Propulsion device for operation with a plurality of fuels...

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 27/02 (2006.01)

Patent

CA 2665132

The present invention relates to a propulsion device for an aircraft. The propulsion device comprises a propulsion unit (1) and an energy converter (4). The energy converter (4) is is adapted for providing propulsion energy to the propulsion unit (1) by a first fuel. Furthermore, the energy converter (4) is adapted for providing propulsion energy to the propulsion unit (1) by a second fuel. The propulsion unit (1) adapted for generating forward thrust by the propulsion energy.

La présente invention concerne un dispositif de propulsion destiné à un avion. Le dispositif de propulsion comprend une unité de propulsion (1) et un convertisseur d'énergie (4). Le convertisseur d'énergie (4) est adapté afin de fournir une énergie de propulsion à l'unité de propulsion (1) à l'aide d'un premier combustible. De plus, le convertisseur d'énergie (4) est adapté afin de fournir une énergie de propulsion à l'unité de propulsion (1) à l'aide d'un second combustible. L'unité de propulsion (1) est adaptée afin de générer une poussée vers l'avant à l'aide de l'énergie de propulsion.

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