Abstract: An apparatus and a method are disclosed for measuring a characteristic of an analyte particle. An apparatus for measuring a characteristic of an analyte particle includes a heat flux sensor configured to be maintained at a temperature. The heat flux sensor includes first and second electrical connections, and a top interconnect membrane bridging the first and second electrical connections. The apparatus further includes an emitter configured to eject an analyte particle to cause the analyte particle to collide with the top interconnect membrane of the heat flux sensor.

Abstract: NMSET and related device uses and improvements to the forces generated. Laminar flow control systems benefit from NMSET and related devices as they simplify installation and are easier to retrofit on existing aircraft. Necessary temperature gradients can me generated by using a heated material with the sides at different energy accommodation coefficients. Surface geometries can be used to increase the force generated. Photovoltaic film can be embedded into the membrane, providing a source of energy that can offset the power required for desired thrust. Intake scoops improve the air flow through the micro thrusters and surface geometries, and airflow diffusers increase air flow interaction with the hotter surface resulting in higher thrust outputs.

Abstract: An apparatus that is capable of propelling a gas includes a first layer and a second layer arranged in a stack, mechanism for heating and/or cooling the first layer and the second layer to form a hot layer and a cold layer, and a through hole in the stack. A surface of both the hot layer and the cold layer is exposed in an interior of the through hole. The mechanism for heating and/or cooling the first and second layers controls the hot layer to be hotter than an ambient temperature of the gas, and the cold layer to be colder than the ambient temperature of the gas.

Abstract: A thermal transpiration device and method of making the same. The device includes a pair of membranes having predetermined thicknesses in order to provide the device with strength and rigidity. The thickness of a portion of each membrane is reduced in the area where thermal transpiration occurs in order to optimize the effectiveness of the thermal transpiration device without scarifying structural integrity of the device.

Abstract: Conveying systems and methods are provided that selectively controls gas-propelling devices to move objects over the conveyer table at different speeds and in different directions. The systems and methods include a conveyer table having of an array of gas-propelling devices that propel gas from a surface of the table. Each of the of gas-propelling devices can have layers arranged in a stack and a through-hole in the stack and the table. The surfaces of each of the layers are exposed in the interior of the through hole and a heating/cooling device selectively heats and/or cools the layers to generate thrust.

Abstract: A replaceable thrust generating structure for an air vehicle, which includes one or more mounts, which are attachable to the air vehicle, and a thrust generating structure attached to each of the one or more mounts, and wherein the thrust generating structure includes an NMSET element.

Abstract: A distributed thruster based gas compressor, the compressor including an enclosed housing having an inlet aperture exposed to a source of ambient gas; at least one pressure producing device formed over the inlet aperture and adapted to produce a pressure, the pressure producing device being formed of distributed thrusters, such as Nano Molecular Solid-state Electrodynamics Thrusters (NMSETs); a control unit coupled to the first pressure producing device; and wherein the control unit controls the pressure producing device to produce the pressure to cause the ambient gas to be compressed in the housing.

Abstract: Apparatus and methods for generating a partial vacuum in a cavity are disclosed. In one method, a suction unit is disposed on a surface and includes a plurality of embedded suction generation devices that suction gas therethrough. The suction generating devices are powered-on to form a cavity defined by at least the surface and the suction unit and gas is evacuated from the cavity to generate the partial vacuum.

Abstract: A method and apparatus to control movement of a vehicle using a plurality of thrust-producing devices formed in at least one control surface is disclosed. A supply of power to the plurality of thrust-producing devices that are configured to propel gas through the control surface to produce thrust is controlled such that a physical displacement of the control surface is generated. The physical displacement is in accordance with the supply of power to the plurality of thrust-producing devices and controls the movement of the vehicle.

Abstract: A non-fouling, bypass filter is disclosed. The filter is formed of a tapered structure having particulate material filtering properties. The tapered structure has an open base and a closed top, with its exterior surface being exposed to a gas/fluid stream to be filtered. A gas/fluid stream generating device generates a gas/fluid stream that is drawn into the tapered structure's interior and that is filtered due to the particulate material filtering properties of the tapered structure. The external profile of the conically shaped structure is adapted to cause a plurality of gas/fluid streams from the ambient gas/fluid to flow against the exterior surface of the tapered structure to prevent the building up of particulate material on the exterior surface.

