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    • 71. 发明申请
    • METHOD AND DEVICE FOR PROGRAMMING A PROJECTILE
    • 用于编程项目的方法和装置
    • US20140007760A1
    • 2014-01-09
    • US13563803
    • 2012-08-01
    • Henry Roger FRICK
    • Henry Roger FRICK
    • F42C11/06F41G9/00
    • F42C11/065F41A21/32F41G9/00F42C11/008F42C17/04G01P3/665
    • An inductive or capacitative programming of a projectile is disclosed. A waveguide is used for the programming, the electromagnetic field being concentrated in the waveguide. The used programming unit includes at least one waveguide which is preferable located and/or integrated in the region of the muzzle, for example in front of the muzzle brake. A transmission coupler for the transmission is fed by a signal generator. The information relating to the projectile is modulated to the carrier frequency in the modulator. A reception coupler integrated on/in the projectile is electrically interconnected to a store or processor in the projectile. The reception coupler receives the modulated signal and transmits it to the processor which is where the eventual programming takes place.
    • 公开了一种对弹丸的感性或电容性编程。 波导用于编程,电磁场集中在波导中。 所使用的编程单元包括至少一个波导,其优选位于和/或集成在枪口的区域中,例如在枪口制动器的前面。 用于传输的传输耦合器由信号发生器馈送。 与射弹相关的信息调制到调制器的载波频率。 集成在射弹上的接收耦合器与射弹中的存储或处理器电互连。 接收耦合器接收调制信号并将其发送到最终编程发生的处理器。
    • 72. 发明授权
    • Programming device for the fuse of a projectile
    • 射弹保险丝编程装置
    • US08490533B2
    • 2013-07-23
    • US12897178
    • 2010-10-04
    • Laurent ReynardFabrice Sanchez
    • Laurent ReynardFabrice Sanchez
    • F42C17/00
    • F42C17/04F42C11/04
    • A programming device for the fuse of a projectile using programming coils transmitting a programming signal by induction to a receiver integral with the fuse, wherein the programming coils are integral with a substantially cylindrical wall of a corridor in which the projectile translates axially, the programming coils being made in the form of several elementary coils each encircling a ferrite core parallel to the axis of the corridor, the coils being distributed along several lines parallel to the corridor axis, the coils of one line being longitudinally staggered with respect to the coils of the neighboring line or lines.
    • 用于使用编程线圈的编程线圈的编译装置的编程装置,所述编程线圈通过感应传递编程信号到与所述保险丝集成的接收器,其中所述编程线圈与所述抛射体在轴向平移的走廊的基本上圆柱形的壁成一体,所述编程线圈 被形成为几个基本线圈的形式,每个线圈围绕平行于走廊轴线的铁氧体磁芯,线圈沿着与走廊轴线平行的几条线分布,一条线圈相对于线圈的纵向交错排列 相邻线或线。
    • 75. 发明授权
    • Simple and effective self regulating inductive power transfer system
    • 简单有效的自调节感应电力传输系统
    • US08054651B2
    • 2011-11-08
    • US12376548
    • 2007-08-03
    • Keith Graham Pollard
    • Keith Graham Pollard
    • H02M3/335
    • H02J50/12F42C11/04F42C17/04H02J5/005H02J50/80
    • An inductive power transfer system for coupling a power source to a load across an air gap is provided, including a primary unit and a secondary unit separable from the primary unit and arranged to receive power inductively from the primary unit when placed proximate thereto. The system includes a multi stage comparator for monitoring operating conditions within the secondary unit and feedback loop for transmitting a feedback signal to the primary unit when predetermined operating conditions are detected within the secondary unit. The primary unit is arranged to operate in a low power mode where power is applied to the primary winding for a minimal period during each switching cycle when no feedback signal is received and a high power mode where power is applied to the primary winding for the majority of each switching cycle when a feedback signal is received. The power transfer system functions by applying bursts of power from the primary to the secondary unit, the bursts becoming more frequent and of longer duration as the load on the secondary unit increases or the air gap increases, so as to transfer more power or maintain power as air gap losses increase. The bursts of power will also change their duration and frequency in correspondence with variations of the input power supply to the primary unit, so as to maintain the voltage regulation of the power delivered to the secondary unit.
    • 提供了一种用于将电源耦合到穿过气隙的负载的感应功率传输系统,包括主单元和与主单元可分离的次级单元,并且被布置成在靠近其处放置时从主单元感应地接收功率。 该系统包括用于监视次级单元内的操作条件的多级比较器和用于在次级单元内检测到预定操作条件时将反馈信号发送到主单元的反馈回路。 主单元被布置成在低功率模式下工作,其中在没有接收到反馈信号的每个开关周期期间对初级绕组施加功率最小的周期,并且对于大多数情况,向主绕组施加功率的高功率模式 当接收到反馈信号时,每个开关周期。 电力传输系统通过从初级单元施加突发电力来工作,当次级单元上的负载增加或气隙增加时,突发变得更加频繁,持续时间更长,从而传递更多功率或维持功率 随着气隙损失的增加。 功率的突发也将随着对主单元的输入电源的变化而改变其持续时间和频率,以便保持传送到次级单元的功率的电压调节。
    • 77. 发明授权
    • Apparatus and method for securing firearms and cartridges
    • 用于固定枪支和药筒的装置和方法
    • US07770316B2
    • 2010-08-10
    • US10537978
    • 2003-09-12
    • Herbert Meyerle
    • Herbert Meyerle
    • F41A17/00
    • F41A17/063F41A17/066F41A19/58F41A19/69F42B5/08F42C11/00F42C17/04F42C19/06F42C19/12
    • The present invention relates to a method and an apparatus for firing a cartridge for firearms or a method and an apparatus for securing the firing of a cartridge for firearms. The present invention provides a cartridge comprising a securing mechanism. In a further preferred embodiment of the present invention, the firearm reads an identity from the cartridge and calculates a cartridge password from said identity together with further data. Said cartridge password is transmitted to the cartridge. The cartridge itself decides whether it fires or not.Thus, the present invention provides apparatuses and methods with which a securing of a firearm against accidental and/or unauthorized use is provided. Furthermore, the apparatus and method according to the present invention not only allow a securing of the firearm, but also a securing of the cartridge against accidental, improper and/or unauthorized firing.
