Invention Grant
US08714905B2 Method and a device for balancing pressure in a turbojet bearing enclosure 有权
方法和用于平衡涡轮喷气轴承外壳中的压力的​​装置

Method and a device for balancing pressure in a turbojet bearing enclosure
Abstract:
A pressure-balancing device for balancing pressure in at least one bearing enclosure of a turbojet, the enclosure including a mechanism feeding the bearing with lubricating liquid, an air intake, at least one sealing system placed between the stator and the rotor in front of and/or behind the bearing, a recovery mechanism recovering the lubricating liquid, and a removal mechanism removing the mixture of air and of traces of lubricating liquid towards a venting circuit. Downstream from the bearing enclosure and in the venting circuit, the balancing device includes a regulator system regulating the air removal flow rate, thereby enabling the flow rate to be variable as a function of the speed of the engine, to remain non-zero, and, at high speeds, to be lower than when the regulator system is not included.
Information query
Patent Agency Ranking
0/0