We are a global leader in custom oil flow and temperature control devices

for direct drive and geared engine architectures. We provide aircraft turbine

system performance enhancements via custom flow modulation,

which includes flight critical applications in oil modulation, controlled bearing

cooling flow, thermal management, heat exchanger bypass and your specific valves.

Features & Benefits Highlights

• Leading fuel, oil, actuation, air, and combustion systems

• Innovative systems approach to integrate fight critical, customized functionality while minimizing piece

parts

• Highly reliable and cost-effective solutions delivered within severely condensed program schedules

• High reliability and lower risk with technology based on millions of flight hours

Hydraulic Filter Assembly

The valve is supplied with an integrated, high-capacity filter. The broad range filter protects the internal

hydraulic control components from large oil-borne contaminants that might cause the hydraulic

components to stick or operate erratically. The filter is supplied with a visual indicator which shows when

the recommended pressure differential has been exceeded and thus replacement of the element is

necessary.

LVDT Position Feedback Sensors

The SonicFlo control valves use a dual-coil, dual-rod LVDT for position feedback. The LVDT is factory set

to give 0.7 Vrms feedback at minimum position and 3.5 Vrms feedback at maximum position, when

supplied with 7 Vrms excitation at 3000 Hz.

Trip Relay Valve Assembly

The SonicFlo™ valve uses a solenoid-operated trip relay circuit to operate a high capacity, three-way,

two-position, hydraulically operated valve. This trip relay circuit consists of four functional elements: the

trip relay solenoid valve, the trip relay supply orifice, the hydraulically operated trip valve, and the trip

relay volume.

In the normal run mode, the trip relay solenoid valve is closed, which prevents the trip relay volume from

bleeding to the hydraulic return. As a result, high-pressure oil is fed into the trip relay circuit through the

supply orifice, which quickly pressurizes the trip circuit to supply pressure. When the trip circuit pressure

increases above 1100 kPa (160 psig), the three-way relay valve shifts position so that the common port

connects the control port of the servo-valve to the lower piston cavity of the actuator, allowing the servo

valve to position the throttle valve.

The solenoid valve opens when it is de-energized. Opening the solenoid valve causes the trip circuit to be

connected to drain. This in turn causes the three-way relay valve to shift position so that the common port

is connected to the hydraulic drain circuit, and isolated from the hydraulic supply. As the pressure falls

within the lower piston cavity, the return spring rapidly returns the valve plug to the downward position,

closing the control valve and shutting off fuel to the engine.

Triple Coil Electrohydraulic Servo Valve Assembly

The hydraulic actuator assembly uses a two-stage hydraulic servo valve to modulate the position of the

actuator output shaft and thereby control the gas fuel valves. The first stage torque motor utilizes a triple

wound coil, which controls the position of the first and second stage valves in proportion to the total

electric current applied to the three coils.

If the control system requires a rapid movement of the valve to send more fuel to the turbine, total

current is increased well above the null current. In such a condition, control port PC1 is connected to

supply pressure. The flow rate delivered to the piston cavity of the actuator is proportional to the total

current applied to the three coils. Thus, the opening velocity is also proportional to the current (above

null) supplied to the torque motor.

If the control system requires a rapid movement to close the gas fuel valve, the total current is reduced

well below the null current. In such a condition, port PC1 is connected to the hydraulic drain circuit. The

flow rate from the piston cavity to drain is proportional to the magnitude of the total current below the

null value. Thus, the closing velocity is also proportional to the current (below null) supplied to the torque

motor.

Introduction

The SonicFlo™ valve controls the flow of gas fuel to the combustion system of an industrial or utility gas

turbine. The unique design yields a linear flow characteristic unaffected by discharge pressure up to a

pressure ratio (P2/P1) of at least 0.8. The design also integrates the valve and actuator into a compact

assembly. The key characteristics of this valve are a highly linear critical gas flow versus stroke

relationship at constant upstream pressure. The integral actuator is a single-acting spring-loaded design

for failsafe operation. The actuator includes an onboard hydraulic filter for last chance filtration of the

fluid to ensure reliability of the servo valve and actuator. The servo valve is electrically redundant with

triple coil design. Feedback for the actuator is provided by a dual coil, dual rod LVDT (linear variable

differential transformer) directly coupled to the hydraulic piston.

Near the null current, the four-landed valve isolates the control port from the hydraulic supply and drain,

balancing the piston pressure against the spring to maintain a constant position. The control system,

which regulates the amount of current delivered to the coils, modulates the current supplied to the coil to

obtain proper closed loop position of the valve.