Abstract: A solid-state device that is capable of imparting a directional momentum via thermoelectric microelements. High surface area is used to enhance the efficiency of heat transfer. The device can be operated in adiabatic mode in order to minimize thermal emissions.

Abstract: NMSET and related device uses and improvements to the forces generated. Laminar flow control systems benefit from NMSET and related devices as they simplify installation and are easier to retrofit on existing aircraft. Necessary temperature gradients can me generated by using a heated material with the sides at different energy accommodation coefficients. Surface geometries can be used to increase the force generated. Photovoltaic film can be embedded into the membrane, providing a source of energy that can offset the power required for desired thrust. Intake scoops improve the air flow through the micro thrusters and surface geometries, and airflow diffusers increase air flow interaction with the hotter surface resulting in higher thrust outputs.

Abstract: A method and device for creating a temperature gradient among a plurality of temperature gradient devices. Each device is formed of a first layer of conductive material having a top surface and a bottom surface. The first layer is adjacent to a second layer of conductive material and has electrical resistive heating properties. A power supply is used to provide a current flow through at least the first layer when the power supply is activated. When activated, the resulting current flow causes the second layer to heat and thus create a temperature gradient between the bottom surface of the second layer and the top surface of the first layer. Activation of the power supply is controlled by a control unit so that activation of adjacent temperature gradient devices is avoided for a predetermined time after activation of the first temperature gradient device.

Abstract: A movable support platform is disclosed that includes a platform, a skirt coupled to a periphery of the platform that provides an enclosed space below the platform that retains pressurized gas, and a thrust propulsion device coupled to the platform for pressurizing gas in the enclosed space. The thrust propulsion device includes an array of gas-propelling devices “distributed thrusters” that propel gas into the enclosed space below the platform. The distributed thrusters may be comprised of Nano Molecular Solid-state Electrodynamic Thrusters (“NMSET”).

Abstract: A solid-state device that is capable of imparting a directional momentum via thermoelectric microelements. High surface area is used to enhance the efficiency of heat transfer. The device can be operated in adiabatic mode in order to minimize thermal emissions. The thermoelectric microelements include at least a hot layer and a cold layer arranged in a stack and means for heating and/or cooling the hot and cold layers so that the cold layer has a lower temperature than the hot layer; and at least one through hole in the stack wherein an entire length of the through hole is up to 10 times of a mean free path of a gas in which the device is immersed and/or is not greater than 1500 nm.

Abstract: A movable support platform is disclosed that includes a platform, a skirt coupled to a periphery of the platform that provides an enclosed space below the platform that retains pressurized gas, and a thrust propulsion device coupled to the platform for pressurizing gas in the enclosed space. The thrust propulsion device includes an array of gas-propelling devices “distributed thrusters” that propel gas into the enclosed space below the platform. The distributed thrusters may be comprised of Nano Molecular Solid-state Electrodynamic Thrusters (“NMSET”).

Abstract: A distributed thruster based gas compressor, the compressor including an enclosed housing having an inlet aperture exposed to a source of ambient gas; at least one pressure producing device formed over the inlet aperture and adapted to produce a pressure, the pressure producing device being formed of distributed thrusters, such as NMSET; a control unit coupled to the first pressure producing device; and wherein the control unit controls the pressure producing device to produce the pressure to cause the ambient gas to be compressed in the housing.

Abstract: A replaceable thrust generating structure for an air vehicle, which includes one or more mounts, which are attachable to the air vehicle, and a thrust generating structure attached to each of the one or more mounts, and wherein the thrust generating structure includes an NMSET element.

Abstract: A non-fouling, bypass filter is disclosed. The filter is formed of a tapered structure having particulate material filtering properties. The tapered structure has an open base and a closed top, with its exterior surface being exposed to a gas/fluid stream to be filtered. A gas/fluid stream generating device generates a gas/fluid stream that is drawn into the tapered structure's interior and that is filtered due to the particulate material filtering properties of the tapered structure. The external profile of the conically shaped structure is adapted to cause a plurality of gas/fluid streams from the ambient gas/fluid to flow against the exterior surface of the tapered structure to prevent the building up of particulate material on the exterior surface.

Abstract: A thermal transpiration device and method of making the same. The device includes a pair of membranes having predetermined thicknesses in order to provide the device with strength and rigidity. The thickness of a portion of each membrane is reduced in the area where thermal transpiration occurs in order to optimize the effectiveness of the thermal transpiration device without scarifying structural integrity of the device.