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公开(公告)号：EP0356422A4
公开(公告)日：1992-06-10
申请号：EP87906689
申请日：1987-04-21
发明人： GRANDOS, NORMAN
CPC分类号： G01S13/345 , F42C13/045
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公开(公告)号：EP0352861A2
公开(公告)日：1990-01-31
申请号：EP89201942.3
申请日：1989-07-24
CPC分类号： F02D41/3058 , F02B3/06 , F02B69/06 , F02B75/02 , F02B2075/025 , F02B2075/027 , F02D13/0215 , F02D13/028 , F02D35/023 , F02D41/2422 , F02D2041/001 , F02D2200/0418 , F02D2400/04 , F02N19/004 , F02P5/1502 , Y02T10/18 , Y02T10/46
摘要： A method of and apparatus for starting and accelerating a vehicle through a range of vehicle speeds during which the vehicle internal combustion engine is operated in a plurality of different operating modes is disclosed. The engine may first be cranked in a compressionless mode preparatory to starting and then run in a second mode at a relatively low speed for a warm-up interval as a six-stroke cycle engine where each engine cylinder cycle includes an essentially adiabatic compression and expansion. The system may then convert to a third mode of operation as a four-stroke cycle engine during normal engine operation. Different operating modes are available during this normal operation. Under high demand conditions, the engine may be run as a conventional inefficient but effective throttled engine or converted to operation in a fourth mode as a two-stroke cycle engine. The vehicle management system includes a first read only memory for storing a fixed table of engine operating parameters corresponding to various engine conditions, and a random access second storage means for storing a table of engine operating parameters corresponding to various engine conditions with the second table being initially the same as the first table. The system responds to sensed engine conditions to modify the parameters in the second table and controls the vehicle in accordance with the parameters stored in the second table. Both short term modification to accommodate dynamic changes in the sensed engine conditions and long term modification to compensate for relatively slow changes in the engine and the management system are made to the information in the random access memory. The modifications may be on an overall engine basis or an individual cylinder basis.
摘要翻译： 公开了一种用于通过车辆内燃机以多种不同操作模式操作的车速范围来启动和加速车辆的方法和装置。 发动机可以首先在无压模式下起动，然后以六冲程发动机的相对较低的速度在第二模式下以预热间隔运行，其中每个发动机气缸循环包括基本上绝热的压缩和膨胀 。 然后，在正常的发动机运转期间，系统可以转换成作为四冲程循环发动机的第三操作模式。 在正常操作期间可以使用不同的操作模式。 在高需求条件下，发动机可以作为传统的低效但有效的节流发动机运转，或者作为二冲程循环发动机转换成第四模式的操作。 车辆管理系统包括：第一只读存储器，用于存储与各种发动机状况相对应的发动机运行参数的固定表;以及随机存取第二存储装置，用于存储与各种发动机状况相对应的发动机运行参数表，第二表是 最初与第一张表相同。 系统响应感测到的发动机状况以修改第二表中的参数，并根据存储在第二表中的参数来控制车辆。 对随机存取存储器中的信息进行短期修改以适应感测到的发动机条件的动态变化和长期修改以补偿发动机和管理系统中相对较慢的变化。 这些修改可以在整体引擎基础上或单独的气缸的基础上。
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4.发明公开METHOD AND APPARATUS FOR PRECISION SURVEYING USING BROADCAST SATELLITE SIGNALS 失效用于使用广播卫星信号进行精确测量的方法和设备
公开(公告)号：EP0264431A1
公开(公告)日：1988-04-27
申请号：EP87903097.0
申请日：1987-04-15
发明人： HATCH, Ronald, R.
CPC分类号： G01S5/02
摘要： Procédé et appareil pour déterminer avec exactitude et précision les coordonnées de position d'un récepteur (15) situé en un endroit prédéterminé à l'aide de signaux transmis par une pluralité de satellites (13) en orbite et d'informations provenant d'un deuxième récepteur (17) situé en un endroit de référence dont les coordonées sont connues. Des mesures de la phase porteuse effectuées par les deux récepteurs sur tous les signaux d'arrivée du satellite sont incorporées dans une matrice spéciale carrée (31) de filtrage d'informations, ce qui permet de mesurer de manière pratique le bruit de phase des horloges satellites et récepteurs, cette mesure étant utilisée pour corriger ensuite les mesures de phase. Les coordonnées de position de l'endroit inconnu sont déterminées par un processus spécial en trois étapes qui produit successivement une solution hyperbolique, une solution pseudo-distance Doppler, et une solution de couloirs résolus.
摘要翻译： 一种方法和设备，用于使用从轨道中的多个卫星（13）发射的信号和来自轨道的信息来准确和准确地确定接收机（15）在预定位置处的位置坐标， 第二接收器（17）位于坐标已知的参考位置。 由两个接收机对所有卫星到达信号进行载波相位测量，并入一个特殊的方形信息滤波矩阵（31），这使得可以方便地测量时钟的相位噪声。 卫星和接收机，这个测量被用来随后校正相位测量。 未知位置的位置坐标由特定的三步过程确定，该过程连续产生双曲线解，伪距离多普勒解和解决走廊的解决方案。
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公开(公告)号：EP0150526B1
公开(公告)日：1988-01-20
申请号：EP84201715.4
申请日：1984-11-26
发明人： Barker, Robert Leroy
CPC分类号： B63B22/003 , B64D17/38
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公开(公告)号：EP0150526A2
公开(公告)日：1985-08-07
申请号：EP84201715.4
申请日：1984-11-26
发明人： Barker, Robert Leroy
CPC分类号： B63B22/003 , B64D17/38
摘要： @ Sonobuoy parachute shroud line ends are attached to a cup mounted in and adjacent one end of the sonobuoy outer casing. A heavy ejection spring is beneath the cup for forcibly ejecting the cup outwardly from the one end of the casing. The cup is retained in the casing against the spring force by a pair of partially overlapping elongated plates each having one end releasably inserted in a circumferential slot in the outer casing, the slots being adjacent the casing one end and diametrically opposed. The upper plate is in retentive contact near the other of its ends by a first retainer rod pivoted at one of its ends to the cup bottom surface. The first rod contacts the upper plate near the pivoted rod end and is in retentive contact near its other end with a second retainer rod pivoted at one of its ends to the cup bottom surface. The second rod contacts near its pivoted end the first rod and is in retentive contact at its other end with a one shot spring motor driven pin. The location of the points of contact between the plates, the upper plate and the first rod, the first and second rods and the pin and the second rod provide lever arms that result in a very high mechanical advantage between the retaining force of the pin on the second rod and the ejection spring force. Upon ejection, the cup, parachute, and shroud lines are ejected and other sonobuoy components are released from the outer casing.
