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    ROTARY INTERNAL COMBUSTION ENGINE WITH PILOT SUBCHAMBER AND IGNITION ELEMENT
    1.
    发明申请
    ROTARY INTERNAL COMBUSTION ENGINE WITH PILOT SUBCHAMBER AND IGNITION ELEMENT 审中-公开

    公开(公告)号：US20200011234A1

    公开(公告)日：2020-01-09

    申请号：US16574650

    申请日：2019-09-18

    Applicant: PRATT & WHITNEY CANADA CORP.

    Inventor： Michael GAUL ,  Andre JULIEN ,  Bruno VILLENEUVE

    IPC: F02B53/12 ,  F01C1/22 ,  F02B19/10 ,  F02B53/10 ,  F02B55/08 ,  F02B19/12 ,  F02B53/02 ,  F02M53/02 ,  F02P19/02

    Abstract: A rotary engine includes an insert having a pilot subchamber defined therein and communicating with the internal cavity of the engine. A pilot fuel injector has a tip in communication with the pilot subchamber. An ignition element extends into an element cavity defined through the insert adjacent the pilot subchamber. The element cavity is in communication with the pilot subchamber through a communication opening defined in the insert between the element cavity and the pilot subchamber. The communication opening is smaller than a portion of the ignition element adjacent the communication opening such as to prevent the portion of the ignition element from completely passing through the communication opening upon breaking off of the portion of the ignition element from a remainder of the ignition element. An outer body for a rotary engine and a method of combusting fuel in a rotary engine are also provided.

    COMPOUND ENGINE ASSEMBLY WITH MOUNT CAGE
    5.
    发明申请
    COMPOUND ENGINE ASSEMBLY WITH MOUNT CAGE 审中-公开
    复合发动机总成与安装笼

    公开(公告)号：US20160245171A1

    公开(公告)日：2016-08-25

    申请号：US15047362

    申请日：2016-02-18

    Applicant: Pratt & Whitney Canada Corp.

    Inventor： Sylvain LAMARRE ,  Mike FONTAINE ,  Andre JULIEN ,  Michael GAUL ,  Jean THOMASSIN ,  Lazar MITROVIC ,  Ilya B. MEDVEDEV ,  Sergey USIKOV ,  Andrey ZOLOTOV

    IPC: F02C3/10 ,  F02B39/04 ,  F02B37/00

    CPC classification number: F02C3/10 ,  F02B37/004 ,  F02B39/04 ,  F02C7/20 ,  F02C7/25 ,  F05D2220/40 ,  Y02T50/53

    Abstract: A compound engine assembly with an engine core including at least one internal combustion engine, a turbine section, and a compressor having an outlet in fluid communication with an inlet of the engine core. A casing is connected to the turbine section, compressor and engine core. A mount cage is connected to mounts attached to the casing between the compressor and a hot zone including the turbine section and exhaust pipe(s). The struts are separated from the hot zone by at least one firewall. The mount cage may include a plurality of struts all extending from the mounts away from the turbine section and engine core. The casing may be a gearbox module casing through which the turbine shaft in engaged with the engine shaft. The mount cage may be completely contained within an axial space with the turbine section and exhaust pipe(s) being located outside of the axial space.

    Abstract translation: 具有包括至少一个内燃机，涡轮部分和具有与发动机芯的入口流体连通的出口的压缩机的发动机芯的复合发动机组件。 壳体连接到涡轮部分，压缩机和发动机核心。 安装架连接到在压缩机和包括涡轮部分和排气管的热区之间附接到壳体的安装件。 支柱通过至少一个防火墙与热区隔开。 安装架可以包括多个支柱，其全部从支架延伸离开涡轮部分和发动机芯。 壳体可以是齿轮箱模块壳体，涡轮轴通过该外壳与发动机轴接合。 安装架可以完全容纳在轴向空间内，涡轮部分和排气管位于轴向空间的外部。

    COMPOUND ENGINE ASSEMBLY WITH CONFINED FIRE ZONE
    8.
    发明申请
    COMPOUND ENGINE ASSEMBLY WITH CONFINED FIRE ZONE 审中-公开
    复合发动机装配有限制的火区

    公开(公告)号：US20160245185A1

    公开(公告)日：2016-08-25

    申请号：US14864112

    申请日：2015-09-24

    Applicant: PRATT & WHITNEY CANADA CORP.

    Inventor： Sylvain LAMARRE ,  Andre JULIEN ,  Michael GAUL ,  Jean THOMASSIN ,  Ilya B. MEDVEDEV ,  Sergey USIKOV ,  Andrey ZOLOTOV

    IPC: F02C7/36 ,  F02C3/04 ,  F23M11/02

    CPC classification number: F02C7/36 ,  F01C1/22 ,  F01C11/008 ,  F02C3/04 ,  F02C6/12 ,  F02C7/25 ,  F05D2220/323 ,  F05D2230/51 ,  F05D2230/72 ,  F05D2250/312 ,  F05D2260/4031 ,  F05D2300/121 ,  F05D2300/171 ,  F23M11/02

    Abstract: A compound engine assembly with an engine core including at least one internal combustion engine, a turbine section including a turbine shaft in driving engagement with the engine shaft, and a compressor, and a firewall. The compressor is located on one side of the firewall, and the turbine section and the engine core are located on the other side. The assembly may include a gearbox module with the turbine section and the engine core located on a same side of the gearbox module casing and the compressor located on the opposite side of the gearbox module casing, and with the firewall extending from the gearbox module casing. One or more rotatable accessory may be located on a same side of the firewall as the compressor. A method of reducing fire hazard in a compound engine assembly is also discussed.

    Abstract translation: 具有包括至少一个内燃机的发动机芯的复合发动机组件，包括与发动机轴驱动接合的涡轮轴的涡轮部分，以及压缩机和防火墙。 压缩机位于防火墙的一侧，涡轮部分和发动机核心位于另一侧。 组件可以包括齿轮箱模块，其中涡轮部分和发动机芯位于齿轮箱模块壳体的同一侧并且压缩机位于齿轮箱模块壳体的相对侧上，防火墙从齿轮箱模块壳体延伸。 一个或多个可旋转附件可以位于防火墙与压缩机相同的一侧。 还讨论了在复合发动机组件中减少火灾危险的方法。

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