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1. 发明授权

US5024395A Stepping mechanism for rotary motions 失效
标题翻译：旋转运动的步进机构
公开(公告)号：US5024395A
公开(公告)日：1991-06-18
申请号：US363342
申请日：1989-06-06
申请人： Walter Kranz , Heinz Tillmann
发明人： Walter Kranz , Heinz Tillmann
IPC分类号： F16H27/04 , F16H31/00
CPC分类号： F16H27/04 , F16H31/003 , F42B10/663
摘要： The invention relates to a stepping mechanism for rotary motions with a driven switching wheel (9) which comprises at least one wheel-side stop (10), with an escapement mechanism having at least one pawl (12) which cooperates with said wheel-side stop, and with an actuating device (3, 17) for the pawl. Pursuant to the invention, a miniaturizable stepping mechanism is provided which is of a simple design and which permits reliable positioning of the switching wheel into preselected individual rotational positions. According to the invention, this is achieved in that the escapement mechanism of the stepping mechanism comprises a brake (20) displaceable under the action of force, with a run-up edge (21) lying in the region of each pawl (12) on to which the wheel-side stop (10) runs up before striking the pawl (12) to thereby displace the brake. Preferably, the brake and the pawls are arranged on a rocker (20, 13) for each, these being pivotable about a common rotary shaft (14) not lying in the axis of rotation (A) of the stepping mechanism. The stepping mechanism can be used for the control (i.e. steering) of missiles. To this end the switching wheel is preferably connected with a rotary nozzle body (1) which, via a thrust nozzle (8), delivers a propellant jet approximately in a radial direction.
摘要翻译：本发明涉及一种具有从动转换轮（9）的旋转运动的步进机构，该转动轮包括至少一个车轮侧止动件（10），其中擒纵机构具有至少一个棘爪（12），所述棘爪与所述车轮侧并且具有用于棘爪的致动装置（3,17）。根据本发明，提供了一种小型化的步进机构，其具有简单的设计，并且允许切换轮可靠地定位到预选的各个旋转位置。根据本发明，这是通过这样来实现的：步进机构的擒纵机构包括在力作用下可移动的制动器（20），其中位于每个棘爪（12）的区域中的上升边缘（21）位于在撞击棘爪（12）之前，车轮侧挡块（10）向上运动，从而使制动器移位。优选地，制动器和棘爪分别布置在摇臂（20,13）上，这些可绕着不位于步进机构的旋转轴线（A）的公共旋转轴（14）枢转。步进机构可用于导弹的控制（即转向）。为此，切换轮优选地与旋转喷嘴体（1）连接，旋转喷嘴体（1）通过推力喷嘴（8）大致沿径向输送推进剂射流。

2. 发明授权

US4589594A Thrust nozzle system 失效
标题翻译：推力喷嘴系统
公开(公告)号：US4589594A
公开(公告)日：1986-05-20
申请号：US605286
申请日：1984-04-30
申请人： Walter Kranz
发明人： Walter Kranz
IPC分类号： F02K1/78 , F02K9/80 , F42B19/01 , F42B15/033
CPC分类号： F42B10/663
摘要： The invention relates to a thrust nozzle system, especially for steering arojectile, having a nozzle arrangement (3) which is fed by a propellant source, for example a gas source. The nozzle system is arranged in a housing having at least one exhaust port (11) provided in the housing, and has a control (14) for steering a thrust jet (18) of the nozzle arrangement through the exhaust port. The invention provides a thrust nozzle system of simple construction which is especially suitable for a high miniaturization, and which permits a flexible thrust impulse forming. For this purpose the thrust nozzle system (2) has a rotating nozzle or a swinging nozzle body (3) which is rotatable relative to the housing about an axis, driven by the propellant, for example by the gas stream (P) from the gas source. The drive of the rotating nozzle body is preferably achieved by an acentric thrust nozzle (10) itself. Due to the low mass and hence low inertia of the nozzle body (3), it may be caused to rotate fast. A braking arrangement (14) is provided for the rotating nozzle body for steering the thrust jet (18) in a defined direction. Such a thrust nozzle system may serve for many uses, for example in conjunction with a secondary injection system or a hot gas motor.
摘要翻译：本发明涉及一种特别用于转向抛射体的推力喷嘴系统，其具有由推进剂源例如气体源供给的喷嘴装置（3）。喷嘴系统布置在具有设置在壳体中的至少一个排气口（11）的壳体中，并且具有用于通过排气口转向喷嘴装置的推力射流（18）的控制器（14）。本发明提供了一种结构简单的推力喷嘴系统，特别适用于高度小型化，并且允许柔性的推力冲击形成。为此目的，推力喷嘴系统（2）具有旋转喷嘴或摆动喷嘴体（3），该主体可相对于外壳绕轴承转动，该轴线由推进剂驱动，例如来自气体的气流（P）资源。旋转喷嘴体的驱动优选通过中心推力喷嘴（10）本身实现。由于喷嘴体（3）的质量低，因此惯性较小，可能会使其快速旋转。为旋转喷嘴体提供制动装置（14），用于沿着确定的方向转向推力射流（18）。这种推力喷嘴系统可以用于许多用途，例如与二次喷射系统或热气体马达相结合。

