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81. 发明申请

WO98042170A1 CIRCULAR STRIPLINE PACKAGE INCORPORATING A LOW NOISE AMPLIFIER 审中-公开
标题翻译：包含低噪声放大器的圆形条带包装
公开(公告)号：WO98042170A1
公开(公告)日：1998-09-24
申请号：PCT/US1998/004921
申请日：1998-03-12
IPC分类号： H05K9/00 , F42B15/01 , H01L20060101 , H01P5/08 , H03F3/00 , H03F3/19 , H03F3/60 , H04B1/10 , H05K20060101 , H05K5/00
CPC分类号： H01L23/66 , H01L2223/6644 , H01L2924/0002 , H01L2924/00
摘要： A circular low noise amplifier package (10) having an X-band MMIC low noise amplifier (16) disposed therein, that may be preferably used with an existing stripline receiver board (11) employed in a missile. The package (10) has three input/output ports symmetrically located around the package (10), including DC bias, RF input, and RF output ports. The package (10) mounts directly into the stripline receiver board (11) as a drop-in replacement for an isolator used in the existing stripline receiver board (11). The circular low noise amplifier package (10) having a top cover (12), an upper RF gasket (13), a package lid (14), a hermetic low noise amplifier module (15) containing a low noise amplifier chip (16), a lower RF gasket (17), and a bottom cover (18). The amplifier module (15) has feedthrough pins (21) that extend through the outer wall thereof and couple to the low noise amplifier chip (16). The top and bottom covers (12, 18) are used to secure the amplifier package (10) to the stripline receiver board (11). The upper and lower RF gaskets (13, 17) aid in improving an RF ground. The package lid (14) is seam sealed to the amplifier module (15) to hermetically seal the entire package (10).
摘要翻译：具有设置在其中的X波段MMIC低噪声放大器（16）的圆形低噪声放大器封装（10），其可优选地与在导弹中使用的现有带状线接收板（11）一起使用。封装（10）具有对称地位于封装（10）周围的三个输入/输出端口，包括DC偏置，RF输入和RF输出端口。封装（10）直接安装在带状线接收板（11）中，作为现有带状线接收器板（11）中使用的隔离器的替换。具有顶盖（12），上RF垫片（13），封装盖（14），包含低噪声放大器芯片（16）的封闭式低噪声放大器模块（15）的圆形低噪声放大器封装（10），下部RF垫片（17）和底盖（18）。放大器模块（15）具有穿过其外壁延伸并耦合到低噪声放大器芯片（16）的馈通引脚（21）。顶盖和底盖（12,18）用于将放大器封装（10）固定到带状线接收器板（11）。上下RF垫片（13,17）有助于改善RF接地。包装盖（14）被接缝密封到放大器模块（15）以气密地密封整个包装（10）。

82. 发明申请

WO9726550A2 DEVICE FOR SEEKING, DISCOVERING AND TRACKING AIR TARGETS 审中-公开
标题翻译：设备的搜索，发现和跟踪飞行目的地
公开(公告)号：WO9726550A2
公开(公告)日：1997-07-24
申请号：PCT/DE9700064
申请日：1997-01-16
申请人： DORNIER GMBH , OBKIRCHER BERNT
发明人： OBKIRCHER BERNT
IPC分类号： F41G7/00 , F41G7/22 , F42B15/01 , G01S3/786
CPC分类号： F41G7/007 , F41G7/2253 , F41G7/2293 , G01S3/786
摘要： Seeking, discovering and tracking flying targets by means of a missile with an i/r seeking head in a launching tube in which there is an i/r device.
摘要翻译：搜索，发现和通过用红外寻头，它位于一个发射管导弹的跟踪装置空中目标，所述的红外光学器件上发射管可用。

