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1. 发明授权

US07100360B2 Pulsed combustion engine 有权
标题翻译：脉冲内燃机
公开(公告)号：US07100360B2
公开(公告)日：2006-09-05
申请号：US10608238
申请日：2003-06-27
申请人： Bradley C. Sammann , Wendell V. Twelves, Jr. , Gary D. Jones , James W. Norris , Harvey L. Klein , James E. Jones , Stephen K. Kramer , Douglas A. Thonebe
发明人： Bradley C. Sammann , Wendell V. Twelves, Jr. , Gary D. Jones , James W. Norris , Harvey L. Klein , James E. Jones , Stephen K. Kramer , Douglas A. Thonebe
IPC分类号： F02K3/02
CPC分类号： F02K7/02 , F02C3/16 , F02C3/165 , F02C5/02 , F02C5/04 , F02C5/11 , F02K3/06 , F02K7/075
摘要： A pulsed combustion device includes a support structure and a combustor carousel supported by the support structure and rotating relative thereto about an axis. The carousel has a number of combustion conduits in a circumferential array. Each conduit cyclically receives a charge and discharges combustion products of the charge.
摘要翻译：脉冲燃烧装置包括支撑结构和由支撑结构支撑并相对于其围绕轴线旋转的燃烧器转盘。圆盘传送带具有多个周向排列的燃烧管道。每个管道周期性地接收电荷并排出电荷的燃烧产物。

2. 发明授权

US5374296A Lance carriage 失效
标题翻译：喷枪
公开(公告)号：US5374296A
公开(公告)日：1994-12-20
申请号：US90121
申请日：1993-09-22
申请人： Gary D. Jones
发明人： Gary D. Jones
IPC分类号： C21C5/46 , F27D3/16
CPC分类号： C21C5/462 , F27D3/16
摘要： An elongate lance (4) is raised or lowered by means of a carnage (7) which is guided by vertical channels (8). The lance has lateral projections (18) whereby it is supported in a cradle (17) mounted to carriage (7) via springs (29). The apparatus permits the lance lower end (12) to be submerged in bath (3) and permits restricted lateral movement of the lance lower end.
摘要翻译： PCT No.PCT / AU92 / 00017 Sec。 371日期：1993年9月22日 102（e）日期1993年9月22日PCT提交1992年1月17日PCT公布。公开号WO92 / 13246 日期：1992年8月6日。通过由垂直通道（8）引导的屠体（7）将细长的喷枪（4）升高或降低。喷枪具有横向突起（18），由此其通过弹簧（29）支撑在安装到滑架（7）的支架（17）中。该装置允许喷枪下端（12）浸没在浴（3）中并且允许喷枪下端的受限横向运动。

3. 发明授权

US07697134B1 Correlation spectrometer 有权
标题翻译：相关光谱仪
公开(公告)号：US07697134B1
公开(公告)日：2010-04-13
申请号：US11593386
申请日：2006-11-06
申请人： Michael B. Sinclair , Kent B. Pfeifer , Jeb H. Flemming , Gary D. Jones , Chris P. Tigges
发明人： Michael B. Sinclair , Kent B. Pfeifer , Jeb H. Flemming , Gary D. Jones , Chris P. Tigges
IPC分类号： G01J3/04
CPC分类号： G01J3/457 , G01J3/02 , G01J3/0208 , G01J3/021 , G01J3/0229 , G01J2001/4242
摘要： A correlation spectrometer can detect a large number of gaseous compounds, or chemical species, with a species-specific mask wheel. In this mode, the spectrometer is optimized for the direct measurement of individual target compounds. Additionally, the spectrometer can measure the transmission spectrum from a given sample of gas. In this mode, infrared light is passed through a gas sample and the infrared transmission signature of the gasses present is recorded and measured using Hadamard encoding techniques. The spectrometer can detect the transmission or emission spectra in any system where multiple species are present in a generally known volume.
摘要翻译：相关光谱仪可以用物种特异性掩模轮检测大量气态化合物或化学物质。在这种模式下，光谱仪被优化用于直接测量单个目标化合物。另外，光谱仪可以测量给定的气体样品的透射光谱。在这种模式下，红外光通过气体样品，并使用Hadamard编码技术记录和测量气体的红外透射特征。光谱仪可以检测在通常已知体积中存在多种物质的任何系统中的透射或发射光谱。

