公开(公告)号：US06536208B1

公开(公告)日：2003-03-25

申请号：US09890237

申请日：2001-10-31

申请人： Joachim Kretschmer

发明人： Joachim Kretschmer

IPC分类号： F02K948

CPC分类号： F02K9/48 ,  F02K9/52

摘要： Device for supplying fuel for a rocket propulsion unit has a first and at least a second fuel circuit for respective different fuels. Each fuel is brought to an increased energy level by a pump and is supplied for combustion by way of injection elements. The first fuel is heated in cooling channels extending in a propulsion chamber wall before the fuel is supplied for combustion, and the first fuel is subsequently fed to at least the turbines assigned to the pumps. A heat exchanger is provided in which the fuel coming from the turbines is in a heat exchange with a fuel coming from a pump. A heat exchanger especially usable in the device for supplying fuel is provided.

摘要翻译： 用于为火箭推进单元供应燃料的装置具有用于各种不同燃料的第一和至少第二燃料回路。 每个燃料通过泵达到增加的能量水平，并通过注入元件供给燃烧。 第一燃料在燃料供应燃烧之前在推进室壁中延伸的冷却通道中被加热，并且第一燃料随后被送入至少分配给泵的涡轮机。 提供了一种热交换器，其中来自涡轮机的燃料与来自泵的燃料进行热交换。 提供了特别可用于供应燃料的装置的热交换器。

公开(公告)号：US06286925B1

公开(公告)日：2001-09-11

申请号：US08946643

申请日：1997-10-07

申请人： Joachim Heinzl ,  Alfred Zollner ,  Peter Möstl ,  Gerhard Beurer ,  Joachim Kretschmer

发明人： Joachim Heinzl ,  Alfred Zollner ,  Peter Möstl ,  Gerhard Beurer ,  Joachim Kretschmer

IPC分类号： B41J2938

CPC分类号： B41J29/38 ,  B41J2/04525 ,  B41J2/04541 ,  B41J2/04568 ,  B41J2/04581 ,  B41J2/04588 ,  B41J2/04591 ,  B41J2202/10

摘要： The printhead has a multitude of adjacently arranged channels with piezo-electrical shear converters. The impulse form for activation of the converters—depending upon the number of simultaneously activated neighboring channels—is changed in such manner that the exit velocity of the ink droplets is constant. This makes it possible to obtain a better print image.

摘要翻译： 打印头具有多个相邻布置的通道，带有压电式电动剪切转换器。 用于激活转换器的脉冲形式（取决于同时激活的相邻通道的数量）以使得墨滴的出口速度恒定的方式改变。 这样可以获得更好的打印图像。

公开(公告)号：US07571610B2

公开(公告)日：2009-08-11

申请号：US10804124

申请日：2004-03-19

申请人： Joachim Kretschmer

发明人： Joachim Kretschmer

IPC分类号： F02K1/00

CPC分类号： F02K9/976

摘要： Extendible exhaust nozzle bell for rocket engine of aircraft or spacecraft includes a first part with smaller diameter fixedly arranged on motor of engine and a second part with larger diameter arranged in flexible manner with respect to first part. In a front stowed position, second part is located surrounding first part closer to the rocket motor and, in a rear operating position, first part is arranged further away from the rocket motor. A closed volume that can be acted on by a gaseous fluid causes an extension of the second part of the exhaust nozzle bell from the stowed position into the operating position. The closed volume is formed at least in part by a deformable rolling bellows arrangement coupled between the flexibly arranged second part of the exhaust nozzle bell and a fixed part of the rocket engine or of the aircraft or spacecraft.

摘要翻译： 飞机或航天器的火箭发动机的可扩展排气喷嘴钟包括固定地布置在发动机马达上的较小直径的第一部分和相对于第一部分以柔性方式布置的具有较大直径的第二部分。 在前部收起位置，第二部分位于靠近火箭发动机的第一部分周围，并且在后部操作位置，第一部分布置成远离火箭发动机。 可以由气态流体作用的封闭体积导致排气喷嘴钟罩的第二部分从收起位置延伸到操作位置。 闭合容积至少部分地由耦合在排气喷嘴钟的柔性布置的第二部分和火箭发动机或飞行器或航天器的固定部分之间的可变形滚动波纹管布置形成。

公开(公告)号：US06637188B2

公开(公告)日：2003-10-28

申请号：US09985313

申请日：2001-11-02

申请人： Peter Bichler ,  Hans Immich ,  Joachim Kretschmer ,  Günther Schmidt

发明人： Peter Bichler ,  Hans Immich ,  Joachim Kretschmer ,  Günther Schmidt

IPC分类号： F02K942

CPC分类号： F02K9/64

摘要： A combustion chamber for a rocket engine expels a hot stream of gas and has a cooling device. The inner wall of the combustion chamber adjoins the cooling device and contains depressions formed in such a way that the stable outer layer of the stream of gas that forms in the proximity of the inner wall of the combustion chamber during operation of the combustion chamber is destabilized in the area of the depressions.

