FIELD: machine building.
SUBSTANCE: invention relates to a crooked connecting rod. A crooked connecting rod (31) couples the first and second units which are movable in respect to each other and through which a flow circulates in the space limited by them, the connecting rod is fitted by at least one first and one second rotation centres (35, 38) made so that to provide for the turn of the connecting rod (31) in respect to the said first and second units respectively. The connecting rod (31) can be set so that the curve (40) is upstream in respect to the second rotation centre (38). The second rotation centre (38) can be rigidly fixed in the second movable unit. The connecting rod (31) has at least two parts (33, 37) coupled with each other by at least one element (39a, 39b) for self-alignment. A nacelle of a bypass turbojet engine is proposed as well, a panel of a movable cowl is connected to the stationary structure of a turbojet engine bullet by means of at least one above crooked connecting rod (31) which is installed so that it is able of rotating around the first and the second rotation centres (35, 38) respectively on the panel of a jet section and on the stationary structure.
EFFECT: increased stability of connecting rod, improved operating parameters of an engine due to obtaining optimal aerodynamic characteristics of the connecting rod.
12 cl, 13 dwg
