Abstract: A charged particle induction apparatus and method comprising a high power light emitting means, such as a laser array, in operable communication with a high energy output means to accomplish initiation of at least two concentric plasma channels in atmosphere extending from the Earth's surface to the charge-rich upper atmosphere, including the ionosphere, for the transmission of charged particles therethrough to ground using the surrounding atmosphere as an insulator. The transmitted energy is drawn down (due to an artificially created potential) through the conductive plasma channels to collection means.

Abstract: A closed plasma channel (“CPC”) superconductor which, in a first embodiment, is comprised of an elongated, close-ended vacuum conduit comprising a cylindrical wall having a longitudinal axis and defining a transmission space for containing an ionized gas of vapor plasma (hereinafter “plasma components”), the plasma components being substantially separated into regionalized channels parallel to the longitudinal axis in response to a static magnetic field produced within the transmission space. Each channel is established along the entire length of the transmission space. At least one channel is established comprised primarily of free-electrons which provide a path of least resistance for the transmission of energy therethrough. Ionization is established and maintained by the photoelectric effect of a light source of suitable wavelength to produce the most conductive electrical transmission medium.

Abstract: A closed plasma channel (“CPC”) superconductor which, in a first embodiment, is comprised of an elongated, close-ended vacuum conduit comprising a cylindrical wall having a longitudinal axis and defining a transmission space for containing an ionized gas of vapor plasma (hereinafter “plasma components”), the plasma components being substantially separated into regionalized channels parallel to the longitudinal axis in response to a static magnetic field produced within the transmission space. Each channel is established along the entire length of the transmission space. At least one channel is established comprised primarily of free-electrons which provide a path of least resistance for the transmission of energy therethrough. Ionization is established and maintained by the photoelectric effect of a light source of suitable wavelength to produce the most conductive electrical transmission medium.

Abstract: A method and apparatus for transmission of charged particles along a laser-induced conduction path of concentric plasma channels in atmosphere. The apparatus comprises a high power laser array in operable communication with a high energy output means to accomplish initiation of at least two concentric plasma channels in atmosphere, a second energy source for outputting the charged particles to be transmitted, and means for introducing the charged particles to be transmitted into the wall of at least one of the laser-induced conduction channels. Other embodiments further include means for inducing the energy across the conduction path to a target capable of receiving and storing the energy, and a plurality of charging rods bearing a negative or positive charge and in communication with each conductive channel for shaping and stabilizing the charge transmitted therethrough.

Abstract: A charged particle induction apparatus and method comprising a high power light emitting means, such as a laser array, in operable communication with a high energy output means to accomplish initiation of at least two concentric plasma channels in atmosphere extending from the Earth's surface to the charge-rich upper atmosphere, including the ionosphere, for the transmission of charged particles therethrough to ground using the surrounding atmosphere as an insulator. The transmitted energy is drawn down (due to an artificially created potential) through the conductive plasma channels to collection means.

Abstract: An actuator assembly includes a motor assembly, a harmonic drive gearbox, an actuator, and an electromagnet brake device. The actuator assembly is fairly compact in size and the electromagnetic brake device is a non-contact type of devices, making it less prone to wear as compared to many other brake devices.

Abstract: An actuator assembly includes a motor assembly, a harmonic drive gearbox, an actuator, and an electromagnet brake device. The actuator assembly is fairly compact in size and the electromagnetic brake device is a non-contact type of devices, making it less prone to wear as compared to many other brake devices.

Abstract: An aircraft engine starter assembly provides for liquid cooling of the clutch assembly and overrunning engine by integrating a pitot pump in the system. The system includes a starter motor, a torque transfer connection, a clutch assembly and the pitot pump. The torque transfer connection is adapted to be coupled to the aircraft engine. The clutch assembly is coupled to one of the starter motor or the torque transfer connection. The pitot pump is coupled to one or both of the torque transfer or the clutch assembly via a first oil line and a second oil line. The pitot pump comprises a pitot tube in fluidic communication with an oil reservoir for the delivery of oil under pressure to lubricate one or both of the torque transfer or the clutch assembly.

Abstract: A turbofan gas turbine propulsion engine includes a multi-speed transmission between the high pressure and low pressure turbines and associated high pressure and low pressure starter-generators. The multi-speed transmission reduces the operating speed range from the low pressure turbine to its associated starter-generator, and is configurable to allow the starter-generator associated with the low pressure turbine to supply starting torque to the engine.

Abstract: The present invention provides an apparatus for providing a visual indication of oil pressure comprising: a housing defining an exterior and an interior region wherein the interior region defines a sealing surface of the housing, the housing further defining an inlet providing fluid communication between the interior region of the housing and the exterior of the housing; a piston moveably disposed within the interior region of the housing so as to slide between a pressurized position and a depressurized position; a piston face defined by the piston wherein the piston face receives oil pressure admitted through the inlet and into the interior region of the housing; at least one low friction seal disposed on the piston so as to provide a sealing engagement between the piston and the sealing surface of the interior region of the housing; a visual indicator connected to the piston so that the visual indicator displays a visual indication of oil pressure when the piston is in the pressurized position; and a spring

Abstract: A compressor system that is configured to compress the fluid from low pressure source to a higher pressure magnitude is powered from the same low pressure fluid source. The compressor system includes two piston assemblies that are coaxially coupled to one another, and that are of differing cross sectional areas. The low pressure fluid is used to move the larger piston assembly, which is in turn used to move the smaller piston assembly. Low pressure fluid is selectively admitted to the smaller piston assembly, and movement thereof is used to compress the low pressure fluid to a higher pressure magnitude. The compressor system uses a fluidic bistable amplifier, which also coupled to the low pressure fluid source, to control low pressure fluid flow to the larger piston assembly, to thereby control its movement.

Abstract: Methods and apparatus are provided for monitoring an aircraft accessory. The apparatus comprises a processor associated with said aircraft accessory, a transducer coupled to said processor and operable to produce parametric data relating to said aircraft accessory and a memory coupled to said processor having baseline parametric data residing therein, wherein said baseline parametric data comprises the parametric data obtained during an acceptance test procedure. The method comprises installing a transducer configured to produce parametric data relating to said aircraft accessory, coupling said transducer to a processor associated with said aircraft accessory, coupling said processor to a memory associated with said aircraft accessory, recording baseline parametric data relating to said aircraft accessory in said memory during an acceptance test procedure for said aircraft accessory.

Abstract: An air turbine starter valve able to open despite being frozen shut. Dual actuators apply sufficient torque upon an air turbine starter valve to overcome obstructions presented by frozen moisture. By applying separate and generally-aligned torques, the actuators are able to provide sufficient force to overcome the adhesion provided by frozen moisture between the valve plate and adjacent structures.

Abstract: An air turbine starter valve able to open despite being frozen shut. Dual actuators apply sufficient torque upon an air turbine starter valve to overcome obstructions presented by frozen moisture. By applying separate and generally-aligned torques, the actuators are able to provide sufficient force to overcome the adhesion provided by frozen moisture between the valve plate and adjacent structures.