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    APPARATUS FOR COMBUSTING A FUEL AT HIGH PRESSURE AND HIGH TEMPERATURE, AND ASSOCIATED SYSTEM
    1.
    发明申请
    APPARATUS FOR COMBUSTING A FUEL AT HIGH PRESSURE AND HIGH TEMPERATURE, AND ASSOCIATED SYSTEM 有权
    用于燃烧高压和高温燃料的装置及相关系统

    公开(公告)号：US20120073261A1

    公开(公告)日：2012-03-29

    申请号：US13220439

    申请日：2011-08-29

    申请人： Miles R. Palmer ,  Rodney John Allam ,  Glenn William Brown, JR. ,  Jeremy Eron Fetvedt

    发明人： Miles R. Palmer ,  Rodney John Allam ,  Glenn William Brown, JR. ,  Jeremy Eron Fetvedt

    IPC分类号： F02C3/20 ,  F23M5/08 ,  F23D14/62 ,  F23L7/00 ,  F23D1/00 ,  F23C1/12

    CPC分类号： F23L7/007 ,  F02C3/26 ,  F23C5/32 ,  F23C7/08 ,  F23C2900/03004 ,  F23D1/005 ,  F23J15/027 ,  F23L7/00 ,  F23L9/00 ,  F23L2900/07002 ,  F23M5/085 ,  F23M2900/05004 ,  Y02E20/322 ,  Y02E20/344

    摘要： A combustor apparatus is provided, comprising a mixing arrangement for mixing a carbonaceous fuel with enriched oxygen and a working fluid to form a fuel mixture. A combustion chamber is at least partially defined by a porous perimetric transpiration member, at least partially surrounded by a pressure containment member. The combustion chamber has longitudinally spaced apart inlet and outlet portions. The fuel mixture is received by the inlet portion for combustion within the combustion chamber at a combustion temperature to form a combustion product. The combustion chamber directs the combustion product longitudinally toward the outlet portion. The transpiration member is configured to substantially uniformly direct a transpiration substance therethrough toward the combustion chamber, such that the transpiration substance is directed to flow helically about the perimeter and longitudinally between the inlet and outlet portions, for buffering interaction between the combustion product and the transpiration member. Associated systems are also provided.

    摘要翻译： 提供了一种燃烧器装置，其包括用于混合含碳燃料和富氧的混合装置和工作流体以形成燃料混合物。 燃烧室至少部分地由多孔周边蒸腾构件限定，至少部分地被压力容纳构件包围。 燃烧室具有纵向间隔开的入口和出口部分。 燃料混合物被入口部分接收以在燃烧室内在燃烧温度下燃烧以形成燃烧产物。 燃烧室将燃烧产物纵向引导到出口部分。 蒸腾构件构造成基本均匀地将蒸腾物质引导通过其朝向燃烧室，使得蒸腾物质被引导以围绕周边螺旋地流动并且在入口部分和出口部分之间纵向流动，以缓冲燃烧产物和蒸腾作用之间的相互作用 会员。 还提供了相关系统。

    Apparatus for combusting a fuel at high pressure and high temperature, and associated system
    2.
    发明授权
    Apparatus for combusting a fuel at high pressure and high temperature, and associated system 有权
    用于在高压和高温下燃烧燃料的装置以及相关系统

    公开(公告)号：US08986002B2

    公开(公告)日：2015-03-24

    申请号：US13220439

    申请日：2011-08-29

    申请人： Miles R. Palmer ,  Rodney John Allam ,  Glenn William Brown, Jr. ,  Jeremy Eron Fetvedt

    发明人： Miles R. Palmer ,  Rodney John Allam ,  Glenn William Brown, Jr. ,  Jeremy Eron Fetvedt

    IPC分类号： F23C7/00 ,  F23L7/00 ,  F23J15/02 ,  F23M5/08

    CPC分类号： F23L7/007 ,  F02C3/26 ,  F23C5/32 ,  F23C7/08 ,  F23C2900/03004 ,  F23D1/005 ,  F23J15/027 ,  F23L7/00 ,  F23L9/00 ,  F23L2900/07002 ,  F23M5/085 ,  F23M2900/05004 ,  Y02E20/322 ,  Y02E20/344

