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1. 发明授权

US09193290B2 Removable storage arrangement for a vehicle 有权
标题翻译：车辆可移动存储装置
公开(公告)号：US09193290B2
公开(公告)日：2015-11-24
申请号：US13554095
申请日：2012-07-20
申请人： Robert R. Lazarevich , David B. Reed , Peter W. Mattes , Gary D. Lock
发明人： Robert R. Lazarevich , David B. Reed , Peter W. Mattes , Gary D. Lock
IPC分类号： B60R7/00 , B60R11/00 , B60P3/14 , B60R7/02 , B60R7/04 , B60R9/00 , B60R11/06
CPC分类号： B60P3/14 , B60R7/02 , B60R7/04 , B60R9/00 , B60R11/06
摘要： A cargo management system can include a receptacle and a removable storage device. The receptacle can be formed relative to an exterior panel of the vehicle and can have a rear wall spaced apart from an outer surface of the exterior panel. The outer surface can have a first contour. The removable storage device can be removably received in the receptacle and selectively secured to the vehicle. The storage device can include an upper portion, a lower portion and a latch mechanism. The upper portion can be pivotable relative to the lower portion to provide access to an interior of the storage device. The latch mechanism can selectively secure the storage device to the vehicle when in a stored position in the receptacle. An outer surface of the upper portion and the lower portion can include a second contour, where the second contour can substantially match the first contour.
摘要翻译：货物管理系统可以包括插座和可移动存储装置。容器可以相对于车辆的外部面板形成，并且可以具有与外部面板的外表面间隔开的后壁。外表面可以具有第一轮廓。可移动存储装置可以可拆卸地容纳在容器中并选择性地固定到车辆上。存储装置可以包括上部，下部和闩锁机构。上部部分可相对于下部部分枢转，以提供对存储装置内部的通路。当处于容器中的存储位置时，闩锁机构可以将存储装置选择性地固定到车辆。上部和下部的外表面可以包括第二轮廓，其中第二轮廓可以基本上匹配第一轮廓。

2. 发明授权

US06241468B1 Coolant passages for gas turbine components 有权
标题翻译：燃气轮机部件的冷却液通道
公开(公告)号：US06241468B1
公开(公告)日：2001-06-05
申请号：US09401993
申请日：1999-09-23
申请人： Gary D Lock , Martin L G Oldfield
发明人： Gary D Lock , Martin L G Oldfield
IPC分类号： F01D514
CPC分类号： F01D5/186 , F05D2250/323
摘要： A gas turbine engine component, typically either a turbine blade or vane or combustor, comprising a wall (40) with a first surface (39) which is adapted to be supplied with a flow of cooling air, and a second surface (38) which is adapted to be exposed to a hot gas stream (50). The wall (40) further having defined therein a plurality of passages (57), the passages (57) defined by passage walls (54), which interconnect a passage inlet (31) in said first surface (39) to a passage outlet (32) in said the second surface (38). The passages (57), cooling air and the hot gas stream (50) arranged such that in operation a flow (52) of cooling air is directed through said passages (57) to provide a flow (36) of cooling air over at least a portion of the second surface (39). The cross sectional area of each of the passages (57) progressively decreasing overall, in the direction of cooling air flow (52) through the passage (57), such that in use the flow of cooling air (52) through the passage (57) is accelerated. The passage walls (54) of the cooling passages (57) preferably diverging laterally across the wall (40) of the component whilst perpendicular to the wall (40) they converge so that overall the cross-sectional area decreases.
摘要翻译：一种燃气涡轮发动机部件，通常是涡轮机叶片或叶片或燃烧器，其包括具有第一表面（39）的壁（40），第一表面（39）适于被供应冷却空气流，第二表面（38）适于暴露于热气流（50）。进一步在其中限定有多个通道（57）的壁（40），由通道壁（54）限定的通道（57），其将所述第一表面（39）中的通道入口（31）与通道出口 32）在所述第二表面（38）中。通道（57），冷却空气和热气流（50）被布置成使得在操作中冷却空气的流动（52）被引导通过所述通道（57），以提供至少冷却空气的流（36）第二表面（39）的一部分。每个通道（57）的横截面积在通过通道（57）的冷却空气流（52）的方向上逐渐减小，使得在使用中通过通道（57）的冷却空气（52）的流动）加速。冷却通道（57）的通道壁（54）优选地横向穿过部件的壁（40）发散，同时垂直于壁（40）会聚，使得横截面积总体减小。

