Invention Grant
- Patent Title: Airframe panel for aircraft and aircraft wing
- Patent Title (中): 飞机和飞机机翼的机身面板
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Application No.: US14161047Application Date: 2014-01-22
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Publication No.: US09381993B2Publication Date: 2016-07-05
- Inventor: Yoshifumi Hosokawa , Hideto Motohashi , Kouhei Murakami , Toshinari Fujii
- Applicant: MITSUBISHI AIRCRAFT CORPORATION
- Applicant Address: JP Aichi
- Assignee: MITSUBISHI AIRCRAFT CORPORATION
- Current Assignee: MITSUBISHI AIRCRAFT CORPORATION
- Current Assignee Address: JP Aichi
- Agency: Pearne & Gordon LLP
- Priority: JP2013-11748 20130125
- Main IPC: B64C1/00
- IPC: B64C1/00 ; B64C3/26 ; B64C3/18

Abstract:
An airframe panel for aircraft having stringers and ribs which enables reduction of the workload of the shimming operation includes a plurality of stringers provided on the inner surface of a lower skin along the spanwise direction of a wing, and a plurality of ribs provided along the chordwise direction of the wing. In a part of the panel in which a rib is provided, a flat support surface connects the two adjacent stringers. In another part of the panel in which no rib is provided, a stepped surface connects the two adjacent stringers where the stepped surface includes a thin-walled groove, and thick-walled bases to be connected to the stringers located at both sides of the groove.
Public/Granted literature
- US20140209745A1 AIRFRAME PANEL FOR AIRCRAFT AND AIRCRAFT WING Public/Granted day:2014-07-31
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