Bombardier Inc.

Short Brothers Plc

Clinton Eric Tanner

Scott Black

Thomas Ahn

Thomas Nelson

Otto Bobis

Aircraft pitch control systems and methods are disclosed. In one exemplary embodiment, an aircraft pitch control system comprises a movable horizontal stabilizer and an elevator movably coupled to the horizontal stabilizer. The elevator is electronically geared to the horizontal stabilizer.

Aircraft pitch control system with electronically geared elevator

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.

System and method for improving a stall margin of an aircraft

Aircraft pitch control systems and methods are disclosed. An aircraft pitch control system () comprises a movable horizontal stabilizer () and an elevator () movably coupled to the horizontal stabilizer. The elevator is electronically geared to the horizontal stabilizer.

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Senneville, Canada

Clinton Eric Tanner