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公开(公告)号：US07677471B2
公开(公告)日：2010-03-16
申请号：US11751840
申请日：2007-05-22
CPC分类号： F23R3/28 , F23D11/107 , F23D11/383 , F23R2900/00017 , F23R2900/00018 , Y10T29/49405 , Y10T29/49426 , Y10T29/49432
摘要： A modular fuel nozzle configuration is defined which permits lower-cost manufacturing operations such as injection moulding to be employed. Also described is a method of making such a component.
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公开(公告)号：US07617683B2
公开(公告)日：2009-11-17
申请号：US11300476
申请日：2005-12-15
CPC分类号： F02C7/222 , F05D2230/60 , F05D2230/70
摘要： A fuel supply assembly for a gas turbine engine including a manifold portion with a transfer conduit, a fuel nozzle with an entry conduit and disconnectable means for retaining the transfer and entry conduits in mating engagement with one another.
摘要翻译： 一种用于燃气涡轮发动机的燃料供应组件，其包括具有传送管道的歧管部分，具有入口导管的燃料喷嘴和用于保持彼此配合接合的传送和进入导管的可拆卸装置。
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公开(公告)号：US20090159725A1
公开(公告)日：2009-06-25
申请号：US11960761
申请日：2007-12-20
CPC分类号： B05B7/0441 , B05B7/10 , F23R3/283
摘要： A modular fuel nozzle air swirler for a gas turbine engine has a body defining a fuel passage extending between an inlet end and a discharge end of the body. An annular cap is removably secured to the discharge end of the body via cooperating interlocking members.
摘要翻译： 用于燃气涡轮发动机的模块化燃料喷嘴空气旋流器具有限定在主体的入口端和排出端之间延伸的燃料通道的主体。 环形盖通过配合的互锁构件可拆卸地固定到主体的排放端。
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公开(公告)号：US07467467B2
公开(公告)日：2008-12-23
申请号：US11239110
申请日：2005-09-30
申请人： Lev Alexander Prociw
发明人： Lev Alexander Prociw
IPC分类号： B21D53/02
CPC分类号： B22F7/004 , B22F2998/00 , F28D7/04 , F28D9/04 , F28F13/003 , F28F21/087 , F28F2255/18 , F28F2265/16 , Y10T29/4935 , Y10T29/49357 , Y10T29/49366 , Y10T29/49369 , B22F3/11 , B22F3/10
摘要： A method for manufacturing a heat exchanger, including forming at least one flexible heat exchanging assembly with first and second adjacent conduits defined therein, shaping the flexible heat exchanging assembly, and heating the heat exchanging assembly to transform at least a portion of the flexible heat conducting material into a rigid heat conducting material.
摘要翻译： 一种用于制造热交换器的方法，包括形成至少一个具有限定在其中的第一和第二相邻导管的柔性热交换组件，使所述柔性热交换组件成形，以及加热所述热交换组件以将至少一部分柔性导热 材料变成刚性导热材料。
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公开(公告)号：US20070234724A1
公开(公告)日：2007-10-11
申请号：US11220849
申请日：2005-09-08
IPC分类号： F02C7/22
CPC分类号： F02C7/222 , F05D2240/55
摘要： A fuel manifold of gas turbine engines comprises a tube for fluid communication with a fuel source and for connection with at least one fuel nozzle tip to thereby define a fuel conveying passage. There is a means for providing a redundant seal around the tube and covering substantially an entire length thereof to reduce a risk of fuel leakage of the fuel conveying passage.
