flow directed toward the inner wall of the baffle sleeve insert, by the canted throughbores in the flow baffle;

    e. an annular cavity in the valve body, that surrounds the pressure-tap holes to communicate fluid pressure sensed by the holes to an adjacent pressure sensing line integrated within the valve body.

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