    摘要： A combustor apparatus is provided, comprising a mixing arrangement for mixing a carbonaceous fuel with enriched oxygen and a working fluid to form a fuel mixture. A combustion chamber is at least partially defined by a porous perimetric transpiration member, at least partially surrounded by a pressure containment member. The combustion chamber has longitudinally spaced apart inlet and outlet portions. The fuel mixture is received by the inlet portion for combustion within the combustion chamber at a combustion temperature to form a combustion product. The combustion chamber directs the combustion product longitudinally toward the outlet portion. The transpiration member is configured to substantially uniformly direct a transpiration substance therethrough toward the combustion chamber, such that the transpiration substance is directed to flow helically about the perimeter and longitudinally between the inlet and outlet portions, for buffering interaction between the combustion product and the transpiration member. Associated systems are also provided.

    摘要翻译： 提供了一种燃烧器装置，其包括用于混合含碳燃料和富氧的混合装置和工作流体以形成燃料混合物。 燃烧室至少部分地由多孔周边蒸腾构件限定，至少部分地被压力容纳构件包围。 燃烧室具有纵向间隔开的入口和出口部分。 燃料混合物被入口部分接收以在燃烧室内在燃烧温度下燃烧以形成燃烧产物。 燃烧室将燃烧产物纵向引导到出口部分。 蒸腾构件构造成基本均匀地将蒸腾物质引导通过其朝向燃烧室，使得蒸腾物质被引导以围绕周边螺旋地流动并且在入口部分和出口部分之间纵向流动，以缓冲燃烧产物和蒸腾作用之间的相互作用 会员。 还提供了相关系统。

    APPARATUS FOR COMBUSTING A FUEL AT HIGH PRESSURE AND HIGH TEMPERATURE, AND ASSOCIATED SYSTEM
    4.
    发明申请
    APPARATUS FOR COMBUSTING A FUEL AT HIGH PRESSURE AND HIGH TEMPERATURE, AND ASSOCIATED SYSTEM 有权
    用于燃烧高压和高温燃料的装置及相关系统

    公开(公告)号：US20110083435A1

    公开(公告)日：2011-04-14

    申请号：US12872364

    申请日：2010-08-31

    申请人： Miles R. Palmer ,  Rodney John Allam ,  Glenn William Brown, JR.

    发明人： Miles R. Palmer ,  Rodney John Allam ,  Glenn William Brown, JR.

    IPC分类号： F02C1/00 ,  F23D1/00 ,  F23L7/00 ,  F02C3/20

    CPC分类号： F23D1/00 ,  B01D53/34 ,  B01J19/00 ,  F23G7/065 ,  F23J15/027 ,  F23L7/002 ,  F23L7/007 ,  F23L2900/07001 ,  F23L2900/07002 ,  F23L2900/07003 ,  F23L2900/07007 ,  F23L2900/07008 ,  F23M5/08 ,  F23M2900/05004 ,  F23R3/002 ,  F23R2900/03041 ,  Y02E20/12 ,  Y02E20/322 ,  Y02E20/344

    摘要： A combustor apparatus is provided, comprising a mixing arrangement for mixing a carbonaceous fuel with enriched oxygen and a working fluid to form a fuel mixture. A combustion chamber is at least partially defined by a porous perimetric transpiration member, at least partially surrounded by a pressure containment member. The combustion chamber has longitudinally spaced apart inlet and outlet portions. The fuel mixture is received by the inlet portion for combustion within the combustion chamber at a combustion temperature to form a combustion product. The combustion chamber further directs the combustion product longitudinally toward the outlet portion. The porous transpiration member is configured to substantially uniformly direct a transpiration substance laterally therethrough, about the perimeter thereof defining the combustion chamber and longitudinally between the inlet and outlet portions, toward the combustion chamber for buffering interaction between the combustion product and the porous transpiration member. Associated systems are also provided.

