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21. 发明授权

US08365538B2 High temperature-resistant sealing assembly, especially for gas turbines 失效
标题翻译：耐高温密封组件，特别适用于燃气轮机
公开(公告)号：US08365538B2
公开(公告)日：2013-02-05
申请号：US11992434
申请日：2006-09-20
申请人： Tobias Buchal , Gregor Frank , Uwe Gruschka , Joachim Krützfeldt , Kai-Uwe Rogos , Axel Schaberg
发明人： Tobias Buchal , Gregor Frank , Uwe Gruschka , Joachim Krützfeldt , Kai-Uwe Rogos , Axel Schaberg
IPC分类号： F02C7/12
CPC分类号： F01D9/023 , F05D2230/642 , F05D2240/57 , F05D2260/201 , F16J15/0887
摘要： The invention relates to a high temperature-resistant sealing assembly comprising a sealing segment and a component border which is connected to the sealing segment. A flexible sealing element is provided in order to joining the sealing segment and the component border. The invention is characterized in that the flexible sealing element compensates both thermal expansions and relative movements of the component border and the components resting against the sealing segment. The flexible sealing element and the sealing segment are subject to little wear and have a long service life. The invention further relates to a combustion chamber that is equipped with a high temperature-resistant sealing assembly as well as a gas turbine encompassing such a combustion chamber.
摘要翻译：本发明涉及一种耐高温密封组件，其包括密封段和连接到密封段的部件边界。提供柔性密封元件以便连接密封段和部件边界。本发明的特征在于，柔性密封元件补偿组件边界的热膨胀和相对运动，以及抵靠密封段的部件。柔性密封元件和密封段磨损少，使用寿命长。本发明还涉及一种配备有耐高温密封组件的燃烧室以及包围这种燃烧室的燃气轮机。

22. 发明申请

US20100146985A1 High Temperature-Resistant Sealing Assembly, Especially for Gas Turbines 失效
标题翻译：耐高温密封组件，特别适用于燃气轮机
公开(公告)号：US20100146985A1
公开(公告)日：2010-06-17
申请号：US11992434
申请日：2006-09-20
申请人： Tobias Buchal , Gregor Frank , Uwe Gruschka , Joachim Krützfeldt , Kai-Uwe Rogos , Alex Schaberg
发明人： Tobias Buchal , Gregor Frank , Uwe Gruschka , Joachim Krützfeldt , Kai-Uwe Rogos , Alex Schaberg
IPC分类号： F02C7/12 , F16J15/02 , F16J15/08 , F16J15/06 , F01D25/00 , F02C3/04
CPC分类号： F01D9/023 , F05D2230/642 , F05D2240/57 , F05D2260/201 , F16J15/0887
摘要： The invention relates to a high temperature-resistant sealing assembly comprising a sealing segment and a component border which is connected to the sealing segment. A flexible sealing element is provided in order to joining the sealing segment and the component border. The invention is characterized in that the flexible sealing element compensates both thermal expansions and relative movements of the component border and the components resting against the sealing segment. The flexible sealing element and the sealing segment are subject to little wear and have a long service life. The invention further relates to a combustion chamber that is equipped with a high temperature-resistant sealing assembly as well as a gas turbine encompassing such a combustion chamber.
摘要翻译：本发明涉及一种耐高温密封组件，其包括密封段和连接到密封段的部件边界。提供柔性密封元件以便连接密封段和部件边界。本发明的特征在于，柔性密封元件补偿组件边界的热膨胀和相对运动，以及抵靠密封段的部件。柔性密封元件和密封段磨损少，使用寿命长。本发明还涉及一种配备有耐高温密封组件的燃烧室以及包围这种燃烧室的燃气轮机。

23. 发明申请

US20090252612A1 Blade and gas turbine 审中-公开
标题翻译：叶片和燃气轮机
公开(公告)号：US20090252612A1
公开(公告)日：2009-10-08
申请号：US10561279
申请日：2004-05-27
申请人： Fathi Ahmad , Tobias Buchal , Michael Dankert , Gernot Lang , Michael Scheurlen
发明人： Fathi Ahmad , Tobias Buchal , Michael Dankert , Gernot Lang , Michael Scheurlen
IPC分类号： F01D5/14
CPC分类号： F01D5/282 , B23P15/04 , F01D5/14 , F01D5/147 , F01D5/284 , F05D2230/61
摘要： The invention relates to a turbomachine, in particular to a gas turbine and to a method for accelerating a temperature modification of a rotor shaft rotationally mounted in said turbomachine. The aim of said invention is to develop a device and a method for the turbomachine making it possible to reduce the size of a radial split of the turbomachine in order to obtain greater degree of efficiency. The inventive turbomachine comprises a rotor rotationally mounted in the case of the turbomachine, a feeding channel embodied in the rotor for introducing a fluid and an outlet channel embodied in the rotor for removing said fluid. An inlet orifice of the feeding channel is disposed further inside than the outlet orifice of the outlet channel, and means influencing a liquid flow is formed of an actuating device dependent on centrifugal force. Methods for cooling the rotor only by decelerating the gas turbine and for heating the turbomachine rotor by heating fluid flowing therethrough are also disclosed.
摘要翻译：本发明涉及一种涡轮机，特别涉及一种燃气轮机，以及用于加速旋转安装在所述涡轮机中的转子轴的温度变化的方法。本发明的目的在于开发一种用于涡轮机的装置和方法，从而可以减小涡轮机径向分流的尺寸，以获得更高的效率。本发明的涡轮机包括旋转地安装在涡轮机的壳体中的转子，在转子中实现的用于引入流体的进料通道和实施在转子中的用于去除所述流体的出口通道。进料通道的入口孔设置在出口通道的出口孔的内侧，影响液体流动的装置由取决于离心力的致动装置形成。还公开了仅通过使燃气轮机减速并通过加热流过其中的流体来加热涡轮机转子来冷却转子的方法。

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