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公开(公告)号：US11988172B2
公开(公告)日：2024-05-21
申请号：US16952928
申请日：2020-11-19
申请人： Raytheon Company
发明人： Shawn Coffee , Saifur Ahmed , Steven D. Jacob , Thomas K. Harward
CPC分类号： F02K9/94 , F02K9/95 , F42B15/01 , F42C11/065 , F42C15/40
摘要： An ignition safety device (ISD) used in an ignition system of a missile is configured to selectively control the ignition of two or more pulses or stages of a rocket motor propulsion system, based on a flight profile mode selection of a flight velocity mode, in which the missile is configured to travel at an optimized flight velocity, or a flight distance mode, in which the missile is configured to travel an optimized flight distance. The ISD is configured to selectively ignite the pulses or stages substantially simultaneously upon selection of the flight velocity mode, or in a delayed sequential manner upon selection of the flight distance mode. The ISD is also configured to selectively inhibit the delayed sequential ignition of the pulses or stages in the event of incidental ground or water impact of the missile after ignition of the primary pulse or stage.
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公开(公告)号：US11913762B1
公开(公告)日：2024-02-27
申请号：US17571685
申请日：2022-01-10
摘要： A networked electronic ordnance system is provided. The system includes a first plurality of pyrotechnic devices connected to a first network bus. The system further includes a first bus controller connected to the first network bus. The system further includes a second plurality of pyrotechnic devices connected to a second network bus. The system further includes a second bus controller connected to the second network bus. The system further includes a bus interface circuit connected to the first bus controller by a first electrical connection and connected to the second bus controller by a second electrical connection.
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公开(公告)号：US20230324158A1
公开(公告)日：2023-10-12
申请号：US18333456
申请日：2023-06-12
申请人： JD Pharma, LLC
发明人： Joseph Dan Palo
IPC分类号： F42C15/00 , F42C19/08 , F42C15/42 , F42C19/04 , F42C19/10 , F41A17/08 , F42C15/40 , C06B21/00
CPC分类号： F42C15/00 , F42C19/0823 , F42C15/42 , F42C19/04 , F42C19/10 , F42C19/08 , F41A17/08 , F42C15/40 , C06B21/0091 , F42B5/02
摘要： Various types of structures, along with associated systems, are disclosed herein and configured for responding to an energy wave for changing a state of a mechanism to which said structures are operatively coupled. In at least one embodiment, the structure provides a material selectively changeable upon exposure to the energy wave to cause at least a portion of the material to mechanically degrade from a first state to a second state. When the material is in the first state, the material forms a mechanical or electrical link with the mechanism such that a force or an electrical current can be transmitted through the structure. When the material is in the second state, degradation of at least the portion of the material disrupts the mechanical or electrical link and inhibits transmission of the force or electrical current through the structure.
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公开(公告)号：US11604054B2
公开(公告)日：2023-03-14
申请号：US17422041
申请日：2020-01-24
发明人： Michiel Jacobus Kruger , Daniel Auguste Maurissens , Andre Louis Koekemoer , Albertus Abraham Labuschagne
摘要： A detonator which is initiated by a shock tube event which is validated if a processor determines that a fusible link was not fused by a shock tube event at a predetermined time interval before light generated by the shock tube event is detected.
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公开(公告)号：US20220290959A1
公开(公告)日：2022-09-15
申请号：US17753340
申请日：2020-08-13
申请人： BAE SYSTEMS plc
摘要： The present invention relates to the control of weapons, particularly weapons which are controlled via a communications link, possibly at some distance from the weapon's location. The invention is to an apparatus comprising safety-critical and non-safety-critical functional parts wherein at least one of a plurality of safety-critical functional parts is only connected to at least one other of the plurality of safety-critical functional parts.
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公开(公告)号：US11385007B2
公开(公告)日：2022-07-12
申请号：US16865705
申请日：2020-05-04
发明人： Michael J. Balk , Larry G. Linde
IPC分类号： F41A17/08 , H04B7/185 , F42B22/24 , F42B23/24 , F41H13/00 , H04W88/16 , G05D1/00 , F41G9/00 , F41G3/32 , F42B23/00 , F42C15/40 , F42C15/42 , F41A17/06 , B64C39/02 , F41H11/08
摘要： An area denial system may be operationally placed with communication latency compensation. The area denial system may include a plurality of munitions, one or more sensor devices, and a command and control unit, networked together and having a command and control latency for communication between the command and control unit and the remainder of the area denial system. Latency compensation may include determining a first target position, determining a first predicted position area for the target using the command and control latency and the first target position, receiving an authorization to arm one or more of the munitions, determining a second target position, and determining that the second target position is outside a threshold distance from a first authorized munition of the one or more authorized munitions, and in response, de-authorizing the first authorized munition.
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公开(公告)号：US11309880B2
公开(公告)日：2022-04-19
申请号：US15849648
申请日：2017-12-20
申请人： The Boeing Company
IPC分类号： H03K17/082 , H02H3/10 , F41G7/00 , F42C15/40 , F42D1/05
摘要： Embodiments described herein provides a low-complexity solution and current protection for a current driver that provide current pulses to pyrotechnic initiators. The current drivers include current limiters that prevent high current transients during a current pulse. Further, a duration of the current pulse is controlled based on a thermal limit of the current driver to prevent thermal damage to the current driver. One embodiment comprises an apparatus that includes a control circuit and a current driver. The current driver is electrically couplable to a pyrotechnic initiator. The current driver includes a power switch circuit electrically coupled to a supply rail that supplies a current to a high side of the pyrotechnic initiator in response to receiving a drive signal from the control circuit.
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公开(公告)号：US20220065604A1
公开(公告)日：2022-03-03
申请号：US17413141
申请日：2019-12-17
申请人： BAE SYSTEMS plc
摘要： According to an aspect of the invention, there is provided a fuze arming system for a submunition, comprising: a first stage, arranged to detect launch of the submunition and its associated carrier; a second stage, arranged to detect expulsion of the submunition from the carrier, and to at least partially arm a submunition fuze based on such detection; wherein the second stage is unable to at least partially arm the submunition fuze without the first stage detecting launch of the submunition and its associated carrier.
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公开(公告)号：US11220359B1
公开(公告)日：2022-01-11
申请号：US16400912
申请日：2019-05-01
摘要： A networked electronic ordnance system is provided. The system includes a first plurality of pyrotechnic devices connected to a first network bus. The system further includes a first bus controller connected to the first network bus. The system further includes a second plurality of pyrotechnic devices connected to a second network bus. The system further includes a second bus controller connected to the second network bus. The system further includes a bus interface circuit connected to the first bus controller by a first electrical connection and connected to the second bus controller by a second electrical connection.
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公开(公告)号：US20200025543A1
公开(公告)日：2020-01-23
申请号：US16434697
申请日：2019-06-07
发明人： KARL KAUTZSCH
摘要： A device produces an arming criterion for a fuze for a partly spinning munition. The munition has a first part which spins and a second part without or with little spin during flight of the munition. The device includes a sensor for outputting a characteristic variable for a relative rotation between the first part and the second part and a control unit for producing the arming criterion when the characteristic variable fulfils a flying criterion. The fuze for the partly spinning munition, which has at least one arming criterion, includes the device for providing the arming criterion or one of the arming criteria. The partly spinning munition includes the fuze with the device.
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