公开(公告)号：US3852710A

公开(公告)日：1974-12-03

申请号：US27293572

申请日：1972-06-13

申请人： AIRCRAFT INSTR INC

发明人： HERNANDEZ R

IPC分类号： G01C19/44 ,  G08G5/00

CPC分类号： G01C19/44

摘要： A combination gyrohorizon instrument for aircraft which visually indicates in addition to the dial display presentation of the instrument, by means of signal lamps appropriately placed with respect to the instrument dial and an audible signal indicative of energization of any one of the signal lamps, departures from straight and level flight that exceed reasonable limits of pitch and bank. The signal lamps, indicating ''''nose up,'''' ''''nose down, '''' ''''left wing down'''' and ''''right wing down'''' are in circuits energized by a first switching means controlled by the relative rotational position of the inner and outer gimbals of the instrument for sensing departure beyond reasonable safety limits in one direction or the other in the pitch axis, i.e., either ''''nose up'''' or ''''nose down'''' flight, and a second switch means controlled by the relative rotation position of the outer gimbal and the instrument casing for sensing departure beyond reasonable limits in the roll axis, i.e., either ''''left wing down'''' or ''''right wing down'''' flight.

摘要翻译： 用于飞行器的组合陀螺仪仪器，除了通过适当放置在仪表盘上的信号灯和指示任何一个信号灯通电的可听信号之外，还可以直观地指示仪器的拨号显示器显示。 直线和水平飞行超过音高和银行的合理限制。 指示“上升”，“下降”，“左翼下降”和“右翼下降”的信号灯由通过仪器的内部和外部万向面的相对旋转位置控制的第一切换装置通电 用于在一个方向或在俯仰轴上的另一个方向（即，“向上”或“向下”）飞行中感测出超出合理的安全限制，以及由外部万向架和仪器的相对旋转位置控制的第二开关装置 用于感测离开超出滚轴轴线合理限度的外壳，即“左翼下降”或“右翼下降”飞行。

公开(公告)号：US3723963A

公开(公告)日：1973-03-27

申请号：US3723963D

申请日：1969-04-03

申请人： AIRCRAFT INSTR INC

发明人： HERNANDEZ R

IPC分类号： G01C19/32 ,  G08G5/00

CPC分类号： G01C19/32 ,  Y10T74/1218

摘要： A combination gyrohorizon instrument for aircraft which visually indicates in addition to the dial display presentation of the instrument, by means of signal lamps appropriately placed with respect to the instrument dial, departures from straight and level flight that exceed reasonable limits of pitch and bank. The signal lamps, indicating ''''nose up'''', ''''nose down'''', ''''left wing down'''' and ''''right wing down'''' are in circuits energized by a first switching means controlled by the relative rotational position of the inner and outer gimbals of the instrument for sensing departure beyond reasonable safety limits in one direction or the other in the pitch axis, i.e., either ''''nose up'''' or ''''nose down'''' flight, and a second switch means controlled by the relative rotational position of the outer gimbal and the instrument casing for sensing departure beyond reasonable limits in the roll axis, i.e., either ''''left wing down'''' or ''''right wing down'''' flight.

摘要翻译： 用于飞机的组合陀螺仪仪器，除了通过适当放置在仪表盘上的信号灯之外，还可以直观地显示超出合理的音高和银行限制的直升机和水平飞行器，除了仪表的拨号显示器显示之外。 指示“上升”，“下降”，“左翼下降”和“右翼下降”的信号灯由通过仪器的内部和外部万向面的相对旋转位置控制的第一切换装置激励的电路中 用于在一个方向或俯仰轴上的另一个方向（即，“向上”或“向下”）飞行中感测超出合理的安全限制，以及由外部万向架和仪器的相对旋转位置控制的第二开关装置 用于感测离开超出滚轴轴线合理限度的外壳，即“左翼下降”或“右翼下降”飞行。