Patent ID: 8912925

Claim:
An aircraft ( 1 , 1 ′, 1 ″, 1 ′″) capable of hovering, comprising: a fuselage ( 2 ) with a nose ( 5 ); a tail rotor ( 4 ) fitted to a tail fin projecting from said fuselage ( 2 ) at the opposite end of said nose ( 5 ); a cockpit ( 6 ) housing an instrument console ( 7 ); and a windscreen ( 50 , 50 ′, 50 ″, 50 ′″) arranged in a front side of said aircraft ( 1 , 1 ′, 1 ″, 1 ′″); said windscreen ( 50 , 50 ′, 50 ″, 50 ′″) comprising an edge ( 55 ) which confines a visualization area ( 59 ) visible by an operator; said aircraft ( 1 , 1 ′, 1 ″, 1 ′″) further comprising displaying means ( 58 ) capable to display at least one visual information ( 20 , 25 ) associated to at least one flight parameter: at least in part inside said cockpit ( 6 ); and/or at least in part outside said cockpit ( 6 ); and/or at least in part on said windscreen ( 50 , 50 ′, 50 ″, 50 ′″); said visual information ( 20 , 25 ) being visible by said operator inside said visualization area ( 59 ), at least when said aircraft ( 1 , 1 ′, 1 ″, 1 ′″) is in a normal flight configuration; said visual information ( 20 , 25 ) comprising at least one first image ( 25 ) associated at least to the orientation of said aircraft ( 1 , 1 ′, 1 ″, 1 ′″) relative to the earth; characterized in that said first image ( 25 ) comprises at least one line ( 26 ) parallel, in use, to the line of horizon; said line ( 26 ) being, in use, visible to said operator on said console ( 7 ), when said aircraft ( 1 , 1 ′, 1 ″, 1 ′″) is sloped relative to a horizontal plane with said nose ( 5 ) at a higher height than said tail rotor ( 4 ).