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
- Patent Title: Method and a device for balancing pressure in a turbojet bearing enclosure
- Patent Title (中): 方法和用于平衡涡轮喷气轴承外壳中的压力的装置
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Application No.: US12934784Application Date: 2009-03-24
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Publication No.: US08714905B2Publication Date: 2014-05-06
- Inventor: Ion Fintescu , Laurent Gille , Jean-Pierre Mourlan
- Applicant: Ion Fintescu , Laurent Gille , Jean-Pierre Mourlan
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR0851923 20080326
- International Application: PCT/FR2009/050500 WO 20090324
- International Announcement: WO2009/125120 WO 20091015
- Main IPC: F04D27/02
- IPC: F04D27/02

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.
Public/Granted literature
- US20110188992A1 METHOD AND A DEVICE FOR BALANCING PRESSURE IN A TURBOJET BEARING ENCLOSURE Public/Granted day:2011-08-04
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