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公开(公告)号：WO2018067253A1
公开(公告)日：2018-04-12
申请号：PCT/US2017/050012
申请日：2017-09-05
Applicant: STRASSER, James
Inventor： STRASSER, James
Abstract: A combustion management device for generating a thrust burst to impart a physical impulse. In operation, a combustion chamber, defined by a valve unit (33), is primed to a set pressure and fueled by fuel injectors (23). An ignitor (22) then initiates combustion. Under force of combustion, the valve unit is moved, pulling an exhaust valve (18) from an exhaust port (16), releasing combustion products as thrust. Work may be derived from the travel of the valve unit, independent of the thrust generated. After combustion, a return mechanism returns the valve unit to the start position, ready to repeat the process. Simple design, and valve operations needing little more than pressure differentials to function, make for simplified construction, and more modular applications.
Abstract translation: 用于产生推力脉冲以传递物理脉冲的燃烧管理装置。 在操作中，由阀单元（33）限定的燃烧室被灌注至设定压力并由燃料喷射器（23）供给燃料。 点火器（22）然后开始燃烧。 在燃烧的作用下，阀单元移动，从排气口（16）拉出排气阀（18），释放燃烧产物作为推力。 工作可能来源于阀门单元的行程，与产生的推力无关。 燃烧后，返回机构将阀门单元返回到起始位置，准备重复此过程。 简单的设计和阀门操作只需要比差压更多的功能，使结构更简单，模块化程度更高。
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公开(公告)号：WO2015143362A1
公开(公告)日：2015-09-24
申请号：PCT/US2015/021815
申请日：2015-03-20
Inventor： BRAUN, Eric, M. , LU, Frank, K.
CPC classification number: H02K7/1876 , F01N5/02 , F02B27/008 , F02C5/02 , F02C5/12 , F02C6/10 , F02G5/02 , F02K7/02 , F02K7/06 , F05D2220/76 , F05D2260/16 , F23C15/00 , F23R3/10 , F23R3/28 , F23R3/42 , F23R7/00 , Y02T10/146 , Y02T50/671
Abstract: In one embodiment, a power generation system includes a pulse detonation engine including a combustion chamber, a linear power generator including a working chamber, and a nozzle positioned between the combustion chamber and the working chamber that expands exhaust gas expelled from the combustion chamber, wherein the nozzle increases thermodynamic efficiency of the system.
Abstract translation: 在一个实施例中，发电系统包括：包括燃烧室的脉冲爆震引擎，包括工作室的线性发电机和位于燃烧室和工作室之间的喷嘴，其扩大从燃烧室排出的废气，其中 喷嘴提高了系统的热力学效率。
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3.发明申请BUCKYBALL SPHERE EXTRUDED FROM A CENTRAL POINT TO A BUCKYBALL FORMING PANELS FOR WIND POWER TURBINES AND A CLOSED BUCKYBALL SPHERE WITHIN A LARGER OPEN BUCKYBALL SPHERE FORMING A FLOATING AMPHIBIOUS WATER PROPULSION PADDLE WHEEL AND BUOYANT VACUUMED SPHERE WITH XENON ELECTRICAL CONTROL OF BUOYANCY 审中-公开BUCKYBALL球从一个中心点挤压成一个BUCKYBALL成型面板风力涡轮机和一个封闭的球形球在一个更大的开放BUCKYBALL球体形成一个浮动两侧水推进桨叶轮和浮力与氙气电气控制浮力减弱球体浮力
公开(公告)号：WO2009145808A2
公开(公告)日：2009-12-03
申请号：PCT/US2008/087295
申请日：2008-12-17
Applicant: ZORNES, David, A.
Inventor： ZORNES, David, A.
IPC: B64B1/58
CPC classification number: F02C5/02 , B63H5/02 , F01D1/00 , F01D1/34 , F02C3/165 , F03B17/00 , F05B2240/40 , F05B2250/132 , F05D2240/40 , F05D2250/132 , Y02E10/20 , Y02T50/672
Abstract: A planer hexagon curve extruded to a center point providing six isosceles triangle panels with the shortest edge being one of the six planer hexagon curves forms a buckyball hexagon extrusion that naturally provide pentagon extrusions. A buckyball hexagon extrusion is one of twenty that array at equidistant angles around twelve pentagons at equidistant angles in groups into an open cell buckyball sphere. A closed cell buckyball within a larger open cell buckyball sphere share a common center point and other extrusion angles that have utility for: a water paddle wheel for propulsion that floats, a tire, a wind turbine, and an air turbine.
