专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

81. 发明授权

US1791606A Setting electric projectile fuses 失效
标题翻译：设置电抛丸保险丝
公开(公告)号：US1791606A
公开(公告)日：1931-02-10
申请号：US27046528
申请日：1928-04-16
申请人： RHEINISCHE METALLW & MASCHF
发明人： HERBERT RUHLEMANN
IPC分类号： F42C11/00 , F42C11/04 , F42C11/06 , F42C17/04
CPC分类号： F42C11/00 , F42C11/04 , F42C11/06 , F42C17/04

82. 发明授权

US1711693A Electric fuse for projectiles 失效
标题翻译：射弹电熔丝
公开(公告)号：US1711693A
公开(公告)日：1929-05-07
申请号：US24493228
申请日：1928-01-06
申请人： RHEINISCHE METALLW & MASCHF
发明人： HERBERT RUHLEMANN
IPC分类号： F42C11/00 , F42C11/04 , F42C11/06 , F42C17/04
CPC分类号： F42C11/06 , F42C11/00 , F42C11/04 , F42C17/04

83. 发明授权

US10202209B2 Launch vehicle and system and method for economically efficient launch thereof 有权
公开(公告)号：US10202209B2
公开(公告)日：2019-02-12
申请号：US15852815
申请日：2017-12-22
申请人： 8 RIVERS CAPITAL, LLC
发明人： Miles R. Palmer
IPC分类号： B64G1/40 , B64G1/00 , F42B6/00 , F41A1/04 , F42B15/10 , F42B15/12 , F41B6/00 , F02K9/95 , F41F1/00 , F42C11/00 , F41F3/04 , F42C11/04
摘要： The present disclosure relates to a launch system, a launch vehicle for use with the launch system, and methods of launching a payload utilizing the launch vehicle and/or the launch system. The disclosure can provide for delivery of the payload at a terrestrial location, an Earth orbital location, or an extraorbital location. The launch vehicle can comprise a payload, a propellant tank, an electrical heater wherein propellant, such as a light gas (e.g., hydrogen) is electrically heated to significantly high temperatures, an exhaust nozzle from which the heated propellant expands to provide an exhaust velocity of, for example, 7-16 km/sec, and sliding electrical contacts in electrical connection with the electrical heater. The launch vehicle can be utilized with the launch system, which can further comprise a launch tube formed of concentric electrically conductive tubes, as well as an electrical energy source, such as a battery bank and associated inductor.

84. 发明申请

US20170158356A1 LAUNCH VEHICLE AND SYSTEM AND METHOD FOR ECONOMICALLY EFFICIENT LAUNCH THEREOF 审中-公开
公开(公告)号：US20170158356A1
公开(公告)日：2017-06-08
申请号：US15440552
申请日：2017-02-23
申请人： 8 Rivers Capital, LLC
发明人： Miles R. Palmer , Glenn William Brown, JR.
IPC分类号： B64G1/00 , F42C11/00 , F41F3/04 , F42C11/04 , B64G1/40 , F42B15/10
摘要： The present disclosure relates to a launch system, a launch vehicle for use with the launch system, and methods of launching a payload utilizing the launch vehicle and/or the launch system. The disclosure can provide for delivery of the payload at a terrestrial location, an Earth orbital location, or an extraorbital location. The launch vehicle can comprise a payload, a propellant tank, an electrical heater wherein propellant, such as a light gas (e.g., hydrogen) is electrically heated to significantly high temperatures, and an exhaust nozzle from which the heated propellant expands to provide an exhaust velocity of, for example, 7-16 km/sec. The launch vehicle can be utilized with the launch system, which can further comprise a launch tube formed of at least one tube, which can be electrically conductive and which can be combined with at least one insulator tube. An electrical energy source, such as a battery bank and associated inductor, can be provided.

85. 发明授权

US09279645B2 Electronic detonator 有权
标题翻译：电子雷管
公开(公告)号：US09279645B2
公开(公告)日：2016-03-08
申请号：US14381970
申请日：2013-01-09
申请人： DETNET SOUTH AFRICA (PTY) LTD
发明人： Craig Charles Schlenter , Herman Van Der Walt
IPC分类号： F42B3/10 , F42B3/12 , F42C11/00 , F42C11/04
CPC分类号： F42B3/10 , F42B3/122 , F42C11/008 , F42C11/04
摘要： An electronic detonator (10) which includes a housing (12) which contains an explosive charge (18), an initiating element (20), a control circuit (24), at least one coil (32) having a plurality of windings (30) in a tubular configuration, and a magnet (40) wherein passage of the magnet (40) through the coil (32) creates voltage to which the control circuit (24) is responsive, and a connector (46) for connecting a shock tube (48) to the housing (12).
摘要翻译：一种电子雷管（10），包括容纳爆炸物（18）的壳体（12），起动元件（20），控制电路（24），至少一个线圈（32），其具有多个绕组）和磁体（40），其中磁体（40）通过线圈（32）的通过产生响应于控制电路（24）的电压;以及连接器（46），用于连接冲击管（48）连接到壳体（12）。

