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The development of a long life rolling element bearing for use under severe conditions is fundamental and important technology from an economic and environmental standpoint. Previously, NTJ2 was developed as a semi-heat resistant long life bearing steel, using silicon as an alloying element to enhance its heat resistance and life. It is thought, though, that the demand for a bearing material that can withstand higher temperatures and have a longer life than NTJ2 will be needed in the future. Thus, a new heat resistant, long life material called STJ2 was developed optimizing the alloying elements in the silicon-alloyed bearing steel. The new steel has good dimensional stability to 250°C, long life and is very resistant to surface damage.

A new methodology for determining the steady-state flow force on a hydraulic spool valve has been developed. From a solid model of the valve and valve body, a commercially available CFD package automeshes the volume grid and determines the 3D steady-state flow field and forces on the valve within 36 CPU hrs. This numerical approach enables the quick determination of optimal valve design aimed at improved valve controllability and reduced wear in the hydraulic circuit. To demonstrate this methodology, several simulations were performed aimed at investigating the influence of valve design and valve operating conditions on the steady-state flow force experienced by the valve. The numerical simulations showed that a tapered spool geometry can introduce significant variations in the axial and radial forces (30%).

In October 1985, a new wind tunnel was completed and put into operation at the Nissan Technical Center. This paper describes its main specifications and performance features, and gives results of a number of experiments using the new facility. It is a closed-circuit wind tunnel of the so-called Göttingen type, with a semi-open test section. The test section is equipped with two different nozzles, which are used interchangeably depending on the type of testing being carried out. The larger nozzle has a maximum wind velocity of 190 kmh, and a cross-section 4 m high by 7 m wide. The other is 3 m high by 5 m wide and has a maximum wind velocity of 270 kmh. All of the testing equipment in the tunnel, including the axial-flow fan, six-component aerodynamic balance, and traverse system, are operated automatically by a control system made up of several computers linked together. The most notable feature of this wind tunnel is the large reduction that has been made in background noise.