| 摘要 |
PROBLEM TO BE SOLVED: To provide a rolling bearing to be used in an aircraft or space attitude control equipment for reducing a torque fluctuation range while eliminating sound generation in a cage. SOLUTION: The full-ball type rolling ball bearing for supporting the rotor of the aircraft or the space attitude control equipment comprises only an outer ring 1, an inner ring 2, and a rolling element 3 (a ball), wherein no cage exists. Thus, no sliding site exists between a cage guide face and a bearing ring and between a cage pocket face and the rolling element 3 (the ball). COPYRIGHT: (C)2007,JPO&INPIT
|
