IP Library Granted Patent US 9,597,843
Granted Patent B2
US 9,597,843 · App. 14/278,205 · Granted Mar 21, 2017

Method and apparatus for layup tooling

Inventors: Matthew S. Stauffer (West Chester, PA); Douglas R. Ludin (Malvern, PA)
Assignee: THE BOEING COMPANY
B29C70/30B29C33/0011B29C33/40B29C33/76B29C70/32B29C33/38B29C33/3842B29K2079/085B33Y10/00B33Y80/00Y02T50/433Y10T29/49842
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Quick Facts
Patent No.
US 9,597,843
App. No.
14/278,205
Granted
Mar 21, 2017
Kind
B2
Abstract

One example of the present disclosure relates to a tool for laying up composite material to form a workpiece having a target contour. The tool includes a support structure including an elongated member having a longitudinal axis, and support plates connected to the elongated member and spaced apart from each other along the longitudinal axis. The elongated member includes a metallic material. The tool also includes a non-metallic backing structure connected to the support plates, the non-metallic backing structure comprising a working surface that includes a backing contour complementary to the target contour.

Claims (25)

1. A method of forming a tool for laying up composite material to form a workpiece having a target contour, the method comprising:

additively manufacturing a non-metallic backing structure comprising a working surface that includes a backing contour complementary to the target contour;

manufacturing a support structure comprising support plates and an elongated member; and

attaching the non-metallic backing structure to the support structure.

2. The method of claim 1 , wherein additively manufacturing the non-metallic backing structure comprises:

additively manufacturing plural backing-structure portions, and

joining the plural backing-structure portions to form the non-metallic backing structure.

3. The method of claim 1 , wherein manufacturing the support structure comprises subtractively manufacturing the support plates and coupling the support plates to the elongated member.

4. The method of claim 3 wherein the support plates are subtractively manufactured without machining any surface of the support plates.

5. The method of claim 3 , wherein coupling the support plates to the elongated member comprises:

allowing all but one or all of the support plates to float relative to the elongated member along a longitudinal axis of the elongated member with a sliding fit; and

restraining at least one of the support plates from rotating relative to the elongated member.

6. The method of claim 5 , wherein coupling the support plates to the elongated member further comprises:

inserting the elongated member through a first opening formed in at least one of the support plates;

positioning a first portion of a bushing support adjacent to the first opening and the elongated member;

positioning a second portion of the bushing support between the first opening and the elongated member, wherein the second portion is disposed opposite to the first portion about the elongated member; and

securing the first portion and the second portion of the bushing support to the at least one of the support plates.

7. The method of claim 5 , wherein coupling the support plates to the elongated member further comprises:

fixedly attaching at least one bracket to at least one of the support plates;

allowing the at least one bracket to float relative to the elongated member with the sliding fit along the longitudinal axis; and

restraining the at least one bracket from rotating relative to the elongated member.

8. The method of claim 1 , wherein:

additively manufacturing the non-metallic backing structure comprises forming ribs located on a surface opposite of the working surface, and

attaching the non-metallic backing structure to the support structure comprises securing the ribs to the support structure.

9. The method of claim 3 , wherein the support plates are subtractively manufactured by water-jet cutting the support plates.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 15, 2014
From: STAUFFER, MATTHEW S.; LUDIN, DOUGLAS R.
To: THE BOEING COMPANY
Reel/Frame 032900/0799 →
Continuity (1)
Related Publication 20150328842A1 · Nov 19, 2015