    摘要翻译： 提供了一种燃烧器装置，其包括用于混合含碳燃料和富氧的混合装置和工作流体以形成燃料混合物。 燃烧室至少部分地由多孔周边蒸腾构件限定，至少部分地被压力容纳构件包围。 燃烧室具有纵向间隔开的入口和出口部分。 燃料混合物被入口部分接收以在燃烧室内在燃烧温度下燃烧以形成燃烧产物。 燃烧室进一步将燃烧产物纵向引向出口部分。 多孔蒸腾构件被构造成基本上均匀地引导蒸发物质围绕其限定燃烧室的周边并且纵向在入口部分和出口部分之间横向通过其朝向燃烧室缓冲燃烧产物和多孔蒸腾构件之间的相互作用。 还提供了相关系统。

    ENERGY-SAVING ELECTRICAL POWER SYSTEM
    7.
    发明申请
    ENERGY-SAVING ELECTRICAL POWER SYSTEM 审中-公开
    节能电力系统

    公开(公告)号：US20100314940A1

    公开(公告)日：2010-12-16

    申请号：US12484728

    申请日：2009-06-15

    申请人： Miles R. Palmer ,  Glenn William Brown, JR.

    发明人： Miles R. Palmer ,  Glenn William Brown, JR.

    IPC分类号： H02J3/14 ,  H02H1/00

    CPC分类号： H02J3/14 ,  H02J13/0062 ,  H02J13/0079 ,  H02J13/0086 ,  Y02B70/3225 ,  Y02E60/74 ,  Y04S10/30 ,  Y04S20/222 ,  Y10T307/469

    摘要： An electrical power system includes one or more protective devices in a plurality of electrical distribution panels. Each protective device has a power switch connectable between an electrical power source for the system and an electrical load and an operating-mode control switch whose state determines the power switch's operating mode. A computer is remotely-located relative to the electrical distribution panels. Each of the protective devices is operable such that: if the operating-mode control switch is in a first state, the power switch opens and closes according to instructions stored within the protective device; and if the operating-mode control switch is in a second state, the power switch is controllable based on instructions from the remotely-located computer.

    摘要翻译： 电力系统包括多个配电盘中的一个或多个保护装置。 每个保护装置具有可在系统的电源和电负载之间连接的电源开关以及状态决定电源开关的工作模式的操作模式控制开关。 计算机相对于配电盘远程定位。 每个保护装置可操作使得：如果操作模式控制开关处于第一状态，则电源开关根据存储在保护装置内的指令而打开和关闭; 并且如果操作模式控制开关处于第二状态，则可以基于来自位于远程的计算机的指令来控制电源开关。

    Transformable gun launched aero vehicle
    8.
    发明授权
    Transformable gun launched aero vehicle 有权
    可变形枪发射航空车

    公开(公告)号：US06260797B1

    公开(公告)日：2001-07-17

    申请号：US09229599

    申请日：1999-01-13

    申请人： Miles R. Palmer

    发明人： Miles R. Palmer

    IPC分类号： B64C356

    CPC分类号： F42B15/00 ,  B64C39/024 ,  B64C2201/044 ,  B64C2201/084 ,  B64C2201/088 ,  B64C2201/105 ,  B64C2201/121 ,  B64C2201/126 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/205 ,  B64D1/22 ,  B64D37/04 ,  B64D37/06 ,  B64D37/12 ,  B64D39/00

    摘要： A transformable gun launched aero vehicle having a ballistic projectile configuration and an aeroplane configuration includes a cylinder forming a shell of the vehicle in the ballistic projectile configuration and wings deployable from the cylinder. The wings are capable of achieving sufficient lift for sustained flight in the aeroplane configuration. The cylinder forms a fuselage of the vehicle in the aeroplane configuration. A wing includes plural rib elements, plural inflatable tubes where each tube is braced by the plural rib elements, and a wind shell disposed around the plural inflatable tubes and the plural rib elements. The vehicle includes an inflatable tail section that is inflated while the vehicle is in the aeroplane configuration. The vehicle includes a parachute that is reversibly deployable from a nose portion of the vehicle. The vehicle includes at least one landing rod. Each landing rod is reversibly extendable from the vehicle. A landing controller controls a first landing rod to extend after the vehicle has begun to vertically descend. The vehicle includes a folding propeller deployable from the fuselage in the aeroplane configuration. The vehicle includes a control system, and the control system includes a module to determine when the vehicle has reached a first predetermined state that defines an initiation of a transition from the ballistic projectile configuration to the aeroplane configuration.

