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    COMPOUND ENGINE ASSEMBLY WITH DIRECT DRIVE OF GENERATOR
    65.
    发明申请
    COMPOUND ENGINE ASSEMBLY WITH DIRECT DRIVE OF GENERATOR 有权
    具有直接驱动发电机的复合发动机总成

    公开(公告)号：US20160376023A1

    公开(公告)日：2016-12-29

    申请号：US14750207

    申请日：2015-06-25

    Applicant: Pratt & Whitney Canada Corp.

    Inventor： Richard ULLYOTT ,  Anthony JONES ,  Andre JULIEN ,  Jean THOMASSIN

    IPC: B64D41/00 ,  H02K7/18 ,  F02C3/10

    CPC classification number: B64D41/00 ,  B64D2013/0611 ,  F01C1/22 ,  F01C11/008 ,  F02C3/10 ,  H02K7/1815 ,  H02K7/1823 ,  Y02T50/44 ,  Y02T50/53

    Abstract: A compound engine assembly for use as an aircraft auxiliary power unit, having an engine core including internal combustion engine(s) in driving engagement with an engine shaft, a generator having a generator shaft directly engaged to the engine shaft such as to be rotatable at a same speed, a compressor having an outlet in communication with the engine core inlet, and a turbine section having an inlet in communication with the engine core outlet and configured to compound power with the engine core. The turbine section may include a first stage turbine having an inlet in communication with the engine core outlet, and a second stage turbine having an inlet in communication with the first stage turbine outlet. A method of providing electrical power to an aircraft is also discussed.

    Abstract translation: 一种用作飞机辅助动力单元的复合发动机组件，其具有包括与发动机轴驱动接合的内燃机的发动机芯，具有直接接合到发动机轴的发电机轴，该发电机轴可以在 相同的速度，具有与发动机芯入口连通的出口的压缩机，以及涡轮部分，其具有与发动机芯出口连通的入口并且被配置成与发动机芯体相互补给动力。 涡轮机部分可以包括具有与发动机芯出口连通的入口的第一级涡轮机和具有与第一级涡轮机出口连通的入口的第二级涡轮机。 还讨论了向航空器提供电力的方法。

    COMPOUND CYCLE ENGINE
    66.
    发明申请
    COMPOUND CYCLE ENGINE 有权
    化学循环发动机

    公开(公告)号：US20160069255A1

    公开(公告)日：2016-03-10

    申请号：US14944343

    申请日：2015-11-18

    Applicant: Pratt & Whitney Canada Corp.

    Inventor： Sebastien BOLDUC ,  Mike FONTAINE ,  Luc LANDRY ,  Jean THOMASSIN

    IPC: F02B53/02 ,  F02B37/00 ,  F02C7/36 ,  F02C6/00 ,  F02C5/00 ,  F02B53/10 ,  F02B55/14

    CPC classification number: F02B53/02 ,  F01C1/22 ,  F01C11/002 ,  F01C11/008 ,  F02B37/005 ,  F02B53/10 ,  F02B55/14 ,  F02B2053/005 ,  F02C5/00 ,  F02C6/00 ,  F02C6/12 ,  F02C7/36 ,  F05D2210/12 ,  F05D2220/32 ,  F05D2220/60 ,  Y02T10/144 ,  Y02T10/17

    Abstract: A compound cycle engine having an output shaft, at least two rotary units each including an internal combustion engine with the rotor of each rotary unit mounted on the output shaft and in driving engagement therewith, and a turbine including a rotor in driving engagement with the output shaft. The exhaust port of each rotary unit housing is in fluid communication with the flowpath of the turbine upstream of its rotor. The turbine is disposed co-axially between two of the rotary units. The engine may further include a compressor in fluid communication with the inlet port of each housing and a second turbine having an inlet in fluid communication with the flowpath of the first turbine downstream of its rotor. A method of compounding rotary engines is also discussed.

