公开(公告)号：US4337685A

公开(公告)日：1982-07-06

申请号：US677236

申请日：1976-04-12

申请人： German Munding ,  Wolfgang Muller ,  Heinrich Strobl

发明人： German Munding ,  Wolfgang Muller ,  Heinrich Strobl

IPC分类号： F41A1/04 ,  F41F1/04

CPC分类号： F41A1/04

摘要： In an apparatus for generating a propellant gas, such as is used in propeng projectiles, at least one rotation chamber acts as a propellant gas generator containing a ring-shaped flow of propellant. A closed circuit is connected to the chamber for circulating a liquid propellant to it. Either monergolic or hypergolic propellants can be used with the rotation chamber being formed of at least two sub-chambers when hypergolic propellants are used. The two sub-chambers are connected by an overflow weir. The closed circuit which is provided for each of the chambers involved in the generation of the propellant gas, includes a valve for regulating the quantity of propellant disposed in a ring-shaped flow within the chamber. The valve regulates the amount of propellant required for the gas-generating operation. Further, the closed circuit includes an arrangement for sealing flow into and out of the rotation chamber or chambers during the generation of the propellant gas so that a rapid pressure buildup can be attained.

摘要翻译： 在用于产生推进剂气体的装置中，例如用于推进射弹的装置中，至少一个旋转室用作包含推进剂的环形流的推进剂气体发生器。 闭合回路连接到腔室，用于将液体推进剂循环到其上。 当使用全参数推进剂时，可以使用单一或高压推进剂，其中旋转室由至少两个子室形成。 两个子室通过溢流堰连接。 为涉及产生推进剂气体的每个室提供的闭路包括用于调节设置在室内的环形流中的推进剂的量的阀。 阀调节气体产生操作所需的推进剂量。 此外，封闭回路包括用于在产生推进剂气体期间密封流入和流出旋转室或室的装置，从而可以获得快速的压力积聚。

公开(公告)号：US4099445A

公开(公告)日：1978-07-11

申请号：US862637

申请日：1969-09-22

申请人： Dietrich Singelmann ,  Heinrich Strobl ,  German Munding

发明人： Dietrich Singelmann ,  Heinrich Strobl ,  German Munding

IPC分类号： F41A1/04 ,  F41F1/04

CPC分类号： F41A1/04

摘要： A propelling or driving force generating system for propelling a device such as projectile in a fire arm comprises a combustion chamber cylinder formed at the end of a barrel containing a bore for the passage of a projectile and in which is movable in pressure differential piston. The piston includes an annular ring portion having surfaces on respectively axially opposite ends which are exposed to pressure forces existing in intermediate chambers defined between these surfaces and end walls of the surrounding cylinder in widened annular portions of the cylinder. The cylinder and piston are provided with one or more passages for the passage of a propellant component into the combustion chamber. The various propellant components which are preferably of a nature such that they will react hypergolically, are connected through valve means in these passages and by a central plunger element of said valve means into the combustion chamber. Reaction of the components generates combustion gases in the combustion chamber to force the piston backwardly in a working stroke and to produce a force for expelling the projectile through the bore at the opposite end of the combustion chamber. The construction is characterized by an arrangement which provides an additional moving force on the piston in order to aid its working stroke movement at the initial stage of such movement.

摘要翻译： 用于推进诸如在火臂中的射弹的装置的推进或驱动力产生系统包括形成在桶的端部处的包含用于射弹通过的孔并且在压差活塞中可移动的燃烧室。 活塞包括环形环部分，其具有在分别轴向相对端部上的表面，其暴露于限定在这些表面之间的中间室中的压力和围绕气缸的加宽的环形部分中的周围气缸的端壁。 气缸和活塞设置有一个或多个通道，用于将推进剂部件通入燃烧室。 各种推进剂组分优选地具有这样的性能，使得它们能够通过这些通道中的阀装置和所述阀装置的中心柱塞元件连接到燃烧室中。 这些组件的反应在燃烧室中产生燃烧气体，以在工作行程中向后推动活塞，并产生用于通过在燃烧室的相对端处的孔排出射弹的力。 该结构的特征在于在活塞上提供额外的移动力的装置，以便在这种移动的初始阶段帮助其工作冲程运动。

