Patent ID: 8408801

Claim:
An oiling nozzle for use in a thrust bearing, in which said oiling nozzle is arranged between pads disposed in positions facing a thrust surface of a thrust collar that protrudes outwardly in a radial direction from a rotor shaft and along a circumferential direction of the rotor shaft, said oiling nozzle comprising: a cylindrical stem; and a rectangular mainframe that is connected with said cylindrical stem, said rectangular mainframe having: convex parts on opposite sides of said rectangular mainframe at a middle position along an axis of said oiling nozzle extending in a direction from said rectangular mainframe toward said cylindrical stem, said convex parts each having the appearance of a semicircular disk as seen looking along the axis in the direction from said rectangular mainframe toward said cylindrical stem for fitting into concave parts in sides of the pads, and a top portion located on a side of said rectangular mainframe that is opposite to a side of said rectangular mainframe on which said cylindrical stem is located, said top portion having a plurality of nozzle holes for ejecting lubricating oil that has been supplied from a bottom portion of said cylindrical stem toward a space between the thrust collar and the pads, wherein at least one of said plurality of nozzle holes is formed perpendicular to a longitudinal direction of said rectangular mainframe and at least one other of said plurality of nozzle holes is formed at a slant to the longitudinal direction of said rectangular mainframe as seen looking along the axis in the direction from said rectangular mainframe toward said cylindrical stem; wherein said top portion of said rectangular mainframe has two lateral faces that slope to a top face, a front face, and two intermediate faces positioned between said two lateral faces and said front face so as to connect said two lateral faces and said front face, and wherein said two lateral faces have a number of said plurality of nozzle holes therein and said two intermediate faces each have at least one of said plurality of nozzle holes therein.