US 5,551,478 A · Multiplexing hydraulic control network with latching valves

Abstract

A hydraulic control system for a jet aircraft engine has an electronic control that commands a pair of torque motors to ultimately control the position of each one of a plurality of two-position, "latching" hydraulic actuator valves. A first torque motor is operable with a three-position, on/off hydraulic valve. The second torque motor operates in conjunction with a second valve to control the linear position of the spool of a multiplexer selector valve. The multiplexer selector valve has a plurality of positions that the spool can be linear translatable to. At each position is located a pair of control ports to which are ultimately connected one side of each of a pair of corresponding hydraulic actuator valves. The actuator valves may comprise fuel or air valves. A selected fuel or air actuator valve is translated between one of its two positions by translating the spool of the multiplexer selector valve to the appropriate position and then porting high pressure hydraulic fluid to that actuator valve for a predetermined period of time. The control system can asynchronously chose any fuel or air actuator valve to translate, as necessary, at any point in time.

Claims21

Dependent claims

A fluid control system, comprising:

a. a first fluid at a first predetermined pressure;
b. a second fluid at a second predetermined pressure;
c. a multiplexer selector valve having an input port selectably connectable with the first fluid and being translatable between a plurality of discrete physical positions, each position corresponding to a selected one of a plurality of selector valve output ports, the selector valve being operable to connect the first fluid selectably connected at the selector valve input port to the selected one of the plurality of selector valve output ports;
d. means for translating the selector valve between the plurality of selector valve output ports;
e. a plurality of actuator valves, each one of the actuator valves being connectable with a corresponding at least one of the plurality of selector valve output ports, each one of the actuator valves being translatable between two positions by application of the first fluid thereto, wherein the means for translating is operable to translate the selector valve to a fail-safe position, the selector valve being operable to direct the first fluid to each of the plurality of actuator valves when the selector valve is in the fail-safe position;
and
f. means for selecting the first fluid to be applied to a selected at least one of the actuator valves for a predetermined time to cause translation of the selected at least one of the actuator valves.

4 more elements

A hydraulic control system for a jet aircraft engine that has a plurality of variable parameters that vary with the control of passage of hydraulic fluid through corresponding hydraulic actuators, the hydraulic control system comprising:

a. a first hydraulic fluid at a first pressure;
b. a second hydraulic fluid at a second pressure;
c. a multiplexer selector valve having an input that is connectable with at least one of the first and second hydraulic fluids and having a movable spool that is linearly translatable between a plurality of selector output ports to connect at least one of the first and second hydraulic fluids to a selected one of the plurality of selector valve output ports;
d. means for translating the spool of the multiplexer selector valve to select one of a plurality of discrete physical locations of the spool, one at least of the discrete physical spool locations corresponding to at least two of the selector valve output ports;
e. a plurality of actuator valves, each one of the actuator valves being connectable with a corresponding one of the plurality of valve output ports, each actuator valve having a movable element that is translatable between two positions to control the passage of a control fluid therethrough, the control fluid passing through the actuator valve being associated with one of the plurality of variable parameters of the jet aircraft engine;
f. means for selecting the first hydraulic fluid to be applied to a selected at least one of the actuator valves for a predetermined time to thereby cause translation thereof;
g. means for selecting the second hydraulic fluid to be applied to at least one of the actuator valves to thereby cause non-translation thereof;
h. means for holding at least one of the actuator valves in a stationary position when the second hydraulic fluid is applied to the corresponding at least one of the actuator valves by the means for selecting the second hydraulic fluid.

5 more elements

Dependencies are inferred from the claim text.

Multiplexing hydraulic control network with latching valves

Life of this patent

Multiplexing hydraulic control network with latching valves

Life of this patent

Abstract

Claims21