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公开(公告)号：US11267552B2
公开(公告)日：2022-03-08
申请号：US16261486
申请日：2019-01-29
申请人： DASSAULT AVIATION
发明人： Aurélien Merlet , Zdenek Johan , Ximun Loyatho , Gilbert Roge
摘要： An aircraft portion includes a fuselage oriented in a longitudinal direction, an airfoil made up of at least one pair of wings arranged on either side of the fuselage in a transverse direction orthogonal to the longitudinal direction, and an airfoil-fuselage junction fairing at the interface between the airfoil and the fuselage. The junction fairing has, in a vertical plane, a lower profile and, in a horizontal plane, a horizontal profile at the junction of the outer surface of the junction fairing with the convex side of each wing. The horizontal profile and/or the lower profile successively has, in the longitudinal direction, a convex front segment, a concave intermediate segment, and a convex rear segment.
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公开(公告)号：US11745849B2
公开(公告)日：2023-09-05
申请号：US17560625
申请日：2021-12-23
申请人： DASSAULT AVIATION
发明人： Aurélien Merlet , Zdenek Johan , Ximun Loyatho , Gilbert Roge
摘要： An aircraft portion includes a fuselage oriented in a longitudinal direction, an airfoil made up of at least one pair of wings arranged on either side of the fuselage in a transverse direction orthogonal to the longitudinal direction, and an airfoil-fuselage junction fairing at the interface between the airfoil and the fuselage. The junction fairing has, in a vertical plane, a lower profile and, in a horizontal plane, a horizontal profile at the junction of the outer surface of the junction fairing with the convex side of each wing. The horizontal profile and/or the lower profile successively has, in the longitudinal direction, a convex front segment, a concave intermediate segment, and a convex rear segment.
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公开(公告)号：US20220111947A1
公开(公告)日：2022-04-14
申请号：US17560625
申请日：2021-12-23
申请人： DASSAULT AVIATION
发明人： Aurélien Merlet , Zdenek Johan , Ximun Loyatho , Gilbert Roge
摘要： An aircraft portion includes a fuselage oriented in a longitudinal direction, an airfoil made up of at least one pair of wings arranged on either side of the fuselage in a transverse direction orthogonal to the longitudinal direction, and an airfoil-fuselage junction fairing at the interface between the airfoil and the fuselage. The junction fairing has, in a vertical plane, a lower profile and, in a horizontal plane, a horizontal profile at the junction of the outer surface of the junction fairing with the convex side of each wing. The horizontal profile and/or the lower profile successively has, in the longitudinal direction, a convex front segment, a concave intermediate segment, and a convex rear segment.
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