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2022 | OriginalPaper | Buchkapitel

Strength Design and Research of Fuselage Opening Zone of Civil Aircraft

verfasst von : Kaijun Yin, Yinli Zhang, Renjun Sun

Erschienen in: Proceedings of the 5th China Aeronautical Science and Technology Conference

Verlag: Springer Singapore

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Abstract

There are many cabin doors in the fuselage of civil aircraft, that can cause fuselage stiffness and transfer of load discontinuity. In order to keep structural integrity and transfer of load of aircraft, cutout of fuselage should be strengthened to hold and transmit the surrounding load. The compare between the opening fuselage and integrity fuselage are formulated through a theoretical analysis. The principle and the method to strengthen the fuselage with large opening are successfully applied on the aircraft in the preliminary design stage and can be used to guide the structure preliminary design.

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Metadaten
Titel
Strength Design and Research of Fuselage Opening Zone of Civil Aircraft
verfasst von
Kaijun Yin
Yinli Zhang
Renjun Sun
Copyright-Jahr
2022
Verlag
Springer Singapore
DOI
https://doi.org/10.1007/978-981-16-7423-5_3

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