Abstract translation: 一个平面六角曲线挤压到一个中心点上，提供六个等腰三角形面板，其最短边缘是六个平面六角曲面中的一个，形成一个自然形成五边形挤压的巴基球六角挤压。 Buckyball六边形挤出是以十二个五边形以相等的角度以等距的角度以等距的角度排列成开放式细胞巴基球的二十个之一。 在一个更大的开放式巴基球中的闭孔巴基球拥有一个共同的中心点和其他挤压角，可用于以下用途：用于浮动推进的水桨叶轮，轮胎，风力涡轮机和空气涡轮机。
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公开(公告)号：WO01006102A1
公开(公告)日：2001-01-25
申请号：PCT/US1999/016305
申请日：1999-07-19
Abstract: An efficiency enhanced turbine engine and method for a turbine engine having a rotor (25) and a fluid flow path (31) that extends through compression (63), combustion (65), and expansion (67) or turbine stages with fluid flowing through the fluid flow path driving the rotor. The turbine engine has one or more stator-rotor-stator (24-25-24) assemblies, and uses a flat rotor disk with turbine blades (57/58). Capturing of fluid during combustion enables elevation of the temperature and pressure while maintaining the fluid at near constant volume during combustion. Fluid is caused to reenter the rotor a plurality of times to provide cyclic exposure of the moving parts of the turbine engine to different portions of the engine cycle for reducing the average temperature of the moving parts and thereby allow higher compression ratios and combustion temperatures.
Abstract translation: 一种用于涡轮发动机的效率提高的涡轮发动机和方法，其具有通过流体流过的压缩（63），燃烧（65）和膨胀（67）或涡轮级延伸的转子（25）和流体流动路径（31） 流体流动路径驱动转子。 涡轮发动机具有一个或多个定子转子 - 定子（24-25-24）组件，并且使用具有涡轮叶片的平转子盘（57/58）。 在燃烧期间捕获流体可以提高温度和压力，同时在燃烧过程中将流体保持在接近恒定的体积。 导致流体重新进入转子多次，以提供涡轮发动机的运动部分对发动机循环的不同部分的循环曝光，以减少运动部件的平均温度，从而允许更高的压缩比和燃烧温度。
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5.发明申请
公开(公告)号：WO2017106689A1
公开(公告)日：2017-06-22
申请号：PCT/US2016/067242
申请日：2016-12-16
Applicant: NORTH AMERICAN WAVE ENGINE CORPORATION
Inventor： MAQBOOL, Daanish
Abstract: A pulse combustor system for efficiently operating a pulse combustor. The pulse combustor system includes the pulse combustor and a duct. The pulse combustor has a combustion chamber defining an internal space, a conduit having a first end in fluid communication with the internal space and a second end in fluid communication with an environment outside of the pulse combustor system, and a fuel injector configured to inject fuel into the internal space of the combustion chamber. The duct has two openings, with one opening disposed adjacent to the second end of the conduit. The pulse combustor system has an average operating frequency, and the duct has a length that is about one quarter of a wavelength corresponding to the average operating frequency. The pulse combustor and the duct each has a central longitudinal axis, and the two axes are substantially aligned.
