Patent application number | Description | Published |
20130064688 | Integrated Direct Drive Starter/Generator for Turbines - A starter/generator machine for a turbine with a turbine enclosure, an air duct, and a plurality of fan blades is provided. The starter/generator machine includes a plurality of stator elements spaced at intervals in a ring shape adjacent to the air duct and a plurality of rotor elements mounted on the fan blades. The stator elements and the rotor elements are mounted to interact magnetically to exert a force sufficient to move the rotor elements. The stator elements are shaped to minimize air flow interference and are formed with a core, at least one pole, and multiple windings. The spacing between the stator elements and the rotor elements forms an air gap on the order of 5-10 mm, and the number of stator elements is different from the number of rotor elements. | 03-14-2013 |
20130104949 | THERMOELECTRIC CONVERTER DEVICES | 05-02-2013 |
20130112806 | DRIVE SYSTEM WITH HARMONIC DRIVE FOR SELF-PROPELLED AIRCRAFT WHEEL - A drive system with harmonic drive designed to meet the high power and torque requirements required to drive an aircraft independently on the ground is provided. The drive system includes an electric motor driven by a harmonic drive assembly that may be configured to be integral with the motor. This drive system with harmonic drive can be effectively installed in an existing aircraft nose wheel or main wheel without changes to other components. | 05-09-2013 |
20130126711 | LOW LIGHT VISION AND THERMAL IMAGING DEVICES WITH COOL CHIP COOLING - Improved low light vision and thermal imaging devices are provided. The devices of the present invention employ thermionic or thermotunneling cooling, with or without Avto Metals™, to ensure efficient operation under conditions of low illumination or the complete absence of illumination to detect emitted or reflected infrared and visible light radiation, significantly reducing thermal noise to produce superior image resolution and sensitivity within a small, lightweight footprint that will have a wide range of military, law enforcement, civilian, and other applications. | 05-23-2013 |
20130314545 | LOW LIGHT VISION AND THERMAL IMAGING DEVICES WITH COOL CHIP COOLING - Improved low light vision and thermal imaging devices are provided. The devices of the present invention employ thermionic or thermotunneling cooling, with or without Avto Metals™, to ensure efficient operation under conditions of low illumination or the complete absence of illumination to detect emitted or reflected infrared and visible light radiation, significantly reducing thermal noise to produce superior image resolution and sensitivity within a small, lightweight footprint that will have a wide range of military, law enforcement, civilian, and other applications. | 11-28-2013 |
Patent application number | Description | Published |
20090280050 | Apparatus and Methods for Casting Multi-Crystalline Silicon Ingots - Apparatuses and methods for making a multi-crystalline silicon ingot by directional solidification comprising two or more moveable heat shields located beneath the crucible, the heat shields being opened in a controlled manner to remove heat and produce a high quality silicon ingot. | 11-12-2009 |
20090288591 | Crystal Growth Apparatus for Solar Cell Manufacturing - The present invention(s) provide an apparatus for forming a rod, which is also sometimes referred to as an ingot or boule, which can be subsequently diced to form multiple substrates that may be utilized to form a solar cell device. The substrate may be a monocrystalline, or polycrystalline, substrate made by use of a CZ type crystal pulling technology. In one embodiment, the crystal pulling apparatus is used to form a substrate used form a solar cell device. In one embodiment, a feed material is delivered to a crucible using a vibratory feeder assembly and is heated using a novel heater assembly to allow a CZ type crystal pulling process to be performed. | 11-26-2009 |
20130119190 | Motor for Driving Aircraft, Located Adjacent to Undercarriage Wheel - The invention disclosed is a self-propelled aircraft undercarriage for driving an aircraft on the ground, comprising: an axle; a strut supporting said axle; at least one wheel rotatably mounted on said axle; and drive means for driving said at least one wheel; characterized in that said drive means is disk shaped and is external to said wheel. In one embodiment of the invention, said drive means is mounted on said axle between said strut and said wheel. In a second embodiment, said drive means is mounted on said axle, on the side of said wheel furthest from said strut. | 05-16-2013 |
