Design Method for Pressurised and Non-Pressurised Tail Cargo Door’s Fairings Compartment in Transport Category Aircraft

نویسندگان

چکیده

Abstract The method for determining the main parameters of tail cargo doors transport category aircrafts is developed. A methodology ascertainment these has been described. An example based on an existing aircraft considered. Gathered were information pertaining to necessary design, operational and regulatory requirements international organisations Federal Aviation Regulations (FAR), Certification Specification (CS) (AR). principle dimensions compartment, floor hitting platforms, in form a ramp with pressure door ladders, presented initial data. Considering described loading unloading, as well landing, operations, dependence length ascertained. designing fairings fuselage part presented. features compartment have determined, together those its components their varieties, depending scheme door. Information provided structural elements selection.

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ژورنال

عنوان ژورنال: Prace Instytutu Lotnictwa

سال: 2023

ISSN: ['2545-2835', '2300-5408', '0509-6669']

DOI: https://doi.org/10.2478/tar-2023-0017