4. 发明授权

US6102610A Brittle composite structure for resiliently accomodating thermal expansion 失效
标题翻译：用于弹性适应热膨胀的脆性复合结构
公开(公告)号：US6102610A
公开(公告)日：2000-08-15
申请号：US726978
申请日：1996-10-07
申请人： Mark E. Palusis , Carlos G. Figueroa , Daniel C. Friedberg , Gary D. Jones , Gunther Eichhorn
发明人： Mark E. Palusis , Carlos G. Figueroa , Daniel C. Friedberg , Gary D. Jones , Gunther Eichhorn
IPC分类号： F02K1/80 , F02K1/82 , F16B5/02 , F23R3/00
CPC分类号： F23R3/007 , F02K1/80 , F02K1/822 , F16B5/0241 , F23R3/002 , F05D2260/30 , F05D2300/21 , F05D2300/211 , Y02T50/672 , Y02T50/675 , Y10T403/35 , Y10T403/45 , Y10T403/7123 , Y10T403/7135
摘要： Two composite parts, such as sheet and a hollow gas turbine liner tile, are fastened together using a fastening system that includes a journal bearing that fits in a bore in the sheet and springs to support a bolt fastener that is tightened to hold the parts together. Resilient spacers are placed between the sheet and the liner. The springs may comprise a stack of rings, each ring being a tightly wound helical spring, giving the ring a hollow cross section and resilient qualities.
摘要翻译：诸如片材和中空燃气涡轮机衬垫瓦的两个复合部件使用紧固系统紧固在一起，紧固系统包括嵌合在片材中的孔中的轴颈轴承和用于支撑螺栓紧固件，该螺栓紧固件被紧固以将部件保持在一起。弹性间隔物放置在片材和衬垫之间。弹簧可以包括一叠环，每个环是紧密缠绕的螺旋弹簧，使环具有中空横截面和弹性质量。

5. 发明授权

US06285287B1 Alarm device 有权
标题翻译：报警装置
公开(公告)号：US06285287B1
公开(公告)日：2001-09-04
申请号：US09737787
申请日：2000-12-15
申请人： Heather Jones , Sharon Jones , Gary D. Jones
发明人： Heather Jones , Sharon Jones , Gary D. Jones
IPC分类号： G08B1314
CPC分类号： G08B15/004
摘要： A alarm device for warding off an imminent attack by generating loud warning sounds and generating attention. The alarm device includes a housing including a front wall, a back wall, a pair of side walls and a pair of end walls and designed for securely coupling to a user; a first sound generating device is coupled within the housing and is operationally coupled to a first such that the first sound generating device produces a first sound when the first switch is actuated; a second sound generating device is coupled within the housing operationally coupled to a second switch such that the second sound generating device produces a second sound when the second switch is actuated; and a power source is operationally coupled to the first switch and the second switch such that the power supply provides power to the first sound generating device and the second sound generating device when the first switch and the second switch are actuated.
摘要翻译：一种用于通过产生大声警告声并产生注意来防止即将发生的攻击的报警装置。报警装置包括壳体，其包括前壁，后壁，一对侧壁和一对端壁，并被设计用于牢固地联接到使用者; 第一声音产生装置联接在壳体内并且可操作地耦合到第一声音产生装置，使得当第一开关被致动时，第一声音产生装置产生第一声音; 第二声音产生装置联接在壳体内，可操作地耦合到第二开关，使得当第二开关被致动时，第二声音产生装置产生第二声音; 并且电源可操作地耦合到第一开关和第二开关，使得当第一开关和第二开关被致动时，电源向第一声音产生装置和第二声音产生装置提供电力。

