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31. 发明申请

US20100303606A1 TURBOMACHINE COMPRESSOR WHEEL MEMBER 有权
标题翻译：涡轮压缩机轮子会员
公开(公告)号：US20100303606A1
公开(公告)日：2010-12-02
申请号：US12473352
申请日：2009-05-28
申请人： Kenneth Damon Black
发明人： Kenneth Damon Black
IPC分类号： F01D25/12 , F01D5/18
CPC分类号： F01D5/06 , F01D25/12 , F02C6/08 , F04D29/321 , F04D29/584
摘要： A turbomachine includes a rotor assembly including a wheel member. The wheel member includes a first portion that extends to a second portion through an intermediate portion. The intermediate portion partially defines a first wheel space and a second wheel space. The wheel member further includes a rotor inertia belt member arranged at the second portion. The rotor inertia belt member includes an extraction air cavity. The extraction air cavity includes an inlet, a first plurality of extraction air passages each including an inlet section and an outlet section, the outlet section leading into the first wheel space, and a second plurality of extraction air passages each including an inlet portion and an outlet portion, the outlet portion leading into the second wheel space.
摘要翻译：涡轮机包括包括轮构件的转子组件。轮构件包括通过中间部分延伸到第二部分的第一部分。中间部分部分地限定第一车轮空间和第二车轮空间。轮构件还包括布置在第二部分处的转子惯性带构件。转子惯性带构件包括提取空气腔。提取空气腔包括入口，每个包括入口部分和出口部分的第一多个提取空气通道，通向第一车轮空间的出口部分和第二多个提取空气通道，每个抽吸空气通道包括入口部分和出口部分，出口部分通向第二轮空间。

32. 发明申请

US20100272558A1 Turbine rotor support apparatus and system 有权
标题翻译：涡轮转子支撑装置及系统
公开(公告)号：US20100272558A1
公开(公告)日：2010-10-28
申请号：US11656245
申请日：2007-01-22
申请人： Kenneth Damon Black , Gregory Allan Crum , Scott Michael Elam
发明人： Kenneth Damon Black , Gregory Allan Crum , Scott Michael Elam
IPC分类号： F01D25/16
CPC分类号： F01D25/162 , F01D25/28
摘要： An apparatus to support a rotor of a turbine engine disposed upon a support surface is disclosed. The apparatus includes a housing, a rotor support bearing disposed within the housing, and a support leg in operable communication with the housing and in direct structural connection with the support surface.
摘要翻译：公开了一种用于支撑设置在支撑表面上的涡轮发动机的转子的装置。该装置包括壳体，设置在壳体内的转子支撑轴承以及与壳体可操作地连通并与支撑表面直接结构连接的支撑腿。

33. 发明申请

US20100111679A1 Asymmetrical gas turbine cooling port locations 有权
标题翻译：不对称燃气轮机冷却端口位置
公开(公告)号：US20100111679A1
公开(公告)日：2010-05-06
申请号：US12289567
申请日：2008-10-30
申请人： Kenneth Damon Black
发明人： Kenneth Damon Black
IPC分类号： F02C7/12
CPC分类号： F01D11/24 , F01D25/14 , F01D25/26 , F05D2230/642 , F05D2240/14
摘要： A method is disclosed for improving a turbine's thermal response during transient and steady state operating conditions in which the flow of cooling fluid in the turbine's casing is caused to be asymmetrical relative to the horizontal and vertical symmetry planes of the casing so that the turbine's cooling symmetry planes are rotated relative to its geometric symmetry planes and thereby the heat transfer at locations in the casing with increased mass is increased.
摘要翻译：公开了一种用于在瞬态和稳态操作条件期间改善涡轮机热响应的方法，其中涡轮机壳体中的冷却流体相对于壳体的水平和垂直对称平面不对称，使得涡轮机的冷却对称性平面相对于其几何对称平面旋转，从而增加了质量增加的壳体中位置处的热传递。

34. 发明申请

US20090097968A1 APPARATUS AND METHOD FOR CLEARANCE CONTROL OF TURBINE BLADE TIP 失效
标题翻译：涡轮叶片间隙控制装置及方法
公开(公告)号：US20090097968A1
公开(公告)日：2009-04-16
申请号：US11871430
申请日：2007-10-12
申请人： Henry Grady Ballard, JR. , Bradley James Miller , Kenneth Damon Black
发明人： Henry Grady Ballard, JR. , Bradley James Miller , Kenneth Damon Black
IPC分类号： F01D17/16 , F01D25/24 , F01D11/22
CPC分类号： F01D11/22
摘要： An inner shell for a rotating machine including at least one segment; and at least one complementary segment in operable communication with the at least one segment, the segments forming a support structure for a shroud ring; wherein the at least one segment and the at least one complementary segment are individually moved to change a set of dimensions defined by the at least one segment and the at least one complementary segment. A method for controlling a dimension of the shroud ring in a rotating machine is also disclosed.
摘要翻译：一种用于旋转机器的内壳，包括至少一个段; 以及与所述至少一个段可操作地连通的至少一个互补段，所述段形成用于护罩环的支撑结构; 其中所述至少一个区段和所述至少一个互补区段被单独移动以改变由所述至少一个区段和所述至少一个互补区段限定的一组维度。还公开了一种用于控制旋转机器中的护罩环的尺寸的方法。

35. 发明申请

US20090053046A1 METHOD, SYSTEM AND APPARATUS FOR TURBINE DIFFUSER SEALING 有权
标题翻译：用于涡轮增压器密封的方法，系统和装置
公开(公告)号：US20090053046A1
公开(公告)日：2009-02-26
申请号：US11844058
申请日：2007-08-23
申请人： Kenneth Damon Black , Scott Michael Elam , Prashant Kantappa Patil
发明人： Kenneth Damon Black , Scott Michael Elam , Prashant Kantappa Patil
IPC分类号： F01D11/08 , F02C7/20
CPC分类号： F01D25/30 , F01D25/26
摘要： A turbine diffuser is disclosed. The turbine diffuser includes a diffuser segment having a forward end and an aft end with a flange disposed at the aft end of the diffuser segment. The diffuser segment is joinable to an adjacent diffuser segment via the flange, which includes a seal retainer that is securedly connectable in a radial direction with a seal.
摘要翻译：公开了一种涡轮扩散器。涡轮扩散器包括具有前端和后端的扩散器段，其具有设置在扩散器段的后端处的凸缘。扩散器段可通过凸缘连接到相邻的扩散器段，凸缘包括可沿径向可密封地与密封连接的密封保持器。

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