Invention Grant
- Patent Title: Main wing structure of aircraft
- Patent Title (中): 飞机主翼结构
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Application No.: US11978717Application Date: 2007-10-30
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Publication No.: US07938360B2Publication Date: 2011-05-10
- Inventor: Jun Nakazawa , Kazuhide Hasegawa , Hirohide Azuma
- Applicant: Jun Nakazawa , Kazuhide Hasegawa , Hirohide Azuma
- Applicant Address: JP Tokyo
- Assignee: Honda Motor Co., Ltd.
- Current Assignee: Honda Motor Co., Ltd.
- Current Assignee Address: JP Tokyo
- Agency: Birch, Stewart, Kolasch & Birch, LLP
- Priority: JP2006-302637 20061108
- Main IPC: B64B1/24
- IPC: B64B1/24 ; B64C3/28

Abstract:
Plural regions are defined within a main wing by a plurality of spars and ribs. Of these regions, predetermined regions extending from a main wing connecting portion of the pylon to an internal space of a leading edge skin are used as wiring/piping accommodating chambers for collectively accommodating wiring and piping which provide communication between an engine and a fuselage, a predetermined region adjacent to parts of the wiring/piping accommodating chambers is used as a landing device accommodating chamber for accommodating a landing device and predetermined regions adjacent to other parts of the wiring/piping accommodating chambers are used as fuel tanks. Thus, the maintainability is improved as compared with the case where the wiring and the piping are distributed within the main wing. In addition, because the wiring/piping accommodating chambers are isolated from the landing device accommodating chamber and the fuel tanks, the operational reliability can be improved.
Public/Granted literature
- US20080149761A1 Main wing structure of aircraft Public/Granted day:2008-06-26
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