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1. 发明授权

US08839761B2 Augmenter for compound compression engine 有权
标题翻译：复合压缩发动机增压器
公开(公告)号：US08839761B2
公开(公告)日：2014-09-23
申请号：US12830604
申请日：2010-07-06
申请人： Alan B. Minick , Alfred Little
发明人： Alan B. Minick , Alfred Little
IPC分类号： F02B53/08 , F02B53/04 , F02B53/00 , F02B41/06 , F01C11/00 , F01C1/22
CPC分类号： F02B53/00 , F01C1/22 , F01C11/004 , F02B41/06 , Y02T10/17
摘要： A rotary engine includes a first rotary unit operable to provides a first phase of compression to a fresh air charge drawn in through an inlet port to the first rotary unit. A second rotary unit in communication with the first rotary unit through a first passage, the second rotary unit operable to provide a second phase of compression to the first phase of compression, a combustion phase and a first phase of expansion, the second rotary unit in communication with the first rotary unit through a second passage such that the first rotary unit provides a second phase of expansion to the first phase of expansion and an exhaust phase that exhausts the first rotary unit via an exhaust port. A first fuel injector is in communication with the second rotary unit operable to initiate the combustion phase and a second fuel injector is in communication with the first rotary unit operable to selectively initiate augmented operation.
摘要翻译：旋转发动机包括第一旋转单元，其可操作以将第一相压缩提供给通过第一旋转单元的入口吸入的新鲜空气。第二旋转单元，其通过第一通道与第一旋转单元连通，第二旋转单元可操作以向第一压缩阶段，燃烧阶段和第一膨胀阶段提供第二压缩阶段，第二旋转单元通过第二通道与第一旋转单元连通，使得第一旋转单元向第一膨胀阶段提供第二膨胀阶段，以及通过排气口排出第一旋转单元的排气相。第一燃料喷射器与可操作以启动燃烧阶段的第二旋转单元连通，并且第二燃料喷射器与第一旋转单元连通，可操作以选择性地启动增强操作。

2. 发明申请

US20100269782A1 Augmenter For Compound Compression Engine 有权
标题翻译：复合压缩发动机增压器
公开(公告)号：US20100269782A1
公开(公告)日：2010-10-28
申请号：US12830604
申请日：2010-07-06
申请人： Alan B. Minick , Alfred Little
发明人： Alan B. Minick , Alfred Little
IPC分类号： F02B53/10
CPC分类号： F02B53/00 , F01C1/22 , F01C11/004 , F02B41/06 , Y02T10/17
摘要： A rotary engine has a first rotary unit and a second rotary unit. The first rotary unit has a chamber containing a remaining compressed air charge. After combustion in the second rotary unit, the resulting second unit exhaust is in fluid communication with said remaining compressed air charge via a second passageway. An injector is in fluid communication with said remaining compressed air charge in the first rotary unit. The injector injects fuel into the mixture containing the remaining compressed air charge in the first rotary engine and the second unit exhaust from the second rotary engine. This mixture is combusted either with a spark or via auto (diesel) ignition. In this way, the engine produces additional useful work by combusting the remaining compressed air charge and additional fuel. Alternatively, the injector described in the first rotary unit may be located in the second passageway. The injector in the first rotary unit or in the second passageway may be selectively activated throughout the engine's mission.
摘要翻译：旋转发动机具有第一旋转单元和第二旋转单元。第一旋转单元具有包含剩余压缩空气装料的室。在第二旋转单元燃烧之后，所得到的第二单元排气通过第二通道与所述剩余的压缩空气进料流体连通。喷射器与第一旋转单元中的所述剩余压缩空气进料流体连通。喷射器将燃料喷入含有第一旋转发动机中剩余的压缩空气的混合物和来自第二旋转发动机的第二单元排气的混合物中。该混合物通过火花或汽油（柴油）点火燃烧。以这种方式，发动机通过燃烧剩余的压缩空气装料和附加燃料来产生额外的有用功。或者，第一旋转单元中描述的喷射器可以位于第二通道中。在整个发动机的使命中，可以选择性地启动第一旋转单元或第二通道中的喷射器。

