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Hybrid propulsion vertical take-off and landing aircraft equipped with an on-board automatic energy management system
Hybrid propulsion vertical take-off and landing aircraft equipped with an on-board automatic energy management system
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机译：混合推进垂直起飞和着陆飞机，配备了板载自动能源管理系统
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摘要
Hybrid propulsion vertical take-off and landing aircraft fitted with an on-board automatic energy management system Vertical take-off and landing (VTOL) aircraft comprising a thermal engine electricity generator, an electrical energy storage assembly, a electric motorization of thrusters ensuring the propulsion and / or lift of the aircraft and an on-board energy management system automatically selecting the most suitable source of energy to be delivered to the thrusters according to a predetermined flight plan, the mass of the aircraft and the available electrical energy and fuel resources, the on-board energy management system comprising a computer (46; 22, 32, 40) configured to: acquire data representative of safety constraints, constraints environmental, and economic constraints, determine an optimal route between a starting point and an ending point based on the data thus acquired its, estimate the consumption of electrical energy or fuel necessary to travel this optimal route, compare the consumption thus obtained with the available electrical energy (20) and fuel (16) resources, and selectively activate the heat engine (14) of which it provides control and monitoring, and / or the electrical energy storage assembly (20) during this optimal journey, the computer being further configured to shut off the heat engine during takeoff and landing of the aircraft and when passing through a regulated area prohibiting noise pollution and pollutant emissions. Figure for the abstract: Fig. 1.
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