用于空陆两用飞机的离合器装置
用于空陆两用飞机的离合器装置
本公开内容涉及一种位于空陆两用飞机(100)的传动系统的发动机(101)和螺旋桨(102)之间的离合器装置(1)。离合器装置(1)包括发动机轴(2)、螺旋桨轴(3)、静止离合器装置外壳(4)，以及被旋转锁定到螺旋桨轴(3)并相对于螺旋桨轴(3)轴向可滑动的接合构件(5)。接合构件(5)包括第一接合结构(6)，用于接合与发动机轴(2)相关联的相应接合结构(7)，从而将离合器装置(1)设置在旋转推进扭矩可通过接合构件(5)从发动机轴(2)被传送到螺旋桨轴(3)的螺旋桨推进模式中。此外，接合构件(5)还包括第二接合结构(8)，用于接合与离合器装置外壳(4)相关联的相应接合结构(9)，从而将离合器装置(1)设置在螺旋桨轴(3)通过接合构件(5)被旋转锁定到离合器装置外壳(4)的螺旋桨锁定模式中。本公开内容还涉及一种包括这种离合器装置(1)的空陆两用飞机(100)。
The present disclosure relates to a clutch arrangement (1) for being located between an engine (101) and a propeller (102) of a drivetrain of a roadable aircraft (100). The clutch arrangement (1) comprises an engine shaft (2), a propeller shaft (3), a stationary clutch arrangement housing (4), and an engagement member (5) which is rotationally locked to and axially slidable relative to propeller shaft (3). The engagement member (5) comprises a first engagement structure (6) for engaging a corresponding engagement structure (7) associated with the engine shaft (2) for setting the clutch arrangement (1) in a propeller propulsion mode, in which rotational propulsion torque can be transmitted from the engine shaft (2) to the propeller shaft (3) via the engagement member (5). Moreover, the engagement member (5) further comprises a second engagement structure (8) for engaging a corresponding engagement structure (9) associated with the clutch arrangement housing (4) for setting the clutch arrangement (1) in a propeller locked mode, in which the propeller shaft (3) is rotationally locked to the clutch arrangement housing (4) by means of the engagement member (5). The present disclosure also relates to a roadable aircraft (100) comprising such a clutch arrangement (1).
Dokumentinformationen
用于空陆两用飞机的离合器装置
2022-09-30
Patent
Elektronische Ressource
Chinesisch