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21. 发明申请

US20120020805A1 REVERSE CAVITY BLADE FOR A GAS TURBINE ENGINE 有权
标题翻译：用于燃气涡轮发动机的反向空心叶片
公开(公告)号：US20120020805A1
公开(公告)日：2012-01-26
申请号：US12843832
申请日：2010-07-26
申请人： Gabriel L. Suciu , James D. Hill , Gary M. Stetson
发明人： Gabriel L. Suciu , James D. Hill , Gary M. Stetson
IPC分类号： F01D5/14 , B23P15/02
CPC分类号： F01D5/147 , F01D5/18 , F01D5/225 , F01D5/30 , F05D2220/321 , Y10T29/49318 , Y10T29/49336
摘要： A rotor blade for a turbine engine includes an airfoil section which extends from a platform section opposite a root section, the airfoil section defines a cavity which extends from an airfoil tip section toward a root section.
摘要翻译：用于涡轮发动机的转子叶片包括从与根部相对的平台部分延伸的翼型部分，翼型部分限定从翼型部分朝向根部部分延伸的空腔。

22. 发明授权

US07578652B2 Hybrid vapor and film cooled turbine blade 有权
标题翻译：混合蒸汽和薄膜冷却涡轮叶片
公开(公告)号：US07578652B2
公开(公告)日：2009-08-25
申请号：US11542097
申请日：2006-10-03
申请人： James W. Norris , James D. Hill
发明人： James W. Norris , James D. Hill
IPC分类号： F01D5/14
CPC分类号： F01D5/18 , F01D5/082 , F01D5/181 , F01D5/187 , F01D5/3007 , F05D2260/202 , F05D2260/205 , F05D2260/207 , F05D2260/22141
摘要： An apparatus for a gas turbine engine includes an airfoil defining a leading edge and a trailing edge, a root located adjacent to the airfoil, a vapor cooling system, and a film cooling system for cooling the airfoil in conjunction with the vapor cooling system. The vapor cooling system includes a vaporization section located within the airfoil and a condenser section located within the root.
摘要翻译：一种用于燃气涡轮发动机的装置包括限定前缘和后缘的翼型件，与翼型件相邻的根部，蒸汽冷却系统以及用于与蒸气冷却系统一起冷却翼型件的薄膜冷却系统。蒸气冷却系统包括位于机翼内部的蒸发部分和位于根部内部的冷凝器部分。

23. 发明申请

US20090148282A1 3D CONTOURED VANE ENDWALL FOR VARIABLE AREA TURBINE VANE ARRANGEMENT 有权
标题翻译：用于可变区域涡轮风扇装置的3D轮廓端板
公开(公告)号：US20090148282A1
公开(公告)日：2009-06-11
申请号：US11953478
申请日：2007-12-10
申请人： Michael G. McCaffrey , Eric A. Hudson , James D. Hill , Shankar S. Magge , Joel H. Wagner
发明人： Michael G. McCaffrey , Eric A. Hudson , James D. Hill , Shankar S. Magge , Joel H. Wagner
IPC分类号： F01D1/02
CPC分类号： F01D17/162 , F02C9/22
摘要： A turbine section of a gas turbine engine includes an arcuate vane platform segment having a substantially flat surface over which a rotational turbine vane may swing.
摘要翻译：燃气涡轮发动机的涡轮机部分包括具有基本上平坦的表面的弧形叶片平台段，旋转涡轮叶片可绕其旋转。

