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公开(公告)号:US3738594A
公开(公告)日:1973-06-12
申请号:US3738594D
申请日:1971-08-16
Applicant: MC DONNELL DOUGLAS CORP
CPC classification number: B64C13/00
Abstract: A controlling mechanism for a direct lift control system which is utilized primarily during the landing phase of aircraft flight to reduce the response time of the aircraft to longitudinal or pitch commands. The system incorporates modulated spoilers to affectuate augmented vertical control of the flight path of the aircraft without necessarily changing the pitch attitude thereof. When the aircraft is preparing to land and the flaps are placed at the desired landing flap angle, the mechanism raises the spoilers on each wing symmetrically to a predetermined bias position. The mechanism thereafter causes the spoilers to operate up and down from this bias position in response to elevator commands generated either manually by the pilot or automatically by the autopilot. The mechanism also includes means to disengage the system automatically during stalls, go-arounds, landing rollout, or manually whenever the pilot desires.
Abstract translation: 一种用于直升机控制系统的控制机构,主要用于飞机飞行着陆阶段,以减少飞机对纵向或俯仰指令的响应时间。 该系统包括调节的扰流板,以影响飞行器的飞行路径的增强垂直控制,而不必改变其俯仰姿态。 当飞机准备着陆并且襟翼被放置在期望的襟翼角度时,该机构将每个翼上的扰流板对称地提升到预定的偏置位置。 此后的机构使得扰流板响应于由驾驶员手动产生的电梯命令或通过自动驾驶仪自动地从该偏置位置上下运行。 该机构还包括在停机,复飞,着陆推出期间或者当飞行员期望时手动断开系统的手段。
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公开(公告)号:US3789692A
公开(公告)日:1974-02-05
申请号:US3789692D
申请日:1972-05-04
Applicant: MC DONNELL DOUGLAS CORP
CPC classification number: B64C13/24 , Y10T74/20213
Abstract: A mechanical mixer for producing a spoiler controlling output by predeterminately combining lateral, speed brake, ground spoiler and direct lift control inputs. The mixer accomplishes this through the use of cams, followers, summing linkage, and override devices.
Abstract translation: 用于制造扰流器的机械混合器,通过预先组合横向,速度制动器,地面扰流板和直接升降控制输入来控制输出。 混合器通过使用凸轮,跟随器,求和连接和覆盖设备实现这一点。
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公开(公告)号:US3746284A
公开(公告)日:1973-07-17
申请号:US3746284D
申请日:1971-11-03
Applicant: MC DONNELL DOUGLAS CORP
IPC: B64C13/04
CPC classification number: B64C13/04
Abstract: A control wheel steering device for manually applying override changes in aircraft attitude during autopilot control. Electrical signals fed to a flight guidance computer are varied by pilot pressure on a spring which deflects and in turn modulates an electronic transducer.
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