Potential NASA applications include those application where a valve can cycle at high frequencies. These applications include liquid rocket engine combustion stability control, where the principles being applied to combustion control for gas turbine engines can be applied. In this application, the ability to modulate the propellant flow at frequencies above 1,000 Hz may be advantageous. A second potential application is in high frequency valves for pulsing space engines such as the Pulse Inductive Thrusters. These units require valves that operate a flow rates and pulse frequencies similar to the current ACCV. In addition they require very long life, as these low force thrusters operate for very long periods of time. The effort being proposed will provide solutions that are applicable to both of these applications.
The valve has a direct application to active combustion control in gas turbines. The valve allows precise time dependent fuel control required for lean-burn combustor operability. The small size, internal cooling capability and high frequency modulation capability of 1,000 Hz makes it directly applicable for use in this application. The benefit of harsh environment operation is the ability to maximize the flow modulation control authority due to close proximity to the fuel injector. The valve also has application to combustion stability control in commercial liquid fueled rocket engines. Using active combustion control in rocket engines has the potential to save millions of dollars in development costs and reduce development schedules
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