Patent ID: 11891996
Assignee: ATLAS COPCO AIRPOWER, NAAMLOZE VENNOOTSCHAP
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F | IPC F

Claim 5:
6. The compressor element according to claim 1, wherein the at least one oil injector (6) is arranged on the housing (3) at a distance from the at least one intermediate element (5) and wherein the at least one oil nozzle (8a, 8b, 8c) is biased towards the at least one intermediate element (5) and is configured to eject oil from the at least one oil nozzle (8a, 8b, 8c), wherein the ejected oil is adapted to impact an injection location (10), wherein an area of the injection location (10) is smaller than 10 mm2.