Abstract: Provided is a method and apparatus for the identification of one or more liquid and/or gaseous components in a fluid using Electrochemical Impedance Spectroscopy with a wide range of frequencies. In the preferred embodiment the method of measuring the concentration and/or constituents of a sample including heavy metal ions, uses two or more frequency bands. The measurements from the first frequency band are combined with measurements in the second frequency band such that the concentration of a certain constituent is established in real time (or near real time). A-priori knowledge is used in the combination, and the a-priori knowledge is related to measurements of certain materials at earlier times.

Abstract: A Process Energy Intensity Monitoring and Diagnostic System designed to evaluate the amount of energy input into a process and the resulting product output, and comparing the resulting energy intensity (energy per unit produced) calculation with a statistical average, or preferred value. Further, the system will isolate energy intensity data points that occur outside statistically derived upper or lower control limits. The system will collect information from specific equipment within a manufacturing or production process. This information will be transmitted to the central database that will store, calculate, and deliver real time and historical consumption, production, and energy intensity data to connected client devices. Client devices may include computers, smartphones, or web browsers.

Abstract: An automatic test equipment (ATE) unit, which incorporates a mass interconnect system. The mass interconnect system is provided with a universal mounting table for use with receiver and test interface modules for electronically mounting and testing a variety of different types of electronic components or unit under test thereon. The mounting table test interface module incorporates MEMS based spring contacts to provide high-speed micro test-channels in order to establish signal connectivity between the components or unit under test and the tester, and which maintain the signal integrity up to 50 GHz without significant signal loss distortion.

Abstract: A Process Energy Intensity Monitoring and Diagnostic System designed to evaluate the amount of energy input into a process and the resulting product output, and comparing the resulting energy intensity (energy per unit produced) calculation with a statistical average, or preferred value. Further, the system will isolate energy intensity data points that occur outside statistically derived upper or lower control limits. The system will collect information from specific equipment within a manufacturing or production process. This information will be transmitted to the central database that will store, calculate, and deliver real time and historical consumption, production, and energy intensity data to connected client devices. Client devices may include computers, smartphones, or web browsers.

Abstract: An automatic test equipment (ATE) unit, which incorporates a mass interconnect system. The mass interconnect system is provided with a universal mounting table for use with receiver and test interface modules for electronically mounting and testing a variety of different types of electronic components or unit under test thereon. The mounting table test interface module incorporates MEMS based spring contacts to provide high-speed micro test-channels in order to establish signal connectivity between the components or unit under test and the tester, and which maintain the signal integrity up to 50 GHz without significant signal loss distortion.

Abstract: Disclosed is a fuel composition for the control and/or removal of persistent engine deposits. Said fuel composition comprises a major amount of hydrocarbons boiling in the gasoline range fuel, a hydrocarbyl-substituted polyoxyalkylene amine and a glycol ether component; and is useful for the prevention and control engine deposits.

Abstract: The first-stage buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table I wherein Z is a perpendicular distance from a plane normal to a radius of the turbine centerline and containing the X and Y values with the Z value commencing at zero in the X, Y plane at the radially innermost aerodynamic section of the airfoil and X and Y are coordinates defining the airfoil profile at each distance Z. The X, Y and Z values may be scaled as a function of the same constant or number to provide a scaled-up or scaled-down airfoil section for the bucket.

Abstract: The second-stage buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in inches in Table I wherein Z is a perpendicular distance from a plane normal to a radius of the turbine centerline and containing the X and Y values with the Z value commencing at zero in the X, Y plane at the radially innermost aerodynamic section of the airfoil and X and Y are coordinate values defining the airfoil profile at each distance Z. The X, Y and Z values may be scaled as a function of the same constant or number to provide a scaled-up or scaled-down airfoil section for the bucket.