83. 发明申请

WO2021257031A1 A MINIATURE MISSILE SYSTEM GUIDED TO A TARGET IN DISTRIBUTED SWARMS 审中-公开
公开(公告)号：WO2021257031A1
公开(公告)日：2021-12-23
申请号：PCT/TR2021/050574
申请日：2021-06-14
申请人： ROKETSAN ROKET SANAYİİ TİCARET A. Ş.
发明人： ATEŞOĞLU, Mustafa Özgür , MUHİDDİNOĞLU, Abdullah Alp , GÖRÜR, Bilge Kaan , ALTINTAŞ, Oğuz Han
IPC分类号： F42B15/08 , F42B30/00 , F42B15/01 , F41G7/30 , G05D1/10 , F41G7/22
摘要： The present invention relates to a distributed missile system having multiple miniature missile units (n) comprising the following; an elongated body (10) with a warhead (11); a drive motor (12) fixed to the body (10); a fin (14) that is provided in the body (10) and that rotates the body (10) towards a predetermined course during the cruise by being driven with the drive motor (12) and a controller (40) connected to the drive motor (12) to control the fin (14) position. The missile system comprises at least one relative awareness sensor (30) that scans the outer periphery of the body (10) by collecting 360° environmental awareness data (v) and transmits a signal to the controller (40).

84. 发明申请

WO2021251932A1 LASER-GUIDED MINIATURE MISSILE SYSTEM FOR HYBRID THREATS 审中-公开
公开(公告)号：WO2021251932A1
公开(公告)日：2021-12-16
申请号：PCT/TR2021/050545
申请日：2021-06-07
申请人： ROKETSAN ROKET SANAYİİ TİCARET A. Ş.
发明人： ATEŞOĞLU, Mustafa Özgür , YÜKSEL, Muhammed , TEKEREK, Ali Şimşek , SEÇKİN UZEL, Öznur Cansu , MUHİDDİNOĞLU, Abdullah Alp
IPC分类号： F41G7/22 , F42B15/01
摘要： The present invention relates to a laser-guided miniature missile system comprising a launch station (70); and a miniature missile (30) that is provided in said launch station (70), that has an elongated body (32) configured such that it may be launched from a canister (10) or a launch pod (20). The inventive miniature missile system comprises; a remote control station (80) that is connected such that it communicates by means of an RF receiver/transmitter (74) of the launch station (70) accommodated on a mobile vehicle (1) and an opposite RF receiver/transmitter (82); a central controller (72) that triggers a canister (10) or a launch pod (20) such that they launch the miniature missile (30) by means of a pod control member (76) driven by determining a launch command transmitted from the control station (80) to the launch station (70); and a flight controller (38) to the which the central controller (72) is connected such that said central controller (72) ensures signal transmission in a storage mode and that is mounted on the body (32) that activates a flight motor (38) at a predetermined flight motor activation time (t2) by being configured such that it can interrupt the signal communication with the central controller (72) subsequent to a launching moment (t0).

85. 发明申请

WO2021091601A2 WING MOUNTED SEEKER 审中-公开
公开(公告)号：WO2021091601A2
公开(公告)日：2021-05-14
申请号：PCT/US2020/041920
申请日：2020-07-14
申请人： BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC.
发明人： FREY, Jr., Robert D. , AFFLECK, Maxwell L. , BATCHELDER, Jason H. , CULLEN, Joseph P. , ROBICHAUD, Matthew H.
IPC分类号： F41G7/26 , F41G7/24 , F41G7/22 , F41G7/2246 , F41G7/226 , F41G7/2293 , F42B10/60 , F42B15/01 , F42B15/105 , G01J1/0214 , G01J1/0219 , G01J1/0252 , G01J1/0407 , G01J1/0422 , G01J11/00
摘要： An optical seeker assembly having an optical detector located within the wing or canards of a precision guided munition. The optical seeker provides on-wing processing that generates low bandwidth detection data that can be easily transferred to a primary CPU located within the main body or fuselage of the precision guided munition. The on-wing processing reduces or eliminates the need for optical fibers extending between an optical wedge and an optical detector to reduce the likelihood of optical fibers from impeding in the mechanical deployment of the wing and reduces losses. The reduction or elimination of optical fibers between the optical wedge and the optical detector further enables the optical detection assembly to have a higher pixel ratio or transmitting raw data between the wedge and the detector by sending sampled detection data across a low bandwidth link to a CPU in the main body.