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公开(公告)号：EP0478069A1
公开(公告)日：1992-04-01
申请号：EP91202403.1
申请日：1991-09-18
发明人： Richeson, William E.
CPC分类号： G01D5/2412 , G01F23/263
摘要： In a preferred embodiment, a capacitive sensor element which includes a metal plate which is flat and smooth and hard-coated with a dielectric material, such as an oxide. The dielectric surface slidingly contacts a smooth metal plate, such as hardened steel, with the capacitance of the sensor element varying with the area of contact of the two plates. Aluminum oxide provides an excellent dielectric surface. The sensor may be constructed in a number of configurations and can be ruggedly constructed for harsh environments. In a further embodiment, a metal member having a hard-coated dielectric material on the surface thereof is partially immersed in a conductive liquid to form a capacitive liquid level sensing element.
摘要翻译： 在优选实施例中，电容式传感器元件包括金属板，该金属板是平坦光滑的，并且被诸如氧化物之类的介电材料硬涂覆。 电介质表面滑动地接触平滑的金属板，例如硬化钢，传感器元件的电容随两个板的接触面积而变化。 氧化铝提供优良的电介质表面。 传感器可以构造成多种构造，并且可以坚固地构造用于恶劣的环境。 在另一个实施例中，在其表面上具有硬涂覆电介质材料的金属部件被部分地浸没在导电液体中以形成电容式液位传感元件。
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8.发明公开Method and apparatus for automatic flux-gate compass calibration 失效Methode und Apparat zur automatischen Kalibrierung eines Flussschaltkompasses。
公开(公告)号：EP0382290A1
公开(公告)日：1990-08-16
申请号：EP90200226.0
申请日：1990-01-31
发明人： Wanous, Richard
IPC分类号： G01C17/38
CPC分类号： G01C17/38
摘要： A system for automatically compensating for changes in permanent magnetism in a vehicle in which a flux-gate compass is installed. Calibration is initially performed by rotating the vehicle through a full circle and determining from the flux-gate outputs the degree of distortion suffered by an ideally circular performance characteristic. Subsequent flux-gate readings are compensated in accordance with parameters generated during calibration. Parameters relating to offset or displacement of the characteristic are automatically and continually updated to compensate for changes in permanent magnetism of the vehicle, such as might be caused by loading or unloading the vehicle.
摘要翻译： 一种用于自动补偿其中安装有磁通门罗盘的车辆中的永磁变化的系统。 最初通过使车辆旋转整圈进行校准，并从磁通门输出确定由理想循环性能特征所遭受的失真程度。 随后的磁通门读数根据校准期间生成的参数进行补偿。 与特征的偏移或位移有关的参数将被自动并持续更新，以补偿车辆的永久性变化，例如可能由于装载或卸载车辆而引起的。
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公开(公告)号：EP0316043A3
公开(公告)日：1989-11-15
申请号：EP88202488.8
申请日：1988-11-08
发明人： Webb, George
摘要： The invention relates to a safe and arm mechanism for an exploding projectile to be fired from a rifled gun. The projectile first experiences axial and angular acceleration which moves a setback ball (11) to initially arm the mechanism. A third projectile parameter, angular velocity, functions to lock the ball in the armed position. During projectile flight, a spin actuated escapement mechanism moves toward a fully armed position, but may be precluded from reaching that fully armed position by a command arm arrangement. The projectile is then fully armed when a command arm signal releases the arrangement and the escapement mechanism is allowed to complete its motion to the fully armed position. When the projectile strikes a target, it experiences axial deceleration which moves a contact ball (17) partway to a detonating position. After the projectile passes through the target surface and into a void, e.g., into the hull of a ship, the deceleration ceases and the contact (17) ball moves under centrifugal force to a final position to detonate the projectile. Movement of the setback ball (11) functions as one primary safety lock to preclude operation of the escapement mechanism. At rest, the ball (11) is positioned above a leaf spring. Axial and angular acceleration of the projectile depresses the spring (19) and the ball moves to another position. This motion releases the rotor (13) of the escapement mechanism. The rotor (13) is weighted so that rotation of the projectile causes it to tend to rotate. The cam follower of an electronically controlled actuator engages a cam track in the rotor and limits this rotation in stages from the fail safe position to an intermediate position where a command arming signal is required before the rotor (13) moves into the fully armed position. In the fully armed position, a contact ball (17) is brought into alignment with a switch housing. When the projectile strikes a target and decelerates, the contact (17) ball moves upwardly into an annular region and when that deceleration ceases and the projectile is in a void such as inside a ship's hull, the ball (17) moves rearwardly and outwardly in the annular area connecting a pair of contacts and detonating the device some distance beyond the point of impact.
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