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    LIGHT MULTIPURPOSE AIRCRAFT
    1.
    发明申请
    LIGHT MULTIPURPOSE AIRCRAFT 审中-公开
    轻型多用途飞机

    公开(公告)号：US20100012767A1

    公开(公告)日：2010-01-21

    申请号：US12448511

    申请日：2006-12-25

    申请人： Oleg Fedorovich Demchenko ,  Nikolai Nikolaevich Dolzhenkov ,  Konstantin Fedorovich Popovich ,  Vladimir Petrovich Shkolin ,  Arkady Iosifovich Gurtovoi ,  Vladimir Grigorievich Kuznetsov ,  Vyacheslav Nikolaevich Nikitin ,  Vyacheslav Mikhailovich Ilin ,  Viktor Lavrentievich Bozhanov ,  Valery Grigorievich Kodola

    发明人： Oleg Fedorovich Demchenko ,  Nikolai Nikolaevich Dolzhenkov ,  Konstantin Fedorovich Popovich ,  Vladimir Petrovich Shkolin ,  Arkady Iosifovich Gurtovoi ,  Vladimir Grigorievich Kuznetsov ,  Vyacheslav Nikolaevich Nikitin ,  Vyacheslav Mikhailovich Ilin ,  Viktor Lavrentievich Bozhanov ,  Valery Grigorievich Kodola

    IPC分类号： B64C39/00 ,  B64C1/00 ,  F41A23/00

    CPC分类号： B64D1/04 ,  B64D7/00 ,  F41F3/06

    摘要： A light multi-purpose aircraft comprises a fuselage (1); a wing (2); a fin assembly (3); a landing gear (4); a main power plant (5); an auxiliary power plant (7); pylons (10); outboard suspension objects (9) arranged on the undersurface and at the ends of the wing (2); at least one outboard suspension object (9) being arranged on the undersurface of the wing (2) and at least one outboard suspension object (9) being arranged at each end of the wing (2); a gun mount (8) or a guidance and tracking mount arranged in the lower part of the fuselage (1); a controlling integrated complex of airborne electronic equipment (17) with an electric power supply system (16) and an armament control complex (19) incorporating an on-board electronic guidance and tracking system (20); a defense system (21); a multi-purpose control panel (22); a group interaction system (23); an armament control system (24) which are related to each other and to the controlling integrated complex of airborne electronic equipment (17) through a multiplexer information exchange channel; the armament control system (24) comprising a matching and logic unit (25); an emergency unloading unit (26); at least one data distribution and conversion unit (27); executive units (28); units for switching outboard suspension objects (29); a unit for switching a gun mount or guidance and tracking mount (30); components of the armament control system (24) being linked by a local channel of information exchange, the number of the executive units (28) and the units for switching outboard suspension objects (29) being consistent with the number of outboard suspension objects (9).

    摘要翻译： 轻型多用途飞机包括机身（1）; 翼（2）; 翅片组件（3）; 起落架（4）; 主要发电厂（5座）; 辅助发电厂（7）; 塔架（10）; 布置在翼面（2）的下表面和末端的外侧悬挂物（9）; 至少一个外侧悬挂物体（9）布置在机翼（2）的下表面上，并且至少一个外侧悬挂物体（9）布置在机翼（2）的每个端部处; 机架（1）的下部安装有枪架（8）或引导和跟踪座架; 机载电子设备（17）与电力供应系统（16）和装有车载电子引导和跟踪系统（20）的装备控制综合体（19）的控制集成复合体; 防务体系（21） 多用途控制面板（22）; 组交互系统（23）; 通过多路复用器信息交换通道相互关联的机载控制系统（24）和机载电子设备（17）的控制集成复合体; 所述装备控制系统（24）包括匹配和逻辑单元（25）; 紧急卸载单元（26）; 至少一个数据分配和转换单元（27）; 执行单位（28）; 用于切换外侧悬挂物体的装置（29）; 用于切换枪支座或引导和跟踪座（30）的单元; 武装控制系统（24）的组件通过本地信息交换信道链接，执行单元（28）的数量和用于切换外侧悬挂物体（29）的单元与外侧悬挂物体（9）的数量一致 ）。

    LIGHT MULTI-PURPOSE AIRCRAFT
    2.
    发明申请
    LIGHT MULTI-PURPOSE AIRCRAFT 审中-公开
    轻型多用途飞机

    公开(公告)号：US20100327112A1

    公开(公告)日：2010-12-30

    申请号：US12450712

    申请日：2007-07-11

    申请人： Oleg Fedorovich Demchenko ,  Nikolai Nikolaevich Dolzhenkov ,  Konstantin Fedorovich Popovich ,  Vladimir Petrovich Shkolin ,  Vitaly Jurievich Naryshkin ,  Valery Grigorievich Kodola ,  Georgy Aleksandrovich Fedotov

    发明人： Oleg Fedorovich Demchenko ,  Nikolai Nikolaevich Dolzhenkov ,  Konstantin Fedorovich Popovich ,  Vladimir Petrovich Shkolin ,  Vitaly Jurievich Naryshkin ,  Valery Grigorievich Kodola ,  Georgy Aleksandrovich Fedotov

