Pneumatic actuator low flow servo valve
US-2016208702-A1 · Jul 21, 2016 · US
US2016208694A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016208694-A1 |
| Application number | US-201514599802-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jan 19, 2015 |
| Priority date | Jan 19, 2015 |
| Publication date | Jul 21, 2016 |
| Grant date | — |
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A valve system includes a valve, a valve controller, and a heat exchanger. The valve is configured to open and close a control device in response to a working fluid. The controller controls the flow of the working fluid to and from the valve. The heat exchanger is mounted between the valve and the valve controller. The heat exchanger receives the working fluid from the valve, cools the working fluid using a cooling stream, and delivers cooled working fluid to the valve controller.
Opening claim text (preview).
1 . A valve system comprising: a valve configured to open and close a control device in response to a working fluid; a valve controller for controlling the flow of the working fluid to and from the valve; and a heat exchanger mounted between the valve and the valve controller, wherein the heat exchanger receives the working fluid from the valve, cools the working fluid using a cooling stream, and delivers cooled working fluid to the valve controller. 2 . The valve system of claim 1 wherein the heat exchanger further comprises multiple working inlets for receiving the working fluid, and multiple cooling inlets for receiving the cooling stream. 3 . The valve system of claim 1 , wherein the heat exchanger is comprised of at least one plate. 4 . The valve system of claim 3 , wherein the heat exchanger comprises: a first plate having a first surface having a first channel configured to receive a cooling stream, and having a second surface having a second channel for receiving a working fluid; a second plate having a first and second surface, wherein the first surface mates to the second surface of the first plate; a third plate having a first surface mating to the second surface of the second plate, wherein the first surface of the third plate has a first channel receives a cooling stream, and wherein the third plate has a second surface; and a fourth plate having a first surface having a first channel configured to receive a working fluid, and having a second surface having a second channel configured to receive a cooling stream, wherein the first surface mates to the second surface of the third plate; 5 . The valve system of claim 4 , wherein the plates are brazed together. 6 . The valve system of claim 1 , wherein the heat exchanger is formed as a single piece. 7 . The valve system of claim 6 , wherein the heat exchanger comprises: a first surface mounted to the valve controller; a second surface mounted to the valve; a first channel for receiving the cooling stream; a second channel adjacent to the first channel, and configured to receive the working fluid; a third channel for receiving the cooling stream, wherein the third channel is adjacent to the second channel; a fourth channel for receiving the working fluid, wherein the fourth channel is adjacent to the third channel; a fifth channel for receiving a cooling stream, wherein the fifth channel is adjacent to the fourth channel. 8 . The valve system of claim 6 , wherein the second channel is configured to deliver the working fluid to the fourth channel. 9 . The system of claim 1 , wherein the heat exchanger comprises: a first surface configured to mount to the valve controller; a second surface configured to mount to the valve; a plurality of cooling channels configured to receive the cooling stream; and a plurality of working channels configured to receive the working fluid, wherein each working channel is adjacent to one or more cooling channels. 10 . The valve system of claim 9 , wherein the working channels are configured to create a single working fluid flow path between the valve and the valve controller. 11 . A gas turbine engine system including the valve system of claim 1 , wherein the gas turbine engine system further comprises a gas turbine engine for delivering the working fluid and the cooling stream to the valve system, wherein the valve is a servo valve, and wherein the valve controller is a torque motor. 12 . The gas turbine engine system of claim 11 , wherein the working fluid is bleed air from the gas turbine engine and the cooling fluid is fan air from the gas turbine engine. 13 . The valve system of claim 1 , wherein the heat exchanger further comprises a bypass passage connecting the valve to the valve controller. 14 . A method comprising: receiving a working fluid in a first passage of a heat exchanger that is mounted between a valve and a valve controller, wherein the heat exchanger directs the working fluid through a first conductive path; receiving a cooling fluid in a second passage of the heat exchanger and directing the cooling fluid through a second conductive path; cooling the working fluid through indirect heat transfer using the cooling fluid; delivering the working fluid to the valve controller from the heat exchanger; exhausting the cooling fluid from the heat exchanger; delivering the working fluid from the valve controller to a bypass path of the heat exchanger; and supplying the working fluid from the heat exchanger to a chamber of the valve. 15 . The method of claim 14 , and further comprising: delivering the working fluid from the chamber to the bypass path; sending the working fluid from the bypass path to the valve controller; and exhausting the working fluid through the valve controller.
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