Abstract: A technique provides a remote adjustment to a portion of an airplane engine. The technique involves attaching a remote adjuster to the portion of the engine at a proximate location to the engine while the engine is not running. The portion is configured to receive a direct manual adjustment from a user while the engine is running and while the user is in direct physical contact with the portion. The technique further involves, after attaching the remote adjuster to the portion of the engine, supplying user input to the remote adjuster at a distal location to the engine to provide a remote adjustment to the portion of the engine through the remote adjuster in place of the direct manual adjustment from the user. The technique further involves, after supplying the user input to the remote adjuster, removing the remote adjuster from the portion of the engine.

Abstract: A monitoring method and device which is capable of determining the overall fitness or condition of the device being monitored while simultaneously detecting unknown or unrecognized vibration frequencies. In addition, setting threshold values corresponding to the environment surrounding the device reduces the incidence of false alarms. False alarms may be controlled while detection of true alarms may be maximized by assigning values indicative of thresholds crossed and averaging the values before issuing an alarm. The monitoring system may also provide detailed information as to the operating condition of the device so as to allow the device to operate closer to its margin of safety. Thus, the device may handle more power or speed, without the need to modify the physical design. In addition, an onboard processing unit may be used to determine when the physical load on the device is approaching its physical limits and warn the operator so as to prevent the device from exceeding those limits.

Abstract: A metallized composite comprising a first thermoplastic layer, a discontinuous intermediate layer comprising discrete islands of metal in an adhesive, and a second thermoplastic layer. The metallized composites of the invention can be employed as reflective surfaces, such as are used as mirrors or substitutes for chrome trim on automobiles. A particularly preferred metal as a component of the discontinuous layer of the composite is indium.

Abstract: Disclosed herein is an interferometric-based materials analysis system (10) that employs a novel combination of laser beam shaping and pointing techniques, the use of a low cost, rugged, and compact diode laser (22) as a detection laser, and the use of signal processing techniques that compensate for inherent instabilities and short-term drift in the diode laser. A matched filter processing technique is disclosed for processing interferometrically-obtained data points from a target being analyzed. The matched filter technique is shown to be especially useful for detecting and analyzing Lamb modes within thin targets, such as a silicon wafer undergoing a rapid thermal processing cycle. Also disclosed is a method and apparatus for interferometrically monitoring a target to determine, in accordance with predetermined criteria, an occurrence of a period of time that is optimum for obtaining a data point.