FIELD: aviation.
SUBSTANCE: invention relates to design of emergency systems providing safe landing of helicopters. Helicopter comprises structural carcass (5), at least one carrying and moving propeller (10) connected to said structural carcass (5), and drive system for actuation of said rotor (10), comprising transmission power transmission box (11) and at least one main engine (12a, 12b). Helicopter additionally comprises several auxiliary engines (21a, 21b, 21c, 21d) fixed on said structural carcass (5) detachably.
EFFECT: enabling creation of additional lift of helicopter in case of helicopter drive system failure.
9 cl, 3 dwg
| Title |
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