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公开(公告)号：US3966120A
公开(公告)日：1976-06-29
申请号：US557622
申请日：1975-03-12
CPC分类号： B05B17/0623 , B01F11/02 , B01F3/04049 , B01F3/0407 , B01F5/0268 , F23D11/345 , G10K11/004
摘要： An ultrasonic spraying device for atomizing a liquid and for breaking up into fine particles any solids contained in the liquid. The device comprises an acoustical horn in which ultrasonic vibration is induced by a generator and having a surface against which liquid may be impinged. The liquid is directed against the surface by one or more conduits that are external of the horn. Means is provided for adjusting the spacing and orientation of the conduits with respect to the impingement surface, for isolating the horn vibrationally from a support upon which the horn is mounted, and the impingement surface may be of several different shapes for controlling the direction in which the impinging liquid is deflected. The invention also relates to the method of utilizing an ultrasonic horn for atomizing liquids and for breaking up solids into small particles.
摘要翻译： 一种用于雾化液体并将包含在液体中的任何固体分解成细颗粒的超声波喷射装置。 该装置包括声喇叭，其中由发生器引起超声波振动，并具有可以撞击液体的表面。 液体通过位于喇叭外部的一个或多个导管指向表面。 提供了用于调节导管相对于冲击表面的间隔和取向的装置，用于将喇叭与安装喇叭的支撑件振动地隔离，并且冲击表面可以具有几种不同的形状，用于控制 冲击液体偏转。 本发明还涉及使用超声波喇叭来雾化液体并将固体分解成小颗粒的方法。
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公开(公告)号：US5105621A
公开(公告)日：1992-04-21
申请号：US745814
申请日：1991-08-16
申请人： Harold C. Simmons , Roger V. Jones
发明人： Harold C. Simmons , Roger V. Jones
CPC分类号： F23D11/36 , F01N3/0256 , F23C5/02 , F23D2211/00 , F23D2214/00 , F23D2900/21003
摘要： A combustor for an exhaust gas system includes a longitudinally compliant fuel conduit for allowing thermal expansion and contraction of other portions of the combustor relative to the fuel conduit while not misaligning the atomizer to which the fuel conduit is attached. The combustor includes an exhaust duct, a combustion chamber, and an air duct in addition to the atomizer and longitudinally complaint fuel conduit. The combustion chamber and air duct are disposed within the exhaust duct so that they are heated by the exhaust gases passing through the exhaust duct. The fuel conduit is disposed within the air duct so that air passing through the air duct keeps the fuel conduit relatively cool.
摘要翻译： 用于废气系统的燃烧器包括纵向兼容的燃料管道，用于允许燃烧器的其它部分相对于燃料管道的热膨胀和收缩，同时不使与燃料管道连接的雾化器不对准。 除了雾化器和纵向投射燃料管道之外，燃烧器还包括排气管道，燃烧室和空气管道。 燃烧室和空气管道设置在排气管道内，使得它们被排气通过排气管道加热。 燃料管道设置在空气管道内，使得通过空气管道的空气使燃料管道相对冷却。
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公开(公告)号：US4365753A
公开(公告)日：1982-12-28
申请号：US180284
申请日：1980-08-22
CPC分类号： F23D11/24 , B05B7/0416 , B05B7/06 , B05B7/10 , F23D11/12
摘要： A gas turbine fuel injection nozzle is disclosed in which the secondary fuel is spread into a very thin film entirely within a region of low air momentum. The fuel is therefore not affected by turbulence, and this results in an evenly circumferentially distributed fuel film at the discharge orifice of the nozzle resulting in an even and extremely fine spray of fuel to enhance proper engine performance.
摘要翻译： 公开了一种燃气轮机燃料喷射喷嘴，其中二次燃料完全在低空气动量区域内扩散成非常薄的膜。 因此燃料不受湍流的影响，并且这导致在喷嘴的排放孔处的均匀的周向分布的燃料膜，导致均匀且极细的燃料喷雾以增强适当的发动机性能。
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公开(公告)号：US4139157A
公开(公告)日：1979-02-13
申请号：US719686
申请日：1976-09-02
申请人： Harold C. Simmons
发明人： Harold C. Simmons
CPC分类号： F23D11/107 , F23R3/28 , F23D2900/11101
摘要： In a nozzle for atomizing fuel into a spray for combustion in gas turbine engines, wherein the atomization is effected by the use of high velocity and/or high density air, and wherein the supply of fuel to two separately metered points is such that at low flow rates the first fuel supply is spread into a thin sheet for atomization but at high flow rates the second fuel supply is spread into a thicker sheet which combines with the thin sheet produced from the first supply, thus resulting in a single spray of constant shape at all operating conditions.