3. 发明授权

US4927096A Rotor setting system in conjunction with aerodynamic body controls 失效
标题翻译：转子设定系统与空气动力学体系控制相结合
公开(公告)号：US4927096A
公开(公告)日：1990-05-22
申请号：US16881
申请日：1987-02-20
申请人： Walter Kranz
发明人： Walter Kranz
IPC分类号： F42B10/64
CPC分类号： F42B10/64
摘要： A rotor setting system in conjunction with an aerodynamic-body control. The setting system is characterized by a rotor which comprises a console, a rotary drive for the rotor, setting members for the control of the aerodynamic body, especially rudders or spoilers, as well as a control unit for the rotor, and further including a control unit on the sides of the aerodynamic body, wherein the two control units cooperate with each other for adjusting the setting members.
摘要翻译：与空气动力学体系控制相结合的转子设定系统。该设置系统的特征在于转子，其包括控制台，用于转子的旋转驱动器，用于控制空气动力体的调整构件，特别是方向舵或扰流板，以及用于转子的控制单元，还包括控制器单元在空气动力体的侧面，其中两个控制单元彼此协作以调节设定构件。

4. 发明授权

US4898342A Missile with adjustable flying controls 失效
标题翻译：导弹与可调飞行控制
公开(公告)号：US4898342A
公开(公告)日：1990-02-06
申请号：US283628
申请日：1988-12-13
申请人： Walter Kranz , Werner Schnabele
发明人： Walter Kranz , Werner Schnabele
IPC分类号： F42B10/60
CPC分类号： F42B10/60
摘要： A missile with adjustable flight controls capable of altering the missile's flight path is disclosed. The missile comprises an electric generator and control electronics. The electric generator is used in this invention both to provide electrical power to the control electronics and to regulate the flight controls. A mechanical connection is created between the generators rotor and the flight controls. The generator is electrically coupled to the control electronics through an electrically variable load. The control electronics alters the load which varies the rotational speed of the generator. This in turn affects the flight controls and the flight path is altered accordingly. The invention is small and compact, allowing its use in small missiles such as mortar or artillery shells.
摘要翻译：公开了一种具有能够改变导弹飞行路径的可调式飞行控制装置的导弹。导弹包括发电机和控制电子装置。发电机在本发明中用于向控制电子设备提供电力并调节飞行控制。在发电机转子和飞行控制器之间产生机械连接。发电机通过电可变负载电耦合到控制电子装置。控制电子装置改变发生器转速的负载。这反过来影响飞行控制，并且相应地改变飞行路径。本发明小而紧凑，允许其用于诸如迫击炮或炮弹之类的小型导弹。

