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1. 发明授权

US07278256B2 Pulsed combustion engine 有权
标题翻译：脉冲内燃机
公开(公告)号：US07278256B2
公开(公告)日：2007-10-09
申请号：US10984461
申请日：2004-11-08
申请人： James W. Norris , Craig A. Nordeen , Wendell V. Twelves, Jr.
发明人： James W. Norris , Craig A. Nordeen , Wendell V. Twelves, Jr.
IPC分类号： F02C5/00
CPC分类号： F23C15/00 , F23R3/002 , F23R3/08 , F23R3/56 , F23R7/00
摘要： A pulsed combustion apparatus includes a conduit having an outer wall and an inner wall. The inner wall has a number of apertures. An interior space is separated from the outer wall by the inner wall. An induction system is positioned to cyclicly admit charges to the interior space. An ignition system is positioned to ignite the charges. Flow directing surfaces are positioned to at least cyclicly direct cooling air through the apertures.
摘要翻译：脉冲燃烧装置包括具有外壁和内壁的导管。内壁具有多个孔。内部空间通过内壁与外壁分离。感应系统被定位成循环地允许电荷到内部空间。定位点火系统以点燃电荷。流动引导表面被定位成至少循环地引导冷却空气通过孔。

2. 发明授权

US07047724B2 Combustion ignition 有权
标题翻译：燃烧点火
公开(公告)号：US07047724B2
公开(公告)日：2006-05-23
申请号：US10334019
申请日：2002-12-30
申请人： Craig A. Nordeen , James W. Norris , Wendell V. Twelves, Jr.
发明人： Craig A. Nordeen , James W. Norris , Wendell V. Twelves, Jr.
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： Distributed initiation (e.g., multipoint or continuous) is utilized to obtain constant volume-like combustion performance in a pulse combustion device in the absence of detonation. A number of such devices may be utilized as turbine engine combustors.
摘要翻译：在不存在爆震的情况下，利用分布式启动（例如，多点或连续）来获得脉冲燃烧装置中恒定体积的燃烧性能。许多这样的装置可以用作涡轮发动机燃烧器。

3. 发明申请

US20100305742A1 System and Method for an Integrated Additive Manufacturing Cell for Complex Components 有权
标题翻译：用于复杂组件的集成添加剂制造单元的系统和方法
公开(公告)号：US20100305742A1
公开(公告)日：2010-12-02
申请号：US12856924
申请日：2010-08-16
申请人： Wendell V. Twelves, JR. , James W. Norris , Bernard J. Raver
发明人： Wendell V. Twelves, JR. , James W. Norris , Bernard J. Raver
IPC分类号： B25J9/00 , G06F17/00
CPC分类号： B23P21/004 , B22F3/1055 , B22F2003/1056 , B23K26/364 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y80/00 , G05B19/4099 , G05B19/4188 , G05B2219/32397 , G05B2219/49016 , Y02P10/295 , Y02P80/40 , Y02P90/24 , Y10T29/51
摘要： An integrated additive manufacturing cell (IAMC) that combines conventional manufacturing technologies with additive manufacturing processes is disclosed. Individual IAMCs may be configured and optimized for specific part families of complex components, or other industrial applications. The IAMCs incorporate features that reduce hardware cost and time and allow for local alloy tailoring for material properties optimization in complex components.
摘要翻译：公开了将常规制造技术与添加剂制造工艺结合在一起的综合添加剂制造单元（IAMC）。单个IAMC可以针对复杂组件或其他工业应用的特定部件系列进行配置和优化。 IAMC结合了降低硬件成本和时间的功能，并允许在复杂组件中进行材料特性优化的局部合金定制。

