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公开(公告)号：US20180195439A1
公开(公告)日：2018-07-12
申请号：US15868900
申请日：2018-01-11
申请人： DYC TURBINES, LLC
发明人： Daih-Yeou CHEN
CPC分类号： F02C7/2365 , F02C7/26 , F23D11/04 , F23D11/06 , F23D11/08 , F23D2206/10 , F23D2900/11101 , F23R3/12 , F23R3/14 , F23R3/28
摘要： An electric motor assisted airblast injector design for gas turbines is disclosed. The electric motor assisted airblast injector assembly consists of an airblast injector, a high speed electric motor and a compressor. The electric motor assisted airblast injector is designed to improve engine light-off and starting reliability without using a fuel staging system to incorporate pressure injectors. A high speed motor is activated during starting to drive a compressor for locally producing pressurized air without sacrificing combustor performance. The pressurized air exiting the air swirler with high velocity penetrates perpendicularly into the fuel spray cone obtained by orifices in the fuel swirler. The amount of pressurized air through the compressor is controlled by motor speed to match fuel starting schedule and produce fuel/air mixture within flammability limits. After engine starting, the high speed motor may cut off as sufficient air pressure differential is available across the combustor.
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公开(公告)号：US20170370591A1
公开(公告)日：2017-12-28
申请号：US15543563
申请日：2016-01-12
摘要： The invention relates to a turbine engine combustion assembly (20), which includes: an annular flame tube (21) including a front wall (23), a rear wall (24) and a bottom (22) arranged facing an engine shaft (30); an injection wheel (41) rotated by said engine shaft (30), partially projecting into the bottom (22) of the flame tube (21) and configured such as to spray fuel into the flame tube by centrifugation; and at least one injector (35), capable of depositing a film of fuel on said injection wheel (41), said combustion assembly being characterised in that said injector (35) is arranged so as to pass through said upstream area of the front wall (23) or the rear wall (24) of the flame tube (21), so that the injection opening thereof (37) opens into said tube (21), opposite the portion (43) of said injection wheel (41) which is located inside said flame tube (21).
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公开(公告)号：US20160312708A1
公开(公告)日：2016-10-27
申请号：US14696655
申请日：2015-04-27
申请人： DYC Turbines, LLC
发明人： Daih-Yeou CHEN
IPC分类号： F02C7/236
CPC分类号： F02C7/2365 , F02C7/26 , F23D11/04 , F23D11/06 , F23D11/08 , F23D2206/10 , F23D2900/11101 , F23R3/12 , F23R3/14 , F23R3/28
摘要： An electric motor assisted airblast injector design for gas turbines is disclosed. The electric motor assisted airblast injector assembly consists of an airblast injector, a high speed electric motor and a compressor. The electric motor assisted airblast injector is designed to improve engine light-off and starting reliability without using a fuel staging system to incorporate pressure injectors. A high speed motor is activated during starting to drive a compressor for locally producing pressurized air without sacrificing combustor performance. The pressurized air exiting the air swirler with high velocity penetrates perpendicularly into the fuel spray cone obtained by orifices in the fuel swirler. The amount of pressurized air through the compressor is controlled by motor speed to match fuel starting schedule and produce fuel/air mixture within flammability limits. After engine starting, the high speed motor may cut off as sufficient air pressure differential is available across the combustor.
摘要翻译： 公开了一种用于燃气轮机的电动机辅助的喷气器喷射器设计。 电动机辅助的喷气器组件包括喷气喷射器，高速电动机和压缩机。 电动机辅助的喷气式喷射器设计用于在不使用燃料分级系统并入压力注射器的情况下提高发动机熄火和启动可靠性。 高速电动机在起动时启动以驱动压缩机以局部生产加压空气而不牺牲燃烧室性能。 离开空气旋流器的加压空气以高速度垂直地穿入由燃料旋流器中的孔口获得的燃料喷雾锥体。 通过压缩机的加压空气量由电机速度控制，以匹配燃料起动时间表，并在燃烧极限内产生燃料/空气混合物。 在发动机启动后，由于在整个燃烧器上有足够的气压差可以切断高速电机。
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公开(公告)号：US08006500B1
公开(公告)日：2011-08-30
申请号：US12021456
申请日：2008-01-29
申请人： Jack W. Wilson, III
发明人： Jack W. Wilson, III
摘要： A combustor for a small gas turbine engine in which a compressor discharges a swirling air flow into the combustor, and a fuel impeller is rotatably connected to the compressor and slings atomized fuel into the combustor in a direction to produce a stagnation zone within the combustor. A plurality of fuel injectors delivers fuel to the inlet end of the fuel impeller. The combustor outlet is a nozzle shape that produces a high enough pressure level in the swirl air flow such that the cooler air flows along the inner combustor wall to form an insulation layer from the hot combustor gas flow within the combustor. The fuel impeller produces a very fine mist of fuel and the stagnation zone produced results in easy starting of the engine and stable combustor burning.
