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    SEAL INCLUDING FLEXIBLE SEAL STRIPS
    2.
    发明申请
    SEAL INCLUDING FLEXIBLE SEAL STRIPS 有权
    密封包括柔性密封条

    公开(公告)号：US20120007318A1

    公开(公告)日：2012-01-12

    申请号：US12832141

    申请日：2010-07-08

    Applicant: Ching-Pang Lee ,  Vincent P. Laurello ,  Chander Prakash ,  Kok-Mun Tham

    Inventor： Ching-Pang Lee ,  Vincent P. Laurello ,  Chander Prakash ,  Kok-Mun Tham

    IPC: F02F11/00 ,  F16J15/44

    CPC classification number: F16J15/3292 ,  F01D11/02 ,  F05D2240/57

    Abstract: A seal member for effecting a seal preventing fluid flow in an axial direction through an annular space formed between two relatively moving components including a rotatable shaft and a stator structure. The seal member includes a plurality of flexible seal strips. Each seal strip includes a planar plate extending radially through the annular space and having a radially outer end supported to the stator structure and a radially inner end defining a tip portion extending widthwise in the axial direction engaged in sliding contact with a peripheral surface of the rotatable shaft. At least one of the seal strips includes a plurality of perforations extending through the seal strip and located between a leading edge and a trailing edge of the seal strip for effecting an increased flexibility of the seal strip adjacent to the tip portion.

    Abstract translation: 一种用于实现密封的密封件，其防止流体沿轴向流动通过形成在包括可旋转轴和定子结构的两个相对移动部件之间的环形空间。 密封构件包括多个柔性密封条。 每个密封条包括平面板，该平面板径向地延伸穿过环形空间并且具有支撑到定子结构的径向外端，以及限定沿轴向方向沿宽度方向延伸的尖端部分的径向内端，该尖端部分与可旋转的 轴。 密封条中的至少一个包括延伸穿过密封条并且位于密封条的前缘和后缘之间的多个穿孔，用于实现与尖端部分相邻的密封条的增加的柔性。

    TURBINE AIRFOIL WITH CURVED SQUEALER TIP
    5.
    发明申请
    TURBINE AIRFOIL WITH CURVED SQUEALER TIP 有权
    涡轮发动机带有弯曲的螺母提示

    公开(公告)号：US20070059182A1

    公开(公告)日：2007-03-15

    申请号：US11162433

    申请日：2005-09-09

    Applicant: Mark Stegemiller ,  Chander Prakash ,  Leslie Leeke ,  Kevin Klasing ,  Ching-Pang Lee

    Inventor： Mark Stegemiller ,  Chander Prakash ,  Leslie Leeke ,  Kevin Klasing ,  Ching-Pang Lee

    IPC: B64C27/46

    CPC classification number: F01D5/20 ,  F05D2250/71 ,  F05D2250/712 ,  Y02T50/67

    Abstract: An airfoil for a gas turbine engine includes a root, a tip, a leading edge, a trailing edge, and opposed pressure and suction sidewalls extending generally along a radial axis. The airfoil includes a tip cap extending between the pressure and suction sidewalls; and spaced-apart suction-side and pressure-side tip walls extending radially outward from the tip cap to define a tip cavity therebetween. The pressure-side tip wall includes a continuously concave curved arcuate portion, at least a section of which extends circumferentially outward from a radial axis of the airfoil.

    Abstract translation: 用于燃气涡轮发动机的翼型件包括根部，尖端，前缘，后缘以及大致沿径向轴线延伸的相对的压力和吸力侧壁。 翼型件包括在压力侧和吸力侧壁之间延伸的顶盖; 并且间隔开的吸入侧和压力侧尖端壁从尖端帽径向向外延伸以在它们之间限定尖端腔。 压力侧末端壁包括连续凹入的弯曲弧形部分，其至少一部分从翼型件的径向轴向向外延伸。

    Triple circuit turbine blade
    6.
    发明授权
    Triple circuit turbine blade 失效
    三回路涡轮叶片

    公开(公告)号：US06984103B2

    公开(公告)日：2006-01-10

    申请号：US10718465

    申请日：2003-11-20

    Applicant: Ching-Pang Lee ,  Steven Robert Brassfield ,  Chander Prakash

    Inventor： Ching-Pang Lee ,  Steven Robert Brassfield ,  Chander Prakash

    IPC: F03D11/00

    CPC classification number: F01D5/187 ,  Y02T50/673 ,  Y02T50/676

    Abstract: A turbine blade includes an airfoil having pressure and suction sidewalls extending between leading and trailing edges, and from root to tip. A dovetail is joined to the airfoil root at a platform. Three internal cooling circuits extend in span inside the airfoil, and each circuit includes a respective inlet channel commencing in axially adjacent alignment in the dovetail. The inlet channels twist together from the dovetail, through the platform, and into the airfoil behind the leading edge in transverse adjacent alignment across the sidewalls.

