Patent ID: 6315244
Filing Date: 2001-11-13
Classification: B64C,B64D

Abstract:
A pronely-piloted aircraft cockpit arrangement comprising;a leg brace substantially conforming to a pilot's leg on two sides, whereinsaid leg brace also conforms to at most seventy-five percent of said pilot's leg on a third side, anda shoulder brace substantially conforming to said pilot's shoulder from the top of said pilot's shoulder to a distance of twenty centimeters down the back of said pilot's shoulder, whereinsaid shoulder brace is shaped with a diminishing clearance so as to retain said pilot's shoulder more tightly as forward force is exerted by said pilot, andflight-control placement lateral to said pilot's body, said flight controls consisting of contstant-rate electronic mechanisms, anda helmet brace positioned to securely restrain and support said pilot's helmet by means of a conformable surface, which contacts the front of said pilot's helmet either above or below said helmet's visor, or in combination.