Brief description of a variable manner in order to limit the flow of a fluid under pressure between a source and a system operates by the fluid.

摘要

The invention relates to a device for limiting the flow rate (38) for a system of the ejector of the rack of the aircraft (10) having at least one propulsion unit to control by means of a fluid (22) actuated by a fluid under pressure coming from a source (24), the rate-limiting device comprising at least: a manifold (26) connected to said source, a receiver (34) provided for supplying fluid under pressure to the propulsion unit, a feed duct (30) mounted between the collector and the receiver, the longitudinal axis (a) of the duct (30) which can rotate around the - latter in order to define a flow orifice of variable dimension of the fluid to the thruster (22).