5. 发明授权

US4674707A Apparatus for stabilizing a flying body 失效
标题翻译：用于稳定飞行体的装置
公开(公告)号：US4674707A
公开(公告)日：1987-06-23
申请号：US796750
申请日：1985-11-08
申请人： Walter Kranz
发明人： Walter Kranz
IPC分类号： F42B10/66 , F42B15/033
CPC分类号： F42B10/66
摘要： The flight path of a flying body, such as an artillery shell, is stabilizedgainst disturbing forces and against pendulum type motions by fluid steering jets ejected from said flying body for causing forces countering the disturbing forces. The steering jets pass through a fluid jet distributing member which has inlet openings communicating with fluid ducts leading to a fluid supply chamber. The distributing member is mounted in the flying body by a spring which permits a deflection or shifting of the distributing member in a direction across a central longitudinal axis of the body. A shift increases the fluid flow cross-sectional area at the inlet openings of the distributing member on its side opposite a disturbing force and decreases the fluid flow cross-sectional area on the side on which the disturbing force is effective, whereby the through-flow of fluid is increased on the opposite side and decreased on the side on which the disturbing force is effective on said flying body for generating the compensating force.
摘要翻译：诸如炮弹的飞行体的飞行路径通过从所述飞行体弹出的流体转向喷射器抵抗扰动力和摆锤式运动而稳定，以产生抵抗扰动力的力。转向射流通过流体喷射分配构件，流体喷射分配构件具有与通向流体供应室的流体管道连通的入口开口。分配构件通过弹簧安装在飞行体中，该弹簧允许分配构件沿着穿过身体的中心纵向轴线的方向偏转或移动。移位增加了分配构件在其与扰动力相反的一侧的入口开口处的流体流动横截面面积，并且减小了干扰力有效的一侧上的流体流动横截面积，从而使通流的流体在相对侧增加，并且在所述飞行体上对干扰力有效的一侧减小以产生补偿力。

6. 发明授权

US5083724A Device for controlling aerodynamic bodies 失效
标题翻译：用于控制空气动力机构的装置
公开(公告)号：US5083724A
公开(公告)日：1992-01-28
申请号：US516290
申请日：1990-04-30
申请人： Walter Kranz
发明人： Walter Kranz
IPC分类号： F42B10/64
CPC分类号： F42B10/64
摘要： A device for controlling aerodynamic bodies with at least one setting member for generating a transversal force on the aerodynamic body. To achieve a simple compact design, setting members are arranged on a rotor where the rotor extends forward from the tip of the aerodynamic body. The setting members are arranged here so that they set the rotor in rotation by the oncoming flow; they are designed, for instance, as a crossed pair of rudders. In addition, the setting members are located asymmetrically to the longitudinal axis of the aerodynamic body, so that they exert at least in some positions of the rotor a transversal force on the aerodynamic body. The position of the rotor can be influenced by means of a braking system.

7. 发明授权

US4979697A Control propulsion unit, especially for exerting transverse forces on a missile 失效
标题翻译：控制推进装置，特别是在导弹上施加横向力
公开(公告)号：US4979697A
公开(公告)日：1990-12-25
申请号：US429411
申请日：1989-10-31
申请人： Walter Kranz
发明人： Walter Kranz
IPC分类号： F02K9/92
CPC分类号： F02K9/92 , F42B10/661
摘要： A control propulsion unit with a solid propellant (4) and a discharge nozzle, through which the propellant gases emerge into the open air, especially to exert transverse forces on a missile. To be able to precisely, quantitatively regulate the transverse forces, in accordance with the invention, it is proposed to extinguish the propellant in a controlled operation by reducing the clamping of the control propulsion unit, for example, by enlarging the discharge port for the propellant gases.
摘要翻译：具有固体推进剂（4）和排放喷嘴的控制推进装置，推进剂气体通过其排出到外部空气中，特别是在导弹上施加横向力。为了能够精确地，定量地调节横向力，根据本发明，建议通过减少控制推进单元的夹紧来在受控操作中熄灭推进剂，例如通过扩大推进剂的排放口气体。

8. 发明授权

US4793571A Missile with aerodynamic control 失效
标题翻译：导弹与空气动力学控制
公开(公告)号：US4793571A
公开(公告)日：1988-12-27
申请号：US69434
申请日：1987-07-02
申请人： Walter Kranz
发明人： Walter Kranz
IPC分类号： F42B10/62 , F41G7/00
CPC分类号： F42B10/62
摘要： A missile, and in particular a shell flying at supersonic velocity, having aerodynamic control. The missile comprises a missile housing and a missile tip which is tiltably connected to the missile housing. Between the missile housing and the shell tip, a positioning device consisting of at least one piezoelectric positioning member and a control circuit is arranged which comprises a voltage source. By applying a voltage to the piezoelectric positioning members, their lengths are changed, whereby the tilting motion of the shell tip is executed.
摘要翻译：导弹，特别是以超音速飞行的壳体，具有空气动力学控制。导弹包括一个导弹罩和一个可与导弹罩倾斜连接的导弹尖。在导弹壳体和壳体末端之间，布置有由至少一个压电定位构件和控制电路组成的定位装置，其包括电压源。通过向压电定位构件施加电压，其长度被改变，由此执行壳尖端的倾斜运动。

