Abstract: A system for controlling blade clearances within a gas turbine engine includes a rotor disk and a rotor blade coupled to the rotor disk. Additionally, the system includes an outer turbine component positioned outward of the rotor blade such that a clearance is defined between the rotor blade and the outer turbine component. Furthermore, the system includes a heat exchanger configured to receive a flow of cooling air bled from the gas turbine engine and transfer heat from the received flow of the cooling air to a flow of coolant to generate cooled cooling air. Moreover, the system includes a valve configured to control the flow of the coolant to the heat exchanger. In this respect, the cooled cooling air is supplied to at least one of the rotor disk or the rotor blade to adjust the clearance between the rotor blade and the outer turbine component.

Abstract: A gas turbine engine having a waste heat recovery system is provided. The gas turbine engine includes a compressor section, a combustion section, a turbine section, and an exhaust section in serial flow order and together defining a core air flowpath, the exhaust section including a primary exhaust flowpath and a waste heat recovery flowpath parallel to the primary exhaust flowpath; and the waste heat recovery system includes a heat source exchanger positioned in thermal communication with a first portion of the waste heat recovery flowpath.

Abstract: An inkjet printer that has a printhead with a nozzle array for ejecting droplets of ink onto a media substrate, a media feed assembly for feeding media passed the printhead in a media feed direction such that the nozzle array and the media substrate are separated by a print gap and, an air flow generation mechanism for generating an air flow in the print gap opposite to the media feed direction.

Abstract: An inkjet printer that has a printhead with a nozzle array for ejecting droplets of ink onto a media substrate, a media feed assembly for feeding media passed the printhead in a media feed direction such that the nozzle array and the media substrate are separated by a print gap and, an air flow generation mechanism for generating an air flow in the print gap opposite to the media feed direction.

Abstract: A remote inspection device is provided for inspecting visually obscured locations. The device is generally comprised of a imager housing and a display housing disposed on opposite ends of a modular, flexible cable. An imaging device and one or more light sources are embedded in the end of the cylindrical imager housing. A display housing is coupled to the other end of the flexible cable and configured to be grasped by a user of the device. A display device supported by the display housing receives a video signal from the imaging device and converts the video signal to a video image. The flexible cable can be removably attached to other components with a detachable coupling. The detachable coupling is adapted to facilitate movement of the coupling through confined spaces and inhibit relative axial rotation. Components of the coupling can have tapered mating surfaces to inhibit longitudinal movement within the coupling.

Abstract: The present invention relates to a method of imaging using multiple doses of an echogenically persistent contrast agent. In particular, it relates to the use of ultrasound energy to eliminate residual echogenicity attributed to the first dose of contrast agent prior to administering a second dose of contrast agent for the purpose of acquiring more images.