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    • 4. 发明授权
    • Rotary pulse detonation engine
    • 旋转脉冲爆震引擎
    • US06725646B2
    • 2004-04-27
    • US10119987
    • 2002-04-10
    • James J. CallasScott B. Fiveland
    • James J. CallasScott B. Fiveland
    • F02K700
    • F02C5/04F02B33/36F02B53/00Y02T50/671
    • A reciprocating internal combustion engine used a crankshaft to develop rotating motion. A rotary pulse detonation engine can be adapted to rotate a shaft. A combustor portion of the rotary pulse detonation engine is spaced from an axis of the shaft a preestablished distance therebetween in a mass member. An intake portion and an exhaust portion of the combustor portion is positioned in a parameter of the mass member. A combustion portion of the combustor portion is interposed the intake portion and the exhaust portion. The combustion portion has a frustoconical first position which converges to form a deflagration wave and progresses into a detonation. The deflagration to detonation transition occurs in the transition region. A combustible fuel and air mixture is combusted in the combustor portion creating a high speed jet exiting the exhaust portion and rotating the shaft.
    • 往复式内燃机使用曲轴来产生旋转运动。 旋转脉冲爆震发动机可以适于旋转轴。 旋转脉冲爆震发动机的燃烧器部分与轴的轴线在质量构件中与其之间的预先设定的距离间隔开。 燃烧器部分的进气部分和排气部分位于质量部件的参数中。 燃烧器部分的燃烧部分插入进气部分和排气部分。 燃烧部分具有会聚在一起的截头圆锥形的第一位置,以形成爆燃波并进入爆轰状态。 爆燃转变发生在过渡地区。 可燃燃料和空气混合物在燃烧器部分中燃烧,产生离开排气部分的高速喷射并旋转轴。
    • 6. 发明申请
    • Alternating Split Cycle Combustion Engine and Method
    • 交替分流循环燃烧发动机和方法
    • US20130298888A1
    • 2013-11-14
    • US13466617
    • 2012-05-08
    • Scott B. Fiveland
    • Scott B. Fiveland
    • F02B41/06F02B33/22
    • F02B33/22F01N13/107F02M26/05
    • An internal combustion engine includes a cylinder that is connectable to an intake manifold through an intake valve, to an exhaust manifold through an exhaust valve, and to a transfer manifold through transfer and combustion valves. A fuel injector associated with the cylinder is adapted to provide fuel to the cylinder. During operation, the cylinder performs an intake stroke, followed by a compression stroke. A compressed charge from the cylinder passes to and is collected in the transfer manifold through the transfer valve. The cylinder is filled by a compressed charge from the transfer manifold through the combustion valve at the same time as the fuel injector provides fuel. The cylinder then undergoes combustion and exhaust strokes. In this way, cylinder operation alternates between combustor and compressor split combustion modes.
    • 内燃机包括通过进气门连接到进气歧管的气缸,通过排气阀连接到排气歧管,以及通过转移和燃烧阀连接到传送歧管。 与气缸相关联的燃料喷射器适于向气缸提供燃料。 在操作期间,气缸执行进气冲程,然后进行压缩冲程。 来自气缸的压缩气流通过转移阀传递到传送歧管中并被收集在传送歧管中。 在燃料喷射器提供燃料的同时,气缸由来自转移歧管的压缩的燃料通过燃烧阀填充。 然后气缸经历燃烧和排气冲程。 以这种方式,气缸操作在燃烧器和压缩机分解燃烧模式之间交替。
    • 7. 发明申请
    • Engine Control System Implementing Lean Burn 6-Stroke Cycle
    • 发动机控制系统实施精益燃烧6冲程循环
    • US20120166066A1
    • 2012-06-28
    • US13263302
    • 2009-12-17
    • Scott B. FivelandWilliam H. Lane
    • Scott B. FivelandWilliam H. Lane
    • F02D41/26
    • F02D41/3017F02B1/12F02B3/06F02B75/021F02D41/3035F02D41/3058F02D41/402F02D2041/3052Y02T10/128Y02T10/44
    • A control system (12) for an engine (10) having a combustion chamber (22) is disclosed. The control system may have a fuel injector (40) configured to selectively inject fuel into the combustion chamber, and a controller (54) in communication with the fuel injector. The controller may be configured to activate the fuel injector during a first compression stroke to initiate fuel injection in an amount and at a timing that results in a stratified lean air/fuel mixture within the combustion chamber during a first combustion event of a six- stroke cycle. The controller may also be configured to activate the fuel injector during a first power stroke to initiate fuel injection in an amount and at a timing that results in a homogenous lean air/fuel mixture within the combustion chamber during a second combustion event of the same six-stroke cycle.
    • 公开了一种用于具有燃烧室(22)的发动机(10)的控制系统(12)。 控制系统可以具有被配置为选择性地将燃料喷射到燃烧室中的燃料喷射器(40)以及与燃料喷射器连通的控制器(54)。 控制器可以被配置为在第一压缩冲程期间激活燃料喷射器以在六冲程的第一燃烧事件期间导致在燃烧室内产生分层的贫空气/燃料混合物的量和时间点开始燃料喷射 周期。 控制器还可以被配置成在第一次功率冲程期间激活燃料喷射器以在相同六次的第二次燃烧事件期间导致在燃烧室内产生均匀的稀薄空气/燃料混合物的量和时间的燃料喷射 中风循环。
    • 9. 发明授权
    • Engine control system having pressure-based timing
    • 发动机控制系统具有基于压力的定时
    • US08028679B2
    • 2011-10-04
    • US12292832
    • 2008-11-26
    • Martin L. WilliScott B. FivelandDavid T. MontgomeryWeidong Gong
    • Martin L. WilliScott B. FivelandDavid T. MontgomeryWeidong Gong
    • F02M1/00
    • F01L1/34F01L1/181F01L1/262F01L13/0015
    • A control system for an engine having a first cylinder and a second cylinder is disclosed having a first engine valve movable to regulate a fluid flow of the first cylinder and a first actuator associated with the first engine valve. The control system also has a second engine valve movable to regulate a fluid flow of the second cylinder and a sensor configured to generate a signal indicative of a pressure within the first cylinder. The control system also has a controller that is in communication with the first actuator and the sensor. The controller is configured to compare the pressure within the first cylinder with a desired pressure and selectively regulate the first actuator to adjust a timing of the first engine valve independently of the timing of the second engine valve based on the comparison.
    • 公开了具有第一气缸和第二气缸的用于发动机的控制系统,其具有可调节第一气缸的流体流动的第一发动机气门和与第一发动机气门相关联的第一致动器。 控制系统还具有可移动以调节第二气缸的流体流动的第二发动机气门和被配置为产生指示第一气缸内的压力的信号的传感器。 控制系统还具有与第一致动器和传感器通信的控制器。 控制器被配置为将第一气缸内的压力与期望的压力进行比较,并且基于该比较,选择性地调节第一致动器以独立于第二发动机气门的定时来调节第一发动机气门的定时。