Systems and methods for lengthening an internal cargo compartment of a fixed-wing freight aircraft to a replaceable tailcone are disclosed herein. The system includes an aircraft and a removable tailcone configured to engage the aft end of the fuselage. The aircraft fuselage includes a cargo compartment and a rear end opening into the cargo compartment. The tail cone, after attachment, encloses a rear end opening of the cargo hold. The tailcone may include an interior volume configured to extend the fuselage cargo hold such that the interior volume defines an aft end of the cargo hold of the freight aircraft. In some examples, the tailcone includes a plurality of segments that may be configured to extend from the aft end of the aircraft to adjust the length of the cargo compartment elongate portion provided by the tailcone.
本文公开了用于将固定翼货运飞机的内部货舱加长至可更换尾锥的系统和方法。该系统包括飞机和构造成与机身的后端接合的可拆卸尾锥。飞机机身包括货舱和进入货舱的后端开口。尾锥在附接后包封货舱的后端开口。尾锥可包括被构造成延伸机身货舱的内部容积,以使内部容积限定货运飞机的货舱的后端。在某些示例中,尾锥包括多个部段,这些部段可被构造成从飞机的后端延伸以调整尾锥提供的货舱加长部分的长度。
Device and method for lengthening aircraft cargo hold with replaceable tail cone
用可更换尾锥加长飞机货舱的装置和方法
19.12.2023
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
PREPARATION METHOD FOR AIRCRAFT CARGO HOLD FLOOR, AND AIRCRAFT CARGO HOLD FLOOR
Europäisches Patentamt | 2024
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