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1. 发明授权

US07937926B2 Integral heater for fuel conveying member 有权
标题翻译：用于燃料输送构件的积分加热器
公开(公告)号：US07937926B2
公开(公告)日：2011-05-10
申请号：US12209730
申请日：2008-09-12
申请人： Lev Alexander Prociw , Harris Shafique , Jason Fish , Bhawan B. Patel
发明人： Lev Alexander Prociw , Harris Shafique , Jason Fish , Bhawan B. Patel
IPC分类号： F02G3/00
CPC分类号： F02C7/222 , F02C7/224 , F23D11/44
摘要： A fuel conveying member for an engine, the fuel conveying member having heating means integrated therein to permit pyrolysis of carbonaceous deposits.
摘要翻译：一种用于发动机的燃料输送构件，所述燃料输送构件具有集成在其中的加热装置，以允许碳质沉积物的热解。

2. 发明授权

US08276387B2 Gas turbine engine fuel conveying member 有权
标题翻译：燃气涡轮发动机燃料输送构件
公开(公告)号：US08276387B2
公开(公告)日：2012-10-02
申请号：US13021172
申请日：2011-02-04
申请人： Lev Alexander Prociw , Harris Shafique , Jason Fish , Bhawan B. Patel
发明人： Lev Alexander Prociw , Harris Shafique , Jason Fish , Bhawan B. Patel
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F02C7/222 , F02C7/224 , F23D11/44
摘要： A fuel conveying member of a gas turbine engine is described and includes a fuel manifold defining an annular fuel flow passage through a body of the fuel manifold. A plurality of fuel nozzles extend from the manifold in fluid flow communication with the annular fuel flow passage. The fuel manifold includes integral attachment lugs thereon for mounting the fuel manifold within the gas turbine engine. The attachment lugs are adapted to receive pins therein and provide a mounting mechanism which allows for thermal expansion of the fuel manifold relative to a surrounding support structure to which the fuel manifold is mounted via the attachment lugs.
摘要翻译：描述了燃气涡轮发动机的燃料输送构件，并且包括限定通过燃料歧管的主体的环形燃料流动通道的燃料歧管。多个燃料喷嘴从歧管延伸，与环形燃料流动通道流体连通。燃料歧管包括其上的用于将燃料歧管安装在燃气涡轮发动机内的一体式附接凸耳。附接凸耳适于在其中容纳销，并且提供安装机构，其允许燃料歧管相对于通过附接凸耳安装到燃料歧管的周围支撑结构的热膨胀。

3. 发明申请

US20090084108A1 INTEGRAL HEATER FOR FUEL CONVEYING MEMBER 有权
标题翻译：用于燃料输送成员的整体加热器
公开(公告)号：US20090084108A1
公开(公告)日：2009-04-02
申请号：US12209730
申请日：2008-09-12
申请人： Lev Alexander Prociw , Harris Shafique , Jason Fish , Bhawan B. Patel
发明人： Lev Alexander Prociw , Harris Shafique , Jason Fish , Bhawan B. Patel
IPC分类号： F02C7/224
CPC分类号： F02C7/222 , F02C7/224 , F23D11/44
摘要： A fuel conveying member for an engine, the fuel conveying member having heating means integrated therein to permit pyrolysis of carbonaceous deposits.
摘要翻译：一种用于发动机的燃料输送构件，所述燃料输送构件具有集成在其中的加热装置，以允许碳质沉积物的热解。

4. 发明申请

US20070234724A1 Redundant fuel manifold sealing arrangement 有权
标题翻译：冗余燃油歧管密封装置
公开(公告)号：US20070234724A1
公开(公告)日：2007-10-11
申请号：US11220849
申请日：2005-09-08
申请人： Lev Alexander Prociw , Harris Shafique
发明人： Lev Alexander Prociw , Harris Shafique
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。

5. 发明授权

US07028484B2 Nested channel ducts for nozzle construction and the like 有权
标题翻译：用于喷嘴结构的嵌套通道导管等
公开(公告)号：US07028484B2
公开(公告)日：2006-04-18
申请号：US10231334
申请日：2002-08-30
申请人： Lev Alexander Prociw , Harris Shafique , John Sokalski , Claude Raymond Pelletier
发明人： Lev Alexander Prociw , Harris Shafique , John Sokalski , Claude Raymond Pelletier
IPC分类号： F02C7/22 , F23R3/00
CPC分类号： F23K5/06 , F02C7/222 , F23R3/283
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。

6. 发明授权

US08074452B2 Nested channel ducts for nozzle construction and the like 有权
标题翻译：用于喷嘴结构的嵌套通道导管等
公开(公告)号：US08074452B2
公开(公告)日：2011-12-13
申请号：US12124593
申请日：2008-05-21
申请人： Lev Alexander Prociw , Harris Shafique , John Sokalski , Claude Raymond Pelletier
发明人： Lev Alexander Prociw , Harris Shafique , John Sokalski , Claude Raymond Pelletier
IPC分类号： F02C7/22 , F23R3/00
CPC分类号： F23K5/06 , F02C7/222 , F23R3/283
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, adapted for conveying fuel flow, is formed in a surface of a gas turbine engine component. The channel includes at least a first discrete conduit and a 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形成有用于输送燃料流的通道。通道包括至少第一离散导管和第二离散导管。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。