公开(公告)号：US5661970A

公开(公告)日：1997-09-02

申请号：US431140

申请日：1995-04-28

申请人： Wolfgang Muller ,  German Munding

发明人： Wolfgang Muller ,  German Munding

IPC分类号： F02K9/38 ,  F02K9/42 ,  F02K9/50 ,  F02K9/56 ,  F02K9/94 ,  F42B10/66 ,  F42B15/00

CPC分类号： F42B10/663

摘要： Thrust-generating device with rocket engines arranged in pairs opposite each other for multiple ignition as well as individual and group activation and with an amount of fuel sufficient for the duration of the mission. The thrust-generating device is designed as a closed, storable, modular unit. The rocket engines are operated with liquid fuel and liquid oxidizing agent. At least one tank is provided for each fuel component. The tanks are in the filled, pressureless state before the activation of the thrust-generating device. The rocket engines and a fuel distributor of block design are integrated within a central bulkhead. The thrust-generating device is surrounded by a sealed outer jacket and is divided by the bulkhead into two separate chambers. The outer jacket is lined on the inside with a "self-sealing" film. The oxidizing agent is stored in one chamber, and the fuel in the other chamber. The empty spaces in the chambers contain an adsorbent filling. A temperature-controlled safety device brings about a pulse-free blow-off of the fuels through at least one pair of engines.

摘要翻译： 具有火箭发动机的推力发生装置彼此成对地布置，用于多个点火以及个人和组激活以及在任务期间足够的燃料量。 推力发生装置被设计为封闭的，可存储的模块化单元。 火箭发动机采用液体燃料和液体氧化剂进行操作。 为每个燃料部件提供至少一个罐。 在启动推力发生装置之前，坦克处于填充的无压力状态。 火箭发动机和块设计的燃料分配器集成在中央舱壁内。 推力发生装置被密封的外套包围，并被隔板分成两个独立的室。 外套在里面衬有“自密封”薄膜。 氧化剂储存在一个室中，另一个室内的燃料。 腔室中的空位包含吸附剂填充物。 温度控制的安全装置通过至少一对发动机产生无脉冲的燃料喷射。

公开(公告)号：US4260194A

公开(公告)日：1981-04-07

申请号：US956787

申请日：1978-11-01

申请人： Friedrich-Karl Blindow ,  Jurgen Decker ,  Heinrich Kluibenschedl ,  German Munding ,  Armin Sowa ,  Harald Wagner

发明人： Friedrich-Karl Blindow ,  Jurgen Decker ,  Heinrich Kluibenschedl ,  German Munding ,  Armin Sowa ,  Harald Wagner

IPC分类号： E21D9/08 ,  E21D9/087 ,  E21D9/10 ,  E21C27/24

CPC分类号： E21D9/1073 ,  E21D9/087 ,  E21D9/1053

摘要： A method of producing an underground cavity in a driving shield advance operation comprises, prior to excavation, forming an annular slot corresponding to the contour and wall thickness of the shield ahead of the shield by using hot gas jets to form the slot and to separate a core from the surrounding rock formation, advancing the shield into the annular slot, and breaking out the core under the protection of the shield. The device for producing the underground cavity comprises a tubular drive shield adapted to be advanced into the cavity and having an interior support wall on which is rotatably supported a support member having an arm carrying a gas jet lance. The gas jet lance advantageously includes at least one gas nozzle directed forwardly to form an inwardly extending cavity ahead of the shield, and one or more nozzle discharges directing the gas laterally. The jet nozzle is rotated after it is advanced into the ground, and the gas jets form an annular slot ahead of the shield which accommodates the shield therein. The shield is then moved into the slot by the usual shield advance cylinders. Walls behind the shield are braced by a lining wall which, for example, may be thin walled rings which may be positioned in place.

