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1. 发明申请

US20040163376A1 Engine having external combustion chamber 有权
公开(公告)号：US20040163376A1
公开(公告)日：2004-08-26
申请号：US10791698
申请日：2004-03-04
发明人： James J. Mehail
IPC分类号： F02C005/00
CPC分类号： F02G3/02
摘要： Provided is an engine having positive displacement chambers containing pistons and an external combustion chamber which utilizes the compression energy in compressed natural gas from a high pressure main line and compressed air in combination with the energy released during combustion of the fuel to drive the pistons. Energy expended compressing the natural gas and air are recovered. Also provided is an electrical generator driven by the engine.

2. 发明申请

US20040083729A1 POWER STROKE ENGINE 失效
标题翻译：动力发动机
公开(公告)号：US20040083729A1
公开(公告)日：2004-05-06
申请号：US10374327
申请日：2003-02-27
发明人： George A. Teacherson
IPC分类号： F02G001/00 , F02G003/00 , F02C005/00 , F02G001/04 , F01B029/10
CPC分类号： F02G1/043
摘要： An engine has a piston with plural end faces that compresses combustible mixtures on both sides of the piston and in each end of a closed cylinder containing the piston. The cylinders are fully enclosed with provision for a power takeoff rod to pass therethrough. Each instant closed cylinder with the dual end faced piston can produce power with each and every single stroke of its reciprocating travel. Multiple power generating methods are disclosed, as is a Hybrid type engine utilizing at least two of the multiple methods in a plurality of cylinders.
摘要翻译：发动机具有多个端面的活塞，该活塞在活塞的两侧和包含活塞的封闭圆筒的每一端压缩可燃混合物。气缸完全封闭，用于使动力输出杆通过。每个具有双端面活塞的即时闭合气缸可以在其往复运动的每一个行程中产生动力。公开了多种发电方法，以及利用多个气缸中的多种方法中的至少两种的混合型发动机。

3. 发明申请

US20020162316A1 Fluidic-piston engine 失效
标题翻译：流体活塞发动机
公开(公告)号：US20020162316A1
公开(公告)日：2002-11-07
申请号：US09847141
申请日：2001-05-02
发明人： Ricardo Conde , Dara Faroughy
IPC分类号： F02G001/00 , F02G003/00 , F02C005/00
CPC分类号： F02G1/044 , F01B21/02 , F02G2244/50 , F02G2270/70
摘要： An external combustion engine comprises a mass of compressible working fluid; a fluidic piston in fluid communication with said working fluid; and a second piston in hydraulic communication with said fluidic piston and in fluid communication with said working fluid.
摘要翻译：外燃机包括一批可压缩的工作流体; 与所述工作流体流体连通的流体活塞; 以及与所述流体活塞液压连通并与所述工作流体流体连通的第二活塞。

4. 发明申请

US20020112464A1 Engine having external combustion chamber 有权
公开(公告)号：US20020112464A1
公开(公告)日：2002-08-22
申请号：US10119041
申请日：2002-04-10
发明人： James J. Mehail
IPC分类号： F02G001/00 , F02G003/00 , F02C005/00 , F02C003/00
CPC分类号： F02G3/02
摘要： Provided is an engine having positive displacement chambers containing pistons and an external combustion chamber which utilizes the energy stored in compressed fuel and compressed air in combination with the energy released during combustion of the fuel to drive the pistons. Energy expended compressing the fuel and air are recovered.

5. 发明申请

US20040216464A1 PULSE COMBUSTION DEVICE 有权
标题翻译：脉冲燃烧装置
公开(公告)号：US20040216464A1
公开(公告)日：2004-11-04
申请号：US10426741
申请日：2003-04-30
发明人： Kirk R. Lupkes
IPC分类号： F02C005/00
CPC分类号： F02K7/06 , F02C5/00 , F02K7/075 , F23C15/00 , F23R7/00
摘要： A pulse combustion device has a number of combustors with upstream bodies and downstream nozzles. Coupling conduits provide communication between the combustors. For each given combustor this includes a first communication between a first location upstream of the nozzle thereof and a first location along the nozzle of another. There is second communication between a second location upstream of the nozzle and a second communication between a second location upstream of the nozzle of a second other combustor and a second nozzle location along the nozzle of the given combustor.

