Patent application number | Description | Published |
20090324438 | Variable flow pumping system - A variable displacement pump and pump control system therefor to pump a fluid at selected pump output flow rates having a variable displacement pump and a fluid volume displacement selection controller to select a volume of fluid to be forced from the pump inlet to the pump outlet by the rotating member during a rotation thereof. A movable lead screw is coupled to the displacement selection controller so as to be capable of altering the position thereof, and a lead screw positioner is provided for selectively moving, or preventing the moving of, the movable lead screw by extending and retracting the lead screw through a threaded opening. | 12-31-2009 |
20110033190 | DIGITAL HARNESS WITH ANALOG INPUTS - A digital data harness, uses a signal specific conditioning circuit to interface with analog sensors. The signal specific conditioning circuits convert data signals from analog to digital and thereby allow the signals to be transmitted over a digital data harness. | 02-10-2011 |
20110139270 | THERMAL SWITCHED COOLING ORIFICE FOR ACTUATION SYSTEMS - An actuator includes features that reduce the energy drawn from the engine by reducing and/or eliminating the flow requirement during normal operating conditions. A normally closed cooling orifice opens responsive to an elevated temperature to allow cooling fluid flow. Once the temperature returns to normal ranges, the thermally expanding material retracts and the valve returns to a closed position to stop cooling flow. | 06-16-2011 |
20110302903 | LUBRICATION DRIVEN GAS TURBINE ENGINE ACTUATION SYSTEM - A lubrication system for a gas turbine engine includes a variable output lubricant pump operable to supply lubricant to an actuator system. | 12-15-2011 |
20120063879 | ENERGY EFFICIENT IPS BLOWER ASSEMBLY - According to the invention a method and apparatus relating to a blower that is used in an environment of particle contaminated air, as with a helicopter engine, is disclosed. The blower has a power input, a fan, a power output attaching to the fan, and a clutch disposed between the power input and the power output whereby the power input may be selectively coupled to the power output to move the fan to vent the particle contaminated air. The clutch, which may be electrically, mechanically or hydraulically engaged, is activated by a user, a particle or altitude sensor, or by a full authority digital electronic controller (“FADEC”). | 03-15-2012 |
20140109584 | MODULATING ELECTRIC LIQUID METERING VALVE WITH FLOW SENSING - A fluid flow valve includes a movable valve piston positioned in a valve body, the valve piston configured to flow a fluid therethrough. A metering window is interactive with the movable valve piston to meter flow through the movable valve piston. A flow meter is positioned at the valve piston to measure a flow rate of fluid through the valve piston. A valve controller is operable connected to the flow meter and the movable valve piston to control position of the valve piston based on flow rate measured at the flow meter. | 04-24-2014 |
20140216245 | HIGH GAIN SERVO VALVE - A servo valve includes a movable throttling member positioned between a first opening and an opposing second opening, and a first inlet port and a second inlet port to convey a fluid flow toward the first and opening, respectively. A first inlet orifice, defined between the first inlet port and a first pressure reaction member, is located between and in fluid communication with the first inlet port and the first opening. A second inlet orifice, is located between and in fluid communication with the second inlet port and the second opening. The second pressure reaction member is secured to the first pressure reaction member at a substantially fixed distance. Each of the first inlet orifice and the second inlet orifice is variable via a change a pressure of the fluid flow downstream of the first inlet orifice and the second inlet orifice. | 08-07-2014 |
20140290266 | FUEL AND ACTUATION SYSTEM FOR GAS TURBINE ENGINE - A fuel system for an aircraft comprises a boost pump, a main fuel pump and a motive pump. The boost pump receives fuel from a storage unit. The main fuel pump receives fuel from the boost pump and delivers fuel to a distribution system. The motive fuel pump receives fuel from the boost pump, routes fuel through the storage unit, and delivers fuel to an actuator. A method for delivering fuel in an aircraft comprises pumping fuel from a fuel tank to a distribution system using a main pump, pumping fuel from a fuel tank to an actuator using a motive pump, and routing fuel from the actuator to the main pump | 10-02-2014 |
20140324238 | SELF POWERED FLUID METERING UNITS - A system includes a metering module that receives fluid through a fluid inlet. The metering module includes a rotating component driven by the fluid, an electric machine, and a controller. The fluid is received from the fluid inlet at an inlet flow rate, and the rotating component provides the fluid to an outlet of the rotating component at an outlet pressure. The electric machine is configured to generate electrical power in response to rotation of the rotating component. The controller is powered by the electrical power generated by the electric machine, and controls a rotational speed of the rotating component to control the outlet pressure. | 10-30-2014 |
20150023776 | FLUID COOLING ARRANGEMENT FOR A GAS TURBINE ENGINE AND METHOD - A fluid cooling arrangement in a gas turbine engine for aerospace propulsion includes an inner structure. Also included is an outer structure disposed radially outwardly of the inner structure, the outer structure and the inner structure defining a bypass flow path. Further included is at least one strut operatively coupling the inner structure to the outer structure. Yet further included is at least one cooling tube formed within the at least one strut, the at least one cooling tube configured to cool a fluid passing through the at least one cooling tube upon convective cooling of the at least one strut as air passes through the bypass flow path and over the at least one strut. | 01-22-2015 |
20150027669 | HEAT EXCHANGER WITH EMBEDDED HEAT PIPES - A heat exchanger is disclosed which includes a plurality of heat exchanger plates. Each plate has a plurality of hollowed out pins arranged in a pin fin pattern. Each plate also includes an inlet aperture and an outlet aperture in fluid communication with one another. A plurality of heat pipes are defined by several of the plurality of hollowed out pins. A wicking material is arranged within the several hollowed out pins. A heat transfer fluid at least partially fills each heat pipe. | 01-29-2015 |
20150034278 | HEAT PIPE MATRIX FOR ELECTRONICS COOLING - A heat pipe system and methods of arranging a heat pipe system are provided. The heat pipe system includes a plurality of heat pipes, with each of the plurality of heat pipes including a hot end thermally coupled to a heat source and a cold end thermally coupled to a heat sink The plurality of heat pipes include a first pair of heat pipes. When the plurality of heat pipes are secured to a rotatable body, the first pair of heat pipes are aligned with and oriented in opposing directions along a first axis of rotation of the rotatable body. | 02-05-2015 |
20150048617 | HEATED BYPASS VALVE FOR HEAT EXCHANGER - A heat exchanger bypass system comprises a liquid circuit, a first fluid circuit, a second fluid circuit, a first heat exchanger, a second heat exchanger, a liquid bypass line and a heated bypass valve. The first heat exchanger thermally couples the first fluid circuit to the liquid circuit. The second heat exchanger thermally couples the second fluid circuit to the liquid circuit. The liquid bypass line circumvents the first heat exchanger. The heated bypass valve controls flow through the liquid bypass line. | 02-19-2015 |