摘要翻译： 在驾驶屏蔽提前操作中产生地下腔的方法包括：在挖掘之前，通过使用热气喷射形成槽，形成与屏蔽前面的屏蔽的轮廓和壁厚相对应的环形槽，以形成槽 从围绕岩层的核心，使盾构进入环形槽，并在盾构的保护下分裂核心。 用于生产地下空腔的装置包括适于前进到空腔中并具有内部支撑壁的管状驱动屏蔽件，可旋转地支撑有支撑构件，支撑构件具有承载气体喷枪的臂。 喷气枪有利地包括至少一个气体喷嘴，其向前指向以在屏蔽件前方形成向内延伸的空腔，并且一个或多个喷嘴排出物横向引导气体。 喷射喷嘴在其进入地面之后旋转，并且气体射流在屏蔽件的前面形成一个环形槽，其中容纳护罩。 然后屏蔽通过通常的屏蔽提前气缸移动到槽中。 护罩后面的墙壁由衬里壁支撑，该衬里壁例如可以是可以定位在适当位置的薄壁环。

公开(公告)号：US4224991A

公开(公告)日：1980-09-30

申请号：US16072

申请日：1979-02-28

申请人： Armin Sowa ,  German Munding

发明人： Armin Sowa ,  German Munding

IPC分类号： E21B36/02 ,  F22B1/26 ,  F23C3/00 ,  F23M5/08 ,  E21B43/24

CPC分类号： F23C3/00 ,  E21B36/025 ,  F22B1/26 ,  F23M5/085 ,  Y02E20/344

摘要： A device for extracting crude oil out of an extraction bore of a previously tapped deposit, comprises, a combustion chamber having at least one reaction chamber portion and an evaporation chamber portion arranged in axial relationship with a constricted nozzle portion therebetween. Advantageously, an additional constricted nozzle portion separates a turbulence chamber from a front reaction chamber and the second constriction separates the front reaction chamber from a rear evaporation chamber. The evaporation chamber in turn feeds through a nozzle section to a narrow discharge into the extraction bore. A fuel and chemical oxygen or an oxygen carrier are directed into the combustion chamber preferably in front of the first constriction and forms high temperature combustion gases into which the water is directed in a manner to intermix the water with the combustion gases and to form superheated steam which is then discharged into the extraction bore. The steam causes the oil in the previously tapped deposit to become less viscous and to flow out of the extraction bore.

摘要翻译： 一种用于从预先挖出的沉积物的提取孔中提取原油的装置包括：燃烧室，具有至少一个反应室部分和与它们之间的收缩喷嘴部分轴向关系的蒸发室部分。 有利地，附加的收缩喷嘴部分将湍流室与前反应室分开，并且第二收缩部将前反应室与后蒸发室分离。 蒸发室又通过喷嘴部分进入到排出孔的窄排放口。 将燃料和化学氧气或氧气载体优选地引导到燃烧室中，优选地在第一收缩部的前方，并且以使得水与燃烧气体混合并且形成过热蒸汽的方式形成水被引导到其中的高温燃烧气体 然后将其排出到提取孔中。 蒸汽导致先前攻丝的沉积物中的油变得较不粘稠并从抽气孔流出。

公开(公告)号：US4190121A

公开(公告)日：1980-02-26

申请号：US871822

申请日：1978-01-24

申请人： Werner Baum ,  German Munding

发明人： Werner Baum ,  German Munding

IPC分类号： E21B7/14 ,  F23C3/00

CPC分类号： E21B7/14 ,  F23C3/00 ,  Y10S266/904

摘要： A thermal drilling device which operates in a rotary or circumferentially oscillatory motion and which is particularly adapted for drilling geological formations comprises a drill body which has an interior combustion chamber with a bottom having an outlet defining a discharge nozzle. Means are provided for adding fuel components into the combustion chamber and for igniting them to generate hot gaseous products of combustion which are discharged through a nozzle slot arranged at the bottom of the combustion chamber. The nozzle slot extends diametrically of the drilling area at the bottom and slot outline or a plurality of slots arranged symmetrically relative to the longitudinal axis of the drilling body.

摘要翻译： 一种以旋转或周向振荡运动操作并且特别适用于钻探地质构造的热钻探装置包括钻体，其具有内部燃烧室，底部具有限定排出喷嘴的出口。 提供了用于将燃料成分添加到燃烧室中并且用于点燃它们以产生热的燃烧气体产物的装置，其通过布置在燃烧室底部的喷嘴槽排出。 喷嘴槽在底部的钻孔区域和狭槽轮廓的直径上延伸，或者相对于钻孔主体的纵向轴线对称地布置的多个槽。