摘要翻译： 用于火箭发动机的燃烧室排出热气流，并具有冷却装置。 燃烧室的内壁与冷却装置相邻并且包含凹陷，其形成为使得在燃烧室操作期间在燃烧室的内壁附近形成的气体流的稳定外层不稳定 在洼地的地区。

公开(公告)号：US20050018014A1

公开(公告)日：2005-01-27

申请号：US10854328

申请日：2004-05-27

申请人： Rene Butty ,  Joachim Kretschmer ,  Markus Moser ,  Daniel Sulser

发明人： Rene Butty ,  Joachim Kretschmer ,  Markus Moser ,  Daniel Sulser

IPC分类号： B41J2/175 ,  B41J2/14

CPC分类号： B41J2/1752

摘要： An ink cartridge is disclosed for insertion into a cartridge receptacle of an inkjet printer. The ink cartridge, on one side wall, has a locking snap member, which protrudes from the side wall and on which a detent edge is embodied, with which the locking snap member can be locked to a locking opening, provided on the cartridge receptacle, in its locking position for locking the ink cartridge in the cartridge receptacle. The locking snap member has a hinged portion, which with its pivot axis extends approximately parallel to the introduction plane (E) of the ink cartridge, in which the ink cartridge is to be inserted into the cartridge receptacle. The hinged portion is adjoined by a detent portion, on which a detent edge extending transversely to the introduction plane (E) is embodied.

摘要翻译： 公开了用于插入喷墨打印机的盒式存储器中的墨盒。 墨盒在一个侧壁上具有锁定卡扣构件，其从侧壁突出并且具有止动边缘，锁定卡扣构件可以通过卡锁部件锁定到设置在墨盒容器上的锁定开口， 在其锁定位置用于将墨盒锁定在墨盒容器中。 锁定卡扣构件具有铰接部分，其枢转轴线大致平行于墨盒的引入平面（E）延伸，墨盒将插入墨盒容器中。 铰接部分由制动部分邻接，其上形成有横向于引入平面（E）延伸的止动边缘。

公开(公告)号：US06470671B1

公开(公告)日：2002-10-29

申请号：US09539043

申请日：2000-03-30

申请人： Joachim Kretschmer

发明人： Joachim Kretschmer

IPC分类号： F02K964

CPC分类号： F02K9/972 ,  B23P15/008 ,  F02K9/34 ,  F02K9/40 ,  F02K9/64 ,  F05D2250/15 ,  F05D2250/25 ,  Y10T29/49346

摘要： A regeneratively coolable nozzle for a rocket engine is formed by winding a tubular material (6) onto a winding mandrel to produce a helical composite structure (5), through which a coolant can flow during operation of the nozzle. The spiral composite structure (5) is fixed temporarily and the fixed composite structure (5) is removed from the winding mandrel. Then an inner heat resistant, load bearing layer (9) is applied to the radially inner hot-gas facing surface (H) of the fixed composite structure (5). The present nozzle is lightweight and withstand a high coolant pressure.

摘要翻译： 用于火箭发动机的再生冷却喷嘴通过将管状材料（6）卷绕到卷绕心轴上以形成螺旋复合结构（5）而形成，在该喷嘴的操作过程中冷却剂可通过该螺旋复合结构流动。 螺旋复合结构（5）暂时固定，固定复合结构（5）从缠绕心轴上移除。 然后，将内部耐热承载层（9）施加到固定复合结构（5）的径向内部热气体对向表面（H）。 本喷嘴重量轻，承受高的冷却液压力。

公开(公告)号：US6164758A

公开(公告)日：2000-12-26

申请号：US199589

申请日：1998-11-25

申请人： Joachim Kretschmer

发明人： Joachim Kretschmer

IPC分类号： B41J2/175 ,  B41J3/51

CPC分类号： B41J2/17546

摘要： Process for re-coding of print heads equipped with electronic codings, whereby the coding of an original print head A is altered in such manner that it is identical to that of another print head B. This is attained by interruption of conductive connections between contacts and the placement of new conductive connections between contacts of the print head A in accordance with the conductive connections of print head B. The re-coding can be designed in reversible as well as irreversible form.

摘要翻译： 用于重新编码装有电子编码的打印头的处理，由此原始打印头A的编码以与另一个打印头B相同的方式改变。这是通过中断触点之间的导电连接和 根据打印头B的导电连接，在打印头A的触点之间布置新的导电连接。重新编码可设计成可逆的以及不可逆的形式。

公开(公告)号：US5638683A

公开(公告)日：1997-06-17

申请号：US356880

申请日：1994-12-15

申请人： Joachim Kretschmer

发明人： Joachim Kretschmer

IPC分类号： B05B1/08 ,  F02K9/44 ,  F02K9/62 ,  F15C1/22 ,  F23R3/28

CPC分类号： B05B1/08 ,  F02K9/44 ,  F02K9/62 ,  F15C1/22

摘要： A fluidic nozzle which is flown through by a singular injection jet and which periodically deflects the injection jet. The nozzle has a nozzle channel, whose cross section is expanded in relation to the injection jet, and with control openings opening into the nozzle channel downstream close to the neck of the nozzle for injecting a control fluid that brings about the deflection of the jet. The nozzle channel has a channel cross section, which is two-dimensionally expanded in height and width in relation to the cross section of the jet, with a cross-section contour corresponding to the desired distribution cross section, and it is provided with a number of control openings. The control openings are arranged offset in relation to one another in the circumferential direction of the nozzle channel and are activated one after another in sequence to generate a jet movement rotating along the circumference of the nozzle channel.