7. 发明授权

US07738694B2 Calibration of optical patternator spray parameter measurements 有权
标题翻译：光学图案喷雾参数测量的校准
公开(公告)号：US07738694B2
公开(公告)日：2010-06-15
申请号：US11386940
申请日：2006-03-23
申请人： Lev Alexander Prociw , Harris Shafique , Patrice Fiset
发明人： Lev Alexander Prociw , Harris Shafique , Patrice Fiset
IPC分类号： G06K9/00 , G06K9/46
CPC分类号： F23R3/00 , B05B12/004 , G06T7/66 , G06T2207/30108
摘要： The present invention provides a method of calibrating a fuel nozzle patternation system. The method includes testing a master nozzle having desired spray characteristics in the system to determine a virtual origin of the system and then using the virtual origin to replace a fixed spatial origin of the system for testing other nozzles of the same nozzle family.
摘要翻译：本发明提供一种校准燃料喷嘴图案化系统的方法。该方法包括在系统中测试具有期望的喷雾特性的主喷嘴以确定系统的虚拟原点，然后使用虚拟原点替换用于测试同一喷嘴系列的其它喷嘴的系统的固定空间原点。

8. 发明授权

US07559201B2 Redundant fuel manifold sealing arrangement 有权
标题翻译：冗余燃油歧管密封装置
公开(公告)号：US07559201B2
公开(公告)日：2009-07-14
申请号：US11220849
申请日：2005-09-08
申请人： Lev Alexander Prociw , Harris Shafique
发明人： Lev Alexander Prociw , Harris Shafique
IPC分类号： F02C1/00
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. A redundant seal is provided around the tube and covers 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。在管周围设置冗余密封件并且基本上覆盖其整个长度，以减少燃料输送通道的燃料泄漏的风险。

9. 发明授权

US07530231B2 Fuel conveying member with heat pipe 失效
标题翻译：带热管的燃油输送部件
公开(公告)号：US07530231B2
公开(公告)日：2009-05-12
申请号：US11095665
申请日：2005-04-01
申请人： Lev Alexander Prociw , Harris Shafique
发明人： Lev Alexander Prociw , Harris Shafique
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F02C7/224 , F02C7/14 , F02C7/222 , F05D2260/207 , F05D2260/208 , F28D15/0233
摘要： A fuel conveying member in a fuel system of a gas turbine engine includes a heat pipe disposed in heat transfer communication with a fuel flow passage of the fuel conveying member, such that heat is transferred by the heat pipe from a high temperature region to a lower temperature region of the fuel flow passage. The heat pipe has a constant mass or working fluid enclosed within a sealed chamber in heat transfer communication with fuel in said fuel flow passage, said working fluid being self-circulating in a fluid flow having a liquid portion and a vapor portion, said working fluid passively boiling, flowing and condensing to transfer heat from said high temperature region to said lower temperature region.
摘要翻译：燃气轮机的燃料系统中的燃料输送部件具有与燃料输送部件的燃料流路传热连通的热管，使得热量从高温区域传递到下部燃料流路的温度区域。所述热管具有封闭在密封室内的恒定质量或工作流体，与所述燃料流动通道中的燃料传热连通，所述工作流体在具有液体部分和蒸气部分的流体流中自行循环，所述工作流体被动沸腾，流动和冷凝以将热量从所述高温区域传递到所述较低温度区域。

10. 发明授权

US07497012B2 Gas turbine fuel nozzle manufacturing 有权
标题翻译：燃气轮机燃油喷嘴制造
公开(公告)号：US07497012B2
公开(公告)日：2009-03-03
申请号：US11016831
申请日：2004-12-21
申请人： Lev Alexander Prociw , Harris Shafique , Lafleche Gagnon
发明人： Lev Alexander Prociw , Harris Shafique , Lafleche Gagnon
IPC分类号： B21D51/16 , B21K25/00 , F02C3/14 , F02C1/00
CPC分类号： F23D11/38 , B23B1/00 , B23P15/00 , B23P2700/13 , F23D2213/00 , Y10T29/4932 , Y10T29/49346 , Y10T29/494 , Y10T29/49419 , Y10T29/49432
摘要： A method and a pre-shaped workpiece for making at least a portion of a gas turbine fuel nozzle are disclosed having opposed gripping tabs which can be secured to machine tool holders during manufacturing by a machine tool.
摘要翻译：公开了一种用于制造燃气轮机燃料喷嘴的至少一部分的方法和预成形工件，其具有相对的夹紧突片，其可以通过机床在制造过程中固定到机床夹具。

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