3. 发明授权

US07891298B2 Guided projectile 有权
标题翻译：导弹射弹
公开(公告)号：US07891298B2
公开(公告)日：2011-02-22
申请号：US12120355
申请日：2008-05-14
申请人： Alan B. Minick , Stephen Alan Hobart , Frederick Widman , Timothy S. Kokan , Frederic H. Massey
发明人： Alan B. Minick , Stephen Alan Hobart , Frederick Widman , Timothy S. Kokan , Frederic H. Massey
IPC分类号： F42B10/00
CPC分类号： F42B10/663
摘要： A non-propulsive projectile and method of maneuvering the non-propulsive projectile. The non-propulsive projectile includes a divert system with a multiple of valves to maneuver the projectile in response to a control system.
摘要翻译：非推进射弹和非推进射弹的操纵方法。非推进射弹包括一个具有多个阀门的转向系统，以响应于控制系统来操纵射弹。

4. 发明授权

US07823510B1 Extended range projectile 有权
标题翻译：扩展射弹
公开(公告)号：US07823510B1
公开(公告)日：2010-11-02
申请号：US12120345
申请日：2008-05-14
申请人： Stephen Alan Hobart , Timothy S. Kokan , Alan B. Minick , Frederic H. Massey
发明人： Stephen Alan Hobart , Timothy S. Kokan , Alan B. Minick , Frederic H. Massey
IPC分类号： F42B12/20
CPC分类号： F42B10/40
摘要： A projectile and method of extending the range of the projectile. The projectile includes a storage tank operable to release a working fluid through an exhaust manifold to at least partially fill a wake aft of the projectile during projectile flight.
摘要翻译：抛射物和扩大射弹射程的方法。抛射体包括储存罐，其可操作以通过排气歧管释放工作流体，以在射弹飞行期间至少部分地填充射弹的尾迹。

5. 发明申请

US20090159754A1 ROTARY WING SYSTEM WITH ION FIELD FLOW CONTROL 失效
标题翻译：具有离子场流控制的旋转翼系统
公开(公告)号：US20090159754A1
公开(公告)日：2009-06-25
申请号：US11960126
申请日：2007-12-19
申请人： Alan B. Minick
发明人： Alan B. Minick
IPC分类号： B64C11/18 , B64C21/00
CPC分类号： B64C11/18 , B64C23/005 , B64C2230/12 , Y02T50/166
摘要： A rotary-wing system which generates a directed ion field to propel a fluid along a rotary-wing to control at least one boundary layer characteristic.
摘要翻译：旋转翼系统，其产生定向离子场以沿着旋转翼推动流体以控制至少一个边界层特征。

6. 发明授权

US08322981B2 Aircraft fluid diversion inlet louver 有权
标题翻译：飞机液体导流通风台
公开(公告)号：US08322981B2
公开(公告)日：2012-12-04
申请号：US12395849
申请日：2009-03-02
申请人： Stacey H. Light , Alan B. Minick
发明人： Stacey H. Light , Alan B. Minick
IPC分类号： F01D1/02
CPC分类号： F02C7/32 , F02C7/042 , F02C7/047 , F02C7/055
摘要： An inlet system, including for an auxiliary power unit includes an inlet louver mounted to an inlet duct, the inlet louver defines a multiple of vanes positioned to shield the inlet duct from fluids which fall in direction generally transverse to a free stream airflow.
摘要翻译：包括用于辅助动力单元的入口系统包括安装到入口管道的入口百叶窗，入口百叶窗限定了多个叶片，其被定位成将入口管道屏蔽掉，该流体沿着大致横向于自由流气流的方向落下。

