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Invention Grant
CN104875878B 带有容置于引擎机舱内的主起落架的飞机 有权

带有容置于引擎机舱内的主起落架的飞机
Abstract:
本发明提供了一种用于飞机的主起落架，所述飞机包括机身(11)、机翼(13)和位于机翼的每一侧的至少一个喷气式引擎(21)，所述至少一个喷气式引擎(21)容置在附接于机翼的引擎机舱(23)中。主起落架包括位于机翼(13)的每一侧的起落架(25)，所述起落架(25)具有联接于驱动装置(29)的一个或多个机轮(27)，所述驱动装置(29)布置成使所述一个或多个机轮(27)从收起位置移动至展开位置以及反之亦然。引擎机舱(23)包括相对于于喷气式引擎(21)横向定位的腔，所述腔构造成每个起落架的所述一个或多个机轮(27)在收起位置的容置空间。
Abstract(English):

The invention provides a main landing gear for aircraft comprising a fuselage (11), a wing (13) and at least one jet engine (21) at each side of the wing housed in a nacelle (23) attached to the wing. The main landing gear comprises a landing gear (25) at each side of the wing (13) having one or more wheels (27) coupled to a driving device (29) arranged for moving them from a stowed position to a deployed position and vice versa. The engine nacelles (23) include wells located laterally with respect to the jet engines (21) and configured as a housing space of the one or more wheels (27) of each landing gear in its stowed position.

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