86. 发明申请

WO2021034424A2 METHOD AND SYSTEM FOR ELECTRONIC WARFARE OBSCURATION AND SUPPRESSION OF ENEMY DEFENSES 审中-公开
公开(公告)号：WO2021034424A2
公开(公告)日：2021-02-25
申请号：PCT/US2020/041835
申请日：2020-07-13
申请人： LEONARDO ELECTRONICS US INC.
发明人： KEEGAN, Matthew , INNES, John R.M. , REHERMANN, Steven, T.
IPC分类号： F42B12/62 , F42B15/01 , F42B15/08 , F42B10/56 , F42B12/70
摘要： An apparatus, system, and method for deployment of an electronic warfare (EW) asset are provided. The system includes a projectile launching device capable of launching a projectile round. An EW asset is detachably carried by the projectile round. A deployable parachute is attached to the EW asset, wherein the EW asset is configured to be suspended from the parachute when the EW asset is detached from the projectile round. The related method is used for suppression or obscuration of enemy counterfire radar (CFR) system by initiating an EW effect by the EW asset as the EW asset floats towards a ground surface.

87. 发明申请

WO2020025518A1 PROCÉDÉ ET DISPOSITIF DE LOCALISATION D'UN OBJET MOBILE SOUMIS À UNE DYNAMIQUE DE ROTATION SUR LUI-MÊME 审中-公开
公开(公告)号：WO2020025518A1
公开(公告)日：2020-02-06
申请号：PCT/EP2019/070315
申请日：2019-07-29
申请人： AIRBUS DEFENCE AND SPACE SAS
发明人： HENNART, Florent
IPC分类号： G01S19/25 , G01S19/47 , G01S19/26 , G01S19/14 , G01S19/49 , G01S19/24 , F42B10/26 , F42B15/01 , F41G7/22 , F41G7/30 , F41G7/34
摘要： L'invention concerne un dispositif (400) de localisation d'un objet mobile susceptible de subir une dynamique de rotation sur lui-même. Le dispositif comporte un récepteur (410) d'un système de positionnement par satellites, une centrale inertielle (420), et un module hybride de navigation (430). Le module hybride de navigation (430) est configuré pour modéliser d'une part le mouvement d'une antenne (54) du récepteur (410), et d'autre part le mouvement d'un satellite, afin d'estimer une valeur représentative de l'effet Doppler subi par le signal émis par le satellite et reçu par l'antenne. Cette valeur est communiquée à un module d'acquisition (411) du récepteur afin de faciliter une ré-acquisition du signal du satellite suite à une perte du signal provoquée par le mouvement de rotation de l'objet mobile. Le mouvement de l'antenne (54) est notamment estimé grâce à la connaissance de la distance séparant l'antenne d'un centre d'inertie de l'objet mobile.

88. 发明申请

WO2019220076A1 PAYLOAD ACTIVATION DEVICE 审中-公开
公开(公告)号：WO2019220076A1
公开(公告)日：2019-11-21
申请号：PCT/GB2019/051209
申请日：2019-05-01
申请人： BAE SYSTEMS PLC
发明人： MCARTHUR, Gordon John Victor , MILBURN, Aaron John
IPC分类号： B64D1/04 , B64D7/08 , F42B10/14 , F42B15/01 , F42B15/10 , F42C14/06 , F42C15/00 , F42C15/40 , G06F16/38
摘要： The present invention provides a payload activation device. The payload activation device comprises a camera having a fixed focal length, arranged to capture an image of an object on a platform for carrying a payload having the payload activation device, wherein when the payload is in a first position relative to the platform the image of the object is in a first focussed state and when the payload is in a second position relative to the platform the image of the object is in a second focussed state. The payload activation device also comprises a processor configured to determine whether the image of the object is in the first focussed state or the second focussed state and to cause actuation of an activation mechanism within the payload when the image of object is in the second focussed state to activate the payload. The present invention also provides a deployable payload having the payload activation device and an aircraft for carrying the deployable payload.