    Abstract translation: 具有输出轴的复合循环发动机，至少两个旋转单元，每个旋转单元包括内燃机，其中每个旋转单元的转子安装在输出轴上并与其驱动接合;以及涡轮机，包括与输出驱动接合的转子 轴。 每个旋转单元壳体的排气口与其转子上游的涡轮的流动路径流体连通。 涡轮机同轴地设置在两个旋转单元之间。 发动机还可以包括与每个壳体的入口流体连通的压缩机和具有与其转子下游的第一涡轮机的流动路径流体连通的入口的第二涡轮机。 还讨论了一种混合旋转发动机的方法。

    INTERNAL COMBUSTION ENGINE WITH PORT COMMUNICATION
    67.
    发明申请
    INTERNAL COMBUSTION ENGINE WITH PORT COMMUNICATION 有权
    内燃机与港口通信

    公开(公告)号：US20160040588A1

    公开(公告)日：2016-02-11

    申请号：US14887611

    申请日：2015-10-20

    Applicant: Pratt & Whitney Canada Corp.

    Inventor： Jean THOMASSIN ,  Patrick ROUSSEAU ,  Eric-Pierre MARTEL

    IPC: F02B29/08 ,  F02B53/02 ,  F02B53/08

    CPC classification number: F02B29/08 ,  F01C1/22 ,  F02B25/26 ,  F02B29/02 ,  F02B53/02 ,  F02B53/08 ,  F02B57/04 ,  Y02T10/146 ,  Y02T10/17

    Abstract: A method of feeding air to an internal combustion engine having at least first and second internal cavities, including: completing the intake phase of the first combustion chamber of the first internal cavity by feeding compressed air into the first combustion chamber until a maximum volume thereof is reached; during a beginning of the compression phase of the first combustion chamber and a simultaneous beginning of the intake phase of the second combustion chamber of the second internal cavity, feeding compressed air from the first combustion chamber into the second combustion chamber; closing a communication between the first and second combustion chambers and completing the intake phase of the second combustion chamber by feeding compressed air into the second combustion chamber until a maximum volume thereof is reached.

    Abstract translation: 一种将内部空气供给到具有至少第一和第二内部空腔的内燃机的方法，包括：通过将压缩空气送入第一燃烧室来完成第一内部空腔的第一燃烧室的进入相，直到其最大体积为 到达; 在第一燃烧室的压缩阶段的开始阶段和第二内腔的第二燃烧室的进气阶段的同时开始，将压缩空气从第一燃烧室供给到第二燃烧室中; 闭合第一和第二燃烧室之间的连通并且通过将压缩空气送入第二燃烧室来完成第二燃烧室的进气相，直至达到其最大体积。

    COMPOUND CYCLE ENGINE
    68.
    发明申请
    COMPOUND CYCLE ENGINE 审中-公开
    化学循环发动机

    公开(公告)号：US20150275756A1

    公开(公告)日：2015-10-01

    申请号：US14740878

    申请日：2015-06-16

    Applicant: Pratt & Whitney Canada Corp.

    Inventor： Sebastien BOLDUC ,  Mike FONTAINE ,  Luc LANDRY ,  Jean THOMASSIN

    IPC: F02C6/12 ,  F01C1/22 ,  F02B37/00

    CPC classification number: F02C6/12 ,  F01C1/22 ,  F01C11/002 ,  F01C11/008 ,  F02B37/00 ,  F04C2240/30

    Abstract: A compound cycle engine having an output shaft; at least two rotary units each defining an internal combustion engine, a first stage turbine, and a turbocharger is discussed. The first stage turbine includes a rotor in driving engagement with the output shaft between two of the rotary units. The exhaust port of each rotary unit is in fluid communication with the flowpath of the first stage turbine upstream of its rotor. The outlet of the compressor of the turbocharger is in fluid communication with the inlet port of each rotary unit. The inlet of the second stage turbine of the turbocharger is in fluid communication with the flowpath of the first stage turbine downstream of its rotor. The first stage turbine has a lower reaction ratio than that of the second stage turbine. A method of compounding at least two rotary engines is also discussed.

