Provided is an inlet bulkhead for large diameter aircraft engines. The inlet bulkhead, in certain examples, includes an annular body having an outer flange, an inner flange, and a web having a first side and an opposing second side. The web extends from the outer flange to the inner flange. The bulkhead also includes at least one annular stiffener disposed on the first side, and multiple radial stiffeners disposed on the first side, each of which extend from the outer flange to the inner flange. The annular and radial stiffeners may be integrally formed with the web.
提供了一种用于大直径飞机发动机的入口隔板。在某些实例中,入口隔板包括环形主体,该环形主体具有外凸缘、内凸缘和具有第一侧面和相对的第二侧面的腹板。腹板从外凸缘延伸到内凸缘。隔板还包括设置在第一侧上的至少一个环形加强件和设置在第一侧上的多个径向加强件,每个加强件从外凸缘延伸到内凸缘。环形加强件和径向加强件可与腹板一体地形成。
INLET BULKHEAD FOR LARGE DIAMETER AIRCRAFT ENGINES
用于大直径飞机发动机的入口隔板
2021-02-02
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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