Abstract translation: 用于有效地操作脉冲燃烧器的脉冲燃烧器系统。 脉冲燃烧器系统包括脉冲燃烧器和管道。 脉冲燃烧器具有限定内部空间的燃烧室，具有与内部空间流体连通的第一端和与脉冲燃烧器系统外部的环境流体连通的第二端的导管，以及构造成将燃料 进入燃烧室的内部空间。 导管具有两个开口，其中一个开口设置在导管的第二端附近。 脉冲燃烧器系统具有平均工作频率，并且管道的长度约为对应于平均工作频率的波长的四分之一。 脉冲燃烧器和管道各自具有中心纵轴，并且两个轴基本对齐。
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Patent Agency Ranking6.发明申请SYSTÈME DE COMBUSTION À VOLUME CONSTANT POUR TURBOMACHINE DE MOTEUR D'AÉRONEF 审中-公开用于飞机发动机涡轮发动机的恒定体积燃烧系统
公开(公告)号：WO2016132055A1
公开(公告)日：2016-08-25
申请号：PCT/FR2016/050337
申请日：2016-02-15
Applicant: TURBOMECA
Abstract: L'invention concerne un système de combustion à volume constant (3) pour turbomachine, ce système comprenant : - plusieurs chambres de combustion (11-14) régulièrement réparties autour d'un axe longitudinal (AX); - un collecteur (7) torique comprenant une sortie orientée radialement pour alimenter chaque chambre de combustion en air compressé provenant d'un compresseur; - un conduit d'échappement (4 ) torique comprenant une entrée orientée radialement pour collecter les gaz de combustion issus des chambres de combustion (11-14), les chambres de combustion (11-14) étant interposées radialement entre la sortie du collecteur (7) et l'entrée du conduit d'échappement (4); - des moyens de cadencement pour chaque chambre (11-14) de l'admission d'air compressé issu de la sortie du collecteur (7) et de l'éjection de gaz de combustion vers le conduit d'échappement (4).
Abstract translation: 本发明涉及一种用于涡轮发动机的恒定体积燃烧系统（3）。 所述系统包括： - 围绕纵向轴线（AX）规则分布的多个燃烧室（11-14）; - 环形歧管（7），其包括用于从压缩机向每个燃烧室供应压缩空气的径向定向的出口; - 环形排气管（4），其包括用于收集来自燃烧室（11-14）的燃烧气体的径向取向的入口，所述燃烧室（11-14）径向地位于歧管（7）的出口和 排气管（4）的入口; 以及 - 用于从歧管（7）的出口抽吸压缩空气并将燃烧气体朝向排气管（4）喷射的每个室（11-14）的定时装置。
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7.发明申请BUCKYBALL SPHERE EXTRUDED FROM A CENTRAL POINT TO A BUCKYBALL FORMING PANELS FOR WIND POWER TURBINES AND A CLOSED BUCKYBALL SPHERE WITHIN A LARGER OPEN BUCKYBALL SPHERE FORMING A FLOATING AMPHIBIOUS WATER PROPULSION PADDLE WHEEL AND BUOYANT VACUUMED 审中-公开从中央点到BUCKYBALL的BUCKYBALL SPHERE到用于风力涡轮机的BUCKYBALL成型面板和在大型开放式BUCKYBALL球形体中的封闭的BUCKYBALL球体形成浮动的大型水推进器PADDLE WHEEL和BUOYANT VACUUMED
公开(公告)号：WO2009076681A2
公开(公告)日：2009-06-18
申请号：PCT/US2008086900
申请日：2008-12-15
Applicant: ZORNES DAVID A
Inventor： ZORNES DAVID A
IPC: B64B1/06
CPC classification number: F02C5/02 , B63H5/02 , F01D1/00 , F01D1/34 , F02C3/165 , F03B17/00 , F05B2240/40 , F05B2250/132 , F05D2240/40 , F05D2250/132 , Y02E10/20 , Y02T50/672
Abstract: A planer hexagon curve extruded to a center point providing six isosceles triangle panels with the shortest edge being one of the six planer hexagon curves forms a buckyball hexagon extrusion that naturally provide pentagon extrusions. A buckyball hexagon extrusion is one of twenty that array at equidistant angles around twelve pentagons at equidistant angles in groups into an open cell buckyball sphere. A closed cell buckyball within a larger open cell buckyball sphere share a common center point and other extrusion angles that have utility for: a water paddle wheel for propulsion that floats, a tire, a wind turbine, and an air turbine.
