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1. 发明申请

US20100132364A1 FUEL NOZZLE DETACHABLE BURNER TUBE 有权
标题翻译：燃油喷嘴可拆卸燃烧器管
公开(公告)号：US20100132364A1
公开(公告)日：2010-06-03
申请号：US12325559
申请日：2008-12-01
申请人： Geoffrey D. Myers , Scott Simmons , Stephen R. Thomas , Donald Mark Bailey , David Martin Johnson
发明人： Geoffrey D. Myers , Scott Simmons , Stephen R. Thomas , Donald Mark Bailey , David Martin Johnson
IPC分类号： F02C1/00 , B21D39/00
CPC分类号： F23R3/283 , F23R2900/00017 , Y10T29/49826
摘要： A fuel nozzle for use with a combustion chamber defined within a gas turbine engine and a method for assembling the same are provided. The fuel nozzle includes a swirler assembly and a burner tube that is coupled to a support flange in a detachable manner such that an inner surface of the burner tube circumscribes an outer surface of the swirler assembly during fuel nozzle operation.
摘要翻译：提供了一种与燃气涡轮发动机内限定的燃烧室一起使用的燃料喷嘴及其组装方法。燃料喷嘴包括旋流器组件和燃烧器管，其以可拆卸的方式联接到支撑凸缘，使得在燃料喷嘴操作期间燃烧器管的内表面围绕旋流器组件的外表面。

2. 发明授权

US08505304B2 Fuel nozzle detachable burner tube with baffle plate assembly 有权
标题翻译：燃油喷嘴可拆卸燃烧器管与挡板组件
公开(公告)号：US08505304B2
公开(公告)日：2013-08-13
申请号：US12325559
申请日：2008-12-01
申请人： Geoffrey D. Myers , Scott Simmons , Stephen R. Thomas , Donald Mark Bailey , David Martin Johnson
发明人： Geoffrey D. Myers , Scott Simmons , Stephen R. Thomas , Donald Mark Bailey , David Martin Johnson
IPC分类号： F23R3/14
CPC分类号： F23R3/283 , F23R2900/00017 , Y10T29/49826
摘要： A fuel nozzle for use with a combustion chamber defined within a gas turbine engine and a method for assembling the same are provided. The fuel nozzle includes a swirler assembly and a burner tube that is coupled to a support flange in a detachable manner such that an inner surface of the burner tube circumscribes an outer surface of the swirler assembly during fuel nozzle operation.
摘要翻译：提供了一种与燃气涡轮发动机内限定的燃烧室一起使用的燃料喷嘴及其组装方法。燃料喷嘴包括旋流器组件和燃烧器管，其以可拆卸的方式联接到支撑凸缘，使得在燃料喷嘴操作期间燃烧器管的内表面围绕旋流器组件的外表面。

3. 发明授权

US07861528B2 Fuel nozzle and diffusion tip therefor 有权
标题翻译：燃油喷嘴和扩散头
公开(公告)号：US07861528B2
公开(公告)日：2011-01-04
申请号：US11892298
申请日：2007-08-21
申请人： Geoffrey D. Myers , Scott Simmons , Stephen R. Thomas
发明人： Geoffrey D. Myers , Scott Simmons , Stephen R. Thomas
IPC分类号： F02C1/00
CPC分类号： F23R3/28 , F23D11/38 , F23D2209/30 , F23D2900/00018
摘要： A fuel nozzle having a dedicated circuit to cool the diffusion tip with lower part count and reduced complexity. More specifically, the proposed design uses an independent circuit to cool the tip with diffusion fuel or purge air. An impingement plate may be provided to augment the cooling effect.
摘要翻译：具有专用电路的燃料喷嘴，其具有以较低部件数量和降低的复杂度来冷却扩散尖端。更具体地，所提出的设计使用独立的电路来用扩散燃料或吹扫空气来冷却尖端。可以提供冲击板以增加冷却效果。

