Controller assembly

Patent metadata

Field	Value
Publication number	US-11215295-B2
Application number	US-201916580046-A
Country	US
Kind code	B2
Filing date	Sep 24, 2019
Priority date	Oct 8, 2018
Publication date	Jan 4, 2022
Grant date	Jan 4, 2022

Abstract

A controller assembly comprises an electromechanical actuator and a single-stage pneumatic flow switch configured to thermally protect the electromechanical actuator by a supply of cooling fluid. The single-stage pneumatic flow switch is movable between a first mode in which the switch is configured to open a cooling fluid flow passage and a second mode in which the switch is configured to close the cooling fluid flow passage. The electromechanical actuator is coupled to a valve movable between an open and a closed configuration.

First claim

I claim:

1. A controller assembly comprising:
an electromechanical actuator; and
a single-stage pneumatic flow switch configured to thermally protect the electromechanical actuator by a supply of cooling fluid;
wherein the single-stage pneumatic flow switch is movable between a first mode in which the switch is configured to open a cooling fluid flow passage and a second mode in which the switch is configured to close the cooling fluid flow passage;
wherein the electromechanical actuator is coupled to a valve movable between an open configuration and a closed configuration; and
wherein the electromechanical actuator is disposed in a fluid flow outlet of the valve.

2. The controller assembly of claim 1 , wherein, when in the first mode, the single-stage pneumatic flow switch is configured to open a further fluid flow passage and, when in the second mode, the switch is configured to close the further fluid flow passage.

3. The controller assembly of claim 2 , wherein the further fluid flow passage is connected to a control chamber of the valve.

4. The controller assembly of claim 3 , wherein, when in the second mode the single-stage pneumatic flow switch is configured to open a vent flow passage so that the control chamber of the valve is in fluid communication with the vent flow passage.

5. The controller assembly of claim 3 , wherein the further fluid flow passage is connected to a source of fluid at a higher pressure than the pressure across the valve to thereby pressurize the control chamber of the valve.

6. The controller assembly of claim 1 , wherein, when in the first mode, the single-stage pneumatic flow switch is configured to cause the valve to open and, when in the second mode, the switch is configured to cause the valve to close.

7. The controller assembly of claim 1 , wherein the electromechanical actuator is configured to cause the switch to transition between its first and second modes, thereby configured to cause the valve to transition between the open and closed configurations.

8. The controller assembly of claim 1 , wherein the electromechanical actuator comprises a solenoid.

9. A controller assembly comprising:
an electromechanical actuator; and
a single-stage pneumatic flow switch configured to thermally protect the electromechanical actuator by a supply of cooling fluid;
wherein the single-stage pneumatic flow switch is movable between a first mode in which the switch is configured to open a cooling fluid flow passage and a second mode in which the switch is configured to close the cooling fluid flow passage;
wherein the electromechanical actuator is coupled to a valve movable between an open configuration and a closed configuration;
wherein, when in the first mode, the single-stage pneumatic flow switch is configured to open a further fluid flow passage and, when in the second mode, the switch is configured to close the further fluid flow passage;
wherein the further fluid flow passage is connected to a control chamber of the valve;
wherein the further fluid flow passage is connected to a source of fluid at a higher pressure than the pressure across the valve to thereby pressurize the control chamber of the valve; and
wherein the further fluid flow passage is connected to a source of fluid from an upstream side of the valve.

10. A gas turbine engine for an aircraft, the gas turbine engine comprising:
an engine core comprising a turbine, a compressor, and a core shaft connecting the turbine to the compressor;
a fan located upstream of the engine core, the fan comprising a plurality of fan blades;
a controller assembly comprising:
an electromechanical actuator; and
a single-stage pneumatic flow switch configured to thermally protect the electromechanical actuator by a supply of cooling fluid;
wherein the single-stage pneumatic flow switch is movable between a first mode in which the switch is configured to open a cooling fluid flow passage and a second mode in which the switch is configured to close the cooling fluid flow passage; and
wherein the electromechanical actuator is coupled to a valve movable between an open configuration and a closed configuration.

11. The gas turbine engine of claim 10 , wherein the controller assembly is disposed within a valve body, and wherein at least one spoke connects the valve body to the electromechanical actuator; wherein the cooling fluid flow passage is at least partially located within one spoke.

12. The gas turbine engine of claim 11 , wherein the valve body comprises the valve having a control chamber, wherein at least one spoke connects the valve body to the electromechanical actuator and wherein a pressure source is connected to the valve control chamber, the pressure source being at least partially located within one spoke.

Assignees

• Rolls Royce Plc

Inventors

• Murray Christopher A

Classifications

• F16K31/0631

  with ball shaped valve members · CPC title

• F16K49/005 Primary

  Circulation means for a separate heat transfer fluid · CPC title

• F16K31/1226

  the fluid circulating through the piston · CPC title

• F02C9/18 Primary

  by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages {(F02C3/113 takes precedence)} · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title