MANUFACTURING METHOD FOR AIRCRAFT BULKHEAD

The present invention relates to a manufacturing method for an aircraft bulkhead. The aircraft bulkhead is of an arc structure and comprises a Z-shaped cross section, and comprises a flanging area, bending areas, and a web area extending between the bending areas, wherein the web area is fan-shaped....

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Bibliographische Detailangaben
Hauptverfasser: NING, Bo, SU, Jiazhi, CHEN, Lei, LIU, Weiping, WANG, Lin, YAN, Chao, AN, Shenshen, LI, Rupeng, HAN, Xiaoyong, CHEN, Ping, QIU, Chunliang, XIONG, Wenlei
Format: Patent
Sprache:chi ; eng ; fre
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