6. 发明申请

US20040172950A1 Pulse detonation system for a gas turbine engine 失效
标题翻译：燃气轮机的脉冲爆震系统
公开(公告)号：US20040172950A1
公开(公告)日：2004-09-09
申请号：US10383027
申请日：2003-03-06
发明人： Kattalaicheri Srinivasan Venkataramani , Lawrence Butler , William Andrew Bailey
IPC分类号： F02C005/00
CPC分类号： F02C3/165 , F02K3/06 , F02K7/02 , Y02T50/671
摘要： A pulse detonation system for a gas turbine engine having a longitudinal centerline axis extending therethrough, the pulse detonation system includes an air inlet duct in flow communication with a source of compressed air, the air inlet duct including at least one port formed therein for permitting compressed air to flow therethrough, a fuel injector mounted to the air inlet duct in circumferentially spaced relation to each port, and a device mounted to the air inlet duct in circumferentially spaced relation to each fuel injector for initiating a detonation wave. A rotatable ring member is also positioned in coaxial relation around a portion of the air inlet duct, with the ring member including at least one stage of detonation disposed therein. Accordingly, a detonation wave is produced in each detonation stage and combustion gases following each detonation wave create a torque which causes the ring member to rotate. Each detonation stage in the ring member further includes a plurality of circumferentially spaced detonation ducts extending tangentially from an inner surface of the ring member, wherein the detonation ducts are aligned with each port, the fuel injector and the initiation device in a predetermined timing and sequence so that detonation waves are produced therein.
摘要翻译：一种用于燃气涡轮发动机的脉冲爆炸系统，其具有延伸穿过其中的纵向中心线轴线，所述脉冲爆震系统包括与压缩空气源流动连通的空气入口管道，所述进气管道包括形成在其中的至少一个端口，用于允许压缩空气流过其中，安装到空气入口管道的燃料喷射器与每个端口沿周向间隔开的关系;以及装置，其与每个燃料喷射器周向间隔开地安装到空气入口管道，用于启动爆震波。旋转环构件也围绕空气入口管道的一部分以同轴的关系定位，环构件包括设置在其中的至少一个爆震级。因此，在每个爆震阶段产生爆震波，并且在每个爆震波之后的燃烧气体产生使得环件旋转的扭矩。环形构件中的每个爆震阶段还包括多个周向间隔开的从环形构件的内表面切向延伸的爆震导管，其中爆震导管以预定的时间和顺序与每个端口，燃料喷射器和启动装置对准使其中产生爆震波。

7. 发明申请

US20040025489A1 Fluidic-piston engine 审中-公开
标题翻译：流体活塞发动机
公开(公告)号：US20040025489A1
公开(公告)日：2004-02-12
申请号：US10420640
申请日：2003-04-22
发明人： Ricardo Conde , Dara Faroughy
IPC分类号： F02C005/00
CPC分类号： F02G1/044 , F01B21/02 , F02G2244/50 , F02G2270/70
摘要： An external combustion engine includes: a plurality of cavities; a compressible working fluid in fluid communication between each pair of adjacent cavities; and a plurality of hydraulic linkages in reciprocal phase communication between each pair of alternate cavities. In an alternative embodiment the external combustion engine includes: a plurality of cavities; a compressible working fluid in fluid communication between each pair of adjacent cavities; and a plurality of articulated mechanical linkages in reciprocal phase communication between each pair of alternate cavities. In another alternative embodiment the external combustion engine includes: at least four upright cavities disposed substantially equidistant from a central upright axis; a compressible working fluid in fluid communication between each pair of adjacent cavities; and at least one linkage in reciprocal phase communication between each pair of alternate cavities. The at least one linkage may comprise a hydraulic linkage. Alternatively, the at least one linkage may comprise an articulated mechanical linkage.
摘要翻译：一种外燃机包括：多个空腔; 在每对相邻空腔之间流体连通的可压缩工作流体; 以及多个液压联动装置，其在每对交替空腔之间相互连通。在替代实施例中，外燃机包括：多个空腔; 在每对相邻空腔之间流体连通的可压缩工作流体; 以及多个铰接的机械连接件，其在每对交替空腔之间相互连通。在另一替代实施例中，外燃机包括：至少四个直立腔，其基本上等距离设置在中心直立轴线上; 在每对相邻腔之间流体连通的可压缩工作流体; 以及每对交替空腔之间的往复相通中的至少一个连杆。所述至少一个连杆机构可以包括液压联动装置。或者，所述至少一个连杆机构可以包括铰接的机械连接件。

