MULTISTAGE TURBOCHARGING SYSTEM
    1.
    发明申请
    MULTISTAGE TURBOCHARGING SYSTEM 审中-公开
    多级涡轮增压系统

    公开(公告)号:WO2017046788A1

    公开(公告)日:2017-03-23

    申请号:PCT/IL2016/050930

    申请日:2016-08-25

    Abstract: An aircraft engine system configured with a high pressure stage turbocharger assembly and a supplemental stage turbocharger assembly disposed in series with respect to said high pressure stage turbocharger, wherein the supplemental stage turbocharger assembly provides a compressor unit of the high pressure stage turbocharger with substantially constant critical altitude pressure input.

    Abstract translation: 配置有相对于所述高压级涡轮增压器串联设置的高压级涡轮增压器组件和补充级涡轮增压器组件的飞机发动机系统,其中所述补充级涡轮增压器组件提供高压级涡轮增压器的压缩机单元,其具有基本上恒定的关键 高度压力输入。

    VARIABLE EXHAUST CONTROL SYSTEM
    2.
    发明申请
    VARIABLE EXHAUST CONTROL SYSTEM 审中-公开
    可变排气控制系统

    公开(公告)号:WO2016179119A1

    公开(公告)日:2016-11-10

    申请号:PCT/US2016/030477

    申请日:2016-05-02

    Applicant: COBRA AERO LLC

    Abstract: An apparatus for adjusting power and noise characteristics of an internal combustion engine comprises a wall configured to define an engine cylinder that includes a bore and a compression relief passage. A compression relief valve is configured to selectively adjust fluid flow capacity of the compression relief passage. A manifold is configured to be in fluid communication with the exhaust passage and includes an exhaust bypass valve to permit exhaust to at least partially bypass a noise suppressor. Operational characteristics of the engine can be adjusted along a range that extends from a first set of operational characteristics present when both the compression relief valve and the exhaust bypass valve are in a fully open position to a second set of operational characteristics present when both the compression relief valve and the exhaust bypass valve are in a fully closed position.

    Abstract translation: 一种用于调节内燃机功率和噪声特性的装置,包括一个被配置为限定包括孔和压缩释放通道的发动机气缸的壁。 压缩释放阀构造成选择性地调节压缩释放通道的流体流动能力。 歧管构造成与排气通道流体连通,并且包括排气旁通阀,以允许排气至少部分地绕过噪声抑制器。 发动机的操作特性可以沿着从当压缩释放阀和排气旁通阀都处于完全打开位置时存在的第一组操作特性延伸到第二组操作特性的范围来调节,当压缩 安全阀和排气旁通阀处于完全关闭位置。

    SINGLE CYLINDER DIESEL ENGINE
    3.
    发明申请
    SINGLE CYLINDER DIESEL ENGINE 审中-公开
    单缸柴油发动机

    公开(公告)号:WO2016133481A1

    公开(公告)日:2016-08-25

    申请号:PCT/TR2016/050040

    申请日:2016-02-16

    Inventor: ESER, Mustafa

    CPC classification number: F02B63/04 F02B61/00 F02B61/04

    Abstract: The invention relates to a single cylinder diesel engine (A) comprising a cylinder head (2) comprising the intake and exhaust manifold by serving as bearing for valve springs (19) and an injector (23) and enabling high power intake by increasing the efficiency, a governing group (14) adjusting the speed of the single cylinder diesel engine (A) and making desired power adjustment of the single cylinder diesel engine (A), and a combustion chamber providing ideal air movements for combustion affecting the engine performance directly with its design.

    Abstract translation: 本发明涉及一种单缸柴油发动机(A),其包括通过用作阀弹簧(19)的轴承和喷射器(23)而包括进气歧管和排气歧管的气缸盖(2),并且通过提高效率实现高功率摄取 ,调节单缸柴油发动机(A)的速度并进行单缸柴油发动机(A)的所需动力调节的控制组(14),以及直接为 其设计。

