发明名称 Aircraft control equipment for landing approach - has controller with indicators for altitude-time settings and for starting deceleration procedure
摘要 <p>An equipment is used to control the landing approach of an aircraft along its guide path. It controls the deceleration during the deceleration phase of the aircraft. It also indicates to the pilot whether correction is required of the deviation between the total slope and the reference slope. The equipment comprises a display (3) with two indicators (2, 4). When the pilot proceeds with the procedure of glide path capture, he presses the triangle indicator to start the decelerated approach equipment. When the aircraft is at a given first altitude, and first instant in time, the arrow indicator lights-up and informs the pilot to initiate the first deceleration phase and to lower the undercarriage, reset the wing flaps and adjust the engine throttle. When the aircraft is at a given second altitude and instant, the arrow indicator again nforms the pilot to reset the wing flaps.</p>
申请公布号 FR2344001(A2) 申请公布日期 1977.10.07
申请号 FR19760006592 申请日期 1976.03.08
申请人 EQUIPEMENTS NAVIGATION AERIENNE 发明人
分类号 G01S1/02;G05D1/06;(IPC1-7):01C23/00;64D45/04 主分类号 G01S1/02
代理机构 代理人
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