Abstract: A crashworthy cyclic control stick system (10) for use in combination with an energy attenuating stroking crew seat (100) includes a cyclic control stick (11) and an actuating/attenuating mechanism (50). The cyclic control stick (11) includes an upper tube subassembly (14U) having a first hinge fitting (22), a lower tube subassembly (14L) having a second hinge fitting (24), the first hinge fitting (22) being mounted in pivotable combination with the second hinge fitting (24) along a hinge pivot axis (26) the and a locking mechanism (30) mounted in pivotable combination with the first hinge fitting (22) and interactively connected to the second hinge fitting (24) to preclude pivotal movement between the hinge fittings (22, 24).

Abstract: A means for controlling a rotor of a helicopter utilizes cyclic pitch chas to its rotor blades, accomplished with a cyclic control stick. Cyclic control sticks have been a matter of concern in crashing situations. Prior art cyclic sticks are hinged to that they can be pulled out of the way of a pilot thrown forward and down by an impact. A lanyard actuated by the movement of the pilot's seat pulls the cyclic stick away from the pilot. Since such systems require various mechanisms and pulleys there is a need for an improved cyclic stick. A crashworthy cyclic control stick which is pilot actuated to overcome these difficulties is provided herein.

Abstract: A crashworthy helicopter cockpit having a pyrotechnic system actuated by a stroking pilot seat for repositioning the upper portion of the cyclic control stick upon a severe or crash landing that is independent of aircraft electric and hydraulic systems.