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1. 发明授权

US5289687A One-piece cowl for a double annular combustor 失效
标题翻译：一体式整流罩，用于双环形燃烧器
公开(公告)号：US5289687A
公开(公告)日：1994-03-01
申请号：US860398
申请日：1992-03-30
申请人： Eric J. Kress , Joseph F. Savelli , David W. Parry , John M. Koshoffer
发明人： Eric J. Kress , Joseph F. Savelli , David W. Parry , John M. Koshoffer
IPC分类号： F23R3/42 , F23R3/04 , F23R3/28 , F23R3/34 , F23R3/46 , F23R3/50 , F23R3/60
CPC分类号： F23R3/04 , F23R3/283 , F23R3/34 , F23R3/50 , F23R3/60 , Y02T50/675
摘要： A double annular combustor having concentrically disposed inner and outer annular combustors is provided with inner and outer domes. A one-piece cowl is provided upstream of the inner and outer domes in order to form a high pressure region. The one-piece cowl has an inner annular portion, an outer annular portion, and a radial middle portion connecting the inner and outer annular portions. The inner and outer annular portions include scalloped areas therein to facilitate insertion and removal of fuel tubes and nozzles. The cowl middle portion includes a shield to isolate the scalloped areas and the fuel tube from the high pressure region, thereby preventing leakage of air flow and consequential pressure loss from the high pressure region.
摘要翻译：具有同心设置的内外环形燃烧器的双环形燃烧器设置有内圆顶和外圆顶。为了形成高压区，在内圆顶和外圆顶的上游设有一体式整流罩。一体式整流罩具有内环形部分，外环形部分和连接内外环形部分的径向中间部分。内部和外部环形部分包括扇形区域，以便于燃料管和喷嘴的插入和移除。整流罩中部包括用于隔离扇形区域和燃料管与高压区域的屏蔽，从而防止空气流的泄漏和从高压区域引起的压力损失。

2. 发明授权

US5483793A Infrared radiation suppression device 失效
标题翻译：红外辐射抑制装置
公开(公告)号：US5483793A
公开(公告)日：1996-01-16
申请号：US078334
申请日：1970-09-02
申请人： Barry Weinstein , John M. Koshoffer , Roy E. Moyer
发明人： Barry Weinstein , John M. Koshoffer , Roy E. Moyer
IPC分类号： F02K1/38 , F02K1/82 , F02K3/10 , F02K3/06
CPC分类号： F02K1/386 , F02K1/825
摘要： A gas turbine engine of the type generating a hot gas stream and a fan stream includes a mixer having upstream and downstream portions which define first and second chutes for efficiently mixing the streams prior to discharge through an engine nozzle. Means are provided to selectively communicate the downstream chutes with alternate ones of the upstream chutes to cool the downstream mixer portion and reduce the infrared radiation emissions from the nozzle,
摘要翻译：产生热气流和风扇流的类型的燃气涡轮发动机包括具有上游和下游部分的混合器，所述上游和下游部分限定第一和第二滑槽，用于在通过发动机喷嘴排出之前有效地混合流。提供装置以选择性地将下游斜槽与替代的上游滑槽通信，以冷却下游混合器部分并减少来自喷嘴的红外辐射发射，

3. 发明授权

US5239832A Birdstrike resistant swirler support for combustion chamber dome 失效
标题翻译： BIRDSTRIKE耐火SWIRLER支持燃烧室壁
公开(公告)号：US5239832A
公开(公告)日：1993-08-31
申请号：US813613
申请日：1991-12-26
申请人： John M. Koshoffer , James N. Cooper , Mary C. Haas , James N. Reinhold, Jr.
发明人： John M. Koshoffer , James N. Cooper , Mary C. Haas , James N. Reinhold, Jr.
IPC分类号： F02C7/00 , F23R3/28 , F23R3/46 , F23R3/60
CPC分类号： F23R3/283
摘要： A backing support or bumper mounted downstream of the disk shaped flange of the venturi in adjacently lying fuel cup assemblies and extends to a mid portion of each flange to prevent rotation of the flange and possible disengagement of the fuel nozzle in the event of a bird strike or impact by a foreign object on the dome of the combustor or on the flange itself. The invention provides for a single or double supporting bumper faces or a pair of supporting surfaces on the bumper.