3. 发明申请

US20140003919A1 FINNED SEAL ASSEMBLY FOR GAS TURBINE ENGINES 有权
标题翻译：用于气体涡轮发动机的精密密封组件
公开(公告)号：US20140003919A1
公开(公告)日：2014-01-02
申请号：US13534060
申请日：2012-06-27
申请人： Ching-Pang Lee , Kok-Mun Tham , John M. Owen , Gary D. Lock , Carl M. Sangan , Vincent P. Laurello
发明人： Ching-Pang Lee , Kok-Mun Tham , John M. Owen , Gary D. Lock , Carl M. Sangan , Vincent P. Laurello
IPC分类号： F01D11/00
CPC分类号： F01D11/001
摘要： A seal assembly provided between a hot gas path and a disc cavity in a turbine engine includes an annular outer wing member extending from an axially facing side of a rotor structure toward an adjacent non-rotating vane assembly, and a plurality of fins extending radially inwardly from the outer wing member and extending toward the adjacent non-rotating vane assembly. The fins are arranged such that a space having a component in a circumferential direction is defined between adjacent fins. Rotation of the fins during operation of the engine effects a pumping of purge air from the disc cavity toward the hot gas path to assist in limiting hot working gas leakage from the hot gas path to the disc cavity by forcing the hot working gas away from the seal assembly.
摘要翻译：设置在涡轮发动机中的热气体路径和盘腔之间的密封组件包括从转子结构的轴向相对侧朝向相邻的非旋转叶片组件延伸的环形外翼构件，以及径向向内延伸的多个翅片从外翼构件延伸并且朝向相邻的非旋转叶片组件延伸。翅片被布置成使得在相邻翅片之间限定具有圆周方向的部件的空间。在发动机操作期间，翅片的旋转使得吹扫空气从盘腔朝向热气体路径泵送，以通过迫使热的工作气体远离热空气路径来帮助限制热的工作气体从热气体路径泄漏到盘腔中密封组装。

4. 发明申请

US20140021232A1 REMOVABLE STORAGE ARRANGEMENT FOR A VEHICLE 有权
标题翻译：可拆卸的车辆存放安排
公开(公告)号：US20140021232A1
公开(公告)日：2014-01-23
申请号：US13554095
申请日：2012-07-20
申请人： Robert R. Lazarevich , David B. Reed , Peter W. Mattes , Gary D. Lock
发明人： Robert R. Lazarevich , David B. Reed , Peter W. Mattes , Gary D. Lock
IPC分类号： B60R7/00 , B62B1/00
CPC分类号： B60P3/14 , B60R7/02 , B60R7/04 , B60R9/00 , B60R11/06
摘要： A cargo management system can include a receptacle and a removable storage device. The receptacle can be formed relative to an exterior panel of the vehicle and can have a rear wall spaced apart from an outer surface of the exterior panel. The outer surface can have a first contour. The removable storage device can be removably received in the receptacle and selectively secured to the vehicle. The storage device can include an upper portion, a lower portion and a latch mechanism. The upper portion can be pivotable relative to the lower portion to provide access to an interior of the storage device. The latch mechanism can selectively secure the storage device to the vehicle when in a stored position in the receptacle. An outer surface of the upper portion and the lower portion can include a second contour, where the second contour can substantially match the first contour.
摘要翻译：货物管理系统可以包括插座和可移动存储装置。容器可以相对于车辆的外部面板形成，并且可以具有与外部面板的外表面间隔开的后壁。外表面可以具有第一轮廓。可移动存储装置可以可拆卸地容纳在容器中并选择性地固定到车辆上。存储装置可以包括上部，下部和闩锁机构。上部部分可相对于下部部分枢转，以提供对存储装置内部的通路。当处于容器中的存储位置时，闩锁机构可以将存储装置选择性地固定到车辆。上部和下部的外表面可以包括第二轮廓，其中第二轮廓可以基本上匹配第一轮廓。

5. 发明授权

US09121298B2 Finned seal assembly for gas turbine engines 有权
标题翻译：燃气涡轮发动机的翅片密封组件
公开(公告)号：US09121298B2
公开(公告)日：2015-09-01
申请号：US13534060
申请日：2012-06-27
申请人： Ching-Pang Lee , Kok-Mun Tham , John M. Owen , Gary D. Lock , Carl M. Sangan , Vincent P. Laurello
发明人： Ching-Pang Lee , Kok-Mun Tham , John M. Owen , Gary D. Lock , Carl M. Sangan , Vincent P. Laurello
IPC分类号： F04D11/00 , F01D11/00
CPC分类号： F01D11/001
摘要： A seal assembly provided between a hot gas path and a disc cavity in a turbine engine includes an annular outer wing member extending from an axially facing side of a rotor structure toward an adjacent non-rotating vane assembly, and a plurality of fins extending radially inwardly from the outer wing member and extending toward the adjacent non-rotating vane assembly. The fins are arranged such that a space having a component in a circumferential direction is defined between adjacent fins. Rotation of the fins during operation of the engine effects a pumping of purge air from the disc cavity toward the hot gas path to assist in limiting hot working gas leakage from the hot gas path to the disc cavity by forcing the hot working gas away from the seal assembly.
摘要翻译：设置在涡轮发动机中的热气体路径和盘腔之间的密封组件包括从转子结构的轴向相对侧朝向相邻的非旋转叶片组件延伸的环形外翼构件，以及径向向内延伸的多个翅片从外翼构件延伸并且朝向相邻的非旋转叶片组件延伸。翅片被布置成使得在相邻翅片之间限定具有圆周方向的部件的空间。在发动机操作期间，翅片的旋转使得吹扫空气从盘腔朝向热气体路径泵送，以通过迫使热的工作气体远离热空气路径来帮助限制热的工作气体从热气体路径泄漏到盘腔中密封组装。

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