摘要翻译： 燃气涡轮发动机的燃料歧管包括用于与燃料源流体连通并用于与至少一个燃料喷嘴尖端连接从而限定燃料输送通道的管。 存在用于在管周围提供冗余密封并且基本上覆盖其整个长度的装置以减少燃料输送通道的燃料泄漏的风险。
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公开(公告)号：US07263772B2
公开(公告)日：2007-09-04
申请号：US10870542
申请日：2004-06-18
CPC分类号： F23R3/007 , F23M2900/05004 , F23R3/06 , F23R2900/03041 , Y10T29/49345 , Y10T29/49885 , Y10T29/49982 , Y10T29/49986 , Y10T428/12493
摘要： A method of manufacturing a composite wall with an open cell metal foam core layer bonded to an inner cladding layer and an outer cladding layer. The method involves: creating a core substrate of open cell gas permeable foam in a chosen shape; impregnating the open cell foam substrate with metal vapour and depositing a porous layer of metal on exposed internal and external surfaces of the substrate thereby forming the open cell metal foam core through metal vapour deposition; and forming the inner and outer cladding layers upon the metal foam core through spray application of metal or ceramic.
摘要翻译： 一种制造具有接合到内包层和外包层的开孔金属泡沫芯层的复合壁的方法。 该方法包括：以选定的形状产生开孔细胞气体可渗透泡沫的核心基底; 用金属蒸气浸渍开孔泡沫衬底，并在衬底的暴露的内表面和外表面上沉积多孔金属层，从而通过金属气相沉积形成开孔金属泡沫芯; 以及通过金属或陶瓷的喷涂来在金属泡沫芯上形成内层和外层。
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公开(公告)号：US07174717B2
公开(公告)日：2007-02-13
申请号：US10743712
申请日：2003-12-24
申请人： Lev Alexander Prociw
发明人： Lev Alexander Prociw
CPC分类号： F23D11/383 , F23D11/105 , F23D2900/11101 , F23D2900/14021 , F23R3/286 , Y10T29/4932 , Y10T29/49348
摘要： The present invention includes a fuel distributor for a fuel nozzle in a gas turbine engine comprising an inner tubular body and an outer tubular body respectively having an outer body inner surface and an inner body outer surface adapted to be in sealing contact one with the other, at least two helical fuel channels defined in at least one of the inner and outer surfaces and being in fluid communication with a fuel inlet, and a channel exit port for each helical fuel channel. The present invention also includes a method of distributing fuel in a fuel nozzle comprising the steps of providing at least two helical channels in the fuel nozzle, each having a channel exit port, providing a fuel inlet cavity in fluid communication with the helical channels, and flowing fuel in the fuel inlet cavity, the helical channels and the channel exit ports.
摘要翻译： 本发明包括一种燃气涡轮发动机中的用于燃料喷嘴的燃料分配器，其包括内管状体和外管体，其分别具有适于彼此密封接触的外主体内表面和内体外表面， 限定在内表面和外表面中的至少一个中并且与燃料入口流体连通的至少两个螺旋形燃料通道和用于每个螺旋燃料通道的通道出口。 本发明还包括在燃料喷嘴中分配燃料的方法，包括以下步骤：在燃料喷嘴中提供至少两个螺旋通道，每个具有通道出口，提供与螺旋通道流体连通的燃料入口腔，以及 燃料入口腔内的燃料，螺旋通道和通道出口。
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公开(公告)号：US07028484B2
公开(公告)日：2006-04-18
申请号：US10231334
申请日：2002-08-30
摘要： A multiple conduit system for a gas turbine engine, the multiple conduit system extending between a plurality of conduit inlet and outlets. A channel is formed in a surface of a gas turbine engine component, and the channel is adapted for conveying a fluid flow from an inlet to an outlet. At least a first sealing member is disposed within the channel and divides the channel into at least a first discrete conduit and a second discrete conduit. A second sealing member encloses the channel to define the second discrete conduit. The first and second discrete conduits are each adapted to direct an independent fluid flow from respective inlets to respective outlets.
