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    INLET MANIFOLD FOR MULTI-TUBE PULSE DETONATION ENGINE
    3.
    发明公开
    INLET MANIFOLD FOR MULTI-TUBE PULSE DETONATION ENGINE 审中-公开
    摄入量多管脉冲爆震发动机

    公开(公告)号：EP3092397A1

    公开(公告)日：2016-11-16

    申请号：EP14885222.1

    申请日：2014-12-19

    申请人： United Technologies Corporation

    发明人： HILL, James, D. ,  CUOZZO, Michael, J.

    IPC分类号： F02K7/067

    CPC分类号： F02C5/02 ,  F02C5/10 ,  F23R7/00

    摘要： An inlet manifold for a multi-tube pulse detonation engine includes a vaneless diffuser disposed in a first zone to collect an air discharged from a compressor; a vaned diffuser including a plurality of guide vanes disposed in a second zone to slow the air from the compressor; a plenum disposed in a third zone located next to second zone to provide the air from the compressor to chambers; and a splitter disposed in a fourth zone to split the air from the compressor into an airflow required by each pulse detonation tube for detonation.

    VERBRENNUNGSTURBINE MIT DISKONTINUIERLICHER VERBRENNUNG
    6.
    发明公开
    VERBRENNUNGSTURBINE MIT DISKONTINUIERLICHER VERBRENNUNG 有权
    具有不连续BURNS燃气轮机

    公开(公告)号：EP2326815A1

    公开(公告)日：2011-06-01

    申请号：EP09775586.2

    申请日：2009-08-05

    申请人： Gabl, Helmut ,  Lorenz, Edmund ,  Niederl, Franz

    发明人： Gabl, Helmut ,  Lorenz, Edmund ,  Niederl, Franz

    IPC分类号： F02C5/12 ,  F23R7/00 ,  F02K7/06

    CPC分类号： F02C5/12 ,  F02C5/02 ,  F02K7/06 ,  F23R7/00 ,  Y02T50/671

    摘要： The invention relates to a combustion turbine (1) in which combustion is intermittent and which comprises at least one combustion chamber (3) that has intake valves (2) and an ignition device (18). The at least one combustion chamber (3) has no blocking devices at the exhaust end and is therefore constantly open at the exhaust end. A turbine (4), to which a working gas obtained in the combustion chamber (3) can be fed, is arranged downstream of the at least one combustion chamber (3). A flow chamber (5) is arranged axially behind the at least one combustion chamber (3), between the at least one combustion chamber (3) and the turbine (4). The flow chamber (5) is delimited from the at least one combustion chamber (3) by a flow plate (6) or another turbine (7). The invention also relates to a method for operating a combustion turbine (1) as well as a drive system for a machine comprising the claimed combustion turbine (1) as the essential piece.

    Vapor cooling of detonation engines
    7.
    发明公开
    Vapor cooling of detonation engines 审中-公开
    DampfkühlungfürDetonationsmotoren

    公开(公告)号：EP1939408A2

    公开(公告)日：2008-07-02

    申请号：EP07254801.9

    申请日：2007-12-12

    申请人： United Technologies Corporation

    发明人： Norris, James W. ,  Twelves, Wendell V., Jr.

    IPC分类号： F01D25/12 ,  F02C5/02 ,  F02C7/16 ,  F02C7/18

    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 (34) configured to generate detonation waves and a first vapor cooling assembly (40). The combustion chamber assembly (34) defines a flowpath between an inner liner (34A) and an outer liner (34B). The first vapor cooling assembly (40) includes a vaporization section (42A) located adjacent to the flowpath and a condenser section (44A)spaced from the flowpath, and is configured to transport thermal energy from the vaporization section (42A) to the condenser section (44A) through cyclical evaporation and condensation of a working medium sealed within the first vapor cooling assembly (40A).

    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（34）和第一蒸气冷却组件（40）。 燃烧室组件（34）限定内衬（34A）和外衬套（34​​B）之间的流路。 第一蒸气冷却组件（40）包括位于流路附近的蒸发部分（42A）和与该流动路径间隔开的冷凝器部分（44A），并被构造成将热能从蒸发部分（42A）传送到冷凝器部分 （44A）通过密封在第一蒸气冷却组件（40A）内的工作介质的循环蒸发和冷凝。

    Improvements to alternators and improvements to rotary combustion engines
    8.
    发明公开
    Improvements to alternators and improvements to rotary combustion engines 审中-公开
    Verbesserungen an Wechselstromgeneratoren und a rotierenden Brennkraftmaschinen

    公开(公告)号：EP1553682A2

    公开(公告)日：2005-07-13

    申请号：EP05004419.7

    申请日：2000-05-25

    申请人： Harris, David Johnathan

    发明人： Harris, David Johnathan

    IPC分类号： H02K7/18

    CPC分类号： H02K11/046 ,  F02B53/00 ,  F02B63/04 ,  F02B63/042 ,  F02C3/16 ,  F02C5/02 ,  F02C5/04 ,  H02K7/006 ,  H02K7/083 ,  H02K7/085 ,  H02K7/1823 ,  H02K16/00 ,  Y02T50/671

    摘要： The present invention provides improved alternators for use alone or in combination with, for example, rotary interns) combustion engines wherein the alternators are characterised by absence of moveable bearings or mountability to existing driving shafts by use of an aligning plate and through passage through the rotor of the alternator to mount to the driving shaft. The alternators may be further characterised by plural rotors on the rotor driving shaft. The rotary internal combustion engines of the present invention are characterised by fixed size combustion chambers formed of radial recesses around a rotor amongst other features.

    摘要翻译： 本发明提供改进的交流发电机，用于单独使用或与例如旋转实体组合使用）内燃发动机，其中交流发电机的特征在于不存在可移动的轴承或通过使用对准板并通过转子的现有驱动轴的安装性 的交流发电机安装到驱动轴上。 交流发电机的特征还在于转子驱动轴上有多个转子。 本发明的旋转式内燃机的特征在于固定尺寸的燃烧室由转子周围的径向凹部形成。