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1. 发明申请

US20130145744A1 SYSTEM FOR DIRECTING AIR FLOW TO A PLURALITY OF PLENA 有权
标题翻译：用于指导空气流向多个PLENA的系统
公开(公告)号：US20130145744A1
公开(公告)日：2013-06-13
申请号：US13316960
申请日：2011-12-12
申请人： Charles Lo , Ted Alford , Morris Anderson
发明人： Charles Lo , Ted Alford , Morris Anderson
IPC分类号： F02C6/08 , F02C7/12 , F02K3/02
CPC分类号： F01D17/105 , F02C6/08 , F02C7/141 , F02K3/075 , F02K3/115 , Y02T50/675
摘要： A system for directing air flow to separate plena of a compartment that is defined at least by a compartment wall includes a NACA scoop, and a Pitot scoop. The NACA scoop is formed in the compartment wall, and includes two side walls, a bottom wall, and an entrance lip that is defined by the compartment wall and is spaced apart from the bottom wall to form a NACA scoop air inlet. The Pitot scoop is longitudinally aligned with the NACA scoop, includes a Pitot scoop air inlet, a Pitot scoop air outlet, and a Pitot scoop flow passage.
摘要翻译：用于将空气流引导至至少由隔室壁限定的隔室的分隔体的系统包括NACA勺和皮托勺。 NACA勺形成在隔室壁中，并且包括两个侧壁，底壁和由隔室壁限定并与底壁间隔开以形成NACA勺式空气入口的入口唇缘。皮托勺与NACA勺纵向对齐，包括皮托勺空气入口，皮托勺空气出口和皮托勺流道。

2. 发明申请

US20110126512A1 TURBOFAN GAS TURBINE ENGINE AERODYNAMIC MIXER 审中-公开
标题翻译： TURBOFAN气体涡轮发动机动力混合器
公开(公告)号：US20110126512A1
公开(公告)日：2011-06-02
申请号：US12627141
申请日：2009-11-30
申请人： Morris Anderson
发明人： Morris Anderson
IPC分类号： F02K3/06 , F02K1/48
CPC分类号： F02K1/386 , F05D2200/261 , F05D2200/262 , F05D2250/184 , F05D2250/61
摘要： A mixer for a turbofan engine includes a centerbody and a mixer nozzle. The mixer nozzle surrounds at least a portion of the centerbody and is spaced apart to define a core flow path between the mixer nozzle and the centerbody. The mixer nozzle is configured, when bypass air flows through the turbofan engine, to direct at least a portion of the bypass air to impinge on the centerbody. The mixer nozzle includes a plurality of circumferentially spaced mixer lobes that extend axially in a rearward direction and have a cross-section shape defined by a set of equations.
摘要翻译：用于涡轮风扇发动机的混合器包括中心体和混合器喷嘴。混合器喷嘴围绕中心体的至少一部分并且间隔开以限定混合器喷嘴和中心体之间的芯流动路径。当旁路空气流过涡轮风扇发动机时，混合器喷嘴构造成引导至少一部分旁路空气撞击中心体。混合器喷嘴包括沿向后方向轴向延伸并且具有由一组方程定义的横截面形状的多个周向间隔开的混合器凸角。

3. 发明申请

US20100126182A1 FLUSH INLET SCOOP DESIGN FOR AIRCRAFT BLEED AIR SYSTEM 有权
标题翻译：用于飞机吹扫空气系统的冲洗入口设计（FLUSH INLET SCOOP DESIGN FOR AIRCRAFT BLEED AIR SYSTEM）
公开(公告)号：US20100126182A1
公开(公告)日：2010-05-27
申请号：US12275990
申请日：2008-11-21
申请人： Robert Hoover , Morris Anderson , Robert Romano , Jeff Mendoza , Dan Judd , Don Weir
发明人： Robert Hoover , Morris Anderson , Robert Romano , Jeff Mendoza , Dan Judd , Don Weir
IPC分类号： F02C7/04
CPC分类号： F02K3/06 , F01D17/105 , F02C9/18 , Y02T50/672
摘要： A bleed air duct that preferably includes an inlet section configured to include a flush scoop and a louver. The louver is located and configured such that in the desired operating flow range of the duct, the fluid entering the flush scoop is disturbed and as a result creates a low pressure region downstream of the louver. The low pressure region substantially eliminates the generation of any pressure pulses and acoustic resonance also known as Helmholtz resonance.
摘要翻译：排气管道，优选地包括配置成包括冲洗铲斗和百叶窗的入口部分。百叶窗的位置和构造使得在管道的期望的操作流动范围内，进入冲洗铲斗的流体受到干扰，结果在百叶窗下游产生低压区域。低压区域基本上消除了任何压力脉冲和声谐振的产生，也称为亥姆霍兹共振。