4. 发明授权

US5682739A Infrared radiation suppression device 失效
标题翻译：红外辐射抑制装置
公开(公告)号：US5682739A
公开(公告)日：1997-11-04
申请号：US473392
申请日：1995-06-07
申请人： Barry Weinstein , John M. Koshoffer , Roy E. Moyer
发明人： Barry Weinstein , John M. Koshoffer , Roy E. Moyer
IPC分类号： F02K1/38 , F02K1/82 , F02K3/10 , F02K3/06
CPC分类号： F02K1/386 , F02K1/825
摘要： A gas turbine engine of the type generating a hot gas stream and a fan stream includes a mixer having upstream and downstream portions which define first and second chutes for efficiently mixing the streams prior to discharge through an engine nozzle. Means are provided to selectively communicate the downstream chutes with alternate ones of the upstream chutes to cool the downstream mixer portion and reduce the infrared radiation emissions from the nozzle.
摘要翻译：产生热气流和风扇流的类型的燃气涡轮发动机包括具有上游和下游部分的混合器，所述上游和下游部分限定第一和第二滑槽，用于在通过发动机喷嘴排出之前有效地混合流。提供装置以选择性地将下游滑槽与替代的上游滑槽通信，以冷却下游混合器部分并减少来自喷嘴的红外辐射。

5. 发明授权

US5181377A Damped combustor cowl structure 失效
标题翻译：阻燃的COMBUSTOR COWL结构
公开(公告)号：US5181377A
公开(公告)日：1993-01-26
申请号：US685947
申请日：1991-04-16
申请人： Phillip D. Napoli , John M. Koshoffer
发明人： Phillip D. Napoli , John M. Koshoffer
IPC分类号： F23R3/42 , F23R3/00 , F23R3/60
CPC分类号： F23R3/60 , F23R3/002
摘要： A friction-damped combustor cowl is formed of first and second plies of sheet material of mating, generally annular configuration defining a central cowl axis and of axially elongated and aerodynamically contoured configuration have respective fore end portions which are curled to form a cowl leading edge of arcuate cross section and corresponding fore edges which are integrally joined, and respective aft end portions which define a cowl trailing edge and corresponding aft edges which are integrally joined. Surface contact of the contiguous surfaces of the laminated and mating first and second plies provides vibration damping under normal operating conditions in an alternative and combustor cowl, a spring element is received and maintained under compression within the curled leading edge of the combustor cowl and maintains a resilient biasing force maintaining surface contact between the spring element and the interior surface of the curled leading edge, thereby maintaining frictional surface contact and requisite vibration damping under normal operating conditions.

6. 发明授权

US5323604A Triple annular combustor for gas turbine engine 失效
标题翻译：用于燃气轮机的三重环形燃烧器
公开(公告)号：US5323604A
公开(公告)日：1994-06-28
申请号：US976752
申请日：1992-11-16
申请人： Edward E. Ekstedt , Narendra D. Joshi , Adrian M. Ablett , Timothy R. Gresla , John M. Koshoffer , William F. Burke
发明人： Edward E. Ekstedt , Narendra D. Joshi , Adrian M. Ablett , Timothy R. Gresla , John M. Koshoffer , William F. Burke
IPC分类号： F23R3/34 , F02C7/228
CPC分类号： F23R3/34 , F23R3/002 , F23R2900/03043 , Y02T50/675
摘要： In accordance with one aspect of the present invention, a combustor is disclosed having three separate domes, each dome having disposed therein a plurality of circumferentially spaced mixers for uniformly mixing air and fuel. The combustor utilizes a high percentage of the total available combustion air at the dome area in order to maintain a lean mixture of air and fuel during all levels of engine output. Besides providing an unobstructed area in the diffuser dump region upstream of the mixers for the combustion air, sealing means is included to prevent cooling air from entering the combustion chamber until downstream of the primary combustion zone. Heat shields having radial centerbodies are also included between each dome to isolate each primary combustion zone.
摘要翻译：根据本发明的一个方面，公开了一种具有三个独立圆顶的燃烧器，每个圆顶上设置有多个周向间隔开的混合器，用于均匀混合空气和燃料。燃烧器在圆顶区域使用高百分比的总可用燃烧空气，以便在所有级别的发动机输出期间保持空气和燃料的贫混合。除了在用于燃烧空气的混合器上游的扩散器倾卸区域内提供无障碍区域之外，还包括密封装置以防止冷却空气进入燃烧室直到主燃烧区域的下游。每个圆顶之间还包括具有径向中心体的隔热隔离每个主燃烧区。