    Abstract translation: 涡轮叶片包括具有在前缘和后缘之间延伸的压力和吸力侧壁以及从根部到尖端的翼型件。 燕尾榫在平台上连接到翼型根部。 三个内部冷却回路在翼型内部的跨度上延伸，并且每个回路包括相应的入口通道，其从燕尾榫开始轴向相邻对准。 入口通道从燕尾榫通过平台扭转在一起，并且横跨相邻的侧壁横向相邻对齐，并进入前缘的后翼。

    Separator ring for retaining rollers in a thrust bearing
    7.
    发明授权
    Separator ring for retaining rollers in a thrust bearing 失效
    用于将滚子保持在推力轴承中的分隔环

    公开(公告)号：US3999817A

    公开(公告)日：1976-12-28

    申请号：US653959

    申请日：1976-01-30

    Applicant: Chander Prakash Bhateja ,  Richard Lassen Alling ,  Dean Edward Johnston

    Inventor： Chander Prakash Bhateja ,  Richard Lassen Alling ,  Dean Edward Johnston

    IPC: F16C19/30 ,  F16C19/32 ,  F16C33/52 ,  F16C33/54 ,  F16C33/58 ,  F16C33/76 ,  F16C33/38

    CPC classification number: F16C33/543 ,  F16C19/30 ,  F16C19/32 ,  F16C33/52 ,  F16C33/588 ,  F16C33/761

    Abstract: The separator ring to be used with thrust bearings is an annular member with a plurality of circumferentially separated roller engaging portions. The rollers have outer ends constructed to mate with the roller end engaging portions of the annular member. The roller engaging portions on the annular member may be protrusions extending radially inwardly toward the axis of the bearing with the rollers having depressions on the outer ends for receiving the protrusions or alternatively, the roller engaging portions may be radially outwardly extending depressions with the rollers having outer surfaces which fit into the depressions.

    Abstract translation: 与推力轴承一起使用的分离环是具有多个周向分离的辊接合部分的环形构件。 辊的外端构造成与环形构件的辊端接合部配合。 环形构件上的辊接合部分可以是径向向内朝向轴承的轴线延伸的突出部，其中辊在外端具有凹部以用于接收突起，或者可选地，辊接合部分可以是径向向外延伸的凹部，其中辊具有 外表面适合凹陷。

    Seal including flexible seal strips
    8.
    发明授权
    Seal including flexible seal strips 有权
    密封包括柔性密封条

    公开(公告)号：US09206904B2

    公开(公告)日：2015-12-08

    申请号：US12832141

    申请日：2010-07-08

    Applicant: Ching-Pang Lee ,  Vincent P. Laurello ,  Chander Prakash ,  Kok-Mun Tham

    Inventor： Ching-Pang Lee ,  Vincent P. Laurello ,  Chander Prakash ,  Kok-Mun Tham

    IPC: F16J15/32 ,  F01D11/02

    CPC classification number: F16J15/3292 ,  F01D11/02 ,  F05D2240/57

    Abstract: A seal member for effecting a seal preventing fluid flow in an axial direction through an annular space formed between two relatively moving components including a rotatable shaft and a stator structure. The seal member includes a plurality of flexible seal strips. Each seal strip includes a planar plate extending radially through the annular space and having a radially outer end supported to the stator structure and a radially inner end defining a tip portion extending widthwise in the axial direction engaged in sliding contact with a peripheral surface of the rotatable shaft. At least one of the seal strips includes a plurality of perforations extending through the seal strip and located between a leading edge and a trailing edge of the seal strip for effecting an increased flexibility of the seal strip adjacent to the tip portion.