4. 发明申请

US20070089396A1 Eductor swirl buster 失效
标题翻译：电感漩涡破坏
公开(公告)号：US20070089396A1
公开(公告)日：2007-04-26
申请号：US11259700
申请日：2005-10-25
申请人： Morris Anderson
发明人： Morris Anderson
IPC分类号： F02K9/68
CPC分类号： B64D41/00 , B64D2041/002 , F01D25/30 , F02K1/386 , F05D2220/50 , F05D2240/12 , F05D2250/13 , F05D2250/312 , F05D2260/221 , F05D2260/601 , Y02T50/676
摘要： A system is provided in an aircraft that includes a power unit and an eductor. The power unit has a nozzle, and is configured to exhaust gas, a portion of which flows in a swirling motion, through the nozzle. The eductor communicates with the power unit and includes a housing and a plurality of flow straighteners. The housing has an inlet, an outlet, and an inner peripheral surface that defines a flow passage. The inlet is configured to surround at least a portion of the nozzle and to receive the gas, and the outlet is configured to exhaust the gas. The plurality of flow straighteners extend radially inwardly from the housing inner surface into the flow passage and are configured to reduce swirl motion of the gas that flows therethrough. The power unit may be an auxiliary power unit or a turboshaft engine.
摘要翻译：在包括动力单元和喷射器的飞行器中提供系统。动力单元具有喷嘴，并被构造成通过喷嘴排出其一部分以旋转运动流动的气体。喷射器与动力单元连通并且包括壳体和多个流动矫直机。壳体具有入口，出口和限定流动通道的内周表面。入口构造成围绕喷嘴的至少一部分并且接收气体，并且出口构造成排出气体。多个流动矫直机从壳体内表面径向向内延伸到流动通道中并且构造成减少流过其中的气体的旋转运动。动力单元可以是辅助动力单元或涡轮轴发动机。

5. 发明申请

US20050284128A1 Rocket motor nozzle throat area control system and method 有权
标题翻译：火箭发动机喷嘴喉部控制系统及方法
公开(公告)号：US20050284128A1
公开(公告)日：2005-12-29
申请号：US10880858
申请日：2004-06-29
申请人： Morris Anderson , Jason Gratton , George Woessner
发明人： Morris Anderson , Jason Gratton , George Woessner
IPC分类号： F02K9/26 , F02K9/82
CPC分类号： F02K9/26 , F02K9/82
摘要： A solid rocket motor including a combustion chamber, in which propellant is ignited to produce combustion gas, and a nozzle having a throat with an effective flow area, implements a system and method to inject gas into the nozzle throat to control its effective cross sectional flow area. Controlling the effective cross sectional flow area of the nozzle throat in turn controls combustion chamber pressure, thus the burn rate of the propellant in the combustion chamber, and thus the thrust generated thereby.
摘要翻译：一种固体火箭发动机，其包括燃烧室，其中推进剂被点燃以产生燃烧气体，以及具有有效流动面积的喉部的喷嘴，实现了将气体注入喷嘴喉部以控制其有效截面流量的系统和方法区。控制喷嘴喉部的有效截面流动面积又控制燃烧室压力，从而控制燃烧室中的推进剂的燃烧速率，从而控制由此产生的推力。

6. 发明授权

US1904163A Draft device 失效
公开(公告)号：US1904163A
公开(公告)日：1933-04-18
申请号：US53407031
申请日：1931-04-30
申请人： MORRIS ANDERSON F
发明人： MORRIS ANDERSON F
IPC分类号： B60T7/20
CPC分类号： B60T7/20

