Title:
A compound structure panel and the airplane body
Document Type and Number:
Japanese Patent JP6255172
Kind Code:
B2
Abstract:
An aircraft fuselage assembly (100) comprising: first (112) and second (114) skin sections each further comprising a plurality of plies of composite materials and having a mating edge, with the mating edges (116, 118) disposed in edgewise alignment with each other; anda plurality of tabs (120) each extending longitudinally from the mating edge (116) of the first skin (112) section along an interior surface of the second skin (114) section, each tab (120) including an exterior surface (124) in facing registration with a corresponding portion of the interior surface (132) of the second skin (114) section, each of said tabs (120) further including at least one injection hole (142) formed therethrough for injection of bonding material (140) between said exterior surface (124) and said corresponding portion for attaching the first (112) and second (114) skin sections.
Inventors:
Cardin, Litchi E Le
Application Number:
JP2013121460A
Publication Date:
December 27, 2017
Filing Date:
June 10, 2013
Export Citation:
Assignee:
The Boeing Company
International Classes:
B64C1/12; B64C1/00
Domestic Patent References:
| JP2012511986A | ||||
| JP2010521362A | ||||
| JP3050419U | ||||
| JP2008514484A |
Attorney, Agent or Firm:
Sonoda Yoshitaka
Kobayashi Yoshinori
Kobayashi Yoshinori