24. 发明申请

US20080310955A1 Hybrid cooling of a gas turbine engine 有权
标题翻译：燃气轮机的混合冷却
公开(公告)号：US20080310955A1
公开(公告)日：2008-12-18
申请号：US11818035
申请日：2007-06-13
申请人： James W. Norris , Bernard J. Raver , James D. Hill
发明人： James W. Norris , Bernard J. Raver , James D. Hill
IPC分类号： F01D25/10
CPC分类号： F02C7/185 , F02C7/14 , F02C7/224 , F05D2260/205 , F05D2260/207 , F05D2260/213
摘要： A hybrid cooling system for a gas turbine engine includes a vapor cooling assembly and a cooling air cooling assembly. The cooling air cooling assembly is configured to remove thermal energy from cooling air used to cool a first component of the gas turbine engine. The vapor cooling assembly configured to transport thermal energy from a vaporization section to a condenser section through cyclical evaporation and condensation of a working medium sealed within the vapor cooling assembly. The vaporization section is located at least partially within a second component of the gas turbine engine, and the condenser section is located outside the second component.
摘要翻译：用于燃气涡轮发动机的混合冷却系统包括蒸气冷却组件和冷却空气冷却组件。冷却空气冷却组件构造成从用于冷却燃气涡轮发动机的第一部件的冷却空气中去除热能。蒸汽冷却组件被配置成通过循环蒸发和密封在蒸气冷却组件内的工作介质的冷凝将蒸汽部分的热能传送到冷凝器部分。蒸发部分至少部分地位于燃气涡轮发动机的第二部件内，并且冷凝器部分位于第二部件外部。

25. 发明申请

US20080080980A1 Hybrid vapor and film cooled turbine blade 有权
标题翻译：混合蒸汽和薄膜冷却涡轮叶片
公开(公告)号：US20080080980A1
公开(公告)日：2008-04-03
申请号：US11542097
申请日：2006-10-03
申请人： James W. Norris , James D. Hill
发明人： James W. Norris , James D. Hill
IPC分类号： F01D5/18
CPC分类号： F01D5/18 , F01D5/082 , F01D5/181 , F01D5/187 , F01D5/3007 , F05D2260/202 , F05D2260/205 , F05D2260/207 , F05D2260/22141
摘要： An apparatus for a gas turbine engine includes an airfoil defining a leading edge and a trailing edge, a root located adjacent to the airfoil, a vapor cooling system, and a film cooling system for cooling the airfoil in conjunction with the vapor cooling system. The vapor cooling system includes a vaporization section located within the airfoil and a condenser section located within the root.
摘要翻译：一种用于燃气涡轮发动机的装置包括限定前缘和后缘的翼型件，与翼型件相邻的根部，蒸汽冷却系统以及用于与蒸气冷却系统一起冷却翼型件的薄膜冷却系统。蒸气冷却系统包括位于机翼内部的蒸发部分和位于根部内部的冷凝器部分。

26. 发明授权

US06918341B1 Support for securing cantilevered shelving to an insulated unit 失效
标题翻译：支持将悬臂式货架固定在绝缘单元上
公开(公告)号：US06918341B1
公开(公告)日：2005-07-19
申请号：US10054704
申请日：2002-01-24
申请人： John H. Welsch , Robert Welch , Willard J. Sickles , James D. Hill
发明人： John H. Welsch , Robert Welch , Willard J. Sickles , James D. Hill
IPC分类号： A47B47/00 , A47B96/06 , E04B1/61 , E04H5/10 , F25D13/00 , F25D25/02
CPC分类号： E04H5/10 , A47B96/06 , E04B1/6183 , F25D13/00 , F25D25/02
摘要： A support adapted for use between first and second panels at a joint includes a distal end including a flange, an anchoring end including a flange and an anchor, and an intermediate section connecting the distal end and the anchoring end. The intermediate section is shaped to mate with adjoining edges of the first and second panels.
摘要翻译：适于在接头处的第一和第二面板之间使用的支撑件包括包括凸缘的远端，包括凸缘和锚固件的锚定端以及连接远端和锚固端的中间段。中间部分成形为与第一和第二面板的邻接边缘配合。

