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1. 发明授权

US06662703B2 Open bolt firing mechanism for programmable cartridges 失效
标题翻译：打开可编程墨盒的螺栓触发机构
公开(公告)号：US06662703B2
公开(公告)日：2003-12-16
申请号：US10104053
申请日：2002-03-25
申请人： Kevin Sullivan
发明人： Kevin Sullivan
IPC分类号： F42C1704
CPC分类号： F42C17/04 , F41A3/54 , F41A9/40
摘要： An open bolt firing mechanism for programmable cartridges. The mechanism includes a firing bolt having a bolt face configured to engage a programmable cartridge and force the programmable cartridge toward a barrel of the weapon. The mechanism also includes a cradle connected to the bolt for holding the programmable cartridge in a position adjacent to the bolt. The cradle stabilizes the cartridge so that fusing information may be transferred to the programmable cartridge.
摘要翻译：用于可编程墨盒的开放螺栓触发机构。该机构包括具有螺栓面的触发螺栓，所述螺栓面配置成接合可编程盒，并将可编程盒朝向武器的枪管强制。该机构还包括连接到螺栓的支架，用于将可编程盒保持在与螺栓相邻的位置。托架稳定墨盒，以便可以将定影信息传输到可编程墨盒。

2. 发明授权

US06823767B2 Method for fuze-timing an ammunition unit, and fuze-timable ammunition unit 有权
标题翻译：引导弹药单位的引信方法和引燃弹药单位
公开(公告)号：US06823767B2
公开(公告)日：2004-11-30
申请号：US10278989
申请日：2002-10-24
申请人： Karl-Ulrich Vornfett , Jürgen Voss
发明人： Karl-Ulrich Vornfett , Jürgen Voss
IPC分类号： F42C1704
CPC分类号： F42C17/04
摘要： The invention is based on the concept of providing a digital data transmission of the fuze-timing data into a fuze-timable ammunition unit, for example with an HDB-3 (High-Density Bipolar) transmission code and voltage modulation. As is known from asynchronous data transmission, a start byte and a stop byte are respectively positioned in front of and behind the HDB-3 code, and are therefore components of thee fuze-timing data. The fuze-timing time is transmitted numerically as a data byte between the start and stop bytes. Accordingly, the ammunition unit (3) includes fuze-timing electronics (4), which comprise a (voltage) demodulator (30), a (current) modulator (31) and a microprocessor (32) having an RC-oscillator cycle counter (32.1), an RC oscillator (33), a fuze-timing counter (34) and an actuator end stage (36). A firing sensor (35) serves as the fuze-timing-time triggering element at the start of the flight phase. Additionally, operating data of the oscillator (33) are corrected, so simple RC oscillators can be used.
摘要翻译：本发明基于将引信定时数据的数字数据传输提供到例如具有HDB-3（高密度双极）传输码和电压调制的引信时间弹药单元的概念。如从异步数据传输中已知的，起始字节和停止字节分别位于HDB-3代码的前面和后面，并且因此是引信定时数据的组成部分。引信定时时间作为起始和停止字节之间的数据字节数字地传送。因此，弹药单元（3）包括引信定时电子器件（4），其包括（电压）解调器（30），（电流）调制器（31）和具有RC振荡器周期计数器（32.1），RC振荡器（33），引信定时计数器（34）和致动器端级（36）的微处理器（32）。点火传感器（35）在飞行阶段开始时用作引信时间触发元件。此外，振荡器（33）的操作数据被校正，因此可以使用简单的RC振荡器。

3. 发明授权

US06666123B1 Method and apparatus for energy and data retention in a guided projectile 有权
标题翻译：在引导弹体中能量和数据保留的方法和装置
公开(公告)号：US06666123B1
公开(公告)日：2003-12-23
申请号：US10158741
申请日：2002-05-30
申请人： Tovan L. Adams , Eric C. Maugans , W. Norman Lange, Jr.
发明人： Tovan L. Adams , Eric C. Maugans , W. Norman Lange, Jr.
IPC分类号： F42C1704
CPC分类号： F42C17/04 , F42C15/40
摘要： Energy (110) and mission data (108) for a guided projectile are transferred from a projectile setter (102) over an inductive interface (118). The projectile may include energy storage element (114) to store the energy and a data storage element (112) to store the mission data. Precision GPS clock circuitry (316) of the projectile may receive power from a capacitive energy storage (304) element during projectile loading until a flight battery (320) is activated. In one embodiment, the capacitive energy storage element (304) includes at least one super capacitor (322) and a gun-hardened capacitor (324). The clock circuitry (316) may receive power from the gun-hardened capacitor (324) if the super capacitor (322) fails during the launching operation. The capacitive energy storage element (304) may include one-way energy transfer elements (326) coupled between the super capacitor (322) and the gun-hardened capacitor (324). A regulator (312) may be coupled to an output of the capacitive storage element (304) to regulate an input voltage to the clock circuitry (316).
摘要翻译：用于引导弹丸的能量（110）和任务数据（108）通过感应接口（118）从射弹设置器（102）传送。射弹可以包括用于存储能量的能量存储元件（114）和用于存储任务数据的数据存储元件（112）。抛射体的精密GPS时钟电路（316）可以在弹丸加载期间从电容性能量存储（304）元件接收电力，直到飞行电池（320）被激活。在一个实施例中，电容性能量存储元件（304）包括至少一个超级电容器（322）和喷枪硬化电容器（324）。如果超级电容器（322）在发射操作期间失效，则时钟电路（316）可以从硬化电容器（324）接收电力。电容性能量存储元件（304）可以包括耦合在超级电容器（322）和喷枪硬化电容器（324）之间的单向能量传递元件（326）。调节器（312）可以耦合到电容性存储元件（304）的输出端，以调节到时钟电路（316）的输入电压。

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