公开(公告)号：US4076082A

公开(公告)日：1978-02-28

申请号：US734424

申请日：1976-10-21

申请人： Werner Baum ,  German Munding

发明人： Werner Baum ,  German Munding

IPC分类号： E21B7/14 ,  E21C37/16

CPC分类号： E21B7/14 ,  Y10S266/904

摘要： A thermal drilling device which operates in a rotary or circumferentially oscillatory motion and which is particularly adapted for drilling geological formations comprises a drill body which has an interior combustion chamber with a bottom having an outlet defining a discharge nozzle. Means are provided for adding fuel components into the combustion chamber and for igniting them to generate hot gaseous products of combustion which are discharged through a nozzle slot arranged at the bottom of the combustion chamber. The nozzle slot extends diametrically of the drilling area at the bottom and slot outline or a plurality of slots arranged symmetrically relative to the longitudinal axis of the drilling body. In one embodiment the nozzle slot has a radially extending portion with the circumferential width of the slot increasing in a radial outward direction.

摘要翻译： 一种以旋转或周向振荡运动操作并且特别适用于钻探地质构造的热钻探装置包括钻体，其具有内部燃烧室，底部具有限定排出喷嘴的出口。 提供了用于将燃料成分添加到燃烧室中并且用于点燃它们以产生热的燃烧气体产物的装置，其通过布置在燃烧室底部的喷嘴槽排出。 喷嘴槽在底部的钻孔区域和狭槽轮廓的直径上延伸，或者相对于钻孔主体的纵向轴线对称地布置的多个槽。 在一个实施例中，喷嘴狭槽具有径向延伸的部分，其中槽的周向宽度在径向向外的方向上增加。

公开(公告)号：US06519928B2

公开(公告)日：2003-02-18

申请号：US09843155

申请日：2001-04-26

申请人： German Munding ,  Wolfgang Müller ,  Joachim Reinecke ,  Peter Gleich

发明人： German Munding ,  Wolfgang Müller ,  Joachim Reinecke ,  Peter Gleich

IPC分类号： C06D504

CPC分类号： F42B10/66

摘要： A process for the production of a transverse thrust in a flying object in which a defined quantity of a monergol propellent substance is introduced into a propulsion unit, which is arranged transversely relative to a longitudinal axis of the flying object to produce a thrust transverse to the longitudinal axis of the flying object. The propulsion unit has a combustion chamber, a supersonic nozzle connected to the combustion chamber and a source of heat to combust the propellant substance and produce the desired thrust for a prescribed time. The monergol propellent substance, introduced tangentially into the combustion chamber to form a film of the propellent substance on an inside surface of a wall of the combustion chamber; and the film of propellent substance on the wall is combusted by a pyrotechnic source of heat arranged in the wall of the combustion chamber in the vicinity of a throat of the supersonic nozzle to produce hot gases by the combustion of the propellant substance and transverse thrust in the supersonic nozzle. An automatically operated non-return valve without moving parts prevents backflow of combustion gases to the inlet valve.

摘要翻译： 一种用于在飞行物体中产生横向推力的方法，其中将限定量的芒果醇推进剂物质引入到推进单元中，该推进单元相对于飞行物体的纵向轴线横向布置以产生横向于 飞行物体的纵轴。 推进单元具有燃烧室，连接到燃烧室的超音速喷嘴和用于燃烧推进剂物质并产生所需推力达规定时间的热源。 所述芒果型推进剂物质切向地引入燃烧室以在燃烧室的壁的内表面上形成推进剂物质的膜; 并且壁上的推进物质膜被布置在燃烧室壁中的烟火源在超音速喷嘴的喉部附近燃烧，以通过推进剂物质的燃烧产生热气体和横向推力 超音速喷嘴。 没有移动部件的自动操作的止回阀防止燃烧气体回流到入口阀。

公开(公告)号：US3937012A

公开(公告)日：1976-02-10

申请号：US423127

申请日：1973-12-10

申请人： Willi Zeh ,  Werner Beck ,  German Munding

发明人： Willi Zeh ,  Werner Beck ,  German Munding

IPC分类号： F02G1/00 ,  F02K9/52 ,  F02K9/60

CPC分类号： F02G1/00 ,  F02K9/52 ,  F02K9/60

摘要： An arrangement for producing rotational energy, particularly for generating thrust gases in rocket combustion chambers using hypergolically reacting propellants, comprises a rocket combustion chamber having a closed end and a gas discharge end with an impeller mounted in the closed end. The impeller has a plurality of spaced vanes which extend radially and which define flow ducts therebetween having discharge ends which extend substantially tangential to the combustion periphery. The apparatus includes means for directing hypergolically reacting propellant components into the combustion chamber at a location in which they are deposited at the inner radial ends of the flow ducts. The oxygen carrier propellant is supplied radially inside of the other propellant component so that it forms a cooling veil along the impeller. The impeller is advantageously rotatably mounted so that the components are whirled outwardly into the combustion chamber and the individual blades are provided with passages in order to enhance the interreaction of the propellant components.