9. 发明授权

US4223770A Shaft drive alternately for both directions of rotation 失效
标题翻译：轴向两个旋转方向交替驱动
公开(公告)号：US4223770A
公开(公告)日：1980-09-23
申请号：US959143
申请日：1978-11-09
申请人： Walter Kranz
发明人： Walter Kranz
IPC分类号： F01D1/30 , F01D1/34 , F02C7/36 , F16D47/06
CPC分类号： F01D1/34 , F01D1/30 , F02C7/36 , F05D2260/4023 , Y10T477/27 , Y10T477/40 , Y10T477/6425
摘要： A shaft drive alternately for both directions of rotation, comprises, a shaft rotatably supported on bearings having first and second turbines connectable thereto, each including a respective first and second turbine wheel freely rotatable on the shaft in respective opposite first and second directions. The turbine wheels are driven by fluid which rotates the wheels in a selected direction and, in addition, displaces the turbine wheels so that a friction disc carried thereby is engaged with a respective first and second clutch to connect it to the shaft to impart the selected direction of rotation. When the turbine is stopped by not directing the fluid into the blades, in which case the clutch mechanism is moved out of engagement and the turbine wheel may run free of the shaft, the second turbine wheel may be connected in a similar manner by effecting engagement of the associated second clutch with the shaft when the fluid is directed to the second turbine for rotating the turbine wheel.
摘要翻译：交替地为两个旋转方向的轴驱动器包括可旋转地支撑在具有可连接到其上的第一和第二涡轮机的轴承上的轴，每个轴包括相应的第一和第二涡轮机轮，在相应的第一和第二方向上可在轴上自由旋转。涡轮机叶轮由沿着所选方向旋转车轮的流体驱动，并且另外使得涡轮机轮移动，使得由此携带的摩擦盘与相应的第一和第二离合器接合以将其连接到轴，以使所选择的旋转方向当通过不将流体引导到叶片中来停止涡轮机时，在这种情况下，离合器机构移动离开接合并且涡轮机叶轮可以不用轴运行，第二涡轮机叶轮可以通过实现接合而以类似的方式连接当所述流体被引导到所述第二涡轮机以旋转所述涡轮机叶轮时，所述第二离合器与所述轴相关联。

10. 发明授权

US4006755A Electrofluidic converter 失效
标题翻译：电流转换器
公开(公告)号：US4006755A
公开(公告)日：1977-02-08
申请号：US624842
申请日：1975-10-22
申请人： Walter Kranz , Heinz Tillmann
发明人： Walter Kranz , Heinz Tillmann
IPC分类号： F15C1/04 , F15C1/08
CPC分类号： F15C1/04 , Y10T137/2213 , Y10T137/2234
摘要： The converter comprises a plurality of series-connected bistable fluidic elements each having a supply input, two outputs separated by a jet splitter, and two conical inputs. The outputs of each bistable fluidic element are connected to respective control inputs of the next preceding bistable element. Feedback conduits are branched off the outputs of the last fluidic element and connected to the control inputs of the first fluidic element. The feedback conduits are closed or cleared by an electromagnetically operated valve which opens in the direction of fluid flow through the then blocked feedback conduit responsive to a signal from an electric control circuit.
摘要翻译：转换器包括多个串联连接的双稳态流体元件，每个流体元件具有供给输入，由喷射分离器分开的两个输出和两个锥形输入。每个双稳态流体元件的输出连接到下一个前面的双稳态元件的相应控制输入。反馈导管从最后一个流体元件的输出分支并连接到第一流体元件的控制输入。反馈管道由电磁操作的阀门闭合或清除，该阀门响应于来自电气控制电路的信号沿着流过流过阻塞的反馈管道的流体的方向而打开。

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