8. 发明申请

US20030182927A1 Shock wave reflector and detonation chamber 失效
标题翻译：冲击波反射器和爆轰室
公开(公告)号：US20030182927A1
公开(公告)日：2003-10-02
申请号：US10107653
申请日：2002-03-27
申请人： General Electric Company
发明人： Ivett Alejandra Leyva
IPC分类号： F02C005/00
CPC分类号： F23R7/00 , F02K7/02 , F02K7/04
摘要： A shock wave reflector includes a number of reflective units positioned along a longitudinal direction and separated by a gap G. Each reflective unit has a length L. The length L and the gap G are governed by a relationship LnullGnullnull. The variable null characterizes a cell size for a detonation mixture. A detonation chamber includes a receiving end, a discharge end, and a wall extending along a longitudinal direction between the receiving and discharge ends. The detonation chamber further includes a number of reflective units formed in the wall and positioned along the longitudinal direction. The reflective units are separated by a gap G, and each reflective unit has a length L.
摘要翻译：冲击波反射器包括沿着纵向方向定位并由间隙G分开的多个反射单元。每个反射单元具有长度L.长度L和间隙G由关系L + G> =兰德控制。变量lambd表征爆轰混合物的单元尺寸。爆震室包括接收端，放电端和沿着纵向方向在接收端和放电端之间延伸的壁。引爆室还包括形成在壁中并沿纵向方向定位的多个反射单元。反射单元被间隙G隔开，并且每个反射单元具有长度L.

9. 发明申请

US20020134069A1 Combustion chamber system 审中-公开
公开(公告)号：US20020134069A1
公开(公告)日：2002-09-26
申请号：US09813058
申请日：2001-03-20
发明人： Joseph S. Adams
IPC分类号： F02G001/00 , F02G003/00 , F02C005/00
CPC分类号： B25C1/08
摘要： A combustion chamber system having a pre-combustion chamber in communication with a final combustion chamber, where the length of said pre-combustion chamber is substantially greater than its width. The pre-combustion chamber can be curved along all or part of its length, and such curved chamber parts can be nested.

10. 发明申请

US20040194469A1 Pulse detonation system for a gas turbine engine 失效
标题翻译：燃气轮机的脉冲爆震系统
公开(公告)号：US20040194469A1
公开(公告)日：2004-10-07
申请号：US10405561
申请日：2003-04-02
发明人： Lawrence Butler , Kattalaicheri Srinivasan Venkataramani , Kurt David Murrow , Ivett Alejandra Leyva
IPC分类号： F02C005/00
CPC分类号： F23R7/00 , F02C3/165 , F02C5/04 , F02K3/06 , F02K7/005
摘要： A pulse detonation system for a gas turbine engine having a longitudinal centerline axis extending therethrough includes a rotatable cylindrical member having a forward surface, an aft surface, and an outer circumferential surface, where at least one stage of circumferentially spaced detonation chambers is disposed therein. The pulse detonation system further includes a shaft rotatably connected to the cylindrical member and a stator configured in spaced arrangement around the forward surface, the aft surface, and the outer circumferential surface of the cylindrical member and a portion of the shaft. The stator has at least one group of ports formed therein which sequentially align with the detonation chambers as the cylindrical member rotates. In this way, detonation cycles are performed in the detonation chambers of each detonation stage so that reaction forces induced by the detonation cycles create a torque which causes the cylindrical member to rotate. Each detonation chamber includes a first open end located adjacent the outer circumferential surface of the cylindrical member and a second closed end located within a middle portion of the cylindrical member.
摘要翻译：用于具有延伸穿过其中的纵向中心线轴的燃气涡轮发动机的脉冲爆震系统包括具有前表面，后表面和外周表面的可旋转圆柱形构件，其中在其中设置至少一个周向间隔开的爆震腔室。脉冲爆震系统还包括可旋转地连接到圆柱形构件的轴和定子，其围绕圆筒构件的前表面，后表面和外圆周表面以及轴的一部分间隔开地布置。定子具有形成在其中的至少一组端口，随着圆柱形构件的旋转，它们与引爆室顺序对准。以这种方式，在每个爆震阶段的引爆室中进行爆震循环，使得由引爆循环引起的反作用力产生使圆柱形构件旋转的扭矩。每个爆震室包括位于圆柱形构件的外周表面附近的第一开口端和位于圆柱形构件的中间部分内的第二封闭端。

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