4. 发明授权

US07748211B2 Vapor cooling of detonation engines 有权
标题翻译：爆震发动机的蒸气冷却
公开(公告)号：US07748211B2
公开(公告)日：2010-07-06
申请号：US11642010
申请日：2006-12-19
申请人： James W. Norris , Wendell V. Twelves, Jr.
发明人： James W. Norris , Wendell V. Twelves, Jr.
IPC分类号： F02K5/02 , F02K7/00
CPC分类号： F02C5/02 , F01D25/12 , F02C7/16 , F02C7/18 , F02C7/224 , F02K7/02 , F05D2220/40 , F05D2260/2322
摘要： An engine cooling system includes a combustion chamber assembly configured to generate detonation waves and a first vapor cooling assembly. The combustion chamber assembly defines a flowpath between an inner liner and an outer liner. The first vapor cooling assembly includes a vaporization section located adjacent to the flowpath and a condenser section spaced from the flowpath, and is configured to transport thermal energy from the vaporization section to the condenser section through cyclical evaporation and condensation of a working medium sealed within the first vapor cooling assembly.
摘要翻译：发动机冷却系统包括构造成产生爆震波的燃烧室组件和第一蒸气冷却组件。燃烧室组件限定内衬和外衬套之间的流路。第一蒸汽冷却组件包括邻近流动路径定位的蒸发部分和与流动路径间隔开的冷凝器部分，并且构造成通过循环蒸发和密封在内部的工作介质中的冷凝将蒸汽部分的热能传送到冷凝器部分第一蒸汽冷却组件。

5. 发明授权

US08383985B2 System and method for an integrated additive manufacturing cell for complex components 有权
标题翻译：用于复杂部件的集成添加剂制造单元的系统和方法
公开(公告)号：US08383985B2
公开(公告)日：2013-02-26
申请号：US12856924
申请日：2010-08-16
申请人： Wendell V. Twelves, Jr. , James W. Norris , Bernard J. Raver
发明人： Wendell V. Twelves, Jr. , James W. Norris , Bernard J. Raver
IPC分类号： B23K26/12 , G06F19/00
CPC分类号： B23P21/004 , B22F3/1055 , B22F2003/1056 , B23K26/364 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y80/00 , G05B19/4099 , G05B19/4188 , G05B2219/32397 , G05B2219/49016 , Y02P10/295 , Y02P80/40 , Y02P90/24 , Y10T29/51
摘要： An integrated additive manufacturing cell (IAMC) that combines conventional manufacturing technologies with additive manufacturing processes is disclosed. Individual IAMCs may be configured and optimized for specific part families of complex components, or other industrial applications. The IAMCs incorporate features that reduce hardware cost and time and allow for local alloy tailoring for material properties optimization in complex components.
摘要翻译：公开了将常规制造技术与添加剂制造工艺结合在一起的综合添加剂制造单元（IAMC）。单个IAMC可以针对复杂组件或其他工业应用的特定部件系列进行配置和优化。 IAMC结合了降低硬件成本和时间的功能，并允许在复杂组件中进行材料特性优化的局部合金定制。

6. 发明授权

US06886325B2 Pulsed combustion engine 失效
标题翻译：脉冲内燃机
公开(公告)号：US06886325B2
公开(公告)日：2005-05-03
申请号：US10722158
申请日：2003-11-24
申请人： James W. Norris , Wendell V. Twelves, Jr.
发明人： James W. Norris , Wendell V. Twelves, Jr.
IPC分类号： F02C3/16 , F02C5/02 , F02C5/04 , F02C5/11 , F02K3/06 , F02K7/02 , F02K7/075 , F02C3/14
CPC分类号： F02C3/165 , F02C3/16 , F02C5/02 , F02C5/04 , F02C5/11 , F02K3/06 , F02K7/02 , 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. A venturi effect may help control fuel/air charge leakage from a flowpath spanning the carousel and a stationary manifold.
摘要翻译：脉冲式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。文丘里效应可以帮助控制从圆盘传送带和固定歧管的流路中的燃料/空气电荷泄漏。

7. 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。

8. 发明授权

US07777155B2 System and method for an integrated additive manufacturing cell for complex components 有权
标题翻译：用于复杂部件的集成添加剂制造单元的系统和方法
公开(公告)号：US07777155B2
公开(公告)日：2010-08-17
申请号：US11708955
申请日：2007-02-21
申请人： Wendell V. Twelves, Jr. , James W. Norris , Bernard J. Raver
发明人： Wendell V. Twelves, Jr. , James W. Norris , Bernard J. Raver
IPC分类号： B23K26/12 , B23P23/02 , G06F19/00
CPC分类号： B23P21/004 , B22F3/1055 , B22F2003/1056 , B23K26/364 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y80/00 , G05B19/4099 , G05B19/4188 , G05B2219/32397 , G05B2219/49016 , Y02P10/295 , Y02P80/40 , Y02P90/24 , Y10T29/51
摘要： An integrated additive manufacturing cell (IAMC) that combines conventional manufacturing technologies with additive manufacturing processes is disclosed. Individual IAMCs may be configured and optimized for specific part families of complex components, or other industrial applications. The IAMCs incorporate features that reduce hardware cost and time and allow for local alloy tailoring for material properties optimization in complex components.
摘要翻译：公开了将常规制造技术与添加剂制造工艺结合在一起的综合添加剂制造单元（IAMC）。单个IAMC可以针对复杂组件或其他工业应用的特定部件系列进行配置和优化。 IAMC结合了降低硬件成本和时间的功能，并允许在复杂组件中进行材料特性优化的局部合金定制。

