Patent ID: 8839601
Filing Date: 2014-09-23
Classification: F02K,F05D,Y02T

Abstract:
1. A door for a thrust reverser of a nacelle of an aircraft capable of being pivotally mounted on a fixed structure of the nacelle comprising: an internal surface integrated to an annular circulation vein of an air flow; and an external surface for providing external aero dynamic continuity of the nacelle equipped with said thrust reverser, wherein said door being equipped with deflection means of the air flow, positioned at an upstream end of the door and moveably mounted in a deflection plane substantially perpendicular to a plane of the door between a first retracted position in which the deflection means do not penetrate the annular circulation vein when the door is in a closed position, and a second deployed position in which the deflection means will protrude from the door when the door is in an open position, each deflection means being associated at ends thereof with an articulation arm rotationally mobile about a pivot axis substantially perpendicular to the deflection plane allowing a rectilinear displacement of said deflection means in the deflection plane upon passing from the first retracted position to the second deployed position, and said door comprising a door actuator allowing the door to pass from the open position to the closed position, said door actuator being positioned so as to receive and to block adjacent ends of two deflection means in the first retracted position.