An aircraft includes a fuselage and a non-ducted turbine engine. The fuselage has a pocket with an upstream edge and a downstream edge. The dimple is defined by a straight reference line having a length (L) and a maximum depth (h) relative to the straight reference line. A non-ducted turbine engine has an engine core, a nacelle, and a set of blades. First flow ratio (FR1) equal: # imgabs0 #

    一种飞行器,包括机身和非管道式涡轮发动机。机身具有带有上游边缘和下游边缘的凹坑。凹坑由具有长度(L)的直线参考线和相对于直线参考线的最大深度(h)限定。非管道式涡轮发动机具有发动机核心、机舱和一组叶片。第一流量比(FR1)等于:#imgabs0#


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    Titel :

    Aircraft having fuselage housing non-ducted turbine engine


    Weitere Titelangaben:

    具有容纳非管道式涡轮发动机的机身的飞行器


    Beteiligte:

    Erscheinungsdatum :

    08.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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