7. 发明授权

US5117628A Mixed flow augmentor pre-mixer 失效
标题翻译：混合流动辅助器预混合器
公开(公告)号：US5117628A
公开(公告)日：1992-06-02
申请号：US469982
申请日：1990-01-25
申请人： John M. Koshoffer
发明人： John M. Koshoffer
IPC分类号： F02K3/06 , F02K1/38 , F02K1/48 , F02K3/10 , F02K3/105
CPC分类号： F02K1/48 , F02K1/386 , F02K3/10 , F02K3/105 , F05D2260/20 , Y02T50/675
摘要： A mixer arrangement for a bypass type gas turbine engine is disclosed. The mixer is convoluted and generally annular and defines radially and axially extending first and second chutes adapted to receive, respectively, a hot gas stream from the engine core and a cooler gas stream from the fan duct. A pre-mixer is disposed upstream of the mixer and is also convoluted and is aligned in flow communication with the second chutes of the mixer such that the hot gas stream received by the pre-mixer is mixed with the cooler fan air stream received by the second chutes to raise the temperature of the fan air entering an afterburner section of the engine.
摘要翻译：公开了一种用于旁路式燃气涡轮发动机的混合器装置。混合器是回旋的并且大致环形并且限定径向和轴向延伸的第一和第二滑槽，其适于分别接收来自发动机芯的热气流和来自风扇导管的较冷气体流。预混合器设置在混合器的上游并且还被卷积并且与混合器的第二滑槽流动连通地对准，使得由预混合器接收的热气流与由所述混合器接收的冷却器风机气流混合第二滑槽，以提高进入发动机加燃器部分的风扇空气的温度。

8. 发明授权

US4584834A Gas turbine engine carburetor 失效
标题翻译：燃气涡轮发动机化油器
公开(公告)号：US4584834A
公开(公告)日：1986-04-29
申请号：US395536
申请日：1982-07-06
申请人： John M. Koshoffer , Edward E. Ekstedt , Billy P. Samuel , Edward I. Stamm
发明人： John M. Koshoffer , Edward E. Ekstedt , Billy P. Samuel , Edward I. Stamm
IPC分类号： F23R3/04 , F23R3/14 , F23R3/30 , F02C7/22
CPC分类号： F23R3/14 , F23R3/04 , Y02T50/675
摘要： A carburetion assembly including flow control means is provided for controlling a discharge spray angle of a fuel and air mixture thereof. According to one embodiment of the present invention, the flow control means can comprise a plurality of circumferentially spaced apertures in a shroud member which are effective for providing a control portion of compressor airflow in a downstream, axial direction from a swirler stage of the swirler assembly. The apertures provide a predetermined amount of airflow circumferentially about the fuel and air mixture for constraining the mixture and controlling the discharge spray angle thereof.
摘要翻译：提供了包括流量控制装置的化油组件，用于控制其燃料和空气混合物的排放喷雾角度。根据本发明的一个实施例，流量控制装置可以包括在护罩构件中的多个周向间隔开的孔，其有效地用于在旋流器组件的旋流器级的下游轴向方向上提供压缩机气流的控制部分。孔口围绕燃料和空气混合物周向地提供预定量的气流，用于约束混合物并控制其喷射喷射角度。