    はずみ車及びエンジン
    4.
    发明申请
    はずみ車及びエンジン 审中-公开
    飞机和发动机

    公开(公告)号:WO2015141646A1

    公开(公告)日:2015-09-24

    申请号:PCT/JP2015/057773

    申请日:2015-03-16

    CPC classification number: F16F15/31 F02B61/04 F16C3/08 F16F15/30 F16F2230/32

    Abstract: 本発明によるエンジンは、軸線を中心に回転するクランク軸と、円板形状を有し、中心にてクランク軸の軸線に接続されたはずみ車(16)とを備え、はずみ車(16)は、クランク軸に固定される本体部(27)と、本体部(27)に着脱可能に固定される第1分割部材(28)及び第2分割部材(29)とを有し、第1分割部材(28)及び第2分割部材(29)は、本体部(27)に固定されたときに、はずみ車(16)の側面の一部と、はずみ車(16)の二つの円形状底面のうちエンジン本体に対向する底面の一部を形成する。

    Abstract translation: 该发动机具有:以轴线为中心旋转的曲轴; 以及具有圆板形状并且在其中心与曲轴的轴线连接的飞轮(16)。 飞轮(16)具有:固定在曲轴上的主体(27) 以及可移除地固定到主体(27)的第一分割构件(28)和第二分割构件(29)。 当第一分割构件(28)和第二分割构件(29)固定到主体(27)时,飞轮(16)的侧表面的一部分和底表面的面向发动机主体的一部分 形成飞轮(16)的两个圆形底面。

    COOLING OF INTERNAL COMBUSTION ENGINES
    5.
    发明申请
    COOLING OF INTERNAL COMBUSTION ENGINES 审中-公开
    内燃机冷却

    公开(公告)号:WO2015003853A1

    公开(公告)日:2015-01-15

    申请号:PCT/EP2014/061446

    申请日:2014-06-03

    Abstract: An engine assembly (10) for a propeller-driven aircraft is disclosed, the assembly including an engine (11), a drive shaft (13) driven by the engine (11), and a radiator (20) comprising an aperture (24) for receiving the drive shaft (13), the aperture (24) being located such that the radiator (20) substantially circumferentially surrounds the drive shaft (13). The aperture (24) may take various forms, such as a hole within the interior of the radiator (20) or a blind slit formed within the radiator (20).

    Abstract translation: 公开了一种用于推进器驱动飞机的发动机组件(10),该组件包括发动机(11),由发动机(11)驱动的驱动轴(13)和包括孔(24)的散热器(20) 为了接收驱动轴(13),孔(24)被定位成使得散热器(20)基本上周向地围绕驱动轴(13)。 孔(24)可以采取各种形式,例如散热器(20)内部的孔或形成在散热器(20)内的盲缝。

    MARINE FUEL SYSTEM WITH SPILL CONTROL FEATURE
    7.
    发明申请
    MARINE FUEL SYSTEM WITH SPILL CONTROL FEATURE 审中-公开
    具有泄漏控制特征的海洋燃料系统

    公开(公告)号:WO2013043379A1

    公开(公告)日:2013-03-28

    申请号:PCT/US2012/053935

    申请日:2012-09-06

    Inventor: SALER, John, L.

    Abstract: A spill resistant fuel supply system (16) for a marine engine (12). The system (16) includes a generally sealed housing (46) in which is disposed a vapor separator (26), a high pressure pump (28) and/or a suction pump (24). The housing (46) prevents fuel that might leak from these components from openly collecting in the marine vessel (10). The housing (46) includes one or more walls (48, 50, 52) formed with included air columns (58) which act as thermal barriers to reduce the amount of heat energy transferred from the outside in. The included air columns (58) are preferably arrayed in side-by-side fashion and closed at both ends to trap air therein.

    Abstract translation: 一种用于船用发动机(12)的防溢油燃料供应系统(16)。 系统(16)包括大致密封的壳体(46),其中设置有蒸气分离器(26),高压泵(28)和/或抽吸泵(24)。 壳体(46)防止可能从这些部件泄漏的燃料在海洋容器(10)中公开收集。 壳体(46)包括一个或多个壁(48,50,52),其形成有包括的空气柱(58),其用作热障,以减少从外部传递的热能的量。所包括的空气柱(58) 优选以并排方式排列并且在两端封闭以在其中捕获空气。