4. 发明申请

US20100107639A1 FUEL NOZZLE ASSEMBLY FOR USE WITH A GAS TURBINE ENGINE AND METHOD OF ASSEMBLING SAME 失效
标题翻译：用于燃气涡轮发动机的燃料喷嘴组件及其组装方法
公开(公告)号：US20100107639A1
公开(公告)日：2010-05-06
申请号：US12265233
申请日：2008-11-05
申请人： Geoffrey D. Myers , Scott Simmons , Stephen R. Thomas , Donald Mark Bailey
发明人： Geoffrey D. Myers , Scott Simmons , Stephen R. Thomas , Donald Mark Bailey
IPC分类号： F02C7/22 , B05B15/00 , F23R3/28
CPC分类号： F23R3/28 , F16L9/02 , F16L9/18 , F16L51/00 , F23D14/46 , F23D2206/10 , F23D2211/00 , F23D2212/20 , F23R2900/00005
摘要： A fuel nozzle configured to channel fluid toward a combustion chamber within a gas turbine engine and a method for assembling the same are provided. The fuel nozzle includes a first hollow tube fabricated from a first material that has a first coefficient of thermal expansion and a second tube fabricated from a second material that has a second coefficient of thermal expansion that is different from the first coefficient of thermal expansion. The second tube is coupled within the first tube such that the first tube substantially circumscribes the second tube, and the second tube thermally expands approximately at a same rate as the first tube during fuel nozzle operation.
摘要翻译：提供了一种构造成将流体引导到燃气涡轮发动机内的燃烧室的燃料喷嘴及其组装方法。燃料喷嘴包括由具有第一热膨胀系数的第一材料制成的第一中空管和由具有不同于第一热膨胀系数的第二热膨胀系数的第二材料制成的第二管。第二管联接在第一管内，使得第一管基本上包围第二管，并且第二管在燃料喷嘴操作期间以与第一管相同的速率大约膨胀。

5. 发明申请

US20100180599A1 Insertable Pre-Drilled Swirl Vane for Premixing Fuel Nozzle 审中-公开
标题翻译：可预先钻孔的涡流叶片用于预燃燃油喷嘴
公开(公告)号：US20100180599A1
公开(公告)日：2010-07-22
申请号：US12356572
申请日：2009-01-21
申请人： Stephen R. Thomas , Geoffrey D. Myers , Scott Simmons
发明人： Stephen R. Thomas , Geoffrey D. Myers , Scott Simmons
IPC分类号： F23R3/14 , B23P11/00
CPC分类号： F23R3/14 , F23C2900/07001 , F23R3/286 , Y10T29/49323
摘要： A swirl vane is independently connectable to a central hub assembly of a gas turbine. The swirl vane includes a structural body and at least one fuel delivery passage including a corresponding at least one fuel port defined within the structural body. At least one connecting tab is cooperable with the structural body and is connectable to the central hub assembly.
摘要翻译：涡流叶片可独立地连接到燃气轮机的中心轮毂组件。旋流叶片包括结构体和至少一个燃料输送通道，其包括限定在结构体内的对应的至少一个燃料端口。至少一个连接突片与结构体配合并且可连接到中心轮毂组件。

6. 发明申请

US20090050710A1 Fuel nozzle and diffusion tip therefor 有权
标题翻译：燃油喷嘴和扩散头
公开(公告)号：US20090050710A1
公开(公告)日：2009-02-26
申请号：US11892298
申请日：2007-08-21
申请人： Geoffrey D. Myers , Scott Simmons , Stephen R. Thomas
发明人： Geoffrey D. Myers , Scott Simmons , Stephen R. Thomas
IPC分类号： B05B1/00 , B05B15/00
CPC分类号： F23R3/28 , F23D11/38 , F23D2209/30 , F23D2900/00018
摘要： A fuel nozzle having a dedicated circuit to cool the diffusion tip with lower part count and reduced complexity. More specifically, the proposed design uses an independent circuit to cool the tip with diffusion fuel or purge air. An impingement plate may be provided to augment the cooling effect.
摘要翻译：具有专用电路的燃料喷嘴，其具有以较低部件数量和降低的复杂度来冷却扩散尖端。更具体地，所提出的设计使用独立的电路来用扩散燃料或吹扫空气来冷却尖端。可以提供冲击板以增加冷却效果。

