The invention relates to a power device for an aircraft and an aircraft comprising such a power device. The present invention relates to a power plant (151) for an aircraft and a corresponding aircraft, the power plant comprising: a propulsion system (150) comprising a core (152) enclosed in an enclosure (154) and having a combustion chamber (158); a supply tube that delivers dihydrogen to the combustion chamber (158) by passing through the housing (154) at the injection region (210); and a closed enclosure (250) delimited by first and second walls and housing the downstream tube, a treatment system (202, 204, 206) for treating dihydros, and an injection zone (210) wherein the first wall (251a) is formed by a portion of the housing (154). By this arrangement, the footprint and weight of each of the jackets are reduced as at least one wall of the jackets is formed by the outer shell of the propulsion system.
用于飞行器的动力装置和包括这种动力装置的飞行器。本发明涉及一种用于飞行器的动力装置(151)和相应的飞行器,该动力装置包括:推进系统(150),包括核心(152),该核心被包围在外壳(154)中并且具有燃烧室(158);供应管,通过在喷射区(210)穿过外壳(154)而将二氢输送到燃烧室(158);以及封闭的包壳(250),由第一壁和第二壁界定并且容纳下游管、用于处理二氢的处理系统(202,204,206)、以及喷射区(210),其中,第一壁(251a)由外壳(154)的一部分形成。通过这种布置,由于包壳的至少一个壁由推进系统的外壳形成,因此每个包壳的占地面积和重量减小。
Power device for aircraft and aircraft comprising such power device
用于飞行器的动力装置和包括这种动力装置的飞行器
2025-03-18
Patent
Electronic Resource
Chinese
European Patent Office | 2025
|European Patent Office | 2017
|European Patent Office | 2019
|Aircraft tail and aircraft comprising such aircraft tail
European Patent Office | 2024
|DEVICE FOR AIRCRAFT EMERGENCY POWER SUPPLY AND AIRCRAFT EQUIPPED WITH SUCH DEVICE
European Patent Office | 2017
|