    エンジン排気ガス浄化装置
    8.
    发明申请
    エンジン排気ガス浄化装置 审中-公开
    发动机排气净化装置

    公开(公告)号:WO2012026302A1

    公开(公告)日:2012-03-01

    申请号:PCT/JP2011/067952

    申请日:2011-08-05

    Abstract: 低硫黄燃料ではなく従来燃料を使用した場合でも、船舶側の対応により排気ガス規制の達成を可能にしたエンジン排気ガス浄化装置を提供する。メインエンジン(10)から排出される排気ガス中の大気汚染物質を低減及び除去するエンジン排気ガス浄化装置(1)が、メインエンジン(10)の排気系統(L1)に配設されて排気ガスの全量を洗浄処理する排気ガス洗浄装置(40)と、該排気ガス洗浄装置(40)の下流から再循環用排気ガスとして導入した排気ガスの一部をメインエンジン(10)に再度給気させる排気ガス再循環装置(60)とを備えている。

    Abstract translation: 提供了一种发动机废气净化装置,其可以通过解决船舶本身来满足废气法规,即使使用常规燃料而不是低硫燃料。 一种排气净化装置(1),其排出有排气系统(L1)的废气净化装置(40),该发动机废气净化装置(1)能够减少从主发动机(10)排出的废气中的空气污染物, (10),对排气的全部进行净化处理; 以及排气再循环装置(60),其将从废气净化装置(40)的下游引入的作为再循环排气的废气的一部分再供给到主发动机(10) 。

    LUBRICATING APPARATUS FOR A DOSING SYSTEM FOR CYLINDER LUBRICATION OIL AND METHOD FOR DOSING CYLINDER LUBRICATING OIL
    9.
    发明申请
    LUBRICATING APPARATUS FOR A DOSING SYSTEM FOR CYLINDER LUBRICATION OIL AND METHOD FOR DOSING CYLINDER LUBRICATING OIL 审中-公开
    用于缸筒润滑油的调料系统的润滑装置和用于调节气缸润滑油的方法

    公开(公告)号:WO2008009291A1

    公开(公告)日:2008-01-24

    申请号:PCT/DK2007/000364

    申请日:2007-07-19

    Inventor: AAMAND, Jan

    Abstract: There is disclosed a method and a hydraulic lubricating apparatus for dosing cylinder lubricating oil. The dosing system includes a supply line and a return line connected with the lubricating apparatus via each one or more valves for supplying hydraulic oil, a central hydraulic oil feed pump connected with hydraulic cylinders, each having a hydraulic piston and which may be subjected to pressure by hydraulic oil via the supply line, a number of injection units corresponding to a multiple of the cylinder number in the engine and which are connected with each their dosing cylinder with a dosing piston and a supply line for cylinder lubricating oil. In order to provide a system which is reliable and cheap and where there is no risk of disruptions, even if a hydraulic cylinder fails, the lubricating apparatus is designed with a distributor plate which at one side is in contact with the dosing pistons and which at its other side is in contact with two or more hydraulic pistons for displacing the distributor plate for activating the dosing pistons.

    Abstract translation: 公开了一种用于计量汽缸润滑油的方法和液压润滑装置。 配料系统包括供油管线和与润滑装置连接的回油管路,每一个用于供应液压油的阀门,与液压缸连接的中央液压供油泵,每个液压油缸都具有液压活塞并且可能经受压力 通过液压油通过供应管线,多个喷射单元对应于发动机中的气缸数量的倍数,并且每个喷射单元与其每个定量缸连接有配量活塞和用于气缸润滑油的供应管线。 为了提供可靠且廉价的系统,即使没有中断的风险,即使液压缸故障,润滑装置设计有一个分配板,分配板在一侧与定量活塞接触,并且在 其另一侧与两个或更多个液压活塞接触,用于移动用于启动定量活塞的分配器板。

    DIESEL AIRCRAFT ENGINE
    10.
    发明申请
    DIESEL AIRCRAFT ENGINE 审中-公开
    柴油机发动机

    公开(公告)号:WO2007086820A3

    公开(公告)日:2007-09-27

    申请号:PCT/US2005044262

    申请日:2005-12-07

    CPC classification number: F02B75/24 F02B61/04 F02B75/246 Y10T74/2183

    Abstract: The present invention is an engine, including two banks of cylinders in a flat, opposed cylinder arrangement and a crankshaft having a plurality throws, the two throws of each respective pair of throws being disposed adjacent to each and coplanar with respect to each other.

    Abstract translation: 本发明是一种发动机,其包括平坦的相对的气缸装置中的两组气缸和具有多个喷射的曲轴,每个相应的一对喷射器的两个投射相对于彼此相邻并共面设置。

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