公开(公告)号：EP4095033A1

公开(公告)日：2022-11-30

申请号：EP21425028.4

申请日：2021-05-28

申请人： C.I.R.A. (Centro Italiano Ricerche Aerospaziali) - S.C.P.A.

发明人： Ameduri, Salvatore ,  Ciminello, Monica ,  Concilio, Antonio ,  Dimino, Ignazio ,  Galasso, Bernardino ,  Guida, Mariano

IPC分类号： B64C11/20 ,  B64C3/52 ,  B64C27/473 ,  B64C3/18

摘要： A fixed or rotary wing structural module (1) comprises a leading edge structure (2), a torsional actuator (23) mounted on the leading edge structure (2) and comprising a torsion bar (24) and actuating devices (25) operatively coupled to the torsion bar (24). The torsion bar (24) is mounted or mountable on the leading edge structure (2) with a preload torsion, so as to give the structural module (1) a respective predefined twist. The actuation devices (25) are configured to vary a torsional stiffness and/or an angular geometry of the torsion bar (24) so as to vary the twist of the structural module (1) with respect to the predefined twist.

公开(公告)号：EP2727825B1

公开(公告)日：2014-12-17

申请号：EP12425175.2

申请日：2012-10-30

申请人： C.I.R.A. (Centro Italiano Ricerche Aerospaziali) - S.C.P.A.

发明人： Ameduri, Salvatore

IPC分类号： B64C3/50 ,  B64C3/48

CPC分类号： B64C3/48 ,  B64C3/50 ,  Y02T50/14

摘要： A device (1) for varying a geometry of a wing profile for leading edges of wings (2) of aircraft (100) comprising an exposed surface (8) extending parallel to the longitudinal development direction of the wing (2); the exposed surface (8) defines a front portion of the wing profile (9) of the wing (2), exhibits a first and a second engaging portion (6, 7) constrained stably to the wing (2) and a deformable portion (5) interposed between the first and the second engaging portions (6, 7) and mobile in relation to the wing (2) such as to enable variations in shape of the portion of wing profile (9) of the wing (2), The device (1) comprises a mechanism (10), arranged internally of a housing compartment (9a) of the wing profile, configured such as to move relatively to the wing along at least a plane that is transversal to the main development direction thereof and such as to generate a deformation of the deformable portion (5). The device (1) comprises an activating element (13) configured such as to move the mechanism (10) and provided with an actuator (14) configured such as to generate a push (S) and a kinematic mechanism (28) receiving the push (S) generated by the actuator (14) and configured such as to move the mechanism (10). The actuator (14) is positioned and configured such as to generate a push (S) in a transversal direction to the movement plane of the mechanism (10) and the kinematic mechanism (28) generates a corresponding action on the mechanism (10) such as to move the mechanism (10) in the movement plane thereof transversal to the main development direction (A).

公开(公告)号：EP2727825A1

公开(公告)日：2014-05-07

申请号：EP12425175.2

申请日：2012-10-30

申请人： C.I.R.A. (Centro Italiano Ricerche Aerospaziali) - S.C.P.A.

发明人： Ameduri, Salvatore

IPC分类号： B64C3/50 ,  B64C3/48

CPC分类号： B64C3/48 ,  B64C3/50 ,  Y02T50/14

摘要： A device (1) for varying a geometry of a wing profile for leading edges of wings (2) of aircraft (100) comprising an exposed surface (8) extending parallel to the longitudinal development direction of the wing (2); the exposed surface (8) defines a front portion of the wing profile (9) of the wing (2), exhibits a first and a second engaging portion (6, 7) constrained stably to the wing (2) and a deformable portion (5) interposed between the first and the second engaging portions (6, 7) and mobile in relation to the wing (2) such as to enable variations in shape of the portion of wing profile (9) of the wing (2), The device (1) comprises a mechanism (10), arranged internally of a housing compartment (9a) of the wing profile, configured such as to move relatively to the wing along at least a plane that is transversal to the main development direction thereof and such as to generate a deformation of the deformable portion (5). The device (1) comprises an activating element (13) configured such as to move the mechanism (10) and provided with an actuator (14) configured such as to generate a push (S) and a kinematic mechanism (28) receiving the push (S) generated by the actuator (14) and configured such as to move the mechanism (10). The actuator (14) is positioned and configured such as to generate a push (S) in a transversal direction to the movement plane of the mechanism (10) and the kinematic mechanism (28) generates a corresponding action on the mechanism (10) such as to move the mechanism (10) in the movement plane thereof transversal to the main development direction (A).

摘要翻译： 1.一种用于改变飞行器（100）的翼（2）的前缘的翼型的几何形状的装置（1），包括平行于所述翼（2）的纵向展开方向延伸的暴露表面（8）。 暴露表面（8）限定翼（2）的翼型（9）的前部，其表现出稳定地约束到翼（2）的第一和第二接合部分（6,7）和可变形部分 5），其插入在第一和第二接合部分（6,7）之间并相对于机翼（2）可移动，以使得翼（2）的翼型（9）的部分的形状能够变化。 装置（1）包括机构（10），其布置在机翼轮廓的壳体隔室（9a）的内部，其被构造为沿着至少沿其主显影方向横切的平面相对于翼移动， 以产生可变形部分（5）的变形。 所述装置（1）包括一个致动元件（13），其构造成使所述机构（10）移动并设置有致动器（14），所述致动器构造成用于产生推动件（S）和运动机构（28） （14）产生并且构造成使得所述机构（10）移动。 致动器（14）的定位和构造使得沿着横向于机构（10）的运动平面的方向产生推动（S），并且运动机构（28）产生对机构（10）的相应作用， 以使机构（10）沿其移动平面横向于主显影方向（A）移动。