FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely, to method for closing moving element of nacelle. Method of closing moving element (1) contains following phases: by means of power cylinder, moving bonnet being closed is shifted along its stroke length until the bonnet approaches the area of applying closing forces, herewith, the remaining distance to be covered is less than existing idle run of power cylinder, then by means of restraint, moving bonnet stroke is finished while closing the bonnet, where power cylinder location in idle run area is provided.
EFFECT: simplification of bonnet closing process and lowering weight of bonnet closing device.
7 cl, 8 dwg
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