6. 发明授权

US6085581A Method for accurately positioning a device at a desired area of interest 有权
标题翻译：用于将设备精确地定位在期望的感兴趣区域的方法
公开(公告)号：US6085581A
公开(公告)日：2000-07-11
申请号：US195565
申请日：1998-11-18
申请人： Gary D. Jones , Jack E. Houston , Kenneth T. Gillen
发明人： Gary D. Jones , Jack E. Houston , Kenneth T. Gillen
IPC分类号： G01B5/00 , G02B21/00 , G01B5/28 , G01B7/34
CPC分类号： G02B21/0004 , B82Y35/00 , G01Q30/025 , Y10S977/851
摘要： A method for positioning a first device utilizing a surface having a viewing translation stage, the surface being movable between a first position where the viewing stage is in operational alignment with a first device and a second position where the viewing stage is in operational alignment with a second device. The movable surface is placed in the first position and an image is produced with the first device of an identifiable characteristic of a calibration object on the viewing stage. The moveable surface is then placed in the second position and only the second device is moved until an image of the identifiable characteristic in the second device matches the image from the first device. The calibration object is then replaced on the stage of the surface with a test object, and the viewing translation stage is adjusted until the second device images the area of interest. The surface is then moved to the first position where the test object is scanned with the first device to image the area of interest. An alternative embodiment where the devices move is also disclosed.
摘要翻译：一种利用具有观察平移台的表面定位第一装置的方法，所述表面可在观察台与第一装置工作对准的第一位置和观察台与第一装置的操作对准的第二位置之间移动第二设备可移动表面被放置在第一位置，并且在观察台上用校准物体的可识别特征的第一装置产生图像。然后可移动表面被放置在第二位置，并且仅移动第二装置，直到第二装置中的可识别特征的图像与来自第一装置的图像匹配。然后用测试对象在表面的台上更换校准对象，并且调整观察转换级直到第二设备对感兴趣的区域成像。然后将表面移动到第一位置，其中用第一装置扫描测试对象以对感兴趣的区域成像。还公开了设备移动的替代实施例。

7. 发明授权

US5431344A Sliding throat gas turbine engine nozzle 失效
标题翻译：滑动喉咙燃气涡轮发动机喷嘴
公开(公告)号：US5431344A
公开(公告)日：1995-07-11
申请号：US152625
申请日：1993-11-12
申请人： Rudolph J. Novotny , David E. Wendt , Gary D. Jones , James S. Johnson
发明人： Rudolph J. Novotny , David E. Wendt , Gary D. Jones , James S. Johnson
IPC分类号： F02K1/00 , F02K1/12 , F02K1/08 , B64C15/00
CPC分类号： F02K1/002 , F02K1/1261 , Y02T50/671
摘要： Exit area control panels 18 are supported for movement at an angle with respect to the nozzle axis 12. A varying exit area is formed as actuator 26 axially positions the panels 18. In each exit area control panel 18, there is slidably supported a throat area control panel 28, driven by actuator 32. A sliding throat is achieved as the two panels 18,28 are moved in each quadrant. Yaw and pitch vectoring is accomplished with selective positioning of the two panels.
摘要翻译：出口区域控制面板18被支撑成相对于喷嘴轴线12以一定角度运动。当致动器26轴向地定位面板18时，形成变化的出射区域。在每个出口区域控制面板18中，可滑动地支撑着喉部区域控制面板28由致动器32驱动。当两个面板18,28在每个象限中移动时，实现滑动喉部。通过两个面板的选择性定位来实现偏航和俯仰矢量。

8. 发明授权

US06901738B2 Pulsed combustion turbine engine 失效
标题翻译：脉动燃气轮机
公开(公告)号：US06901738B2
公开(公告)日：2005-06-07
申请号：US10608939
申请日：2003-06-26
申请人： Bradley C. Sammann , Wendell V. Twelves, Jr. , Gary D. Jones
发明人： Bradley C. Sammann , Wendell V. Twelves, Jr. , Gary D. Jones
IPC分类号： F02C3/16 , F02C5/02 , F02C5/04 , F02C5/11 , F02C5/00 , F02K3/06
CPC分类号： F02C3/16 , F02C3/165 , F02C5/02 , F02C5/04 , F02C5/11
摘要： A turbine engine has a circumferential array of combustion chamber conduits downstream of the compressor and upstream of the turbine. Means are provided for directing oxygen-containing gas from the compressor to the conduits so as to cyclically feed a gas charge into each conduit through its first port and permit discharge of combustion products of the charge and fuel through both the first and second ports.
摘要翻译：涡轮发动机具有在压缩机下游和涡轮机上游的燃烧室导管的圆周阵列。提供了用于将含氧气体从压缩机引导到管道的装置，以便通过其第一端口循环地将气体进料到每个管道中，并且允许通过第一和第二端口排出燃料和燃料的燃烧产物。

