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    • 2. 发明申请
    • SYSTEM AND METHOD FOR POSITIONING A BODY ALONG CONTINUOUS-RANGE INCLINATION AND ROTATION ANGLES
    • 用于定位身体连续范围倾斜和旋转角度的系统和方法
    • WO2005106609A3
    • 2005-12-15
    • PCT/US2004038443
    • 2004-11-16
    • TEXTRON SYSTEMS CORPCIANCIOLO SALVATORE
    • CIANCIOLO SALVATORE
    • F16M11/10F16M11/12F16M11/14F16M11/18F41A27/06F41F1/06H01Q3/08G05D3/10F16M7/00F41A27/14F41A27/28
    • F16M11/2014F16M11/14F16M11/18F41A27/06H01Q3/08
    • In a system for controlling the inclination angle and rotation angle of a body (22), a rotary actuator (52) is coupled to a base. A pivot actuator (50) is coupled to an output shaft of the rotary actuator (52). The rotary actuator (52) controls the angular position of the pivot actuator (50). A displacement member (34) is coupled to an output shaft of the pivot actuator (50). The pivot actuator (50) controls the linear position of the displacement member (34). A support shaft (48) is pivotably coupled to the displacement member (34). A spherical bearing (37) includes a socket that is coupled to the base and a ball that is coupled to the support shaft (48). In this manner, the angular position and linear position of the displacement member (34) is translated to a corresponding rotation angle and inclination angle in the support shaft (48). This system provides for a continuous range of rotation of the upper body (22) and a continuous range of inclination angles in the upper body (22) relative to the lower base. A corresponding method is also disclosed.
    • 在用于控制主体(22)的倾斜角度和旋转角度的系统中,旋转致动器(52)联接到基座。 枢转致动器(50)联接到旋转致动器(52)的输出轴。 旋转致动器(52)控制枢转致动器(50)的角度位置。 位移构件(34)联接到枢转致动器(50)的输出轴。 枢转致动器(50)控制移位构件(34)的线性位置。 支撑轴(48)可枢转地联接到位移构件(34)。 球面轴承(37)包括联接到基座的球窝和联接到支承轴(48)的球。 以这种方式,位移构件(34)的角位置和线性位置被平移到支撑轴(48)中的相应旋转角度和倾斜角度。 该系统提供上部本体(22)的连续范围的旋转和上部本体(22)中相对于下部基部的连续范围的倾斜角度。 还公开了相应的方法。
    • 3. 发明申请
    • THE PROTECTION OF AIRPLANES AGAINST TERRORISTS AND HIJACKERS
    • 保护飞机抵御恐怖分子和劫持者
    • WO03035471A2
    • 2003-05-01
    • PCT/HU0200092
    • 2002-09-24
    • GOEDE GABOR
    • GOEDE GABOR
    • B64D45/00F41A23/02F41A27/28F41C9/00F42B12/54B64D
    • B64D45/0015B64D2045/0025F41A23/02F41A27/28F41C9/00F42B12/54
    • The device and defence system planned for the protection of airplanes against terrorists and hijackers is described with the following characteristics: It's complex and coherent, and it consists of an extremely strong and hard ceiling cover which is made of plastic or kevlar strengthened by carbon-fibre, and this false ceiling is used in the corridors between the pilot and passenger cabins and in other relevant areas and rooms that has got a great importance in the defence system, and there are hidden launchers - for firing sleeping bullets which cause unconciousness or a paralysed state - placed on mountings above the false ceiling and they can be moved synchronised from the cockpit with hidden mini cameras by electromotors in every direction which are camouflaged as relieves or decorations, and they are connected with the pilot cabin by multy-plug cables or wireless remote transmitters where a security officer is constantly checking the central computer and its monitors to be able to divert any danger in time with the help of the hidden mini cameras and launchers if a terrorist or hijacker attack takes place on the board.
    • 计划保护飞机免遭恐怖分子和劫机者的装备和防御系统具有以下特点:它是复杂和一致的,它包括一个非常坚固和坚固的天花板盖,由塑料或凯夫拉尔加强碳纤维 在飞行员和乘客舱之间的通道以及在防御系统中具有重要意义的其他相关区域和房间的走廊中使用了这个假天花板,还有隐藏的发射器 - 用于发射导致意识不清或瘫痪的子弹 状态 - 放置在假天花板上方的安装位置,并可以通过电动机从驾驶舱与隐藏的迷你相机在每个方向上同步移动,作为减轻或装饰伪装,并通过多插头电缆或无线连接到飞行员舱 远程发射机,其中安全人员不断检查中央计算机及其监视器能够 在隐藏的迷你相机和发射器的帮助下,如果董事会发生恐怖主义或劫持者袭击,则及时转移任何危险。
    • 7. 发明申请
    • A GUN WEAPON INTERFACE UNIT
    • 枪武器接口单元
    • WO2016122430A1
    • 2016-08-04
    • PCT/TR2016/050023
    • 2016-01-29
    • ASELSAN ELEKTRONIK SANAYI VE TICARET ANONIM SIRKETI
    • SERDAR, YukselEROGLU, RafetSARI, SaitMERT, AhmetCOBAN, Ahmet
    • F41G5/06B64D7/06F41A27/28F41G5/18
    • F41G5/18B64D7/06F41A27/28F41G5/06
    • The present invention relates to a gun weapon interface unit (1), which enables to control and fire the gun units (T) of the aircrafts (H), and which basically comprises at least one interface card (2), which is adapted to generate control signals according to the discrete control and condition signals coming to it and to transmit these signals to the gun unit (T) that will be controlled and to establish data communication with a mission computer (G); at least one power card (3) which is adapted to supply the required power; at least one main board (3) on which the interface card (2) and the power card (4) are mounted; at least one filter circuit (5) which is adapted to avoid electromagnetic interference from power lines; at least one data interface (6) which provides a connection interface for receiving data from the pilot mission grip (K), aircraft (H) and/or gun unit (T) and sending data to the gun unit (T); at least one power interface (7) which provides power inlet to supply power to the power card (3); at least one communication interface (8) which provides a connection interface for communication with a mission computer (G); at least one test interface (9) which provides a connection interface for testing the unit via an external computer (B).
    • 枪武器接口单元(1)技术领域本发明涉及一种能够控制和发射飞行器(H)的枪单元(T)并且基本上包括至少一个接口卡(2)的枪武器接口单元(1),其适于 根据离散的控制和状态信号产生控制信号并将这些信号发送到将被控制的枪单元(T),并与任务计算机(G)建立数据通信; 至少一个适于提供所需电力的电源卡(3); 至少一个主板(3),其上安装有接口卡(2)和电源卡(4); 至少一个滤波器电路(5),其适于避免来自电力线的电磁干扰; 至少一个数据接口(6),其提供用于从飞行员任务手柄(K),飞行器(H)和/或枪单元(T)接收数据并向枪单元(T)发送数据的连接接口; 至少一个电源接口(7),其提供电源入口以向所述电源卡(3)供电; 至少一个通信接口(8),其提供用于与任务计算机(G)通信的连接接口; 至少一个测试接口(9),其提供用于经由外部计算机(B)测试所述单元的连接接口。