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1.发明授权System and method for an integrated additive manufacturing cell for complex components 有权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
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。
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2.发明授权System and method for an integrated additive manufacturing cell for complex components 有权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
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。
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3.发明申请System and Method for an Integrated Additive Manufacturing Cell for Complex Components 有权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
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。
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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。
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公开(公告)号：US08028513B2
公开(公告)日：2011-10-04
申请号：US11977874
申请日：2007-10-26
CPC分类号： F02K3/077 , F02C3/073 , F05D2260/40 , Y02T50/672
摘要： An engine for powering a vehicle, such as a military aircraft or a commercial aircraft, is provided. The engine broadly comprises a main core with a plurality of spools with each spool having a plurality of compressor blades and a plurality of turbine blades attached thereto. One of the spools has a first set of fan blades attached thereto. The engine further has a variable bypass turbine fan formed by a second set of fan blades. The second set of fan blades is arranged outboard of the main core. The second set of fan blades may be decoupled from the first set of fan blades.
摘要翻译： 提供用于为诸如军用飞机或商用飞机的车辆供电的引擎。 发动机广泛地包括具有多个阀芯的主芯，每个阀芯具有多个压缩机叶片和附接到其上的多个涡轮叶片。 其中一个卷轴具有附接到其上的第一组风扇叶片。 发动机还具有由第二组风扇叶片形成的可变旁路涡轮风扇。 第二组风扇叶片布置在主芯的外侧。 第二组风扇叶片可以与第一组风扇叶片分离。
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6.发明申请System and method for an integrated additive manufacturing cell for complex components 有权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：US20080201008A1
公开(公告)日：2008-08-21
申请号：US11708955
申请日：2007-02-21
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。
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公开(公告)号：US20120006034A1
公开(公告)日：2012-01-12
申请号：US13243013
申请日：2011-09-23
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： F02C1/00
CPC分类号： F02C7/185 , F02C7/14 , F02C7/224 , F05D2260/205 , F05D2260/207 , F05D2260/213
摘要： A method for cooling components of a gas turbine engine, having first and second sets of components that require cooling, includes removing thermal energy from cooling air, directing the cooling air from which thermal energy has been removed to the first set of components of the gas turbine engine, and transferring thermal energy away from the second set of components of the gas turbine engine using a vaporization cycle of a vapor cooling assembly. Use of the vaporization cycle offsets thermal energy removed from the cooling air.
摘要翻译： 一种用于冷却具有需要冷却的第一组和第二组件的燃气涡轮发动机的组件的方法，包括从冷却空气中去除热能，将已经从其中排出热能的冷却空气引导到气体的第一组分组件 涡轮发动机，并且使用蒸气冷却组件的蒸发循环将热能转移离开燃气涡轮发动机的第二组部件。 蒸发循环的使用抵消了从冷却空气中除去的热能。
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公开(公告)号：US08656722B2
公开(公告)日：2014-02-25
申请号：US13243013
申请日：2011-09-23
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： F02C6/08
CPC分类号： F02C7/185 , F02C7/14 , F02C7/224 , F05D2260/205 , F05D2260/207 , F05D2260/213
摘要： A method for cooling components of a gas turbine engine, having first and second sets of components that require cooling, includes removing thermal energy from cooling air, directing the cooling air from which thermal energy has been removed to the first set of components of the gas turbine engine, and transferring thermal energy away from the second set of components of the gas turbine engine using a vaporization cycle of a vapor cooling assembly. Use of the vaporization cycle offsets thermal energy removed from the cooling air.
摘要翻译： 一种用于冷却具有需要冷却的第一组和第二组件的燃气涡轮发动机的组件的方法，包括从冷却空气中去除热能，将已经从其中排出热能的冷却空气引导到气体的第一组分组件 涡轮发动机，并且使用蒸气冷却组件的蒸发循环将热能转移离开燃气涡轮发动机的第二组部件。 蒸发循环的使用抵消了从冷却空气中除去的热能。
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公开(公告)号：US08056345B2
公开(公告)日：2011-11-15
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： F02C6/04
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。
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公开(公告)号：US20090107109A1
公开(公告)日：2009-04-30
申请号：US11977874
申请日：2007-10-26
IPC分类号： F02K3/00
CPC分类号： F02K3/077 , F02C3/073 , F05D2260/40 , Y02T50/672
摘要： An engine for powering a vehicle, such as a military aircraft or a commercial aircraft, is provided. The engine broadly comprises a main core with a plurality of spools with each spool having a plurality of compressor blades and a plurality of turbine blades attached thereto. One of the spools has a first set of fan blades attached thereto. The engine further has a variable bypass turbine fan formed by a second set of fan blades. The second set of fan blades is arranged outboard of the main core. The second set of fan blades may be decoupled from the first set of fan blades.
摘要翻译： 提供用于为诸如军用飞机或商用飞机的车辆供电的引擎。 发动机广泛地包括具有多个卷轴的主芯，每个卷轴具有多个压缩机叶片和附接到其上的多个涡轮叶片。 其中一个卷轴具有附接到其上的第一组风扇叶片。 发动机还具有由第二组风扇叶片形成的可变旁路涡轮风扇。 第二组风扇叶片布置在主芯的外侧。 第二组风扇叶片可以与第一组风扇叶片分离。
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