7. 发明申请

US20120204535A1 AUGMENTED EXPANDER CYCLE 审中-公开
标题翻译：增加扩展周期
公开(公告)号：US20120204535A1
公开(公告)日：2012-08-16
申请号：US13027868
申请日：2011-02-15
申请人： Alan B. Minick , David C. Gregory
发明人： Alan B. Minick , David C. Gregory
IPC分类号： F02K9/48
CPC分类号： F02K9/46 , F02K9/48 , F02K9/64 , F05D2260/10 , F05D2270/051
摘要： A rocket engine includes a thrust chamber having a cooling channel, which is adapted to provide sustained cracking conditions for a fluid (e.g., kerosene) within the cooling channel under steady-state engine operating conditions. An augmenter having a fluid input communicates with an output of the cooling channel, and an output of the augmenter is in fluid communication with a turbine. A pump is mechanically coupled to the turbine, and provides fluid flow to the inlet of the cooling channel.
摘要翻译：火箭发动机包括具有冷却通道的推力室，其适于在稳态发动机运行条件下为冷却通道内的流体（例如煤油）提供持续的裂解条件。具有流体输入的增压器与冷却通道的输出连通，增压器的输出与涡轮流体连通。泵机械地联接到涡轮机，并且将流体流动提供给冷却通道的入口。

8. 发明申请

US20120018366A1 FLUID SEPARATION SYSTEM WITH REDUCED FOULING 有权
标题翻译：具有减少排水的流体分离系统
公开(公告)号：US20120018366A1
公开(公告)日：2012-01-26
申请号：US13203027
申请日：2009-12-13
申请人： Mark F. Buser , Alan B. Minick
发明人： Mark F. Buser , Alan B. Minick
IPC分类号： B01D63/00
CPC分类号： B01D69/02 , B01D63/10 , B01D65/08 , B01D2313/08 , B01D2313/143 , B01D2313/146 , B01D2321/2016 , B01D2325/08
摘要： A fluid separation system includes a separation membrane having a pattern of features thereon.
摘要翻译：流体分离系统包括其上具有特征图案的分离膜。

9. 发明授权

US08883007B2 Fluid separation system with reduced fouling 有权
标题翻译：流体分离系统结垢减少
公开(公告)号：US08883007B2
公开(公告)日：2014-11-11
申请号：US13203027
申请日：2009-12-13
申请人： Mark F. Buser , Alan B. Minick
发明人： Mark F. Buser , Alan B. Minick
IPC分类号： B01D63/06 , B01D63/10 , B01D69/02 , B01D65/08 , C02F1/44
CPC分类号： B01D69/02 , B01D63/10 , B01D65/08 , B01D2313/08 , B01D2313/143 , B01D2313/146 , B01D2321/2016 , B01D2325/08
摘要： A fluid separation system includes a separation membrane having a pattern of features thereon.
摘要翻译：流体分离系统包括其上具有特征图案的分离膜。

10. 发明申请

US20140077421A1 ADDITIVE MANUFACTURING CHAMBER WITH REDUCED LOAD 有权
标题翻译：具有减少负载的附加制造室
公开(公告)号：US20140077421A1
公开(公告)日：2014-03-20
申请号：US13617775
申请日：2012-09-14
申请人： Alan B. Minick
发明人： Alan B. Minick
IPC分类号： B29C35/08
CPC分类号： B22F3/1055 , B22F2003/1056 , B29C64/153 , B29C64/20 , B33Y10/00 , B33Y30/00 , Y02P10/295
摘要： A disclosed additive manufacturing machine includes a fixed platform defining a work surface for supporting fabrication of a part and a housing defining a chamber over the work surface. A material applicator is supported on the housing for depositing material onto the work surface. An energy directing device is also supported on the housing and directs energy within the chamber to form a part. The housing is movable relative to the work surface therefore moves the energy producing device relative to the work surface to maintain a distance between the energy directing device and a surface of the part during fabrication.
摘要翻译：公开的添加剂制造机器包括固定平台，其限定用于支撑部件制造的工作表面和在工作表面上限定腔室的壳体。材料施加器支撑在壳体上，用于将材料沉积到工作表面上。能量引导装置也支撑在壳体上并且引导室内的能量以形成部件。壳体相对于工作表面是可移动的，因此使能量产生装置相对于工作表面移动，以在制造期间保持能量引导装置与部件表面之间的距离。

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