89. 发明申请

WO2019167333A1 無線通信システムおよび飛しょう体审中-公开
公开(公告)号：WO2019167333A1
公开(公告)日：2019-09-06
申请号：PCT/JP2018/038480
申请日：2018-10-16
申请人：三菱重工業株式会社
发明人：相馬　史人 , 小山　卓哉 , 宇田　秀信 , 梅村　武生
IPC分类号： H04B5/00 , B64D47/00 , F42B15/01 , H04B7/145 , H04W4/48
摘要：無線通信システムは、シールド室形成部と、漏洩導波路と、第１アンテナと、第１機器と、第２アンテナと、第２機器とを具備する。シールド室形成部は、シールド室としての内部空間を、無線通信を遮断する電磁波反射体で覆う。漏洩導波路は、シールド室形成部の内部に配置された第１漏洩部および第２漏洩部を備える。第１アンテナは、シールド室形成部の内部に配置されて、第１漏洩部との間で無線通信可能に構成されている。第１機器は、シールド室形成部の内部に配置されて、第１アンテナを有している。第２アンテナは、シールド室形成部の内部に配置されて、第２漏洩部との間で無線通信可能に構成されている。第２機器は、シールド室形成部の内部に配置されて、第２アンテナを有している。第１機器および第２機器は、相互間で、かつ、漏洩導波路を介して直接的な双方向無線通信を行う。

90. 发明申请

WO2018002580A1 NOSE CONE COMPRISING ELECTRONIC CIRCUIT BOARDS ARRANGED RADIALLY 审中-公开
标题翻译：包括电子电路板在内的鼻锥体
公开(公告)号：WO2018002580A1
公开(公告)日：2018-01-04
申请号：PCT/GB2017/051759
申请日：2017-06-16
申请人： BAE SYSTEMS PLC
发明人： MOORE, Gary, Roy , BICKNELL, Paul
IPC分类号： F42B15/01 , F42B10/46 , F42B30/00 , G06F15/78 , G06F15/80 , H05K7/14 , H05K7/20 , F42B19/00
CPC分类号： F42B15/01 , F42B10/46 , F42B19/005 , F42B30/006 , H05K1/14 , H05K1/141 , H05K3/366 , H05K7/1434 , H05K2201/048 , H05K2201/09027
摘要： The invention relates to A nose cone assembly for a munition, comprising a transducer array operably linked to a transmission assembly, wherein the transducer array is operably connected to a transducer housing, said transducer housing comprising a first and second surface, wherein said transmission assembly is reversibly operably connected to the second surface of said transducer housing, said transmission assembly comprising a control board and a plurality of electronic circuit boards, wherein at least one electronic circuit board is a transceiver circuit board, said electronic circuit boards being reversibly connected to the control board and being arranged along their longest dimension, at an axis substantially perpendicular to the control board and further arranged such that the electronic circuit boards extend radially inwardly to a substantially rotational centre of the control board.
摘要翻译：本发明涉及一种用于军火的鼻锥组件，包括可操作地连接到变速器组件的换能器阵列，其中所述换能器阵列可操作地连接到换能器外壳，所述换能器外壳包括第一和第二第二表面，其中所述传输组件可逆地可操作地连接到所述换能器外壳的第二表面，所述传输组件包括控制板和多个电子电路板，其中至少一个电子电路板是收发器电路板，所述电子电路板可逆地连接到控制板并沿着其最长尺寸布置在基本上垂直于控制板的轴线处，并且还布置成使得电子电路板径向向内延伸到控制板的大致旋转中心。 p>

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