Abstract: A drive circuit for a plurality of piezo-actuated hydraulic pumps for an aircraft, and a hydraulic pump system implementing the same. The drive circuit includes a voltage boost stage that receives a DC input supply voltage and delivers an increased DC output voltage to a high voltage, HV, link point; a plurality of inverter stages coupled in parallel at the HV link point that receive DC voltage from the HV link point and generate an oscillating output voltage for driving a respective piezo-actuated pump; and a control system that controls the output voltage and phase of the inverter stages to drive the plurality of piezo-actuated pumps out of phase. The control system measures the power consumption of each piezo-actuated pump and regulates the output voltage of at least one of the inverter stages to balance the power consumption of each piezo-actuated pump.

Abstract: The present invention is a quick connect receiver adapter assembly for an automatic or semi-automatic rifle, specifically the AR-15 assault rifle. The adapter system is used to quickly exchange barrels on an AR-15 rifle platform, and allows the user to convert the AR-15 from a single caliber weapon to a multi-caliber weapon. The system has a receiver attached portion comprising a three piece locking ring assembly, and separate barrel adapter assembly which can be attached to any caliber barrel suitable for use with the AR-15 assault rifle.

Abstract: The present invention is a quick connect receiver adapter assembly for an automatic or semi-automatic rifle, specifically the AR-15 assault rifle. The adapter system is used to quickly exchange barrels on an AR-15 rifle platform, and allows the user to convert the AR-15 from a single caliber weapon to a multi-caliber weapon. The system has a receiver attached portion comprising a three piece locking ring assembly, and separate barrel adapter assembly which can be attached to any caliber barrel suitable for use with the AR-15 assault rifle.