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公开(公告)号：US09920689B2
公开(公告)日：2018-03-20
申请号：US14211140
申请日：2014-03-14
发明人： M. Razi Nalim
CPC分类号： F02C5/11 , F02C3/02 , F02C3/16 , F02C5/04 , Y02T50/671 , Y10S903/93
摘要： A hybrid propulsion system includes a wave rotor combustion engine operating in parallel with an electrical motor-generator element. The motor-generator element is coupled to the turbine shaft to selectively drive or be driven by the turbine shaft. In one mode of operation, the motor of the motor generator element is powered by a battery to provide rotational energy to the turbine shaft. In another mode of operation, the wave rotor combustion engine drives the generator to recharge the battery. The wave rotor combustion engine may be further directly coupled to auxiliary components without a gearbox to drive the components at substantially the same speed as the turbine shaft. The turbine rotor of the combustion engine includes a plurality of chambers defined by circumferentially spaced curved vanes that improves specific fuel consumption for the engine.
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2.发明授权Methods and apparatus for controlling air flow within a pulse detonation engine 有权用于控制脉冲爆震发动机内气流的方法和装置公开(公告)号：US07980056B2
公开(公告)日：2011-07-19
申请号：US11348869
申请日：2006-02-07
申请人： Adam Rasheed , Anthony John Dean
发明人： Adam Rasheed , Anthony John Dean
IPC分类号： F02C7/04
摘要： A flow control device for use with a pulse detonation chamber including an inlet coupled in flow communication with a source of compressed air. The inlet extends at least partially into the chamber to facilitate controlling air flow into the chamber. The device also includes a body portion extending downstream from and circumferentially around the inlet, wherein the body portion is positioned in flow communication with the inlet.
摘要翻译： 一种用于脉冲爆震室的流量控制装置，包括与压缩空气源流动连通的入口。 入口至少部分地延伸到室中以便于控制进入室的空气流。 该装置还包括从入口的下游和周向延伸的主体部分，其中主体部分定位成与入口流动连通。
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公开(公告)号：US20090286189A1
公开(公告)日：2009-11-19
申请号：US12500887
申请日：2009-07-10
IPC分类号： F23C15/00
CPC分类号： F02C5/11
摘要： A pressure rise combustor is provided with fuel provided at intermittent periods. The fuel is pulsed at timings such that the phase lag between the addition of the fuel and a resultant pressure rise is minimised. The fuel is pulsed such that the unsteady addition of heat reinforces the amplitude of an unsteady pressure fluctuation.
摘要翻译： 压力升高燃烧器设置有间歇期间提供的燃料。 燃料在定时被脉冲化，使得加入燃料和产生的压力上升之间的相位滞后最小化。 燃料被脉冲化，使得不稳定的加热增强了不稳定压力波动的振幅。
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公开(公告)号：US07100360B2
公开(公告)日：2006-09-05
申请号：US10608238
申请日：2003-06-27
申请人： Bradley C. Sammann , Wendell V. Twelves, Jr. , Gary D. Jones , James W. Norris , Harvey L. Klein , James E. Jones , Stephen K. Kramer , Douglas A. Thonebe
发明人： Bradley C. Sammann , Wendell V. Twelves, Jr. , Gary D. Jones , James W. Norris , Harvey L. Klein , James E. Jones , Stephen K. Kramer , Douglas A. Thonebe
IPC分类号： F02K3/02
摘要： A pulsed combustion device includes a support structure and a combustor carousel supported by the support structure and rotating relative thereto about an axis. The carousel has a number of combustion conduits in a circumferential array. Each conduit cyclically receives a charge and discharges combustion products of the charge.
摘要翻译： 脉冲燃烧装置包括支撑结构和由支撑结构支撑并相对于其围绕轴线旋转的燃烧器转盘。 圆盘传送带具有多个周向排列的燃烧管道。 每个管道周期性地接收电荷并排出电荷的燃烧产物。
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公开(公告)号：US20160194087A1
公开(公告)日：2016-07-07
申请号：US14211140
申请日：2014-03-14
发明人： Razi Mohamed Nalim
CPC分类号： F02C5/11 , F02C3/02 , F02C3/16 , F02C5/04 , Y02T50/671 , Y10S903/93
摘要： A hybrid propulsion system includes a wave rotor combustion engine operating in parallel with an electrical motor-generator element. The motor-generator element is coupled to the turbine shaft to selectively drive or be driven by the turbine shaft. In one mode of operation, the motor of the motor generator element is powered by a battery to provide rotational energy to the turbine shaft. In another mode of operation, the wave rotor combustion engine drives the generator to recharge the battery. The wave rotor combustion engine may be further directly coupled to auxiliary components without a gearbox to drive the components at substantially the same speed as the turbine shaft. The turbine rotor of the combustion engine includes a plurality of chambers defined by circumferentially spaced curved vanes that improves specific fuel consumption for the engine.