27. 发明授权

US5896095A Electronic lock with access 失效
标题翻译：电子锁带通道
公开(公告)号：US5896095A
公开(公告)日：1999-04-20
申请号：US852774
申请日：1997-05-07
申请人： James D. Hill , Herman W. Miracle, Jr.
发明人： James D. Hill , Herman W. Miracle, Jr.
IPC分类号： G07C9/00 , G06F7/04 , G07D7/00
CPC分类号： G07C9/00658
摘要： An electronic lock is provided with an emergency technique by which the lock may be possibly opened in the event that the electronic memory used to store the authorized combinations for operation in unlocking of the lock becomes corrupted, damaged or is unable to provide a valid read of storage locations containing combinations. Upon the determination that an invalid read has occurred and that the invalid read has been verified for at least a plurality of additional read cycles, the lock is conditioned to accept an otherwise inoperable master combination for purposes of opening the lock. Under the prescribed conditions, the master combination is capable of opening the lock and providing access to the interior of the container carrying the lock, thus permitting either replacement or repair of the lock and also simultaneously eliminating the need for drilling or other destructive access to the interior of the container.
摘要翻译：电子锁具有紧急技术，通过该技术可以在用于存储锁定解锁操作的授权组合的电子存储器被破坏，损坏或不能提供有效读取的情况下锁定可能被打开包含组合的存储位置。在确定已经发生无效读取并且无效读取已被验证至少多个附加读取周期的情况下，为了打开锁定，锁被调节为接受另外不可操作的主组合。在规定的条件下，主组合能够打开锁并提供进入携带锁的容器的内部，从而允许更换或修理锁，并且同时消除对钻孔或其他破坏性的进入容器内部

28. 发明授权

US09034167B2 Hydrogen/oxygen generator with D.C. servo integrated control 有权
标题翻译：氢气/氧气发生器，具有D.C.伺服集成控制
公开(公告)号：US09034167B2
公开(公告)日：2015-05-19
申请号：US13048677
申请日：2011-03-15
申请人： Timm J. Finfrock , James D. Hill , David A. Bateman, Jr.
发明人： Timm J. Finfrock , James D. Hill , David A. Bateman, Jr.
IPC分类号： C25B1/04 , C25B15/02 , C25B15/08
CPC分类号： C25B1/04 , C25B15/02 , C25B15/08 , Y02E60/366
摘要： A hydrogen/oxygen generation system includes an electrolyzer cell, a servo integrated controller, a power control module, a voltage/current feedback device and a temperature feedback device. Servo closed loop control is used to efficiently and effectively produce hydrogen and oxygen gases.
摘要翻译：氢/氧生成系统包括电解池单元，伺服集成控制器，功率控制模块，电压/电流反馈装置和温度反馈装置。伺服闭环控制用于有效和高效地产生氢气和氧气。

29. 发明授权

US08740567B2 Reverse cavity blade for a gas turbine engine 有权
标题翻译：用于燃气涡轮发动机的反向腔叶片
公开(公告)号：US08740567B2
公开(公告)日：2014-06-03
申请号：US12843832
申请日：2010-07-26
申请人： Gabriel L. Suciu , James D. Hill , Gary M. Stetson
发明人： Gabriel L. Suciu , James D. Hill , Gary M. Stetson
IPC分类号： F01D5/14 , B23P15/02 , F01D5/18 , F01D5/22 , F01D5/30
CPC分类号： F01D5/147 , F01D5/18 , F01D5/225 , F01D5/30 , F05D2220/321 , Y10T29/49318 , Y10T29/49336
摘要： A rotor blade for a turbine engine includes an airfoil section which extends from a platform section opposite a root section, the airfoil section defines a cavity which extends from an airfoil tip section toward a root section.
摘要翻译：用于涡轮发动机的转子叶片包括从与根部相对的平台部分延伸的翼型部分，翼型部分限定从翼型部分朝向根部部分延伸的空腔。

30. 发明授权

US08105019B2 3D contoured vane endwall for variable area turbine vane arrangement 有权
标题翻译：用于可变区域涡轮叶片布置的3D轮廓叶片端壁
公开(公告)号：US08105019B2
公开(公告)日：2012-01-31
申请号：US11953478
申请日：2007-12-10
申请人： Michael G. McCaffrey , Eric A. Hudson , James D. Hill , Shankar S. Magge , Joel H. Wagner
发明人： Michael G. McCaffrey , Eric A. Hudson , James D. Hill , Shankar S. Magge , Joel H. Wagner
IPC分类号： F01D9/02
CPC分类号： F01D17/162 , F02C9/22
摘要： A turbine section of a gas turbine engine includes an arcuate vane platform segment having a substantially flat surface over which a rotational turbine vane may swing.
摘要翻译：燃气涡轮发动机的涡轮机部分包括具有基本上平坦的表面的弧形叶片平台段，旋转涡轮叶片可绕其旋转。

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