25-07-2013 дата публикации
Номер: US20130187009A1
An aircraft (F) with wings () and a system for minimizing the influence of unsteady flow states, wherein the wing consists of a respective main wing (M) and at least one control flap (S) adjustably arranged relative thereto, a adjusting drive () for activating the at least one control flap (S), as well as a sensor arrangement for acquiring the setting position of the control flap (S), wherein the system for minimizing the influence of unsteady flow states exhibits: 3. The aircraft (F) according to claim 2 , characterized in that the system for minimizing the influence of unsteady flow states exhibits:{'b': 15', '16', '10', '10', '11', '12', '11', '12', '1', '1, 'i': a,', 'a;', 'b', 'b', 'a', 'b, 'at least one arrangement () of flow-influencing devices () for influencing the fluid flow over the surface segment (), which are functionally connected with the flight control device, and incorporated in at least one surface segment (; , ) of the main wing (M) of each wing (M; , ) extending in a respective wingspan direction and/or at least one control flap (S),'}{'b': 16', '1', '1', '1', '16, 'i': a', 'b, 'an actuating function that is functionally connected with the flow-influencing devices () to influence the flow in the different segments of a wing (; , ), designed in such a way that the latter, based on the unsteady flow states detected by the detection device and setting position of the control flap (S) acquired by the sensor arrangement, actuate the flow-influencing devices () so as to minimize the influence of unsteady free flow states on the aircraft.'}416. The aircraft (F) according to one of the preceding claims claim 2 , characterized in that the actuating function is functionally integrated with the flight control device claim 2 , so that commands for the flow-influencing devices () are taken into account with respect to controlling the aircraft according to the commands for the adjustable flap.51011121112111516101710111211121716aa;bbabaa;bb. The aircraft (F) ...
Подробнее