Title:
MANUFACTURING METHOD FOR COMPOSITE PANEL FOR AIRPLANE, AND APPARATUS THEREFOR
Document Type and Number:
Japanese Patent JP3632176
Kind Code:
B2
Abstract:
PROBLEM TO BE SOLVED: To provide a method for efficiently manufacturing a composite panel for an airplane by laminating a wide prepreg, a narrow prepreg or the like in individual areas and also cutting them in separate areas in order to realize the high speed lamination of the prepregs and performing the feed of the prepregs by hanging-up aerial feed, and an apparatus therefor.
SOLUTION: A release film is closely brought into contact with a planar table 4 and a planar laminate having a large area is formed by the four-axial control of the wide prepreg 5 of an unidirectional material and/or a cross material on the film. The narrow prepreg 13 is laminated on the film in the same way on another table 12 and the formation of a lattice-like laminate is performed parallelly and, next, the large area laminate and the lattice like laminate are floated along with the release film by blowing off air from the areas under the respective tables. Thereafter, the laminates are aerially fed to be placed on one cutting table 9 and cut into a required shape to form a skin part and a doubler part laminate successively. Both of them are hung up from the cutting table in a curtain state and aerially fed to be placed and laminated on the lamination fixture 22 of a single contour surface to form the composite panel.
Inventors:
Shunichi Sana
Akira Murai
Bando Shunichi
Akira Murai
Bando Shunichi
Application Number:
JP2002173242A
Publication Date:
March 23, 2005
Filing Date:
June 13, 2002
Export Citation:
Assignee:
Kawasaki Heavy Industries, Ltd.
International Classes:
B64C1/00; B29C31/08; B29C70/06; B32B37/00; B64C3/20; B64F5/00; B29L31/30; (IPC1-7): B29C70/06; B29C31/08; B32B31/00; B64C1/00; B64C3/20; B64F5/00
Domestic Patent References:
| JP4344225A | ||||
| JP4122645A | ||||
| JP62144927A |
Attorney, Agent or Firm:
Yujiro Taka