    • 本发明涉及一种用于发射用于火器的枪管的方法和装置,或者一种用于固定用于火器的枪管的发射的方法和装置。 本发明提供了一种包括固定机构的盒。 在本发明的另一优选实施例中,枪支从盒中读取身份,并从其他数据中计算出来自所述身份的盒密码。 所述墨盒密码被传送到墨盒。 墨盒本身决定是否启动。 因此,本发明提供了提供防止意外和/或未经授权使用的枪支固定的装置和方法。 此外,根据本发明的装置和方法不仅允许枪支的固定,而且还可以固定盒来防止意外,不当和/或未经授权的射击。
    • 78. 发明授权
    • Self-contained airborne smart weapon umbilical control cable
    • 自备机载智能武器脐带控制电缆
    • US06941850B1
    • 2005-09-13
    • US10754153
    • 2004-01-09
    • Roy Patrick McMahon
    • Roy Patrick McMahon
    • F41G7/00F42C15/40F42C17/04F41F3/055
    • F42C15/40F41G7/001F41G7/007F42C17/04
    • An umbilical cable for delivering electrical signals between an aircraft and a smart weapon carried by the aircraft. The umbilical cable includes cabling comprising a plurality of conductive wires, a first connector provided on one end of the cabling and configured to connect to the aircraft, and a second connector provided on the other end of the cabling and configured to connect to the smart weapon. The umbilical cable further includes an interface circuit electrically coupled between the first connector and the second connector via the plurality of conductive wires. The interface circuit is configured to receive via the first connector a non-standard combination of signals comprising at least one of data signals, control signals and power signals not receivable directly by the smart weapon to carry out operations. Moreover, the interface circuit is configured to convert the non-standard combination of signals to a set of signals receivable by the smart weapon to carry out operations, and to provide the set of receivable signals to the smart weapon via the second connector.
    • 用于在飞行器和飞机携带的智能武器之间传递电信号的脐带缆。 脐带缆包括布线,其包括多根导线,设置在布线的一端并被配置为连接到飞行器的第一连接器,以及设置在电缆的另一端并被配置成连接到智能武器的第二连接器 。 脐带缆还包括经由多根导线电连接在第一连接器和第二连接器之间的接口电路。 接口电路被配置为经由第一连接器接收包括数据信号,控制信号和智能武器直接不能接收的功率信号中的至少一个的非标准组合,以执行操作。 此外,接口电路被配置为将信号的非标准组合转换成由智能武器可接收的一组信号,以执行操作,并且经由第二连接器向智能武器提供可接收信号的集合。
    • 79. 发明申请
    • System, bypass apparatus and method of operating a store of a first predetermined type
    • 操作第一预定类型的存储器的系统,旁路装置和方法
    • US20040015273A1
    • 2004-01-22
    • US10199867
    • 2002-07-19
    • The Boeing Company
    • James V. LeonardRichard E. MeyerWilliam Joseph Ebert, JR.
    • G06F017/00
    • B64D7/00F41F3/06F41G7/007F42C17/04
    • A system for operating and releasing a store of a first predetermined type includes an aircraft adapted to control the operation of stores of a second predetermined type and a bypass apparatus. The store is releasably secured to the aircraft, and the aircraft is capable of releasing the store. The aircraft is capable of being configured such that a store of the first predetermined type is capable of operating independent of operating instructions. The bypass apparatus is carried by the aircraft and adapted to facilitate operation of the store. The bypass apparatus can store operating instructions and thereafter transmit the operating instructions into the store. As such, after the aircraft releases the store the store is capable of operating according to the operating instructions. Also, the system can include an umbilical cable disposed between the aircraft and the store. The bypass apparatus can, therefore, be disposed within the umbilical cable.
    • 用于操作和释放第一预定类型的存储的系统包括适于控制第二预定类型和旁路装置的存储的操作的飞行器。 商店可拆卸地固定在飞机上,飞机能够释放商店。 该飞机能够被配置成使得第一预定类型的存储器能够独立于操作指令进行操作。 旁路装置由飞行器承载并适于促进商店的操作。 旁路装置可以存储操作指令,然后将操作指令发送到商店。 因此,在飞机释放商店之后,商店能够根据操作说明书进行操作。 此外,系统可以包括设置在飞行器和商店之间的脐带缆。 因此,旁路装置可以设置在脐带缆内。
    • 80. 发明授权
    • Method and apparatus for energy and data retention in a guided projectile
    • 在引导弹体中能量和数据保留的方法和装置
    • US06666123B1
    • 2003-12-23
    • US10158741
    • 2002-05-30
    • Tovan L. AdamsEric C. MaugansW. Norman Lange, Jr.
    • Tovan L. AdamsEric C. MaugansW. Norman Lange, Jr.
    • F42C1704
    • F42C17/04F42C15/40
    • 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).
    • 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。