A power system includes a speed reducer, and a first turboshaft engine and a second turboshaft engine configured to drive the speed reducer. The speed reducer includes an output shaft. The first turboshaft engine is mounted on a first side of the speed reducer, the second turboshaft engine is mounted on a second side of the speed reducer, and the first turboshaft engine and the second turboshaft engine are arranged symmetrically about the output shaft.
POWER SYSTEM AND UNMANNED HELICOPTER
04.02.2021
Patent
Elektronische Ressource
Englisch
Unmanned helicopter propeller hub and unmanned helicopter
Europäisches Patentamt | 2020
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