摘要翻译： 一种用于燃气涡轮发动机的多管道系统，多管道系统在多个管道入口和出口之间延伸。 在燃气涡轮发动机部件的表面上形成通道，并且该通道适于将流体流从输入口输出到出口。 至少第一密封构件设置在通道内，并将通道分成至少第一离散导管和第二离散导管。 第二密封构件封闭通道以限定第二离散导管。 第一和第二离散导管各自适于将独立的流体流从相应的入口引导到相应的出口。
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公开(公告)号：US6125624A
公开(公告)日：2000-10-03
申请号：US61278
申请日：1998-04-17
申请人： Lev Alexander Prociw
发明人： Lev Alexander Prociw
CPC分类号： F02C7/232 , F23K5/18 , F23K2301/203
摘要： The invention relates to an air purge system for preventing coke buildup in gas turbine engine fuel injectors, and in particular in the relatively small orifice pressure atomizers of a primary fuel injector. The inventors have recognized that after engine shutdown, residual engine heat is sufficient to cause fuel on wetted surfaces of the injectors to decompose and deposit coke. Especially critical are small orifices in injectors positioned towards the upper side of an engine, since rising hot gases accumulate and heat the upper engine area significantly for a long period after engine shutdown. Coke buildup leads to narrowing of the fuel injector orifices, and without adequate maintenance leads to uneven burning and eventually can incapacitate the engine. Fuel injectors are often located in relatively inaccessible interior portions of the engine. Extending the service life of an injector can result in significant maintenance cost savings and engine downtime. The air purge system is activated on engine shutdown to continuously exhaust cooling air through the injector orifices for an extended purge period after shutdown, for example 1-1.5 hours. A battery operated air blower connected to the fuel line forces cooling air through the injector until a thermocouple switch deactivates the blower on sensing an injector temperature below 150.degree. F. At this low temperature, coke formation does not occur and during engine operation efficient combustion minimizes coke formation. The invention provides the following benefits: (1) fuel is completely purged over an extended period from the injector; (2) backflow of combustion gases into the injector is impeded by continuous positive pressure and air flow out of the injector; (3) the fuel wetted surfaces of the injectors are more completely dried after long term exposure to purging air flow; and (4) the injectors are air cooled after engine shutdown to maintain injector temperature below the temperature at which coke formation will occur.
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公开(公告)号：US09003804B2
公开(公告)日：2015-04-14
申请号：US13647867
申请日：2012-10-09
申请人： Lev Alexander Prociw
发明人： Lev Alexander Prociw
CPC分类号： F23R3/346 , F23C2201/20 , F23D17/002 , F23N2027/06 , F23R3/36 , F23R3/44 , F23R3/54 , F23R2900/00002
摘要： A multipoint combustion system for a gas turbine engine includes a housing defining a pressure vessel. A master injector is mounted to the housing for injecting fuel along a central axis. A plurality of slave injectors are each disposed outward of the master injector for injecting fuel and air in an ignition plume radially outward of fuel injected through the master injector. The master injector and slave injectors are configured and adapted so the injection plume of the master injector intersects with the ignition plumes of the slave injectors. A primary manifold is included within the pressure vessel for distributing fuel to the slave injectors. An auxiliary manifold is in fluid communication with the auxiliary nozzles of the slave injectors for issuing an auxiliary flow of fuel from the auxiliary nozzles that is separate from the fuel flow of the primary manifold.
摘要翻译： 用于燃气涡轮发动机的多点燃烧系统包括限定压力容器的壳体。 主喷射器安装到壳体上以沿着中心轴线喷射燃料。 多个从动喷射器分别设置在主喷射器的外部，用于将燃料和空气喷射在通过主喷射器喷射的燃料的径向向外的点火羽流中。 主喷射器和从动喷射器被配置和适配，使得主喷射器的喷射羽流与从喷射器的点火羽流相交。 压力容器中包括一个主歧管，用于将燃料分配给从动喷射器。 辅助歧管与从动喷射器的辅助喷嘴流体连通，用于从与主歧管的燃料流分离的辅助喷嘴发出辅助燃料流。
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