PARACHUTING SYSTEM (VERSIONS) Russian patent published in 2014 - IPC B64D17/64 B64D17/74 B64D17/76 B64D17/80 

FIELD: transport.

SUBSTANCE: set of invention relates to aircraft rescue systems. In compliance with first version, proposed system comprises canopy/canopies of the main parachute, pilot parachute and brake parachute. Pilot parachute and brake parachute have common catapult or two separate catapults with common control system. In compliance with second version, proposed system comprises canopy/canopies of the main parachute, pilot parachute and brake parachute. Pilot parachute and brake parachute have two separate catapults with separate control systems. In compliance third first version, proposed system comprises canopy/canopies of the main parachute, pilot parachute and brake parachute. Main parachute and brake parachute have different catapults. In compliance with fourth version, proposed system comprises canopy/canopies of the main parachute and brake parachute. Capsule of any parachute expands towards its outlet at tape angle of 0.1-10 degrees. In compliance with fifth version, proposed system comprises canopy/canopies of the main parachute, pilot parachute and brake parachute. Capsule of any parachute expands towards its outlet at tape angle of 0.1-10 degrees. In compliance with sixth version, parachuting system comprises canopy/canopies. Parachute folded canopy is wrapped by, first, slings and, then, by parachute halyard. In compliance with seventh version, proposed system comprises canopy/canopies of the main parachute, pilot parachute and brake parachute. Parachute is folded with upper side upward and edges of canopies are bent outward.

EFFECT: decelerated descent.

20 cl, 4 dwg