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公开(公告)号:US11505308B2
公开(公告)日:2022-11-22
申请号:US16768160
申请日:2018-11-26
申请人: BOMBARDIER INC.
发明人: Otto Bobis , Clinton Eric Tanner , Scott Black
摘要: A system and a method for improving a stall margin of an aircraft during a climb phase of flight are disclosed. In one embodiment, the method comprises using data indicative of a phase of flight of the aircraft and data indicative of an angle-of-attack, and automatically commanding a deployment of leading edge slats movably attached to wings of the aircraft when the following conditions are true: the aircraft is in a climb phase of flight; and the angle-of-attack equals or exceeds a predefined deployment angle-of-attack threshold value.
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公开(公告)号:US11230368B2
公开(公告)日:2022-01-25
申请号:US16095831
申请日:2017-04-19
申请人: BOMBARDIER INC.
发明人: Thomas Ahn , Clinton Eric Tanner , Thomas Nelson , Scott Black
摘要: Aircraft pitch control systems and methods are disclosed. An aircraft pitch control system (28) comprises a movable horizontal stabilizer (24) and an elevator (26) movably coupled to the horizontal stabilizer. The elevator is electronically geared to the horizontal stabilizer.
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