Abstract: A system for preheating air before it enters the combustion chamber of a gas turbine engine includes a recuperator which extends between, and is supported by, forward and rear headers. Cold air to be pre-heated by the recuperator flows through an entry passage in the forward header, then into and through a first conduit of the recuperator which extends the length of the recuperator. The air then flows through a plurality of cross conduits located at different locations along the length of the recuperator where it becomes heated. Flow of the now-heated air continues into a second conduit in which it is guided toward the combustion chamber. Sleeves are provided, respectively, in the entry passage of the forward header and in the first conduit of the recuperator for maintaining substantially constant the pressure differential between the first and second conduits at all locations along the length of the recuperator.

Abstract: A system for preheating air before it enters the combustion chamber of a gas turbine engine includes a recuperator which extends between, and is supported by, forward and rear headers. Cold air to be pre-heated by the recuperator flows through an entry passage in the forward header, then into and through a first conduit of the recuperator which extends the length of the recuperator. The air then flows through a plurality of cross conduits located at different locations along the length of the recuperator where it becomes heated by the flow of turbine exhaust gas. Flow of the now-heated air continues into a second conduit in which it is guided toward the combustion chamber.

Abstract: An X-ray generating tube with improved thermal performance comprises a stationary disc within a hollow rotating target disc. The target operates at the target metal temperatures limit. The stationary disc is cooled by forced convection with a dielectric liquid. Heat is transferred from the target inwardly and outwardly.

Abstract: A rotating nozzle generator is described for producing electricity from the direct expansion of a liquid to a two-phase mixture of liquid and vapor. The device includes liquid inlet means, a rotor, at least one fluid flow groove along the length of the rotor, which groove changes in size in communication with the liquid inlet means, generator windings on the outer or inner surface of the rotor and fluid outlet means in communication with the fluid flow groove.

Abstract: A rotating nozzle expander is described for the direct expansion of a liquid to a two-phase mixture of liquid and vapor thereby producing mechanical work. The device includes liquid inlet means, at least one fluid flow passage which changes in size in communication with the liquid inlet means, the passage mounted rotatably, the fluid outlet means in communication with the fluid flow passage.