Title:
一体化された繊維複合部品の製造方法
Document Type and Number:
Japanese Patent JP2011517635
Kind Code:
A
Abstract:
The method involves producing removable cores (26-29) into core molds, and applying bar-preforms (30-32) formed with reinforcing carbon fibers on the cores for forming reinforcing elements and arranging the cores at a common structure (23). The cores are supplied with web-like semi-finished products for creating an external shell (33). The common structure is inserted into a closed molding tool and filtered with hardenable plastic material. A fiber composite part is hardened by utilizing pressure and/or temperature, and the cores are removed. An independent claim is also included for a core mold for executing a method for producing an integral fiber composite part.
Inventors:
Ender Tobias
Application Number:
JP2010550109A
Publication Date:
June 16, 2011
Filing Date:
February 12, 2009
Export Citation:
Assignee:
Airbus Opera Zion Gesellschaft Mitt Beschlenktel Haftung
International Classes:
B64C3/18; B29C33/38; B29C41/38; B29C41/42; B29C43/36; B29C43/50; B29C70/06; B64C1/00
Domestic Patent References:
| JPS3622774B1 | ||||
| JPH04265714A | 1992-09-21 | |||
| JPH0365317A | 1991-03-20 | |||
| JPS618122U | 1986-01-18 | |||
| JP2006512240A | 2006-04-13 | |||
| JPH1177701A | 1999-03-23 |
Foreign References:
| US20060062973A1 | 2006-03-23 | |||
| US20030116262A1 | 2003-06-26 | |||
| US20070057123A1 | 2007-03-15 |
Attorney, Agent or Firm:
Satoshi Murakami
Kenichi Tanaka
Kenichi Tanaka