Abstract translation: 平面六边形曲线被挤压到中心点，提供六个等腰三角形面板，最短边缘是六个平面六边形曲线之一，形成一个自然提供五边形挤压的巴基球六边形挤压。 巴克球六边形挤出是二十个阵列之一，以等距离的角度围绕十二个五角形以等距离的角度组成一个开放细胞巴基球。 更大的开放式巴格球球内的闭孔巴氏球共享共同的中心点和其他挤压角度，其具有以下功能：用于浮动的推进器的水盘轮，轮胎，风力涡轮机和空气涡轮机。
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公开(公告)号：WO2008029432A3
公开(公告)日：2008-05-22
申请号：PCT/IT2007000611
申请日：2007-09-04
Applicant: SAPONARA FRANCO
Inventor： SAPONARA FRANCO
CPC classification number: F01D1/026 , F02C5/02 , F05D2240/40 , F05D2250/70 , F05D2250/71
Abstract: Two identical impact turbines with intermittent combustion are arranged in parallel in a common.housing. Air is compressed by intake fans due to centrifugal compression, fuel is injected and ignition is assured with spark plugs. Exhausted working fluid leaves the apparatus via a common outlet. The two turbine wheels are interconnected via giears and have a single power output shaft.
Abstract translation: 具有间歇燃烧的两台相同的冲击涡轮平行布置在共同的位置。 由于离心压缩，空气被进气风扇压缩，燃油喷射，并通过火花塞确保着火。 耗尽的工作流体通过公共出口离开设备。 两个涡轮机轮通过千兆互连，并具有单个动力输出轴。
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公开(公告)号：WO2008029432A2
公开(公告)日：2008-03-13
申请号：PCT/IT2007/000611
申请日：2007-09-04
Applicant: SAPONARA, Franco
Inventor： SAPONARA, Franco
CPC classification number: F01D1/026 , F02C5/02 , F05D2240/40 , F05D2250/70 , F05D2250/71
Abstract: The turbines and the single one play an active role during the pressure, the bursting and exhausting process; they have closed sides which are fixed together into the head. The wings are joint together and they close the space between the tube and the turbines. Pressure is obtained through the centrifuge-force and the intaking propellers which are assembled on the sides of the turbines. Either the two tubes or the single one are in the centre of the turbines whereas the single turbine has a 90° angle tube referring to the turbine and between the tube and the turbine there is a centesimal space. Among all the parts which are fixed together there is no friction.
Abstract translation: 涡轮机和单机在压力，爆破和排气过程中发挥积极作用; 它们具有固定在一起的封闭侧面。 翅膀联合在一起，并且它们封闭管和涡轮机之间的空间。 压力是通过离心力和吸入螺旋桨获得的，这些螺旋桨组装在涡轮机的两侧。 两个管或单个管都是在涡轮机的中心，而单个涡轮机具有指向涡轮机的90°角管，并且在管和涡轮机之间具有中心空间。 固定在一起的所有零件中都没有摩擦。
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公开(公告)号：WO1988010363A1
公开(公告)日：1988-12-29
申请号：PCT/DK1988000094
申请日：1988-06-15
Applicant: MIKKELSEN, Bent
IPC: F02C05/04
Abstract: The invention relates to an internal combustion engine which combines the processes of a 4-stroke- and turbine-engine. The combustion engine includes a turbine (1), a housing (2) and a ringshaped piston (3) relatively movable in a ringshaped combustion chamber which is surrounding the turbine blades (1a). A mechanical coupling for synchronizing the reciprocating motion of the piston with the rotary motion of the turbine is located between the turbine and the piston. The engine preferably fulfills the 4-stroke cycle in one revolution. The combustion engine is also characterized in that it is simple, sturdy and has favourable low speed rotation characteristics. The engine has a clean combustion fulfilling severe environmental requirements without the use of a catalyst.
Abstract translation: 本发明涉及一种组合四冲程和涡轮发动机的过程的内燃机。 内燃机包括涡轮机（1），壳体（2）和环形活塞（3），其环绕涡轮机叶片（1a）的环形燃烧室中相对可移动。 用于使活塞的往复运动与涡轮机的旋转运动同步的机械联接器位于涡轮机和活塞之间。 发动机优选在一圈内实现四冲程循环。 内燃机的特征还在于其简单，坚固，具有良好的低速旋转特性。 发动机具有清洁的燃烧，在不使用催化剂的情况下实现严格的环境要求。
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