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公开(公告)号：US4579507A
公开(公告)日：1986-04-01
申请号：US570068
申请日：1984-01-12
申请人： Charles E. Corrigan , Paul R. Dodge
发明人： Charles E. Corrigan , Paul R. Dodge
CPC分类号： F01D17/162 , F01D17/141 , F01D17/167
摘要： A combustion turbine engine having an improved variable-area turbine stator assembly.
摘要翻译： 具有改进的可变面积涡轮机定子组件的燃气涡轮发动机。
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公开(公告)号：US4497171A
公开(公告)日：1985-02-05
申请号：US333502
申请日：1981-12-22
申请人： Charles E. Corrigan , Paul R. Dodge
发明人： Charles E. Corrigan , Paul R. Dodge
CPC分类号： F01D17/167 , F01D17/141 , F01D17/162
摘要： A combustion turbine engine having an improved variable-area turbine stator assembly defining a flow path for motive fluid. The stator assembly includes a multitude of guide vane members which are movable into and out of the motive fluid flow path to respectively decrease and increase the effective fluid flow area defined thereby.
摘要翻译： 一种燃气涡轮发动机，其具有限定用于运动流体的流动路径的改进的可变区域涡轮机定子组件。 定子组件包括多个导向叶片构件，其能够进入和移出运动流体流动路径，以分别减小并增加由其限定的有效流体流动面积。
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公开(公告)号：US4270883A
公开(公告)日：1981-06-02
申请号：US9201
申请日：1979-02-05
申请人： Charles E. Corrigan
发明人： Charles E. Corrigan
摘要： Improved structure and method for an internally cooled, laminated stator or turbine blade for turbomachinery includes internal cooling passage configurations within each lamina which promote different forms of cooling of the internal or external surfaces of the blade.
摘要翻译： 用于涡轮机械的内部冷却的层压定子或涡轮叶片的改进的结构和方法包括在每个层内的内部冷却通道构造，其促进叶片的内部或外部表面的不同形式的冷却。
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公开(公告)号：US4221539A
公开(公告)日：1980-09-09
申请号：US789371
申请日：1977-04-20
申请人： Charles E. Corrigan
发明人： Charles E. Corrigan
CPC分类号： F01D5/34 , F01D5/147 , F01D5/18 , Y02T50/673 , Y02T50/676
摘要： Improved structure and method for an internally cooled, laminated stator or turbine blade for turbomachinery includes internal cooling passage configurations within each lamina which promote different forms of cooling of the internal or external surfaces of the blade.
摘要翻译： 用于涡轮机械的内部冷却的层压定子或涡轮叶片的改进的结构和方法包括在每个层内的内部冷却通道构造，其促进叶片的内部或外部表面的不同形式的冷却。
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公开(公告)号：US3986720A
公开(公告)日：1976-10-19
申请号：US567532
申请日：1975-04-14
CPC分类号： F01D11/18 , Y02T50/671
摘要： The structure which supports a rotor-surrounding shroud is composed of a material exhibiting a low coefficient of thermal expansion at low temperatures and a high coefficient of thermal expansion at higher temperatures. In this way, low alpha characteristics persist during periods of low temperature operation to provide large cold clearances and acceptable clearances during transient operation, while high alpha characteristics persist during periods of high temperature operation to provide close clearance control at maximum and part-power, steady-state operating conditions. The two-alpha material also finds use with other relatively rotating parts having close clearance relationship therebetween, such as in the stationary portion of a seal structure.
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公开(公告)号：US4597675A
公开(公告)日：1986-07-01
申请号：US481539
申请日：1983-04-04
摘要： Method and apparatus for producing a signal analogous to the means temperature of fluid within a flow path is in a turbo machine. The fluid flowing in the flow path has a nonconstant temperature considered transversely thereto and defining a temperature profile. An elongate thermosiphon is immersed substantially entirely in said fluid flow and extend transversely thereto for sensing a thermal characteristic of the vapor therein.
摘要翻译： 用于产生类似于流动路径内的流体温度的信号的方法和装置在涡轮机中。 在流路中流动的流体具有横向考虑的非恒定温度并且限定温度分布。 细长的热虹吸管基本上完全浸没在所述流体流中并横向延伸以感测其中的蒸气的热特性。
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公开(公告)号：US4347037A
公开(公告)日：1982-08-31
申请号：US195896
申请日：1980-10-14
申请人： Charles E. Corrigan
发明人： Charles E. Corrigan
摘要： Improved structure and method for an internally cooled, laminated stator or turbine blade for turbomachinery includes internal cooling passage configurations within each lamina which promote different forms of cooling of the internal or external surfaces of the blade.
摘要翻译： 用于涡轮机械的内部冷却的层压定子或涡轮叶片的改进的结构和方法包括在每个层内的内部冷却通道构造，其促进叶片的内部或外部表面的不同形式的冷却。
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