首页> 外国专利> ASPIRATING FACE SEAL, GAS TURBINE ENGINE HAVING SAID SEAL, METHOD OF SEALING OF SAID ENGINE AND METHOD OF REPLACING SECONDARY SEAL OF SAID FACE SEAL (VERSIONS)

ASPIRATING FACE SEAL, GAS TURBINE ENGINE HAVING SAID SEAL, METHOD OF SEALING OF SAID ENGINE AND METHOD OF REPLACING SECONDARY SEAL OF SAID FACE SEAL (VERSIONS)

机译:令人兴奋的面部密封,具有燃气密封的燃气轮机发动机,有效的发动机密封方法和替代的快速面部密封第二次密封方法(版本)

摘要

FIELD: instrument making.;SUBSTANCE: aspirating face seal includes a primary seal, a secondary seal, and a biasing device. Primary seal includes a first seal component and a second seal component. First seal component is configured to be coupled to a rotor and rotate with rotor. Secondary seal includes flexible elements and is configured to be disposed between second seal component and a stator housing. Biasing device is coupled to second seal component such that second seal component is biased along an axial direction away from first seal component during a non-operating condition.;EFFECT: technical result of invention is improved dynamic characteristics and longer service life of secondary seal.;24 cl, 4 dwg
机译:技术领域:仪器制造;实质:抽吸面密封件包括主密封件,副密封件和偏压装置。主密封件包括第一密封件和第二密封件。第一密封部件构造成联接至转子并与转子一起旋转。次级密封件包括挠性元件,并且构造成设置在第二密封部件和定子壳体之间。偏压装置联接到第二密封部件,使得在非工作状态下第二密封部件沿着轴向方向远离第一密封部件偏置。效果:本发明的技术结果是改进了动态特性并且延长了第二密封件的使用寿命。 ; 24 cl,4 dwg

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