Abstract: A molten metal impeller having a base portion including a circumferential notch. The notch having a generally radial wall and a generally axial wall, at least one of the radial or axial walls including a plurality of grooves. A ceramic bearing ring is cemented into the notch.

Abstract: A coupling assembly for connecting the aft end of an air duct to the compressor rear shaft in a gas turbine engine includes a retaining ring disposed in the central bore of the compressor rear shaft. The retaining ring has a first set of tabs extending axially therefrom, and the air duct has a second set of tabs extending axially from its aft end. The aft end of the air duct is disposed in the bore and positioned relative to the retaining ring so that the first set of tabs intermeshes with the second set of tabs.

Abstract: The present invention is intended to implement a high-temperature, high-pressure, high-output, high/low-pressure integrated steam turbine provided with a turbine rotor formed as an integral rotor member. It is provided with a high-pressure turbine (3) to which primary steam (20) is supplied, a low-pressure turbine (5) having last-stage turbine rotor blades (47), a turbine rotor (2) formed of an integral rotor member, an integral casing (6), and a downward-exhaust type of exhaust chamber (15); it has a rated power of at least 100 MW; the last-stage turbine rotor blades are rotor blades of an effective blade length of at least 36 inches rotating at 3000 rpm, or are rotor blades of an effective blade length of at least 33.

Abstract: An axial flow fan having impeller blade section fixed in a rotor of a motor where shaft supporting the rotation of the rotor is fitted to intermediate fastening section, and boss, which holds the synthetic resin fan with fan blades, surrounds and firmly connects the intermediate fastening section. The shaft is made from metal, and this allows a secure press fit with the metal intermediate fastening section. The neck joining the intermediate fastening section and the boss has a through hole for the shaft to pass and supporting arms project between boss and intermediate fastening section. In addition, the connecting sections between the shaft and the intermediate fastening section, and the boss and the intermediate fastening section may be knurled.

Abstract: A high toughness heat-resistant steel, a turbine rotor formed of this steel and a method of producing the turbine rotor are described. The heat-resistant steel has a composition consisting essentially of: 0.05 to 0.30 wt % C, 0 to 0.20 wt % Si, 0 to 1.0 wt % Mn, 8.0 to 14.0 wt % Cr, 0.5 to 3.0 wt % Mo, 0.10 to 0.50 wt % V, 2.0 to 5.0 wt % Ni, 0.01 to 0.50 wt % Nb, 0.01 to 0.08 wt % N, 0.001 to 0.020 wt % B, balance Fe and unavoidable impurities. The steel has excellent characteristics in not only tensile strength and toughness at a relatively low temperature condition of a steam turbine such as high/low pressure combined type one but also creep rupture strength at a high temperature condition of this turbine.

Abstract: The apparatus includes a motor with a shaft for rotating a fan. A retaining ring and a thrust washer are located around the shaft on one side of the hub of the fan and a torque washer is located on the outer side of the hub with the end of the shaft extending through a central aperture of the torque washer. The retaining ring supports the thrust washer and the thrust washer engages and supports the hub of the fan. The aperture of the torque washer and the side of the shaft at the end thereof have planar surfaces which engage each other which prevents rotation between the torque washer and the shaft. Bosses are formed on the outer side of the hub which fit into apertures formed through the torque washer outward of the central aperture to transfer torque radially outward to the hub. A screw has a threaded shaft extending through the central aperture of the torque washer and which is screwed into a threaded aperture formed in the end of the motor shaft to tighten the torque washer to the hub.

Abstract: A steam turbine in which principal components to be exposed to high temperatures are all made of ferritic steel, whereby the temperatures of main steam and reheat steam can be increased to 610-660 (° C.). The rotor shaft (23 in FIG. 1) of the steam turbine is made of ferritic forged steel whose 100,000-hour creep rupture strength is at least 15 (kg/mm2) at the service temperature of the rotor shaft. Likewise, the casing (18) is made of ferritic cast steel whose 100,000-hour creep rupture strength is at least 10 (kg/mm2). The steam turbine of high thermal efficiency can be applied to a steam-turbine power plant.