    IPC分类号： B64D7/00 ,  B64D11/00

    CPC分类号： B64D7/00 ,  B64C1/0009 ,  Y02T50/12

    摘要： A light multi-purpose aircraft comprises a fuselage 1; a wing 2; a fin assembly 3; a landing gear 4; main and auxiliary power plants 5; a crew protection system; an integrated complex for controlling a general-purpose aircraft equipment which is engaged through a multiplexer channel with a set of on-board digital computers, electronic control systems of port and starboard engines, a recording and monitoring system, a guidance and landing equipment, a complex control system and is engaged through code communication lines with a fuel control and monitoring system, a voice message equipment, a complex electron display system, characterized in that the crew protection system is made in the form of a multilayer screen of auxiliary and main equipment configured in order of increasing its significance farther and farther away from the shell and load-bearing elements of the fuselage 1; the greatest component density is ensured with due regard for the most likely zones and aspect angles of injury: ˜30° with respect to the surface of approaching the destruction means at the front—from below and on the side—from below of the fuselage forepart, and the integrated complex for controlling a general-purpose aircraft equipment is provided with a crew warning system 12 regarding the fall outside limiting values of destruction aspect angles, the system 12 being connected to the complex electron display system and the voice message equipment.

    摘要翻译： 轻型多用途飞机包括机身1; 一个翅膀2; 翅片组件3; 起落架4; 主，辅电厂5座; 船员保护系统; 用于控制通过多路复用器通道与一组车载数字计算机，端口和右舷发动机的电子控制系统，记录和监视系统，引导和着陆设备， 复杂的控制系统，通过代码通信线路与燃油控制和监控系统，语音留言设备，复杂的电子显示系统，其特征在于机组保护系统以辅助和主设备的多层屏幕的形式 按照使其意义越来越远离机身1的壳体和承载元件的顺序配置; 确保最大的组件密度，同时适当考虑到最可能的区域和方面的伤害角度：相对于在机身前部下方和侧面前方的接近破坏装置的表面〜30° ，并且用于控制通用飞机设备的集成复合体具有关于破坏方面角度的下限外限值的船员警告系统12，系统12连接到复数电子显示系统和语音留言设备。

    AIRCRAFT WITH MULTI-PURPOSE INTEGRATED ELECTRONIC COMPLEX
    3.
    发明申请
    AIRCRAFT WITH MULTI-PURPOSE INTEGRATED ELECTRONIC COMPLEX 审中-公开
    具有多用途集成电子复合体的飞机

    公开(公告)号：US20100133388A1

    公开(公告)日：2010-06-03

    申请号：US12452561

    申请日：2007-07-11

    申请人： Oleg Fedorovich Demchenko ,  Nikolai Nikolaevich Dolzhenkov ,  Konstantin Fedorovich Popovich ,  Vladimir Petrovich Shkolin ,  Arkady Iosifovich Gurtovoi ,  Valery Grigorievich Kodola ,  Vyacheslav Georgievich Kalugin ,  Kirill Veniaminovich Obrosov

    发明人： Oleg Fedorovich Demchenko ,  Nikolai Nikolaevich Dolzhenkov ,  Konstantin Fedorovich Popovich ,  Vladimir Petrovich Shkolin ,  Arkady Iosifovich Gurtovoi ,  Valery Grigorievich Kodola ,  Vyacheslav Georgievich Kalugin ,  Kirill Veniaminovich Obrosov

    IPC分类号： B64C13/00 ,  B64D45/00

    CPC分类号： B64D7/00 ,  F41G1/40 ,  F41G3/22

    摘要： An aircraft (1) at enhanced maneuvering properties comprising a fuselage, a wing, a fin assembly, a landing gear, a power plant, a multi-purpose integrated electronic complex (3), incorporating an information exchange system, a set of on-board digital computers (19) for controlling flight and training and combat operations, an external storage and an information input system, a radio inertial navigation and landing system, a complex aircraft control system, an armament control system, a complex system for electronic display, control and sighting, an emergency warning board, a general-purpose aircraft equipment control system, an on-board objective monitoring system, a speech information control system, an electric power supply system, external and internal lighting facilities, a complex emergency escape system, an electronic power plant control system, characterized in that an optoelectronic vision-sight system (5) comprises an automatic caging system (31) that fixes orientation of visual fields of a laser radar system (24), a narrow-field thermal vision system (25), a wide-field thermal vision system (26), a TV system (27) when a sight line transits to the upper hemisphere and decages thereof during transition to the lower hemisphere; the optoelectronic vision-sight system (5), receive-radiating units of an on-board radar (4) and a periscopic system (30) for bringing visual fields of the optoelectronic system to the upper hemisphere being mounted in a common fastening device.

    摘要翻译： 一种具有增强的机动性能的飞机（1），其包括机身，机翼，翅片组件，起落架，发电厂，多用途集成电子综合体（3），其包括信息交换系统， 用于控制飞行和训练和作战操作的数字计算机（19），外部存储和信息输入系统，无线电惯性导航和着陆系统，复杂的飞行器控制系统，装备控制系统，电子显示器的复杂系统， 控制和瞄准，应急预警板，通用飞机设备控制系统，车载客观监控系统，语音信息控制系统，电力供应系统，外部和内部照明设施，复杂的应急逃生系统， 一种电子发电厂控制系统，其特征在于，光电视觉瞄准系统（5）包括自动笼式系统（31），其固定vis的取向 激光雷达系统（24），窄视场热视觉系统（25），宽视场热视觉系统（26），电视系统（27），当视线转移到上半球时的分数 在过渡到下半球时; 光电视觉系统（5），车载雷达（4）的接收辐射单元和用于将光电系统的视场带到上半球的视光系统（30）安装在公共紧固装置中。