7. 发明授权

US08752389B2 Fuel nozzle assembly for use with a gas turbine engine and method of assembling same 失效
标题翻译：用于燃气涡轮发动机的燃油喷嘴组件及其组装方法
公开(公告)号：US08752389B2
公开(公告)日：2014-06-17
申请号：US12265233
申请日：2008-11-05
申请人： Geoffrey D. Myers , Scott Simmons , Stephen R. Thomas , Donald Mark Bailey
发明人： Geoffrey D. Myers , Scott Simmons , Stephen R. Thomas , Donald Mark Bailey
IPC分类号： F02C1/00
CPC分类号： F23R3/28 , F16L9/02 , F16L9/18 , F16L51/00 , F23D14/46 , F23D2206/10 , F23D2211/00 , F23D2212/20 , F23R2900/00005
摘要： A fuel nozzle configured to channel fluid toward a combustion chamber within a gas turbine engine and a method for assembling the same are provided. The fuel nozzle includes a first hollow tube fabricated from a first material that has a first coefficient of thermal expansion and a second tube fabricated from a second material that has a second coefficient of thermal expansion that is different from the first coefficient of thermal expansion. The second tube is coupled within the first tube such that the first tube substantially circumscribes the second tube, and the second tube thermally expands approximately at a same rate as the first tube during fuel nozzle operation.
摘要翻译：提供了一种构造成将流体引导到燃气涡轮发动机内的燃烧室的燃料喷嘴及其组装方法。燃料喷嘴包括由具有第一热膨胀系数的第一材料制成的第一中空管和由具有不同于第一热膨胀系数的第二热膨胀系数的第二材料制成的第二管。第二管联接在第一管内，使得第一管基本上包围第二管，并且第二管在燃料喷嘴操作期间以与第一管相同的速率大约膨胀。

8. 发明授权

US6018091A Methods for thermally degrading unwanted substances using particular metal compositions 失效
标题翻译：使用特定金属组合物热降解不需要物质的方法
公开(公告)号：US6018091A
公开(公告)日：2000-01-25
申请号：US93280
申请日：1998-06-08
申请人： Stephen R. Thomas
发明人： Stephen R. Thomas
IPC分类号： A62D3/00 , A62D3/30 , A62D3/34 , A62D3/36 , A62D3/37 , A62D3/40 , A62D101/20 , A62D101/22 , A62D101/24 , A62D101/26 , A62D101/28 , A62D101/43 , B09B3/00 , C01B3/02 , C02F11/10 , C01B3/08 , C09K3/00
CPC分类号： A62D3/40 , A62D3/37 , B09B3/00 , A62D2101/22 , A62D2101/28
摘要： Methods and products for thermally degrading unwanted substances is provided which involves contacting such substances with a particulate metal composition in the presence of water and an alkali metal salt, and causing sufficient heat to be generated during such contacting to degrade the substance. The particulate metal compositions include respective quantities of particulate iron and magnesium, and optionally quantities of particulate aluminum and zinc. The compositions generate temperatures on the order of 300-550.degree. F. during such thermal degradations, along with quantities of hydrogen gas and water vapor.
摘要翻译：提供了用于热降解有害物质的方法和产品，其包括在水和碱金属盐的存在下使这些物质与颗粒状金属组合物接触，并且在这种接触期间产生足够的热量以使物质降解。颗粒状金属组合物包括各种量的铁和镁颗粒，以及任选量的颗粒状铝和锌。在这种热降解期间，组合物产生约300-550°F的温度，以及氢气和水蒸汽的量。

