REINFORCED AIRCRAFT FUSELAGE PANEL AND METHOD OF MANUFACTURE.

WIPO Patent Application WO/2010/004159

A3

The invention relates to a fuselage panel (30) made of composite comprising a skin (31) having an opening (40) of which at least part of the contour is reinforced by an in-built composite reinforcement. According to the invention, the said fuselage panel comprises at least one liner (60) made of composite secured to and superposed on the  said reinforced skin portion (32) and at least partially contributing to defining the contour (41) of the opening (40), the said panel (30) further comprising consolidating members (70) each passing at least partially through the said liner (60) and at least partially through the said reinforced skin portion (32). FIGURE 5

JPH0783196	PROBLEM TO BE SOLVED: To manufacture a metal lattice for electromagnetic wave shielding, a transparent article for electromagnetic wave shielding, and a metal lattice for electromagnetic wave shielding.
WO/2022/229580	SEAL FOR A GLAZED ELEMENT OF AN AIRCRAFT
WO/2009/109456	FUSELAGE STRUCTURE FOR AIRPLANE

HARASSE OLIVIER (FR)
PARREAUX-EY FRANCOIS (FR)

PCT/FR2009/051187

March 04, 2010

June 22, 2009

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AIRBUS OPERATIONS SAS (FR)
HARASSE OLIVIER (FR)
PARREAUX-EY FRANCOIS (FR)

B64C1/14; B29C70/30; B29C70/68

WO2001058680A1

2001-08-16

NIU, M.C.Y: "Airframe Structural Design", February 2002, HONG KONG CONMILIT PRESS LTD., HONG KONG, XP002512107

AUGARDE, Eric et al. (56 Boulevard de l'Embouchur, B.P. 27519 TOULOUSE Cedex 2, FR)

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