摘要翻译： 在用于将燃料雾化成用于燃气涡轮发动机中的燃烧的喷嘴的喷嘴中，其中通过使用高速和/或高密度空气来实现雾化，并且其中向两个分开计量的点供应燃料使得在低 流量使第一燃料供应物扩散到薄片中以进行雾化，但是在高流速下，第二燃料供应被扩散到与由第一供应产生的薄片组合的更厚的片材中，从而导致恒定形状的单次喷雾 在所有操作条件下。
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公开(公告)号：US5740967A
公开(公告)日：1998-04-21
申请号：US848791
申请日：1997-05-01
申请人： Harold C. Simmons , Rex J. Harvey
发明人： Harold C. Simmons , Rex J. Harvey
CPC分类号： B05B1/3436 , B05B1/3442 , C23F1/04 , F02M61/162 , F02M61/166 , F02M61/1853 , F23D11/383 , F23D2213/00
摘要： A method of forming an atomizing spray nozzle includes the steps of etching a swirl chamber and a spray orifice in a thin sheet of material. The swirl chamber is etched in a first side of the disk and the spray orifice is etched through a second side to the center of the swirl chamber. Feed slots are etched in the first side of the disk extending non-radially to the swirl chamber such that liquid can be conveyed to the swirl chamber so as to create and sustain the swirling motion. A inlet piece with inlet passage therein is connected with first side of the disk so as to convey liquid to the feed slots of the disk and to enclose the feed slots and swirl chamber. In addition to the method described an atomizing spray nozzle having the configuration described is much improved in its spray characteristics. The present invention also provides a method of forming a number of spray nozzles simultaneously in a single manufacturing process.
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公开(公告)号：US4595143A
公开(公告)日：1986-06-17
申请号：US516006
申请日：1983-07-20
CPC分类号： F23D11/105
摘要： A fuel nozzle wherein a swirl cone (36) is located between a housing (10) and a body (12). Body (12) cooperates with housing (10) to form an air chamber (32) and with cone (36) to form an inner annulus (40). Swirl vanes (34) are angularly mounted between cone (36) and body (12) such that air flowing from chamber (32) into annulus (40) forms a swirling flow pattern. Body (12) is provided with a fuel chamber (16) and radial passages (20) introduce fuel to the swirling air in inner annulus (40) to produce an atomized spray pattern.
摘要翻译： 一种燃料喷嘴，其中旋转锥体（36）位于壳体（10）和主体（12）之间。 主体（12）与壳体（10）配合以形成空气室（32）并具有锥体（36）以形成内环（40）。 漩涡叶片（34）角度地安装在锥体（36）和主体（12）之间，使得从室（32）流入环空（40）的空气形成旋流模式。 主体（12）设置有燃料室（16），并且径向通道（20）将燃料引入内环（40）中的旋转空气以产生雾化喷雾模式。
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公开(公告)号：US5435884A
公开(公告)日：1995-07-25
申请号：US129834
申请日：1993-09-30
申请人： Harold C. Simmons , Rex. J. Harvey
发明人： Harold C. Simmons , Rex. J. Harvey
IPC分类号： B05B1/02 , B05B1/04 , B05B1/34 , B05B3/02 , C23F1/04 , F02M61/16 , F02M61/18 , F23D11/38 , B05D5/00
CPC分类号： B05B1/3436 , B05B1/3442 , C23F1/04 , F02M61/162 , F02M61/166 , F02M61/1853 , F23D11/383 , F23D2213/00
摘要： A method of forming an atomizing spray nozzle includes the steps of etching a swirl chamber and a spray orifice in a thin sheet of material. The swirl chamber is etched in a first side of the disk and the spray orifice is etched through a second side to the center of the swirl chamber. Feed slots are etched in the first side of the disk extending non-radially to the swirl chamber such that liquid can be conveyed to the swirl chamber so as to create and sustain the swirling motion. A inlet piece with inlet passage therein is connected with first side of the disk so as to convey liquid to the feed slots of the disk and to enclose the feed slots and swirl chamber. In addition to the method described an atomizing spray nozzle having the configuration described is much improved in its spray characteristics. The present invention also provides a method of forming a number of spray nozzles simultaneously in a single manufacturing process.
