06-12-2018 дата публикации
Номер: US20180347633A1
A compressor includes a shell, a compression mechanism, a motor assembly, a driveshaft, and a bearing assembly. The driveshaft is drivingly engaged with the motor assembly and the compression mechanism for rotation about an axis and extends from a first end to a second end. The bearing assembly is disposed within the shell and supports the driveshaft for rotation. The bearing assembly includes a bracket, a hub, and a bushing. The bracket is coupled to the shell and includes an aperture. The hub is disposed within the aperture and defines a bore having a radially inwardly extending lip. The bushing includes a first portion and a second portion. The second portion of the bushing includes a plurality of radially extending engagement features. The second portion of the bushing is disposed within the bore of the hub such that the engagement features engage the lip of the hub. 1. A compressor comprising:a shell;a compression mechanism disposed within the shella motor assembly disposed within the shell;a driveshaft drivingly engaged with the motor assembly and the compression mechanism for rotation about an axis, the driveshaft extending from a first end to a second end, the second end having an axially extending passage; a bracket coupled to the shell and having an aperture;', 'a hub disposed within the aperture and defining a bore being a through-hole in the hub, the bore including a radially inwardly extending lip on an end of the hub; and', 'a bushing having a first portion and a second portion, the second portion of the bushing having a plurality of radially extending engagement features, the second portion of the bushing disposed within the bore such that the engagement features engage the radially inwardly extending lip of the hub., 'a bearing assembly disposed within the shell and supporting the driveshaft for rotation, the bearing assembly including'}2. The compressor of claim 1 , wherein the bushing includes a radially extending flange having an upper thrust ...
Подробнее