9. 发明授权

US08468795B2 Diffuser aspiration for a tip turbine engine 有权
标题翻译：尖端涡轮发动机的扩散器抽吸
公开(公告)号：US08468795B2
公开(公告)日：2013-06-25
申请号：US11718525
申请日：2004-12-01
申请人： Gabriel L. Suciu , James W. Norris , Craig A. Nordeen
发明人： Gabriel L. Suciu , James W. Norris , Craig A. Nordeen
IPC分类号： F02K3/02
CPC分类号： F01D5/326 , F02C3/073 , F02C3/08
摘要： A fan-turbine rotor assembly includes a diffuser section (114) which turns and diffuses the airflow from a radial core airflow passage (80) toward an axial airflow direction. Diffuser flow passages communicate with the diffuser passages (144) at a location which reduces separation of the airflow as the airflow is turned from the radial core airflow passage (80) toward an axial airflow direction through airflow aspiration at the potentially turbulent locations.
摘要翻译：风扇 - 涡轮转子组件包括扩散器部分（114），其将来自径向芯气流通道（80）的气流朝向轴向气流方向扩散。扩散器流动通道在一个位置处与扩散通道（144）连通，当气流从径向核心气流通道（80）通过在潜在湍流位置处的气流抽吸朝向轴向气流方向转动时，气流的分离减小。

10. 发明授权

US08104257B2 Tip turbine engine with multiple fan and turbine stages 有权
标题翻译：具有多个风扇和涡轮级的涡轮发动机
公开(公告)号：US08104257B2
公开(公告)日：2012-01-31
申请号：US11719589
申请日：2004-12-01
申请人： James W. Norris , Craig A. Nordeen , Gary Roberge
发明人： James W. Norris , Craig A. Nordeen , Gary Roberge
IPC分类号： F02C3/045
CPC分类号： F02C3/14 , F01D5/022 , F02C3/067 , F02C3/073 , F02K3/068 , F02K3/072 , F05D2260/40311 , Y02T50/673
摘要： A tip turbine engine (10) provides first and second turbines (32) rotatably driven by a combustor (30) generating a high-energy gas stream. The first turbine (32) is mounted at an outer periphery of a first fan (24a), such that the first fan is rotatably driven by the first turbine (32a). The second turbine (32b) is mounted at an outer periphery of a second fan (24b), and is rotatably driven by the high-energy gas stream. In one embodiment, the first turbine (32a) rotatably drives a plurality of stages of first compressor blades (54) in an axial compressor (22) in a first rotational direction, while the second turbine (32b) rotatably drives a plurality of stages of second compressor blades (52) in the axial compressor (22) in a second rotational direction opposite the first. By rotatably driving alternating stages of compressor blades in opposite directions, the efficiency of the axial compressor (22) is increased and/or the number of stages of compressor blades can be reduced. Other variations are described in additional embodiments.
摘要翻译：顶端涡轮发动机（10）提供由可产生高能气流的燃烧器（30）可旋转地驱动的第一和第二涡轮机（32）。第一涡轮（32）安装在第一风扇（24a）的外周，使得第一风扇由第一涡轮机（32a）旋转驱动。第二涡轮（32b）安装在第二风扇（24b）的外周，由高能气流旋转驱动。在一个实施例中，第一涡轮机（32a）以第一旋转方向可旋转地驱动轴向压缩机（22）中的多级第一压缩机叶片（54），而第二涡轮（32b）可旋转地驱动多个级第二压缩机叶片（52）在轴向压缩机（22）中沿与第一压缩机相反的第二旋转方向。通过以相反的方向旋转地驱动压缩机叶片的交替级，轴流式压缩机（22）的效率提高和/或压缩机叶片的级数可以减少。在另外的实施例中描述了其它变型。

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