AIRCRAFT (OPTIONS) AND METHOD FOR LIFTING THE RESCUE BOOK TO THE FUSELAGE OF THE AIRCRAFT

摘要

1. An aircraft capable of flying in a hover mode, comprising a fuselage having an entrance aperture; drive means for moving the rescue cradle; and a first wall adapted to move between a closed position in which it covers the first part of the opening and a first open position providing access to the first part of the opening, wherein the aircraft comprises an element that is connected to the first wall and contains at least one a flat surface, wherein said element is movable relative to the first wall to a first position in which said flat surface forms a supporting surface for the cradle when wall in the first open position, while the first wall is connected to the fuselage with at least rotation about the first axis, and is configured to rotate around the first axis to move between the closed position and the first open position, characterized in that the first wall is made rotatable around the first axis in a given direction of rotation to move from a closed position to a first open position, and rotatable around a first axis in the same direction of rotation for premises from the first open position to the second open position. ! 2. The aircraft according to claim 1, characterized in that said element comprises a first edge operatively connected to the first wall and a second edge opposite the first edge, the second edge being located at a first distance from the first wall when the element is in the first position, and at the second distance