Pneumatic actuator low flow servo valve

Patent metadata

Field	Value
Publication number	US-2016208702-A1
Application number	US-201514599807-A
Country	US
Kind code	A1
Filing date	Jan 19, 2015
Priority date	Jan 19, 2015
Publication date	Jul 21, 2016
Grant date	—

Abstract

A valve system includes a valve for controlling flow of a fluid and a valve controller for providing fluid to control the movement of a valve actuator. The valve includes a flow control device, a modulating chamber, and the valve actuator. The valve actuator is movable within the modulating chamber to open and close the flow control device. The valve controller includes a channel within the valve controller and an inlet port for connecting the channel and a high pressure source. The valve controller also includes an exhaust port for connecting the channel and an ambient pressure and a modulating port connecting the channel to the modulating chamber. The valve controller further includes an armature movable relative to the channel. The armature closes the inlet port and the exhaust port in a first position, the armature opens the inlet port and closes the exhaust port in a second position, and the armature opens the exhaust port and closes the inlet port in a third position. The valve controller also includes an electromagnetic motor adjacent to the channel for moving the armature.

First claim

1 . A valve system comprising:
a valve for controlling flow of a fluid, the valve comprising:
a flow control device;
a modulating chamber; and
a valve actuator movable within the modulating chamber to open and close the flow control device; and
a valve controller for providing fluid to control the movement of the valve actuator, the valve controller comprising:
a channel within the valve controller;
an inlet port for connecting the channel and a high pressure source;
an exhaust port for connecting the channel and an ambient pressure;
a modulating port connecting the channel to the modulating chamber;
an armature movable relative to the channel, wherein the armature closes the inlet port and the exhaust port in a first position, wherein the armature opens the inlet port and closes the exhaust port in a second position, and wherein the armature opens the exhaust port and closes the inlet port in a third position; and
an electromagnetic motor adjacent to the channel for moving the armature.

2 . The valve system of claim 1 , wherein movement of the armature is linear.

3 . The valve system of claim 1 , wherein the valve controller is a torque motor.

4 . The valve system of claim 1 , wherein the inlet port connects to an upstream side of the control device.

5 . The valve system of claim 4 , wherein the valve controller is a torque motor.

6 . The valve system of claim 1 , wherein the control device is a butterfly valve.

7 . The valve system of claim 1 , wherein the valve is a servo.

8 . The valve system of claim 1 and further comprising a controller for sending control signals to the torque motor, wherein the control signals direct the torque motor to open and close the flow control device.

9 . An aircraft environmental cooling system, including the valve system of claim 1 , and further comprising a controller that provides command signals to the valve controller.

10 . The aircraft environmental cooling system of claim 9 , wherein the high pressure source comprises bleed air from a gas turbine engine.

11 . The aircraft environmental cooling system of claim 10 , wherein the valve controller is mounted directly to the valve.

12 . A method for controlling a valve, the method comprising:
electromagnetically driving an armature to open an inlet port of a valve controller, and to close an exhaust port of the valve controller, which connects a high pressure source to a chamber of a valve causing the valve to open; electromagnetically driving the armature to close the inlet port and open the exhaust port, which connects the chamber to ambient, causing the valve to close; and electromagnetically driving the armature to close the inlet port and the exhaust port, which disconnects the chamber from ambient and the high pressure source, causing the valve to maintain its position.

13 . The method of claim 12 , and further comprising:
sending command signals for moving the armature from a controller to the valve controller.

14 . The method of claim 12 , and further comprising:
driving a motor connected to the armature as a function of the command signals.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Schroder Bruce R

Classifications

• F16K31/04

  using a motor · CPC title

• F02C7/18 Primary

  the medium being gaseous, e.g. air {(F02C7/125 takes precedence)} · CPC title

• F16K1/22

  with axis of rotation crossing the valve member, e.g. butterfly valves · CPC title

• F02C6/08

  the gas being bled from the gas-turbine compressor · CPC title

• F16K31/1635 Primary

  for rotating valves · CPC title