9. 发明授权

US06584765B1 Pulse detonation engine having an aerodynamic valve 有权
标题翻译：具有气动阀的脉冲爆震发动机
公开(公告)号：US06584765B1
公开(公告)日：2003-07-01
申请号：US10026236
申请日：2001-12-21
申请人： David E. Tew , Torger J. Anderson , Roy N. Guile , David R. Sobel , Wendell V. Twelves, Jr. , Gary D. Jones
发明人： David E. Tew , Torger J. Anderson , Roy N. Guile , David R. Sobel , Wendell V. Twelves, Jr. , Gary D. Jones
IPC分类号： F02K702
CPC分类号： F23C15/00 , B64G1/401 , B64G1/402 , F02K7/06 , F02K7/067 , F23C2205/10 , F23C2205/20 , Y02T50/67 , Y02T50/671 , Y10T137/86405 , Y10T137/86743
摘要： A pulse detonation engine (10) is provided with an aerovalve (14) for controlling the pressure of injected propellants (Ox, Fuel) in an open-ended detonation chamber (26). The propellants are injected at such pressure and velocity, and in a direction generally toward a forward thrust wall end (16) of the detonation chamber (26), an aerovalve (14) is formed which effectively inhibits or prevents egress of the propellant from the detonation chamber (26). A shock wave (34) formed by the injected propellant acts, after reflection by the thrust wall end (16) and in combination with the aerovalve (14), to compress and conserve, or increase, the pressure of the injected propellant. Carefully timed ignition (28) effects a detonation pulse under desired conditions of maintained, or increased, pressure. Termination of the propellant injection serves to “open” the aerovalve (14), and exhaust of the combusted propellants occurs to produce thrust. Alternate embodiments of propellant injection mechanisms (12, 112) provide pulse valves (24, 122, 124) each having a fixed slotted disk (40, 140, 240) and a rotating slotted disk (42, 142, 242) to provide the desired high speed valving of discrete pulses of propellant for injection.
摘要翻译：脉冲爆震发动机（10）设置有空气阀（14），用于控制开放式爆震室（26）中喷射的推进剂（Ox，Fuel）的压力。推进剂以这样的压力和速度被注入，并且在大致朝向引爆室（26）的向前推力壁端部（16）的方向上注入，形成了一个空气阀（14），其有效地抑制或防止推进剂从爆震室（26）。由喷射的推进剂形成的冲击波（34）在被推力壁端部（16）反射并与空气阀（14）组合之后作用，以压缩并保存或增加喷射推进剂的压力。仔细定时点火（28）会在保持或增加压力的期望条件下产生爆震脉冲。推进剂喷射的终止用于“打开”空气阀（14），并且发生燃烧的推进剂的排气以产生推力。推进剂喷射机构（12,112）的替代实施例提供脉冲阀（24,122,124），每个脉冲阀具有固定的开槽圆盘（40,140,240）和旋转的开槽圆盘（42,142,242）以提供期望的用于注射的推进剂的离散脉冲的高速阀。

10. 发明授权

US5592814A Attaching brittle composite structures in gas turbine engines for resiliently accommodating thermal expansion 失效
标题翻译：在燃气涡轮发动机中安装脆性复合结构，用于弹性适应热膨胀
公开(公告)号：US5592814A
公开(公告)日：1997-01-14
申请号：US360937
申请日：1994-12-21
申请人： Mark E. Palusis , Carlos G. Figueroa , Daniel C. Friedberg , Gary D. Jones , Gunther Eichhorn
发明人： Mark E. Palusis , Carlos G. Figueroa , Daniel C. Friedberg , Gary D. Jones , Gunther Eichhorn
IPC分类号： F02K1/80 , F02K1/82 , F16B5/02 , F23R3/00 , F02C7/20
CPC分类号： F23R3/007 , F02K1/80 , F02K1/822 , F16B5/0241 , F23R3/002 , F05D2260/30 , F05D2300/21 , F05D2300/211 , Y02T50/672 , Y02T50/675 , Y10T403/35 , Y10T403/45 , Y10T403/7123 , Y10T403/7135
摘要： Two composite parts, such as sheet and a hollow gas turbine liner tile, are fastened together using a fastening system that includes a journal bearing that fits in a bore in the sheet and springs to support a bolt fastener that is tightened to hold the parts together. Resilient spacers are placed between the sheet and the liner. The springs may comprise a stack of rings, each ring being a tightly wound helical spring, giving the ring a hollow cross section and resilient qualities.
摘要翻译：诸如片材和中空燃气涡轮机衬垫瓦的两个复合部件使用紧固系统紧固在一起，所述紧固系统包括嵌合在片材中的孔中的轴颈轴承和用于支撑螺栓紧固件，所述螺栓紧固件被紧固以将部件保持在一起。弹性间隔物放置在片材和衬垫之间。弹簧可以包括一叠环，每个环是紧密缠绕的螺旋弹簧，使环具有中空横截面和弹性质量。

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