摘要翻译： 形成雾化喷嘴的方法包括以薄片材料蚀刻涡流室和喷射孔的步骤。 旋转室在盘的第一侧被蚀刻，并且喷孔通过第二侧蚀刻到涡流室的中心。 进料槽在盘的第一侧被蚀刻，其非径向延伸到涡流室，使得液体可被输送到涡流室，从而产生和维持旋转运动。 其中具有入口通道的入口件与盘的第一侧连接，以将液体输送到盘的进料槽并且包围进料槽和涡流室。 除了所述方法之外，具有所述结构的雾化喷嘴在其喷雾特性方面得到了很大改进。 本发明还提供了在单个制造过程中同时形成多个喷嘴的方法。
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公开(公告)号：US4168803A
公开(公告)日：1979-09-25
申请号：US829330
申请日：1977-08-31
CPC分类号： F23D11/107 , F02C7/2365 , F02C7/26 , F23D2900/11101
摘要： A nozzle for atomizing fuel for combustion in a gas turbine engine. During normal operation of the engine, the nozzle uses a portion of the air supplied to the combustion chamber by the engine compressor to atomize fuel flowing through the nozzle. During start-up and low power operation of the engine when flow of engine air through the nozzle would otherwise be of insufficient velocity to cause good atomization of the fuel, additional air from a separate external source is introduced at high velocity into the nozzle in the manner of an ejector. The additional air imparts high velocity to the engine air within the nozzle so that the air from both sources acts on the fuel at the nozzle discharge orifice at high velocity to effect good atomization and spray pattern of the fuel. The nozzle is designed in such a manner as to cause no significant restriction of engine air flow through the nozzle under high power operation of the engine when the external air source is shut off.
摘要翻译： 一种用于雾化燃气涡轮发动机中燃烧燃料的喷嘴。 在发动机的正常操作期间，喷嘴使用由发动机压缩机供应到燃烧室的空气的一部分来雾化流过喷嘴的燃料。 在发动机的起动和低功率运行期间，当发动机空气通过喷嘴的流动否则将不足够的速度以引起燃料的良好雾化时，来自分离的外部源的附加空气以高速度被引入喷嘴中 喷射器的方式。 附加空气将高速度赋予喷嘴内的发动机空气，使得来自两个源的空气以高速度作用在喷嘴排出口处的燃料上，以实现燃料的良好雾化和喷雾模式。 喷嘴的设计方式是在外部空气源被关闭时在发动机的高功率操作下不会对通过喷嘴的发动机气流进行明显的限制。
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公开(公告)号：US5951882A
公开(公告)日：1999-09-14
申请号：US22778
申请日：1998-02-12
申请人： Harold C. Simmons , Rex J. Harvey
发明人： Harold C. Simmons , Rex J. Harvey
IPC分类号： B05B1/02 , B05B1/04 , B05B1/34 , B05B3/02 , C23F1/04 , F02M61/16 , F02M61/18 , F23D11/38 , B05D5/00
CPC分类号： B05B1/3436 , B05B1/3442 , C23F1/04 , F02M61/162 , F02M61/166 , F02M61/1853 , F23D11/383 , F23D2213/00
摘要： A method of forming an atomizing spray nozzle includes the steps of etching a swirl chamber and a spray orifice in a thin sheet of material. The swirl chamber is etched in a first side of the disk and the spray orifice is etched through a second side to the center of the swirl chamber. Feed slots are etched in the first side of the disk extending non-radially to the swirl chamber such that liquid can be conveyed to the swirl chamber so as to create and sustain the swirling motion. A inlet piece with inlet passage therein is connected with first side of the disk so as to convey liquid to the feed slots of the disk and to enclose the feed slots and swirl chamber. In addition to the method described an atomizing spray nozzle having the configuration described is much improved in its spray characteristics. The present invention also provides a method of forming a number of spray nozzles simultaneously in a single manufacturing process.
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公开(公告)号：US4616784A
公开(公告)日：1986-10-14
申请号：US673294
申请日：1984-11-20
CPC分类号： B05B7/0433 , B05B7/0475 , B05B7/10 , F23D1/005
摘要： An atomizing nozzle suitable for use with high-viscosity slurries wherein a body (10) and forming element (40) include passageways (18, 22 and 48) that lead to a conical chamber (65) having a discharge annulus (66). The slurry exits discharge annulus (66) in a cylindrical continuous film. The inside of the film is exposed to swirled, compressed gas from an internal bore (50) of forming element (40) and the outside of the film is exposed to swirled compressed gas in a swirl chamber (72) to atomize and mix the slurry.
摘要翻译： 适用于高粘度浆料的雾化喷嘴，其中主体（10）和成形元件（40）包括通向具有排出环（66）的锥形室（65）的通道（18,22和48）。 浆料以圆柱形连续膜离开排出环（66）。 膜的内部从成形元件（40）的内孔（50）暴露于旋转的压缩气体，并且膜的外部暴露于漩涡室（72）中的涡旋压缩气体以雾化并混合浆料 。
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