Keyword: «helicopter»
The article develops proposals for the constructive improvement of aircraft hydraulic lifting devices of the helicopter with synchronization of their operation.
The article discusses a proposal to introduce an on-board system of active flight safety on a helicopter in order to assist the crew in the event of special cases in flight.
The article discusses the TV3-117 and VK-2500 turboshaft engines currently used on Russian helicopters.
The article presents the main features of the design of a springless torsion sleeve of a load-bearing unit.
The article discusses the construction of a mathematical model for the time-optimal vertical lift of a helicopter. The solution is based on the maximum principle in the presence of restrictions on phase co-ordinates and control. To simplify the algorithm fordetermining optimal control, it is proposed to use a numerical optimization method.