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    • 3. 发明申请
    • FLIGHT SIMULATION DEVICE
    • 飞行模拟装置
    • WO02027694A1
    • 2002-04-04
    • PCT/CZ2001/000054
    • 2001-09-25
    • G09B9/08G09B9/16G09B9/00
    • G09B9/165
    • Flight simulation device containing the simulator cabin, main display screen and instructor's area. One single room contains simulator cabin (1) in front of which the main display screen (2) is located. Horizontal axis (O2) of the screen (2) is above the center (9) of the window of cabin (1), which is followed by instructor's area (3) located on an elevated place. The center (10) of virtual window of instructor's area (3) is above the horizontal axis (O2) of the main display surface (2), and deviation of the center (10) of instructor's area (3) from vertical axis (O1) of the main display screen (2) is equal or smaller than +/- 15 DEG .
    • 飞行模拟装置包含模拟舱,主显示屏和教练区。 一个单一的房间包含在主显示屏(2)所在的前面的模拟器舱(1)。 屏幕(2)的水平轴(O2)位于舱室(1)的窗口的中心(9)上方,其后是位于升高的地方的教练区域(3)。 指导者区域(3)的虚拟窗口的中心(10)在主显示面(2)的水平轴(O2)上方,教练区域(3)的中心(10)与垂直轴(O1)的偏差 )等于或小于+/- 15°。
    • 6. 发明申请
    • METHOD OF BOUNDARY FLIGHT MODE AND OVERLOAD SIMULATION AND DEVICE FOR PERFORMING OF THIS METHOD
    • 边界飞行模式和过载模拟方法及其实现方法
    • WO02027695A2
    • 2002-04-04
    • PCT/CZ2001/000055
    • 2001-09-25
    • G09B9/08A63H27/00G06F19/00G09B9/16
    • G09B9/165
    • Continuos transfer of flight data from simulated aircraft controls to control computer where data is analysed. As soon as the received data correspond to G-load, computer sends signals to squeeze G-suit. The pressure in G-suit corresponds to that experienced by pilot in real aircraft during the same G-load. When computer detects that limit aerodynamic mode has been reached, when vibrations occur, it generates signals to create vibrations of frequency and amplitude equal to those in a real aircraft flying under the same conditions of stalling. Swinging frame (2) with its rear part connected to rear hydraulic cylinder (5) through pressure piping (8), which is feeded from rear hydraulic source (6). It further features a cockpit (4) with inlet (7) connected through upper pressure piping (12) and air valve (9) to pressure air accumulator (11) with compressor (10). Aircraft cockpit (4) controls (21) combined output (21.1) is connected to control computer (20) combined input (20.1), the combined output (20.2) from control computer (20) is connected both with corresponding control input (9.1) of air valve (9) and with rear hydraulic source (6) control input (6.1).
    • 将飞行数据从模拟飞行器控制继续传输到控制计算机,其中分析数据。 收到的数据一旦与G负载相对应,计算机就会发送信号来挤压G-Suit。 G-Suit中的压力对应于在同一G载荷下飞行员在实际飞机中所遇到的压力。 当计算机检测到达到极限空气动力学模式时,当发生振动时,它产生信号,产生频率和振幅的振动,等于在相同失速条件下飞行的真实飞机中的振动。 摆动框架(2),其后部通过从后部液压源(6)供给的压力管道(8)连接到后部液压缸(5)。 它还具有驾驶舱(4),入口(7)通过上压力管道(12)和空气阀(9)连接到带有压缩机(10)的压缩空气蓄能器(11)。 飞机驾驶舱(4)控制(21)组合输出(21.1)连接到控制计算机(20)组合输入(20.1),来自控制计算机(20)的组合输出(20.2)连接相应的控制输入(9.1) 空气阀(9)和后液压源(6)控制输入(6.1)。
    • 10. 发明申请
    • METHODS AND SYSTEMS FOR GENERATING EN-ROUTE VISIBLE TERRAIN DISPLAYS
    • 用于生成可视网络显示屏的方法和系统
    • WO2007078708A3
    • 2007-09-20
    • PCT/US2006047317
    • 2006-12-12
    • BOEING COASPEN SVEN D
    • ASPEN SVEN D
    • G01C23/00
    • G09B9/165G01C23/00
    • Methods and systems for displaying an en-route visible terrain display for an aircraft are provided. The method includes representing each pixel of a terrain display using a geographical location and an elevation above the location, each pixel further represented using at least one of a color value and a grayscale value, receiving a minimum elevation value, setting the at least one of a color value and a grayscale value of the pixels represented by an elevation value less than the received minimum elevation value to a uniform value, and displaying the en-route visible terrain display such that pixels representing terrain that includes an elevation value less than the minimum elevation value are displayed with the uniform value such that non-terrain- impacted, primary-navigation areas of the display are more easily readable.
    • 提供了用于显示航空器的路线可视地形显示的方法和系统。 该方法包括使用位置上方的地理位置和高度来表示地形显示器的每个像素,每个像素使用颜色值和灰度值中的至少一个进一步表示,接收最小标高值,设置至少一个 将由小于接收到的最小仰角值的高度值表示的像素的颜色值和灰度值值均匀化,并且显示所述路径可视地形显示,使得表示包括小于最小值的高度值的地形的像素 高程值以均匀值显示,使得显示器的非受地形影响的主要导航区域更易于阅读。