86. 发明申请

US20120180681A1 Inertially Operated Electrical Initiation Methods 有权
标题翻译：惯性电启动方法
公开(公告)号：US20120180681A1
公开(公告)日：2012-07-19
申请号：US13355495
申请日：2012-01-21
申请人： Jahangir S. Rastegar
发明人： Jahangir S. Rastegar
IPC分类号： F42C11/04 , F42C11/02 , F42C11/00
CPC分类号： F42C11/02 , F42C15/24 , F42C15/40
摘要： A method for electrically initiating an inertial igniter for a munition. The method including: generating a voltage over a duration of an acceleration of the munition; directing a portion of a charge resulting from the voltage and duration to an electrical storage device on board the munition; determining by a circuit, whether the acceleration experienced by the munition is an all-fire condition based on both the voltage and duration of voltage generation and a predetermined accumulated voltage of the electrical storage device; and providing the predetermined accumulated voltage to an initiator when the all-fire condition is determined.
摘要翻译：一种用于电动启动用于弹药的惯性点火器的方法。该方法包括：在弹药的加速持续时间内产生电压; 将由电压和持续时间引起的一部分电荷引导到弹药上的电存储装置; 通过电路确定弹药所经历的加速度是否是基于电压产生的电压和持续时间以及蓄电装置的预定累积电压的全火状态; 以及当确定全火条件时，向起动器提供预定的累积电压。

87. 发明申请

US20100236440A1 Methods and Apparatus For Mechanical Reserve Power Sources For Gun-Fired Munitions, Mortars, and Gravity Dropped Weapons 有权
标题翻译：枪炮，迫击炮和重力下落武器机械储备电源的方法和装置
公开(公告)号：US20100236440A1
公开(公告)日：2010-09-23
申请号：US12407763
申请日：2009-03-19
申请人： Jahangir S. Rastegar
发明人： Jahangir S. Rastegar
IPC分类号： F42C11/04 , F02B63/04 , F42C11/00 , F42C11/02
CPC分类号： F42C15/40 , F42C11/008 , F42C11/02
摘要： A power source including: a power generation device; a mass-spring unit having a mass and an elastic element operatively connected to the power generation device; and one or more retention fingers releasably engaged with the mass-spring unit for retaining the mass-spring unit in a position such that potential energy is stored therein and for releasing the potential energy upon occurrence of an event to generate electrical energy in the power generation device, the one or more retention fingers having a first end fixed at a base and a second end releasably engaged with the mass-spring unit. The occurrence of the event can be one or more of an acceleration and spinning of the base. Also disclosed is a power source having one or more retention fingers that are slidable with respect to a base such that the engagement of the first end is released upon a spinning of the base.
摘要翻译：一种电源，包括：发电装置; 质量弹簧单元，其具有可操作地连接到发电装置的质量和弹性元件; 以及与质量弹簧单元可释放地接合的一个或多个保持爪，用于将质量弹簧单元保持在使得势能存储在其中的位置，并且在发生事件时释放势能以在发电中产生电能所述一个或多个保持指状物具有固定在基部的第一端和与所述质量弹簧单元可释放地接合的第二端。事件的发生可以是基座的加速和旋转中的一个或多个。还公开了一种具有一个或多个保持指状物的电源，其可相对于基座滑动，使得第一端部的接合在基部旋转时释放。