7. 发明申请

US20060032229A1 Effusion momentum control 有权
公开(公告)号：US20060032229A1
公开(公告)日：2006-02-16
申请号：US10919663
申请日：2004-08-16
申请人： Morris Anderson , Hiroshi Kawamura , Luis Flamand
发明人： Morris Anderson , Hiroshi Kawamura , Luis Flamand
IPC分类号： F23R3/42
CPC分类号： F23R3/002 , F23R2900/03041
摘要： A combustor liner for shielding an engine from heat generated in a combustion zone includes a sheet with a cool surface for intercepting a cooling air stream and a hot surface enclosing the combustion zone, the combustor liner further including an array of effusion holes extending from the cool surface to the hot surface to allow a portion of the cooling air stream to pass through the effusion holes into the combustion zone, where a portion of the array includes a plurality of upstream-pointed effusion holes oriented such that each upstream-pointed effusion hole has an orientation obtuse to a direction of main flow in the combustion zone so as to control the momentum of cooling air passing into the combustion zone.

8. 发明授权

US09045998B2 System for directing air flow to a plurality of plena 有权
标题翻译：用于将气流引导到多个斑块的系统
公开(公告)号：US09045998B2
公开(公告)日：2015-06-02
申请号：US13316960
申请日：2011-12-12
申请人： Charles Lo , Ted Alford , Morris Anderson
发明人： Charles Lo , Ted Alford , Morris Anderson
IPC分类号： F02K7/08 , F02K7/10 , F01D17/10 , F02K3/115 , F02K3/075 , F02C7/141
CPC分类号： F01D17/105 , F02C6/08 , F02C7/141 , F02K3/075 , F02K3/115 , Y02T50/675
摘要： A system for directing air flow to separate plena of a compartment that is defined at least by a compartment wall includes a NACA scoop, and a Pitot scoop. The NACA scoop is formed in the compartment wall, and includes two side walls, a bottom wall, and an entrance lip that is defined by the compartment wall and is spaced apart from the bottom wall to form a NACA scoop air inlet. The Pitot scoop is longitudinally aligned with the NACA scoop, includes a Pitot scoop air inlet, a Pitot scoop air outlet, and a Pitot scoop flow passage.
摘要翻译：用于将空气流引导至至少由隔室壁限定的隔室的分隔体的系统包括NACA勺和皮托勺。 NACA勺形成在隔室壁中，并且包括两个侧壁，底壁和由隔室壁限定并与底壁间隔开以形成NACA勺式空气入口的入口唇缘。皮托勺与NACA勺纵向对齐，包括皮托勺空气入口，皮托勺空气出口和皮托勺流道。

9. 发明授权

US08024935B2 Flush inlet scoop design for aircraft bleed air system 有权
标题翻译：用于飞机排气系统的冲洗入口勺设计
公开(公告)号：US08024935B2
公开(公告)日：2011-09-27
申请号：US12275990
申请日：2008-11-21
申请人： Robert Hoover , Morris Anderson , Robert Romano , Jeff Mendoza , Dan Judd , Don Weir
发明人： Robert Hoover , Morris Anderson , Robert Romano , Jeff Mendoza , Dan Judd , Don Weir
IPC分类号： F02C6/04
CPC分类号： F02K3/06 , F01D17/105 , F02C9/18 , Y02T50/672
摘要： A bleed air duct that preferably includes an inlet section configured to include a flush scoop and a louver. The louver is located and configured such that in the desired operating flow range of the duct, the fluid entering the flush scoop is disturbed and as a result creates a low pressure region downstream of the louver. The low pressure region substantially eliminates the generation of any pressure pulses and acoustic resonance also known as Helmholtz resonance.
摘要翻译：排气管道，优选地包括配置成包括冲洗铲斗和百叶窗的入口部分。百叶窗的位置和构造使得在管道的期望的操作流动范围内，进入冲洗铲斗的流体受到干扰，结果在百叶窗下游产生低压区域。低压区域基本上消除了任何压力脉冲和声谐振的产生，也称为亥姆霍兹共振。

10. 发明授权

US3521704A Heat exchanger for recreational vehicle 失效
标题翻译：热交换器用于娱乐车辆
公开(公告)号：US3521704A
公开(公告)日：1970-07-28
申请号：US3521704D
申请日：1968-07-22
申请人： JAMES EARL BRIDEGUM , ANDREW MORRIS ANDERSON
发明人： BRIDEGUM JAMES EARL
IPC分类号： B60P3/36 , F24D17/00 , F28D19/00 , G01M3/00 , F28F11/00
CPC分类号： F28D19/00 , B60P3/36 , F24D17/001 , G01M3/00

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