9. 发明授权

US4008498A Tub pad 失效
标题翻译：浴缸垫
公开(公告)号：US4008498A
公开(公告)日：1977-02-22
申请号：US587991
申请日：1975-06-18
申请人： Stephen R. Thomas
发明人： Stephen R. Thomas
IPC分类号： A61H33/02 , A61H33/06 , A61H9/00
CPC分类号： A61H33/025 , A61H33/06 , A61H2201/0103 , A61H33/6026
摘要： A water fillable pad for positioning on the tub bottom, the top wall of said water fillable pad having a plurality of elongated air tubes serially apertured, and a compressor with a heating element delivering heated compressed air through a manifold tube to said air tube so heated bubbles rise and agitate the tub water around the bather. The water fillable pad has a hingedly connected air inflatable back rest and an air inflatable side pad which drapes over the tube side wall and down to the float surface. A foot drain tray assembly is mounted to the free side edge of the air inflatable side pad member on which a bather can stand after finishing his bath. The foot drain tray assembly can be tucked under the water fillable pad when arching the air inflatable side pad member, thus forming a dome for the bather and a capture space for the discharged air bubbles.
摘要翻译：一种用于定位在桶底部的可填充水垫，所述可填充水垫的顶壁具有多个细长的空气管，其具有多个连续的孔径，以及具有加热元件的压缩机，该加热元件将加热的压缩空气通过歧管管传送到所述加热的空气管气泡上升并搅动浴室周围的水浴。可充水垫具有铰接连接的空气可充气靠背和可膨胀的气垫侧垫，其在管侧壁上覆盖并且向下浮动到浮动表面。脚部排水盘组件安装到可充气的侧垫构件的自由侧边缘上，泳池在完成浴后可以放置在其上。当排出空气可充气侧垫构件时，脚排水盘组件可被卷在可填充水垫下方，从而形成用于沐浴者的穹顶和排出的气泡的捕获空间。

10. 发明授权

US5673553A Apparatus for the destruction of volatile organic compounds 失效
标题翻译：用于破坏挥发性有机化合物的装置
公开(公告)号：US5673553A
公开(公告)日：1997-10-07
申请号：US538308
申请日：1995-10-03
申请人： Luis R. Maese , Ram Srinivasan , Stephen R. Thomas
发明人： Luis R. Maese , Ram Srinivasan , Stephen R. Thomas
IPC分类号： F02C3/20 , F02C7/00 , F23G5/46 , F23G7/06
CPC分类号： F23G5/46 , F02C3/20 , F23G7/065 , F23G2209/142 , Y02E20/12
摘要： A system for the destruction of volatile organic compounds while generating power. In a preferred embodiment the system comprises a combustor and a reaction chamber connected to an exit of the combustor. A primary inlet to the combustor supplies a primary fuel to the combustor. A secondary fuel, comprising air and an amount of one or more volatile organic compounds, is supplied to a compressor, which compresses the secondary fuel and directs the secondary fuel to the combustor and the reaction chamber. The system is suitably configured to enable the stoichiometric reaction of the two fuels in a manner sufficient to destroy the volatile organic compounds contained in the secondary fuel and power a turbine engine connected to an exit of the reaction chamber.
摘要翻译：用于在发电时破坏挥发性有机化合物的系统。在优选实施例中，系统包括连接到燃烧器的出口的燃烧器和反应室。燃烧器的主入口向燃烧器提供主要燃料。将包含空气和一定量的一种或多种挥发性有机化合物的二次燃料供应到压缩机，压缩机压缩二次燃料并将二次燃料引导到燃烧器和反应室。该系统适当地构造成使得能够以足以破坏二次燃料中所含的挥发性有机化合物的方式来实现两种燃料的化学计量反应，并为连接到反应室的出口的涡轮发动机供电。

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