HELICOPTER DIRECT DEPLOYMENT SYSTEM Russian patent published in 2019 - IPC B64D25/08 A62B1/20 

FIELD: aviation.

SUBSTANCE: invention relates to aircraft engineering, particularly, to helicopters direct deployment devices. System of direct deployment from helicopter in hovering mode includes landing device containing cantilever made of pipes with fasteners to helicopter fuselage. Said cantilever is furnished with jib, at the end of which attachment of landing gear suspension is arranged at certain distance from fuselage sliding door. Outside the fuselage opposite to the door opening there is a grate platform lined with pipes. Lower end of cantilever is fixed on tube on inner side of edging, and footboard is suspended to pipe on outer side for landing members. Edge tubes of the edge of the platform are connected to supports of the skid chassis by means of bracket-like attachment units covering the crossbar installed on skid run supports. Bracket hook is connected by braces with brackets installed behind upper opening of door opening. On the vertical part of the console bracket-shaped handles for landing troops are installed. Lattice platform is installed below threshold of door opening.

EFFECT: higher efficiency and safety of deployment from helicopter in hovering mode.

4 cl, 4 dwg