摘要翻译： 混合推进系统包括与电动发电机元件并行操作的波形转子内燃机。 电动发电机元件联接到涡轮轴以选择性地驱动或由涡轮机轴驱动。 在一种操作模式中，电动发电机元件的电动机由电池供电以向涡轮机轴提供旋转能量。 在另一种操作模式下，波轮转子内燃机驱动发电机给电池充电。 波轮转子内燃机可以进一步直接联接到辅助部件而不用齿轮箱，以与涡轮机轴基本相同的速度驱动部件。 内燃机的涡轮机转子包括由周向隔开的弯曲叶片限定的多个室，其改善发动机的特定燃料消耗。
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公开(公告)号：US09359973B2
公开(公告)日：2016-06-07
申请号：US13160840
申请日：2011-06-15
申请人： Soheil Farshchian , Alejandro Juan
发明人： Soheil Farshchian , Alejandro Juan
CPC分类号： F02K7/04 , F02C5/11 , F02K7/067 , F23C15/00 , F23C2900/03004
摘要： Disclosed herein is a valveless multitube pulse detonation engine including: a plurality of detonation tubes, wherein each detonation tube comprises an independent discharge outlet, and the plurality of detonation tubes interconnected at a common air/fuel mixture intake port. In the disclosed engine, an air and fuel mixture is detonated in the detonation tubes simultaneously, and the common air/fuel mixture intake port minimizes back-pressure caused by detonating the air/fuel mixture by directing multiple reverse shock waves into one another and effectively using the back-pressures as reacting surfaces for one another and effectively reducing the effect of back flowing shock waves moving towards upstream. The detonation tubes may be non-linear, and may have independent discharges. The independent discharges may be coupled to an adapter nozzle terminating in a combined exhaust outlet.
摘要翻译： 本文公开了一种无阀多管脉冲爆震发动机，其包括：多个爆管，其中每个爆管包括独立的排放口，并且所述多个引爆管在公共空气/燃料混合物进气口处相互连接。 在所公开的发动机中，空气和燃料混合物同时在引爆管中引爆，并且公共空气/燃料混合物进气口通过将多个反向冲击波相互引导并有效地使由空气/燃料混合物引爆引起的背压最小化 使用背压作为彼此的反应表面，并且有效地减少向上游移动的回流冲击波的影响。 引爆管可以是非线性的，并且可以具有独立的放电。 独立放电可以连接到终止于组合排气出口的适配器喷嘴。
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公开(公告)号：US20120144798A1
公开(公告)日：2012-06-14
申请号：US12964968
申请日：2010-12-10
IPC分类号： F02K7/02
摘要： A detonation chamber and a pulse detonation combustor including a detonation chamber, wherein the detonation chamber includes a plurality of aerodynamic jets disposed adjacent an exterior of a sidewall of the detonation chamber. The detonation chamber further includes a plurality of openings formed in the sidewall of the detonation chamber, wherein each of the plurality of openings is in fluidic communication with one of the plurality of aerodynamic jets. The plurality of aerodynamic jets are adapted to create a plurality of jet flows of a fluid within the detonation chamber during a combustion cycle defining a plurality of initiation obstacles within the detonation chamber to enhance a turbulence of a fluid flow and flame acceleration through the detonation chamber.
摘要翻译： 一个引爆室和一个包括爆震室的脉冲爆炸燃烧室，其中爆炸室包括邻近爆炸室侧壁外部设置的多个空气动力射流。 引爆室还包括形成在爆炸室的侧壁中的多个开口，其中多个开口中的每一个开口与多个空气动力学射流中的一个流体连通。 多个空气动力学射流适于在燃烧循环期间在引爆室内产生流体的多个喷射流，该循环在爆震室内限定多个起始障碍物，以增强流体流动的紊流和通过爆轰室的火焰加速 。
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公开(公告)号：US20060112672A1
公开(公告)日：2006-06-01
申请号：US11262930
申请日：2005-11-01
申请人： Anthony Razzell , Mark Taylor , Samuel Mason , Robert Miller
发明人： Anthony Razzell , Mark Taylor , Samuel Mason , Robert Miller
CPC分类号： F02C5/11
摘要： ABSTRACT A pressure rise combustor is provided with fuel provided at intermittent periods. The fuel is pulsed at timings such that the phase lag between the addition of the fuel and a resultant pressure rise is minimised. The fuel is pulsed such that the unsteady addition of heat reinforces the amplitude of an unsteady pressure fluctuation.
摘要翻译： 摘要提供了一种在间歇期间提供燃料的压力升高燃烧室。 燃料在定时被脉冲化，使得加入燃料和产生的压力上升之间的相位滞后最小化。 燃料被脉冲化，使得不稳定的加热增强了不稳定压力波动的振幅。
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公开(公告)号：US20040123582A1
公开(公告)日：2004-07-01
申请号：US10722158
申请日：2003-11-24
IPC分类号： F02C005/00
摘要： A pulsed combustion device includes a support structure and a combustor carousel supported by the support structure and rotating relative thereto about an axis. The carousel has a number of combustion conduits in a circumferential array. Each conduit cyclically receives a charge and discharges combustion products of the charge. A venturi effect may help control fuel/air charge leakage from a flowpath spanning the carousel and a stationary manifold.
摘要翻译： 脉冲燃烧装置包括支撑结构和由支撑结构支撑并相对于其围绕轴线旋转的燃烧器转盘。 圆盘传送带具有多个周向排列的燃烧管道。 每个管道周期性地接收电荷并排出电荷的燃烧产物。 文丘里效应可以帮助控制从圆盘传送带和固定歧管的流路中的燃料/空气电荷泄漏。
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公开(公告)号：US11867138B2
公开(公告)日：2024-01-09
申请号：US18050714
申请日：2022-10-28
发明人： Daanish Maqbool
CPC分类号： F02K7/20 , F02C5/00 , F02C5/02 , F02C5/10 , F02C5/11 , F02C7/04 , F23R7/00 , F05D2240/35 , F05D2250/324 , F05D2250/511 , F05D2260/85 , F05D2260/99
摘要： A system and method for ram air intake for pulse combustion systems is disclosed that improves the ability of pulse combustions to ingest air into the inlet pipe when the pulse combustion system is moving in a direction opposite the direction the open end of the inlet pipe is facing and the system and method includes the ability to increase the thrust output from the pulse combustion system.
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