| Patent application number | Description | Published |
|---|
| 20100083745 | Method of Dynamically Measuring Stiffness of a Wheel and Tire Assembly - A test machine and method for dynamically testing a tire/wheel assembly. A first laser measurement gage is directed to an inboard rim flange of the wheel to measure radial deflection of the tire/wheel assembly. A second laser measurement gage is directed to the inboard rim flange to measure axial deflection of the tire/wheel assembly. Displacement data and loading data are correlated to provide values for lateral stiffness, radial stiffness and ride stiffness. | 04-08-2010 |
| 20110081229 | METHOD FOR ATTACHING A CONNECTOR TO DEPOSITED MATERIAL - A method for attaching a connector to deposited material includes the steps of depositing material on a substrate using a thin- or thick-film deposition process and attaching at least one connector to the deposited material using a high energy beam welding process. | 04-07-2011 |
| 20120096933 | SENSOR WITH G-LOAD ABSORBING SHOULDER - A sensor is provided and includes a body disposed at a point of measurement interest on a rotor at a radial distance from a centerline thereof and having a substantially cylindrical shape and first and second opposing ends and a sensing end coupled to one of the first and second opposing ends, the other of the first and second opposing ends being coupled to a communication system, the sensing end including a sensing device configured to generate a signal reflective of a detected condition at the point of measurement interest, and at least one of the first and the second opposing ends being formed to define a shoulder portion for absorbing gravitational loading. | 04-26-2012 |
| 20120096934 | COMMUNICATION SYSTEM FOR TURBINE ENGINE - A communication system is provided and includes a sensor to measure a condition at a point of measurement interest defined on a rotor of a turbine at a radial distance from a centerline about which the rotor is rotatable, wiring disposed on the rotor at a radial distance from the centerline, the wiring including a first wiring section coupled to the sensor, a second wiring section and a first connection by which the first and second wiring sections are connectable, a second connection by which the second wiring section transmits a signal reflective of the detected condition to a non-rotating recording element and a temperature compensation module disposed on the second wiring section to adjust the signal. | 04-26-2012 |
| 20120096946 | SENSOR PACKAGING FOR TURBINE ENGINE - A turbine is provided and includes a rotor, which is rotatable about a centerline thereof, a sensor to measure a condition at a point of measurement interest defined on the rotor at a radial distance from the centerline, a communication system by which condition measurements are transmittable from the sensor to a non-rotating recording system and a probe holder to secure the sensor and a portion of the communication system on the rotor proximate to the point of measurement interest. | 04-26-2012 |
| 20120096961 | PROBE HOLDER FOR TURBINE ENGINE SENSOR - A turbine is provided and includes a component having a body, which is rotatable about a rotor centerline and which is formed to define a cavity radially proximate to a point of measurement interest defined at a radial distance from the centerline, a sensor to measure a condition at the point of measurement interest, a communication system by which condition measurements are transmittable from the sensor to a non-rotating recording system and a probe holder insertible into the cavity to secure the sensor proximate to the point of measurement interest. | 04-26-2012 |
| 20120128468 | SENSOR ASSEMBLY FOR USE WITH A TURBOMACHINE AND METHODS OF ASSEMBLING SAME - A method for assembling a sensor assembly for use with a turbomachine is provided. The method includes providing a cover that includes a first portion and a second portion that extends from the first portion. A cavity is defined within the first portion. Moreover, a sensing device that is configured to measure at least one variable of a component of the turbomachine is inserted into the cavity. The second portion is removably coupled to a surface of the turbomachine component such that the cover securely couples the sensing device to the turbomachine component. | 05-24-2012 |
| 20120171037 | PROBE ASSEMBLY FOR USE IN TURBINE ENGINES AND METHOD OF ASSEMBLING SAME - A method of assembling a probe assembly is provided. At least one probe is coupled to an annular tube, wherein the tube includes an interior surface and an exterior surface. The tube also includes at least one first opening that extends between the interior and exterior surfaces and at least one second opening that extends between the interior and exterior surfaces. Moreover, at least one annular flange is coupled to the tube. The flange has a substantially elliptical shape that facilitates substantially preventing the relative rotation of the tube. | 07-05-2012 |
| 20120285237 | INSTRUMENTATION RAKE ASSEMBLY - An instrumentation rake assembly comprises a rake tower capped at an immersed end and mated to a lead carrier at a base end. The rake tower comprises a curved wall oriented along a longitudinal axis and supporting a plurality of probe holders. The curved wall has an inner surface defining an internal passage for carrying instrumentation from the probe holders to the lead carrier. In another aspect, an instrumentation rake assembly comprises a plurality of rake towers, each having a base end and an immersed end, and each rake tower being coupled at its immersed end to one or more other rake towers. | 11-15-2012 |
