Invention Grant
US08640439B2 Hybrid drive for an aircraft 失效
飞机的混合动力

Hybrid drive for an aircraft
Abstract:
A drive device for an aircraft comprises a gas turbine apparatus for generating a first drive energy and electric motor for generating a second drive energy. The gas turbine apparatus and the electric motor are set up in such a way that the drive unit may be provided with at least one of the first drive energy and the second drive energy. The drive unit is set up to generate propulsion using at least one of the first drive energy and the second drive energy.
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