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公开(公告)号：US09631508B2
公开(公告)日：2017-04-25
申请号：US13917075
申请日：2013-06-13
发明人： Daniel Blais , Alain Lewis , Alain C. Martel
CPC分类号： F01D11/02 , F01D11/00 , F01D11/003 , F01D25/12 , F05D2260/232
摘要： A contact seal assembly for a shaft of a gas turbine engine includes a seal runner adapted to be connected to the shaft and rotatable relative to a carbon ring. The seal runner includes concentric inner and outer annular portions radially spaced apart to define at least one internal fluid passage between the inner and outer annular portions of the seal runner.
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公开(公告)号：US20140369832A1
公开(公告)日：2014-12-18
申请号：US13917075
申请日：2013-06-13
发明人： Daniel BLAIS , Alain Lewis , Alain C. Martel
CPC分类号： F01D11/02 , F01D11/00 , F01D11/003 , F01D25/12 , F05D2260/232
摘要： A contact seal assembly for a shaft of a gas turbine engine includes a seal runner adapted to be connected to the shaft and rotatable relative to a carbon ring. The seal runner includes concentric inner and outer annular portions radially spaced apart to define at least one internal fluid passage between the inner and outer annular portions of the seal runner.
摘要翻译： 用于燃气涡轮发动机的轴的接触密封组件包括适于连接到轴并相对于碳环可旋转的密封流道。 密封流道包括径向间隔开的同心的内部和外部环形部分，以在密封流道的内部和外部环形部分之间限定至少一个内部流体通道。
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公开(公告)号：US10526907B2
公开(公告)日：2020-01-07
申请号：US15469619
申请日：2017-03-27
发明人： Daniel Blais , Alain Lewis , Alain C. Martel
摘要： A contact seal assembly for a shaft of a gas turbine engine includes a seal runner adapted to be connected to the shaft and rotatable relative to a carbon ring. The seal runner includes concentric inner and outer annular portions radially spaced apart to define at least one internal fluid passage between the inner and outer annular portions of the seal runner.
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公开(公告)号：US10302523B2
公开(公告)日：2019-05-28
申请号：US15167064
申请日：2016-05-27
摘要： The method for testing the integrity of a seal of a cavity in an engine includes providing a sealed test tank external to the cavity, the test tank having an internal volume that is particularly selected, as described herein. A pressure differential is generated between the test tank and the cavity, by creating an initial test pressure within the test tank that is different than an ambient pressure inside the cavity. Gas flow between the test tank and the cavity is then permitted, and a change in pressure within the test tank is measured, as is a test time required for the pressure inside the test tank to reach a reference pressure. The measured test time is compared with a predetermined reference time, and the integrity of the seal may be confirmed when the test time is greater than or equal to the reference time.
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公开(公告)号：US20170343448A1
公开(公告)日：2017-11-30
申请号：US15167064
申请日：2016-05-27
CPC分类号： G01M3/3281 , G01M3/2869 , G01M15/02 , G01M15/14
摘要： The method for testing the integrity of a seal of a cavity in an engine includes providing a sealed test tank external to the cavity, the test tank having an internal volume that is particularly selected, as described herein. A pressure differential is generated between the test tank and the cavity, by creating an initial test pressure within the test tank that is different than an ambient pressure inside the cavity. Gas flow between the test tank and the cavity is then permitted, and a change in pressure within the test tank is measured, as is a test time required for the pressure inside the test tank to reach a reference pressure. The measured test time is compared with a predetermined reference time, and the integrity of the seal may be confirmed when the test time is greater than or equal to the reference time.
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