摘要翻译： 一种用于小型燃气涡轮发动机的燃烧器，其中压缩机将涡旋空气流排放到燃烧器中，并且燃料叶轮可旋转地连接到压缩机，并且沿着在燃烧器内产生停滞区的方向将雾化的燃料吊起到燃烧器中。 多个燃料喷射器将燃料输送到燃料叶轮的入口端。 燃烧器出口是在涡流空气流中产生足够高的压力水平的喷嘴形状，使得较冷的空气沿着内部燃烧器壁流动，以形成与燃烧器内的热燃烧器气体流的绝缘层。 燃料叶轮产生非常细的燃料雾，并且产生的停滞区导致发动机容易启动和燃烧器燃烧稳定。
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公开(公告)号：US3947230A
公开(公告)日：1976-03-30
申请号：US506928
申请日：1974-09-17
摘要： A combustion chamber device includes a combustion chamber and a rotatable cup-shaped fuel spreader arranged centrally therein. Liquid fuel is supplied to within said cup for being distributed therein and discharged therefrom and intermixed with an air stream supplied to said combustion chamber to form an air-fuel mixture which then is ignited. The spreader cup is located adjacent a combustion zone in the combustion chamber and provided with an enclosing insulation in the form of a layer of axially flowing air. According to the invention, the fuel spreader cup has a substantially straight and cylindrical inner surface with a circumferential shoulder or threshold adjacent the open end, said shoulder having a radial thickness sufficient for maintaining inside said spreader cup a fuel layer of required depth for obtaining a predetermined fuel supply volume in the cup. The spreader cup and the adjacent portions of the combustion chamber are shaped so as to provide around the rotary spreader cup a return-flow zone for the air-fuel-mixture in which is maintained a primary combustion zone, which pre-heats the cup so as to bring same to normally operate as vaporizer, while sufficient air is supplied to the air layer surrounding the cup for avoiding over-heating and boiling of the fuel in the cup.
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公开(公告)号：US3697214A
公开(公告)日：1972-10-10
申请号：US3697214D
申请日：1971-01-12
发明人： TSUJI SHOICHI
IPC分类号： F23D11/04
CPC分类号： F23D11/04
摘要： An oil burner wherein a rotary blower system supplies air to a stationary fuel supply pipe. The pipe has no internal horizontal part except for a short tip of its nozzle. This arrangement counteracts solidification of oil in the supply pipe. Said tip is positioned in such manner that liquid fuel is discharged therefrom centrally of, and in the direction toward, a rotary plate. A blower supplies compressed air to the interstice between housing and plate. From there, a mixture of oil and air then enters a burner ring or the like.
摘要翻译： 一种油燃烧器，其中旋转鼓风机系统向固定燃料供应管道供应空气。 管子没有内部水平部分，除了其喷嘴的短尖端。 这种安排抵消了供应管中油的固化。 所述尖端以这样的方式定位，使得液体燃料从旋转板的中心和朝向旋转板的方向排出。 鼓风机将压缩空气供给壳体和板之间的空隙。 从那里，油和空气的混合物然后进入燃烧器环等。
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公开(公告)号：US3425631A
公开(公告)日：1969-02-04
申请号：US3425631D
申请日：1967-07-07
发明人： HENSLEY MAX J
CPC分类号： F23D11/04
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公开(公告)号：US3220457A
公开(公告)日：1965-11-30
申请号：US13709961
申请日：1961-09-11
发明人： BAILEY FRANK W
IPC分类号： F23D11/04
CPC分类号： F23D11/04
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