    Abstract translation: 一种用于实现密封的密封件，其防止流体沿轴向流动通过形成在包括可旋转轴和定子结构的两个相对移动部件之间的环形空间。 密封构件包括多个柔性密封条。 每个密封条包括平面板，该平面板径向地延伸穿过环形空间并且具有支撑到定子结构的径向外端，以及限定沿轴向方向沿宽度方向延伸的尖端部分的径向内端，该尖端部分与可旋转的 轴。 密封条中的至少一个包括延伸穿过密封条并且位于密封条的前缘和后缘之间的多个穿孔，用于实现与尖端部分相邻的密封条的增加的柔性。

    DAMPING RESONATOR WITH IMPINGEMENT COOLING
    9.
    发明申请
    DAMPING RESONATOR WITH IMPINGEMENT COOLING 有权
    阻尼谐振器与冲击冷却

    公开(公告)号：US20120006028A1

    公开(公告)日：2012-01-12

    申请号：US12832116

    申请日：2010-07-08

    Applicant: Ching-Pang Lee ,  Danning You ,  Reinhard Schilp ,  Chander Prakash

    Inventor： Ching-Pang Lee ,  Danning You ,  Reinhard Schilp ,  Chander Prakash

    IPC: F02C7/24 ,  F02C7/12

    CPC classification number: F01D9/023 ,  F02C7/12 ,  F05D2260/96 ,  F23R3/06 ,  F23R2900/00014

    Abstract: A resonance chamber (42) has an outer wall (32) with coolant inlet holes (34A-C), an inner wall (36) with acoustic holes (38), and side walls (40A-C) between the inner and outer walls. A depression (33A-C) in the outer wall has a bottom portion (50) that is close to the inner wall compared to peaks (37A-C) of the outer wall. The coolant inlet holes may be positioned along the bottom portion of the depression and along a bottom portion of the side walls to direct coolant flows (44, 51) toward impingement locations (43) on the inner wall that are out of alignment with the acoustic holes. This improves impingement cooling efficiency. The peaks (37A-C) of the outer wall provide volume in the resonance chamber for a target resonance.

    Abstract translation: 共振室（42）具有外壁（32），其具有冷却剂入口孔（34A-C），具有声孔（38）的内壁（36）和内壁和外壁之间的侧壁（40A-C） 。 外壁上的凹部（33A-C）具有与外壁的顶部（37A-C）相比靠近内壁的底部部分（50）。 冷却剂入口孔可以沿着凹陷的底部部分并且沿着侧壁的底部部分定位，以将冷却剂流（44,41）引向内壁上与声学不对准的冲击位置（43） 孔。 这提高了冲击冷却效率。 外壁的峰（37A-C）在共振室中提供用于目标共振的体积。

    Discreetly Defined Porous Wall Structure for Transpirational Cooling
    10.
    发明申请
    Discreetly Defined Porous Wall Structure for Transpirational Cooling 有权
    用于旋转冷却的谨慎定义的多孔壁结构

    公开(公告)号：US20110262695A1

    公开(公告)日：2011-10-27

    申请号：US12765004

    申请日：2010-04-22

    Applicant: Ching-Pang Lee ,  Chander Prakash ,  Gary B. Merrill ,  Andreas Heselhaus ,  Andrew J. Burns

    Inventor： Ching-Pang Lee ,  Chander Prakash ,  Gary B. Merrill ,  Andreas Heselhaus ,  Andrew J. Burns

    IPC: B32B3/10

    CPC classification number: F01D5/182 ,  B33Y80/00 ,  F01D5/183 ,  F01D5/184 ,  F05D2230/22 ,  F05D2230/90 ,  F05D2250/18 ,  F05D2250/185 ,  F05D2250/28 ,  F05D2250/30 ,  F05D2260/203 ,  F05D2260/221 ,  Y10T428/24273

    Abstract: A wall structure (32, 42, 68, 70, 80) with layers (A, B, C, D, E) of non-random voids (26A, 26B, 28B, 30B) that interconnect to form discretely defined tortuous passages between an interior (21) and an exterior surface (23) of the wall for transpiration cooling of the wall. A coolant flow (38) through the wall may be metered by restrictions in coolant outlets (31) and/or within the passages to minimize the coolant requirement. Pockets (44) may be formed on the exterior surface of the wall for thermal Insulation (46). The layers may be formed by lamination, additive manufacturing, or casting. Layer geometries include alternating layers (A, B, C) with different overlapping void patterns (42), 3-D lattice structures (70), and offset waffle structures (80).

    Abstract translation: 具有非随机空隙（26A，26B，28B，30B）的层（A，B，C，D，E）的壁结构（32,42,68,70,80），其互连以在 所述壁的内部（21）和外表面（23）用于所述壁的蒸发冷却。 通过壁的冷却剂流（38）可以通过冷却剂出口（31）和/或通道内的限制来计量，以使冷却剂需求最小化。 口袋（44）可以形成在隔热壁的外表面上（46）。 层可以通过层压，添加剂制造或铸造形成。 层几何形状包括具有不同重叠空白图案（42），3-D网格结构（70）和偏置华夫饼结构（80）的交替层（A，B，C）。

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