摘要翻译： 流体喷嘴，其通过单次注射射流流过并且周期性地使喷射射流偏转。 喷嘴具有喷嘴通道，其横截面相对于喷射射流膨胀，并且控制开口在喷嘴通道的下游靠近喷嘴颈部开口，用于喷射引起射流偏转的控制流体。 喷嘴通道具有通道横截面，该横截面相对于喷射器的横截面在高度和宽度上二维地扩大，横截面轮廓对应于期望的分布横截面，并且其设有数字 的控制开口。 控制开口在喷嘴通道的圆周方向上相对于彼此偏移地布置，并且依次被一个接一个地激活，以产生沿着喷嘴通道的圆周旋转的喷射运动。

公开(公告)号：US5351480A

公开(公告)日：1994-10-04

申请号：US89335

申请日：1993-07-12

申请人： Joachim Kretschmer

发明人： Joachim Kretschmer

IPC分类号： F02K1/08 ,  F02K1/09 ,  F02K1/30 ,  F02K1/52 ,  F02K7/16 ,  F02K1/00

CPC分类号： F02K1/30 ,  F02K1/09 ,  F02K7/16

摘要： A jet engine having at least one combustion chamber with a propelling nozzle connected behind it, achieves in a constructionally simple manner and with a high propulsion effect a cross-sectional configuration of a hot gas flow duct bounded by the propelling nozzle that is highly variable with respect to the nozzle throat area as well as to the outlet area. The propelling nozzle contains a divergent lengthening part which is axially movable for the outlet-side expansion of the hot-gas flow duct. In the moved-out position, the lengthening part connects essentially in the corresponding shape to the divergent outlet end of the nozzle outer wall fixed to the engine and, in the moved-in condition, forms together with it an air outlet duct which encloses the fixed nozzle wall end in a ring-shaped manner and whose cross-section can be regulated. In the lower flying speed range, where the propelling nozzle lengthening is not required for the expansion of the outer contour of the hot gas flow duct, a secondary air injection takes place that is uniform along the whole outer circumference of the fixed nozzle end, and in addition, in the interior of the propelling nozzle, for the interior bounding of the hot gas flow duct, a mushroom-shaped central body is arranged which, with its largest cross-section can be axially adjusted between the plane of the smallest cross-sectional surface of the fixed nozzle outer wall and the outlet plane of the moved-out nozzle lengthening.

摘要翻译： 具有至少一个具有连接在其后面的推进喷嘴的燃烧室的喷气发动机实现了结构上简单的方式并具有高推进效果，由推进喷嘴界定的热气流动管道的横截面构造是高度可变的， 相对于喷嘴喉部区域以及出口区域。 推进喷嘴包含一个发散的延长部分，其可以轴向移动，用于热气流道的出口侧膨胀。 在移出位置，延长部分基本上以相应的形状连接到固定到发动机的喷嘴外壁的发散出口端，并且在移动状态下与其一起形成包围 固定喷嘴壁端部为环形，横截面可调节。 在较低的飞行速度范围内，在热气流管的外轮廓膨胀的情况下，不需要推进喷嘴延长的二次空气喷射，沿固定喷嘴端的整个外圆周均匀， 此外，在推进喷嘴的内部，为了热气流动管道的内部界定，设置有蘑菇形中心体，其最大横截面可以在最小横截面的平面之间轴向调节， 固定喷嘴外壁的横截面和移出喷嘴的出口平面延长。

公开(公告)号：US06554381B2

公开(公告)日：2003-04-29

申请号：US09836004

申请日：2001-04-17

申请人： Philippe Georges Locher ,  Markus Bürgin ,  Joachim Kretschmer

发明人： Philippe Georges Locher ,  Markus Bürgin ,  Joachim Kretschmer

IPC分类号： B41J2195

CPC分类号： B41J2/17566 ,  B41J2002/17573 ,  B41J2002/17576 ,  G01F23/366 ,  G01F23/686

摘要： A system is provided for registration of a fluid level of a fluid in the fluid chamber of an invention-specific receptacle (1), in particular of ink in an ink cartridge, with a light source (11) which beams into the chamber of the receptacle, a reflection body (2) which is designed as a float, which moves in the chamber of the receptacle in dependency upon the filling level of the fluid and which variably reflects the light in dependency upon its movement, and a light detector (10) which receives a variable amount of light.