    Abstract translation: 具有输出轴的复合循环发动机; 讨论了至少两个各自限定内燃机，第一级涡轮和涡轮增压器的旋转单元。 第一级涡轮机包括与两个旋转单元之间的输出轴驱动接合的转子。 每个旋转单元的排气口与其转子上游的第一级涡轮机的流动路径流体连通。 涡轮增压器的压缩机的出口与每个旋转单元的入口流体连通。 涡轮增压器的第二级涡轮机的入口与其转子下游的第一级涡轮机的流动路径流体连通。 第一级涡轮机具有比第二级涡轮机更低的反应比。 还讨论了混合至少两个旋转发动机的方法。

    Rotary Internal Combustion Engine with Static Oil Seal
    69.
    发明申请
    Rotary Internal Combustion Engine with Static Oil Seal 有权
    带静油封的旋转式内燃机

    公开(公告)号：US20150040855A1

    公开(公告)日：2015-02-12

    申请号：US13960045

    申请日：2013-08-06

    Applicant: Pratt & Whitney Canada Corp.

    Inventor： Jean THOMASSIN ,  Jean-Gabriel GAUVREAU ,  David GAGNON-MARTIN ,  Bruno VILLENEUVE

    IPC: F02B55/08

    CPC classification number: F02B55/08 ,  F02B2053/005

    Abstract: A stator for a rotary internal combustion engine, with a body having an internal cavity. Each end wall has a scavenging cavity defined therein in fluid communication with the internal cavity through a respective scavenging opening extending through the inner surface thereof, and at least one annular oil seal groove defined in the inner surface thereof concentric with the central bore and located radially outwardly of the scavenging opening. At least one annular oil seal is received in each groove and protrudes from the end wall into the internal cavity for sealing engagement with a surface of a rotor of the engine, each seal being biased axially away from the end wall. A rotary internal combustion engine and a method of limiting radially outwardly directed oil leaks in a rotary engine are also disclosed.

    Abstract translation: 一种用于旋转内燃机的定子，其具有内部空腔。 每个端壁具有限定在其中的扫气腔，其通过延伸穿过其内表面的相应扫气孔与内腔流体连通，以及限定在其内表面中的与中心孔同心并位于径向上的至少一个环形油封槽 向外清扫开口。 至少一个环形油封被容纳在每个凹槽中并且从端壁突出到内腔中以与发动机的转子的表面密封接合，每个密封件被轴向偏离远离端壁。 还公开了旋转式内燃机和限制旋转式发动机中径向向外指向的油泄漏的方法。

    INTERNAL COMBUSTION ENGINE WITH COMMON RAIL PILOT AND MAIN INJECTION
    70.
    发明申请
    INTERNAL COMBUSTION ENGINE WITH COMMON RAIL PILOT AND MAIN INJECTION 有权
    内燃机与普通铁路导管和主注射

    公开(公告)号：US20140261294A1

    公开(公告)日：2014-09-18

    申请号：US13796239

    申请日：2013-03-12

    Applicant: PRATT & WHITNEY CANADA CORP.

    Inventor： Jean THOMASSIN

    IPC: F02B53/10

    CPC classification number: F02B53/10 ,  F01C1/22 ,  F02B19/108 ,  F02B55/14 ,  F02B2275/32 ,  F02D41/3094 ,  F02D41/3827 ,  F02D41/3836 ,  Y02T10/125 ,  Y02T10/142 ,  Y02T10/17

    Abstract: An internal combustion engine including a pilot subchamber, a pilot fuel injector having a tip in communication with the pilot subchamber, an ignition element positioned to ignite fuel within the pilot subchamber, and a main fuel injector spaced apart from the pilot fuel injector. The engine includes a common rail in fluid communication with the main fuel injector and with the pilot fuel injector and a pressure regulating mechanism in fluid communication with the common rail for regulating a fuel pressure therein. A method of combusting fuel in an internal combustion engine is also provided.

    Abstract translation: 一种内燃机，包括导向子室，具有与导向子室连通的尖端的先导燃料喷射器，定位成点燃先导子室内的燃料的点火元件和与先导燃料喷射器间隔开的主燃料喷射器。 发动机包括与主燃料喷射器和引燃燃料喷射器流体连通的共轨，以及与公共轨道流体连通以调节其中的燃料压力的压力调节机构。 还提供了一种在内燃机中燃烧燃料的方法。

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