    摘要翻译： 可变形枪发射具有弹道射弹配置的航空车辆，并且飞机配置包括形成弹道射出构造的车辆壳体的气缸和从气缸展开的翼。 机翼能够在飞机配置中实现足够的升力以持续飞行。 汽缸在飞机配置中形成车辆的机身。 翼包括多个肋元件，多个可充气管，其中每个管由多个肋元件支撑，以及设置在多个可充气管和多个肋元件周围的风壳。 车辆包括在车辆处于飞机配置中时充气的可充气尾部。 车辆包括可从车辆的鼻部部分可逆地展开的降落伞。 车辆包括至少一个着陆杆。 每个着陆杆可从车辆可逆地延伸。 着陆控制器控制第一着陆杆在车辆开始垂直下降之后延伸。 该车辆包括在飞机配置中可从机身部署的折叠螺旋桨。 车辆包括控制系统，并且控制系统包括用于确定车辆何时已经达到第一预定状态的模块，该第一预定状态定义了从弹道射弹配置到飞机配置的转变的开始。

    Synthesis of tetrafluorohydrazine
    9.
    发明授权
    Synthesis of tetrafluorohydrazine 失效
    四氟肼的合成

    公开(公告)号：US4832931A

    公开(公告)日：1989-05-23

    申请号：US241179

    申请日：1988-09-07

    申请人： Miles R. Palmer

    发明人： Miles R. Palmer

    IPC分类号： C01B21/083

    CPC分类号： C01B21/0832

    摘要： High purity tetrafluorohydrazine is synthesized by reacting NF.sub.3 with silicon at an elevated temperature. The reaction occurs only periodically and at a low concentration of NF.sub.3. Immediate cooling of the reaction material produces tetrafluorohydrazine and SiF.sub.4. Alkaline hydrolysis removes substantially all impurities. Tetrafluorohydrazine is further recovered by cryogenic trapping from the remaining impurities.

    摘要翻译： 高纯度四氟肼通过在高温下与NF3反应合成。 反应仅在周期性和低浓度的NF3发生。 立即冷却反应物质产生四氟肼和SiF 4。 碱性水解基本上除去所有的杂质。 通过从剩余杂质中低温捕获进一步回收四氟肼。

    Corrosion inhibitor formulation for molybdenum tungsten and other metals
    10.
    发明授权
    Corrosion inhibitor formulation for molybdenum tungsten and other metals 失效
    钼钨等金属的防腐剂配方

    公开(公告)号：US4719035A

    公开(公告)日：1988-01-12

    申请号：US913612

    申请日：1986-09-26

    申请人： Miles R. Palmer

    发明人： Miles R. Palmer

    IPC分类号： C23F11/10 ,  C09K3/00 ,  C23F11/04

    CPC分类号： C23F11/10

    摘要： The corrosion of molybdenum metal surfaces which come in contact with water-coolant systems is inhibited by the addition of a small amount of a composition containing a combination of a triazole inhibitor, a biocide and a buffering agent. A corrosion inhibiting composition containing benzotriazole as the inhibitor and benzoic acid as both a biocide and buffer proved to be especially effective in preventing the corrosion of molybdenum, tungsten and other metals.

    摘要翻译： 通过加入少量含有三唑抑制剂，杀生物剂和缓冲剂的组合的组合物来抑制与水冷却剂体系接触的钼金属表面的腐蚀。 含有苯并三唑作为抑制剂和苯甲酸作为杀生物剂和缓冲液的腐蚀抑制组合物被证明在防止钼，钨和其他金属的腐蚀方面特别有效。