Ratier-figeac Sas

Didier Delbruel

Julien Serieys

A throttle control lever suitable for controlling the magnitude and direction of thrust of one or more aircraft engines is described. The throttle control lever comprises a frame, a trigger mechanism, a connection element, a cam engagement mechanism, a biasing means, a cam, and a grip suitable for gripping by a user when the throttle control lever is in use, The cam comprises a slot having first and second slot portions and a stop portion. The stop portion extends between and connects the first and second slot portions. The cam engagement mechanism comprises a cam lever and a slot engagement element, the cam lever is pivotally attached to the frame via a cam lever pivot, and the slot engagement element is attached to the cam lever. The trigger mechanism comprises a trigger lever and a trigger, the trigger lever is pivotally attached to the frame via a trigger pivot.

Throttle control levers

A device for connection to an input device actuated by a user comprises: a driving member for connection to the input device; a follower member; wherein motion of the driving member is only transmitted to the follower member after the driving member has been moved by a certain amount; and wherein means are provided to transmit a force back to the user as the driving member is moved in one direction.

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Prévinquières, France

Didier Delbruel