摘要翻译： 用于产生旋转能量的装置，特别是用于在使用高效反应的推进剂的火箭燃烧室中产生推力气体的装置包括具有封闭端的火箭燃烧室和具有安装在封闭端的叶轮的气体排出端。 叶轮具有多个间隔开的叶片，叶片径向延伸并限定在其间的流动管道，其具有基本上与燃烧周边相切延伸的排放端。 该装置包括用于将绝热反应的推进剂组分引导到其在沉积在流动管道的内部径向端处的位置处的燃烧室中的装置。 氧载体推进剂在另一个推进剂组件的径向内部供应，从而沿着叶轮形成冷却面纱。 叶轮有利地可旋转地安装，使得部件向外旋转到燃烧室中，并且各个叶片设置有通道，以便增强推进剂组分的相互作用。

公开(公告)号：US4304308A

公开(公告)日：1981-12-08

申请号：US188937

申请日：1980-09-19

申请人： German Munding ,  Helmut Hopmann ,  Armin Sowa ,  Christian Beckeryordersandforth ,  Walter Terschuren

发明人： German Munding ,  Helmut Hopmann ,  Armin Sowa ,  Christian Beckeryordersandforth ,  Walter Terschuren

IPC分类号： E21B7/14 ,  E21B7/18 ,  E21B43/247 ,  E21C37/16

CPC分类号： E21B43/247 ,  E21B7/14 ,  E21B7/18 ,  Y10S48/06

摘要： A method and apparatus for making holes in coal seams in a coal mining system in which hot working gas is employed to impinge on the coal under high pressure and speed in order to disintegrate it and particularly for making inclined or horizontal holes which connect vertical drill holes which lead from the surface to the coal seam and through which the medium for gasifying the coal underground is blown in. The vertical drill holes which lead from the coal seam to the surface are used for blowing out gasification gases which are produced by the operation as well as for delivering the hot working gas. With the method of the invention, a gasification medium of high temperature and pressure is advantageously produced directly at the locations where the disintegrated coal is gasified, the disintegrated coal being formed by a rocket combustion process. With the invention, a hydrogenating gasification medium is used for gasifying the coal seam, for example, a hydrogen steam or hydrogen steam mixture, so that the gas produced possesses the quality of natural gas. An oxidizing gasification medium such as air may also be supplied for gasifying the drillings. The resulting CO and H.sub.2 O gases which are produced are further burned to CO.sub.2 and H.sub.2 O by the oxidizing gasification medium. The gasification medium is not supplied from the surface but is produced at the location at which the gasification takes place, for example, by injecting into the hot working gas, water or the like, carried along from a rocket combustion process. For the rocket combustion process, a fuel is chosen so that the resulting gas is capable of acting simultaneously as a gasification medium and working gas.

摘要翻译： 一种用于在采煤系统中在煤层中形成孔的方法和装置，其中使用热作用气体在高压和高速下撞击煤，以便将其分解，特别是用于制造连接垂直钻孔的倾斜或水平孔 从地表引入煤层，通过其将煤层气化的介质吹入地下，将从煤层引导到地面的垂直钻孔用于吹出由操作产生的气化气体 以及输送热的工作气体。 利用本发明的方法，有利地在分解煤气化的地方直接生产高温气压的气化介质，通过火箭燃烧过程形成分解的煤。 利用本发明，使用氢化气化介质来气化煤层，例如氢蒸气或氢蒸气混合物，使得产生的气体具有天然气的质量。 还可以提供诸如空气的氧化气化介质来气化钻孔。 所产生的CO和H 2 O气体通过氧化气化介质进一步燃烧到CO 2和H 2 O. 气化介质不是从表面供应的，而是在气化发生的地方产生，例如通过注入从火箭燃烧过程携带的热加工气体，水等中。 对于火箭燃烧过程，选择燃料使得所得气体能够同时作为气化介质和工作气体作用。