Zirconia vane for rotary compressors
AssigneeSumitomo Electric Industries, Ltd.
InventorsTakao Nishioka, Akira Yamakawa, Matsuo Higuchi, Harutoshi Ukegawa
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AssigneeSumitomo Electric Industries, Ltd.
InventorsTakao Nishioka, Akira Yamakawa, Matsuo Higuchi, Harutoshi Ukegawa
Estimating the term…
A zirconia vane used in a rotary compressor, the zirconia vane being formed of a partially stabilized zirconia sintered body containing 92 through 98 molar percent of ZrO.sub.2 and being stabilized with Y.sub.2 O.sub.3, zirconia crystals constituting the zirconia sintered body having a mean grain diameter of 0.1 to 0.6 .mu.m and a maximum grain diameter of not greater than 2 .mu.m, the zirconia sintered body having a mean three-point flexural strength of not less than 120 kg/mm.sup.2 measured in conformity with JIS R1601, a surface of the zirconia sintered body in contact with a rotor of the rotary compressor having a first surface roughness in a direction of rotations of the rotor, specified by a ten-point mean roughness Rz, of not greater than 1 .mu.m and a second surface roughness in a direction perpendicular to the direction of rotation of the rotor, specified by the ten-point mean roughness Rz, of not greater than 0.6 .mu.m. The vane is light-weight and has excellent sliding properties to effectively prevent cohesion and seizure in an atmosphere of a coolant of chlorine-free like an HFC.
A zirconia vane used in a rotary compressor, said zirconia vane comprising a partially stabilized zirconia sintered body containing 92 through 98 molar percent of ZrO.sub.2 and being stabilized with Y.sub.2 O.sub.3, zirconia crystals constituting said zirconia sintered body having a mean grain diameter of 0.1 to 0.6 .mu.m and a maximum grain diameter of not greater than 2 .mu.m, said zirconia sintered body having a mean three-point flexural strength of not less than 120 kg/mm.sup.2 measured in conformity with JIS R1601, a surface of said zirconia sintered body in contact with a rotor of said rotary compressor having a first surface roughness in a direction of rotations of said rotor, specified by a ten-point mean roughness Rz, of not greater than 1 .mu.m and a second surface roughness in a direction perpendicular to the direction of rotations of said rotor, specified by the ten-point mean roughness Rz, of not greater than 0.6 .mu.m.
Dependencies are inferred from the claim text.