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Helicopter aerobatic rig with hingeless rotor
Helicopter aerobatic rig with hingeless rotor
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机译：带有无铰链旋翼的直升机特技飞行架
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摘要
The utility model relates to aircraft engineering and can be used in the creation of simulators of helicopters with a hingeless rotor for the initial training in helicopter training, crew training that simulate the operation of helicopter equipment in regular and special situations, in particular, in helicopter simulators with a hinged rotor, as well as in simulators for cultural entertainment.;The technical model of the claimed utility model is the creation of an efficient flight simulator of the helicopter for inculcating initial piloting skills, training the crew by simplifying the design by increasing reliability, mobility, availability, and accuracy of simulating flight characteristics.;The technical result is achieved by the fact that in the helicopter pilotage stand with a hingeless rotor carrying the control unit, which is a frame structure 4 with the pilot seat 10 fixed to it and the power control elements 5, 6, 7, 9 located in full accordance with ergonomics of the helicopter cockpit, a control unit for the cramped visual environment, a computer complex simulating regular and abnormal operating modes of the helicopter and equipped with an acoustic noise simulation unit containing a programmable lok simulation of flight dynamics and regimes, connected to a control unit, a workplace instructor includes control means and connected to the computing system, according to which the computer complex is based on the input of one main computer 1 with a software for visualization of the quarantine space in various climatic, meteorological conditions, simulating acoustic noises, as well as simulating the operation of the helicopter assemblies and the flight control panels, while the additional monitor 3 simulating the instrument panel introduced with the ability to simulate any existing type of helicopter, without changing the hardware, control knobs cyclic pitch ohm 5 and the pedals of the pitch of the steering screw 8 power controls are equipped with spring loaded mechanisms, made with the possibility of giving the force to the controls proportional to their movements,;The technical result is achieved by the fact that in the flight test stand of the helicopter with a hingeless rotor on the control knobs of the common pitch 6 of the main rotor, a friction brake 9 is made for fixing them in a predetermined position.;The technical result is achieved by the fact that the pilot's stand of the helicopter with the hingeless rotor is connected to the laptop for control and monitoring of the student's actions. ;The technical result is achieved by the fact that in the helicopter pilotage stand with a hinged rotor, the helicopter flight simulator is designed for programmable provision of high accuracy of simulation based on artificial neural network algorithms, providing high-speed computing. 1 N. and 3 z.p. f-ly, 3 ill.
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