A propulsion assembly includes a fan housing (64) and a pod (62) including an air inlet (66) connected to a front end (64.1) of the fan housing (64), a middle section (68) positioned around the fan housing (64), and a rear section (70) cooperating with a rear end (64.2) of the fan housing (64). The intermediate section (68) includes: at least one aerodynamic panel (84) extending from a front edge (68.1) abutting the air inlet (66) to a rear edge (68.1) abutting the rear section (70); and at least one intermediate radial support (86) comprising an inner edge (86.1) connected to the fan housing (64) and an outer edge (86.2) connected to an aerodynamic panel (84) comprising a front edge (84.1) connected to the air inlet (66) by a first connection system (102).
本发明涉及一种推进组件,其包括风扇壳体(64)和吊舱(62),吊舱包括连接至风扇壳体(64)的前端(64.1)的进气口(66)、围绕风扇壳体(64)定位的中间区段(68)以及与风扇壳体(64)的后端(64.2)配合的后部区段(70)。中间区段(68)包括:至少一个空气动力学面板(84),其从邻接进气口(66)的前边缘(68.1)延伸至邻接后部区段(70)的后边缘(68.1);以及至少一个中间径向支撑件(86),其包括连接至风扇壳体(64)的内边缘(86.1)以及连接到空气动力学面板(84)的外边缘(86.2),该空气动力学面板包括通过第一连接系统(102)连接到进气口(66)的前边缘(84.1)。
Aircraft propulsion assembly and aircraft comprising at least one such propulsion assembly
飞行器推进组件及包括至少一个这种推进组件的飞行器
2024-11-29
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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