Patent application number | Description | Published |
20090009011 | Motor using magnetic normal force - A motor is disclosed comprising: at least one stator comprising a magnetic core and at least one magnetic winding, having a cylindrical internal cavity; at least one cylindrical rotor inside said stator, comprising magnetically conductive materials; said rotor having an outer diameter significantly smaller than the inner diameter of said stator, being eccentrically mounted with respect to said stator and able to move within, said fixed member; wherein magnetic normal force is induced in said stator periodically, whereby said rotor is periodically moved by magnetic force with respect to said stator, whereby rotary motion is produced; said motor further having: an output shaft concentric with said stator; transmission means for absorbing oscillation and transmitting rotation; wherein said induced magnetic normal force rotates around the circumference of said stator, such that a contact patch between said rotor and said stator rotates around the inner circumference of said stator; whereby said rotor oscillates and rotates; whereby said transmission means absorb the oscillation of said rotor and transmit the rotation of said rotor to said output shaft; wherein said transmission means is magnetorheostatic fluid. A motor is further disclosed wherein said transmission means comprise bearings and carrier supports, wherein said bearings are used as a clutch. | 01-08-2009 |
20090079297 | Monolithic thermionic converter - A thermionic converter is disclosed comprising a single or multiple hot (emitter) and cold (collector) electrodes mounted side-by-side on a single substrate and a static electromagnetic for guiding electrodes from the emitter to the collector. The thermal path between emitter and collector electrodes is interrupted by cuts or trenches, and electrical connections to the electrodes are routed over a meander-like, high thermal resistance pathway cut into the substrate to further reduce thermal loss. In one embodiment, an Avto metal surface texture of nanoscale indents is provided on one or more of the electrodes to lower a work function. A method for fabricating said monolithic thermionic converter is further disclosed. | 03-26-2009 |
20090114765 | Motor for driving aircraft, located adjacent to undercarriage wheel - The invention disclosed is a self-propelled aircraft undercarriage for driving an aircraft on the ground, comprising: an axle; a strut supporting said axle; at least one wheel rotatably mounted on said axle; and drive means for driving said at least one wheel; characterized in that said drive means is disk shaped and is external to said wheel. In one embodiment of the invention, said drive means is mounted on said axle between said strut and said wheel. In a second embodiment, said drive means is mounted on said axle, on the side of said wheel furthest from said strut. | 05-07-2009 |
20090126369 | Integrated direct drive starter/generator for turbines - A turbine starter/generator machine for a turbine, said turbine comprising: at least one fan blade; at least one turbine enclosure; said starter/generator machine comprising: at least one rotor having rotor elements; at least one stator having stator elements; wherein said stator elements are mounted on said at least one air duct and said rotor elements are mounted on said at least one fan blade; whereby said stator elements magnetically interact with said rotor elements. | 05-21-2009 |
20090127549 | Composite structure gap-diode thermopower generator or heat pump - A thermionic or thermotunneling generator or heat pump is disclosed, comprising electrodes substantially facing one another and separated by spacers disposed between the electrodes, wherein the substrate material for the cathode is preferably a single crystalline silicon wafer while the substrate for the anode is an organic wafer, and preferably a polished polyimide (PI) wafer. On the cathode side, standard silicon wafer processes create the 10-1000 nm thin spacers and edge seals from thermally grown oxide. Either wafer is partially covered with a thin film of material that is characterized by high electrical conductivity and low work function. In one embodiment, the cathode is partially covered with a thin film of Ag—Cs—O. In another embodiment, the anode is additionally covered with a thin film of Ag—Cs—O, in which case the work function of the cathode coating material is reduced further utilizing an Avto Metal structure of nanoscale patterned indents. A method for fabricating said composite structure device is further disclosed. | 05-21-2009 |