An aircraft propulsion assembly including at least one first support that supports an electric propulsion system, at least one first attachment configured to connect the first support and a support structure of an aircraft, at least one second support distinct from and dissociated from the first support supporting a source of electrical energy configured to supply the electric propulsion system with electrical energy, as well as at least one second attachment configured to connect the second support and the support structure. An aircraft may include at least one such propulsion assembly. Given that the second support is distinct from and dissociated from the first support system, vibrations generated by the electric propulsion system are not transmitted to the source of electrical energy.
ENSEMBLE DE PROPULSION ÉLECTRIQUE COMPRENANT AU MOINS DEUX SUPPORTS INDÉPENDANTS, AÉRONEF COMPORTANT AU MOINS UN TEL ENSEMBLE DE PROPULSION ÉLECTRIQUE
ELECTRIC PROPULSION ASSEMBLY COMPRISING AT LEAST TWO INDEPENDENT SUPPORTS, AIRCRAFT COMPRISING AT LEAST ONE SUCH ELECTRIC PROPULSION ASSEMBLY
ELEKTRISCHE ANTRIEBSANORDNUNG MIT MINDESTENS ZWEI UNABHÄNGIGEN TRÄGERN, LUFTFAHRZEUG MIT MINDESTENS EINER SOLCHEN ELEKTRISCHEN ANTRIEBSANORDNUNG
2024-01-03
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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