9. 发明授权

US5596873A Gas turbine combustor with a plurality of circumferentially spaced pre-mixers 失效
标题翻译：具有多个周向间隔的预混合器的燃气轮机燃烧器
公开(公告)号：US5596873A
公开(公告)日：1997-01-28
申请号：US305629
申请日：1994-09-14
申请人： Narendra D. Joshi , John M. Koshoffer
发明人： Narendra D. Joshi , John M. Koshoffer
IPC分类号： F23R3/28 , F23R3/50 , F02C7/08
CPC分类号： F23R3/50 , F23R3/286 , F05B2240/40
摘要： An annular combustor with an air fuel mixer is disclosed including a plurality of mixing tubes having a forward end and an exit end, wherein a longitudinal axis through the exit end for each mixing tube is at both an axial angle and a radial angle to the centerline axis of the mixer. A fuel injector for providing fuel to the forward end of each mixing tube, a fuel manifold in flow communication with each of the fuel injectors, and a fuel supply and control means are provided. High pressure air from a compressor is injected into the mixing tubes and fuel is injected into the mixing tubes from the fuel injectors, wherein the high pressure air and the fuel is uniformly mixed therein so as to produce minimal formation of pollutants when the fuel/air mixture is exhausted out the downstream end of the mixing tubes into the combustor and combusted. The mixing tubes preferably impart a swirl to the fuel/air mixture as it exits into the combustor.
摘要翻译：公开了一种具有空气燃料混合器的环形燃烧器，其包括具有前端和出口端的多个混合管，其中通过每个混合管的出口端的纵向轴线与中心线处于轴向角度和径向角度搅拌机轴。提供一种用于向每个混合管的前端提供燃料的燃料喷射器，与每个燃料喷射器流动连通的燃料歧管以及燃料供应和控制装置。来自压缩机的高压空气被注入到混合管中，并且燃料从燃料喷射器注入到混合管中，其中高压空气和燃料均匀混合在其中，以便当燃料/空气混合物从混合管的下游端排出到燃烧器中并燃烧。混合管优选在燃料/空气混合物离开燃烧器时给予涡流。

10. 发明授权

US4686826A Mixed flow augmentor incorporating a fuel/air tube 失效
标题翻译：混合流量增加器，包含燃料/空气管
公开(公告)号：US4686826A
公开(公告)日：1987-08-18
申请号：US149792
申请日：1980-05-14
申请人： John M. Koshoffer , Richard A. Pfefferle , Harold A. Larson
发明人： John M. Koshoffer , Richard A. Pfefferle , Harold A. Larson
IPC分类号： F02K1/38 , F23R3/20 , F23R3/22 , F02K3/10 , F02K3/04
CPC分类号： F23R3/20 , F02K1/386 , F23R3/22 , Y02E20/344
摘要： In a turbofan jet engine, having a circumferentially rotatable mixer segment capable of orienting the afterburner ignitors and flameholders into the path of either the exhaust gases or bypass air, a fuel-air transfer apparatus for capturing, transporting and the releasing of an enriched fuel-air concentration from the fuel spray bars, on the stationary structure of the jet engine, to the afterburner ignitors and flameholders rigidly attached at the rear of the rotatable segment of the mixer. The enriched fuel-air mixture is transported between a location of reliable fuel availability, through a region of highly turbulent gas flow and is thereafter released while still in an enriched concentration immediately upstream of the ignitors and flameholders, facilitating ignition and sustained operation of the afterburner. The transfer of the fuel-air mixture with the exhaust gases in a confining apparatus precludes the necessity for transferring fuel, by flexible attachment or other means, between the stationary jet engine structure and the rotatable segment of the mixer, upon which the ignitors and flameholders are mounted, while insuring an appropriate fuel-air mixture for ignition and operation of the afterburner.
摘要翻译：在涡轮风扇喷气发动机中，具有能够将加力燃烧器点火器和火焰保持器定向到废气或旁路空气的路径中的周向可旋转的混合器段，用于捕获，运输和释放富集的燃料 - 来自喷气发动机的固定结构上的燃料喷射杆的空气浓度到刚性连接在混合器的可旋转段的后部的加力燃烧器点火器和火焰支架。浓缩的燃料 - 空气混合物在可靠的燃料可用性的位置之间通过高度湍流的气体流动的区域运输，然后在紧邻火焰和火焰保持器上游的富集浓度的同时被释放，促进后燃器的点燃和持续运行。燃料 - 空气混合物与废气在限制装置中的转移排除了在固定的喷气发动机结构和混合器的可旋转部分之间通过柔性附接或其它装置传送燃料的必要性，在该混合器上，点火器和火焰支架同时确保适当的燃料 - 空气混合物用于燃烧器的点火和操作。

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