88. 发明申请

US20080115686A1 METHODS AND APPARATUSES FOR PROJECTILE FUZE SETBACK GENERATOR POWER SOURCE AND PROJECTILES INCLUDING SAME 有权
标题翻译：用于投影式燃料发电机电源的方法和装置以及包括它们的项目
公开(公告)号：US20080115686A1
公开(公告)日：2008-05-22
申请号：US11560991
申请日：2006-11-17
申请人： Scott D. Crist , Mark J. Tomes , Hossein Aliaghai , Erik J. Elmer
发明人： Scott D. Crist , Mark J. Tomes , Hossein Aliaghai , Erik J. Elmer
IPC分类号： F42C11/04 , F42B12/20 , H02K35/02 , H02K7/00 , H02J7/14
CPC分类号： F42C15/24 , F42C11/04 , H02K35/02
摘要： Projectile fuze setback generator power source apparatuses and methods of use and manufacture are disclosed. An explosive projectile contains a fuze with a setback generator and associated fuze electronics. Upon initiation of projectile launch, the setback generator produces a voltage for use by the fuze electronics during flight. The setback generator includes a magnet maintained in place within a surrounding coil by a fastener. When a projectile is fired, rapid acceleration thereof causes the fastener to break and the magnet to be displaced longitudinally within the surrounding coil, which decreases the magnetic field and induces a current in the surrounding coil. The induced current produces a voltage that is stored in a capacitor operably coupled to the setback generators which then is used to power the fuze electronics during flight.
摘要翻译：射弹引信发电机电源装置及使用及制造方法已公开。爆炸性弹药包含一个带有挫折发生器和相关引信电子的引信。在发射弹射器时，挫折发生器在飞行期间产生一个供引信电子使用的电压。挫折发生器包括通过紧固件在周围线圈内保持在适当位置的磁体。当射弹发射时，其快速加速导致紧固件断裂，并且磁体在周围线圈内纵向移位，这减小了磁场并引起了周围线圈中的电流。感应电流产生存储在可操作地耦合到遏制发生器的电容器中的电压，其随后用于在飞行期间为引信电子器件供电。

89. 发明授权

US4286521A Device actuated electrically to trigger a mechanical percussion detonator 失效
标题翻译：电子装置致动以触发机械敲击雷管
公开(公告)号：US4286521A
公开(公告)日：1981-09-01
申请号：US60334
申请日：1979-07-25
申请人： Joseph Marer
发明人： Joseph Marer
IPC分类号： F42C11/04 , F42B3/18 , F42C15/16 , F42C15/31 , F42C15/40 , F42C19/06
CPC分类号： F42B3/18 , F42C15/31
摘要： A device actuated electrically for triggering a mechanical percussion detonator, comprising a tubular container wherein is housed a striker with a percussion pin, an explosive cap actuated electrically and held secure by a cover and a detonator holder containing a mechanical percussion detonator that can be installed or moved afterwards opposite the striker in order to avoid any untimely explosion of the detonator.
摘要翻译：一种用于触发机械敲击雷管的装置，其包括管状容器，其中容纳有具有冲击销的撞针，通过盖电动和保持固定的爆炸帽，以及包含可安装的机械打击式雷管的雷管保持器之后在前锋的对面移动，以避免雷管的任何不合时宜的爆炸。

90. 发明授权

US4204475A Arming-safing system for airborne weapons 失效
标题翻译：机载武器装甲安全系统
公开(公告)号：US4204475A
公开(公告)日：1980-05-27
申请号：US823243
申请日：1969-04-29
申请人： Ronald J. Fowler
发明人： Ronald J. Fowler
IPC分类号： F42C15/40 , F42C15/12 , F42C11/04 , F42C13/04
CPC分类号： F42C15/40
摘要： The system of the present invention basically consists of a detector unit unted in each bomb or airborne weapon and operable upon interception of a signal emitted by an aircraft-mounted source. The required signal for arming is present only in a well defined zone below the aircraft and only in response to pilot command during weapon release. The signal consists of mechanically modulated beam of high-energy photons (gamma rays) emitted by a radioisotope source on the aircraft. The weapon must fall well below the aircraft to see the signal. Geiger-Mueller tubes are used for radiation detectors and the resulting signal is processed to initiate the arming or fuzing sequence. Power for the operation of the detector and associated electronics is transferred through the metallic covering of the weapon by means of a split-core transformer at the time of release. The power transferred is capable of operating the unit for the length of time it would normally take the weapon to fall through the signal zone; after which the weapon returns to a dormant, safe, state if no arming signal has been received.
摘要翻译：本发明的系统基本上由安装在每个炸弹或机载武器中的检测器单元组成，并且可以在拦截由飞机安装的源发射的信号时操作。所需的布防信号仅存在于飞机下方明确定义的区域内，只能在武器释放期间响应飞行员指令。信号由飞机上的放射性同位素源发射的高能光子（γ射线）的机械调制光束组成。武器必须落在飞机下方才能看到信号。 Geiger-Mueller管用于辐射检测器，并且所得到的信号被处理以启动布防或补偿序列。检测器和相关电子设备的操作功能在释放时通过分裂式变压器通过武器的金属覆盖物传递。传输的电力能够在通常通过武器掉落在信号区域的时间长度上操作该装置; 之后如果没有接收到布防信号，武器返回休眠状态。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式