Invention Grant
- Patent Title: Aircraft skin attachment system
-
Application No.: US14489115Application Date: 2014-09-17
-
Publication No.: US09669579B2Publication Date: 2017-06-06
- Inventor: William T. Kline , Charles J. Nelson , Thang D. Phung , Curtis M. Groth , Robert G. Meyer , Peter J. VanVoast , Charles Y. Hu , Geoffrey A. Butler , Dan D. Day , Thomas J. Kennedy , Luis A. Perla , Richard A. Ransom , Justin L. Holland , Erik Lund , Joseph F. Warren
- Applicant: The Boeing Company
- Applicant Address: US IL Chicago
- Assignee: THE BOEING COMPANY
- Current Assignee: THE BOEING COMPANY
- Current Assignee Address: US IL Chicago
- Agency: Yee & Associates, P.C.
- Main IPC: B29C65/00
- IPC: B29C65/00 ; B29C65/02 ; B29C70/44 ; B29C65/26 ; B29C65/48 ; B29C65/50 ; B29C35/02 ; B29C43/36 ; B29C65/18 ; B29C43/10 ; B64F5/10 ; B29K105/06 ; B29L31/00 ; B29C33/02 ; B29C33/30 ; B29C43/52 ; B29C43/58 ; B29L31/30

Abstract:
A method for forming a structural member and a structural member produced thereby includes positioning a first composite section and a second composite section within a tool. The tool has an inner surface and a wall intersection and is supported by a tool platform. The tool platform and a pressure platform are relatively movable between an open position and a closed position. The tool has a non-planar outer surface against which the member may be pressed. A composite splice member is positioned at least partially overlapping both the first composite section and the second composite section to form a joint in the composite structural member. The composite structural member is pressed against the non-planar outer surface of the tool by applying pressure to the joint from a pressure bladder. Heat is applied to the composite structural member at the joint to cure the composite splice member to the first composite section and the second composite section.
Public/Granted literature
- US20150004347A1 Aircraft Skin Attachment System Public/Granted day:2015-01-01
Information query