Daniel M Rotter

US Patent:

8257536, Sep 4, 2012

Filed:

Dec 18, 2008

Appl. No.:

12/337931

Inventors:

Brian G. Robins - Renton WA, US
Darrell D. Jones - Mill Creek WA, US
Kurtis S. Willden - Kent WA, US
Daniel M. Rotter - Lake Forest Park WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

B32B 37/00

US Classification:

156227, 156 52, 156 53, 156 54, 156 56, 156200, 156201, 156202, 156213, 156226, 156463, 156464, 156467, 1564771, 156475

Abstract:

A method and apparatus for a tray, a folding section connected to the tray, and a tape application system. The tray has a channel for receiving an elongate insert for a composite material with a number of layers for a release system. The folding section is capable of folding a number of layers around the elongate insert to cover the elongate insert as the elongate insert is moved through the folding unit. The tape application system is capable of applying a tape to the number of layers for covering the elongate insert to form the release system.

US Patent:

8377247, Feb 19, 2013

Filed:

Dec 22, 2010

Appl. No.:

12/976070

Inventors:

Juan C. Guzman - Seattle WA, US
Douglas A. McCarville - Orting WA, US
Daniel M. Rotter - Lake Forest Park WA, US
Brian G. Robins - Renton WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

B32B 37/10

US Classification:

156285, 156212, 156286, 264510, 264511

Abstract:

A stiffened skin panel of an aircraft that includes an aircraft skin panel of composite material and a composite stringer consolidated with the aircraft skin panel. The stringer has a pair of stringer sides, each extending from a stringer top to a stringer leg. The stringer sides may each extend through a wide radius, smooth continuous curve to a stringer leg. The wide radius, smooth continuous curve may be proximate the base of the stringer side in a region where the stringer side transitions to the stringer leg.

US Patent:

8419402, Apr 16, 2013

Filed:

Jan 13, 2011

Appl. No.:

13/005786

Inventors:

Juan C. Guzman - Seattle WA, US
Douglas A. McCarville - Orting WA, US
Daniel M. Rotter - Lake Forest Park WA, US
Barry P. VanWest - Bellevue WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

B29C 65/00
B64C 1/06

US Classification:

425110, 425393, 425403, 264156, 264275

Abstract:

A method and apparatus for a composite stringer. A method is used for manufacturing a hollow composite stringer. Foam is formed with a mandrel installed into the foam. A composite material and the foam is laid up onto a tool in a form of a stringer. The composite material and the foam in the form of the stringer is cured to form a cured stringer. The mandrel from the foam is removed to form the hollow composite stringer.

US Patent:

8454870, Jun 4, 2013

Filed:

Dec 19, 2008

Appl. No.:

12/339488

Inventors:

William S. Hollensteiner - Kent WA, US
Joseph D. Brennan - Poway CA, US
Jennifer Sue Noel - Kent WA, US
Kurtis Shuldberg Willden - Kent WA, US
Daniel M. Rotter - Lake Forest Park WA, US
Shane Edward Arthur - Belgrade MT, US
Brian G. Robins - Renton WA, US
Darrell D. Jones - Millcreek WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

B29C 70/44

US Classification:

264101, 264257, 264258, 264313, 264319

Abstract:

A method for manufacturing composite parts. A temporary removal layer may be placed on an inner mold line tool. A composite material may be laid up on the inner mold line tool for a composite part. The inner mold line tool may be positioned with the composite part inside an outer mold line tool. The composite part and the temporary removal layer may be transferred from the inner mold line tool to the outer mold line tool. The inner mold line tool and the temporary removal layer may be removed from inside of the outer mold line tool after transferring the composite part and the temporary removal layer to the outer mold line tool.

US Patent:

8465613, Jun 18, 2013

Filed:

Aug 24, 2011

Appl. No.:

13/217109

Inventors:

Daniel M. Rotter - Lake Forest Park WA, US
Michael R. Chapman - Federal Way WA, US
Brad A. Coxon - Everett WA, US
Paul E. Nelson - University Place WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

B29C 51/14

US Classification:

156212, 156200, 156196, 264294, 264295, 264296

Abstract:

Tooling apparatus for forming a composite charge into a contoured composite blade stringer includes an elongate punch and an elongate die flexible along their lengths. The charge is press formed by using the punch to drive the charge into the die. The punch and the die are mounted between a pair of flexible plates. A press coupled with the plates contours the charge by bending the plates into a desired contour.

US Patent:

8529721, Sep 10, 2013

Filed:

Jul 12, 2012

Appl. No.:

13/548057

Inventors:

Brian G. Robins - Renton WA, US
Darrell D. Jones - Mill Creek WA, US
Kurtis S. Willden - Kent WA, US
Daniel M. Rotter - Lake Forest Park WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

B32B 37/00

US Classification:

156227, 156 52, 156 53, 156 54, 156 56, 156200, 156201, 156202, 156213, 156226, 156463, 156464, 156467, 1564771, 156475

Abstract:

A method and apparatus for a tray, a folding section connected to the tray, and a tape application system. The tray has a channel for receiving an elongate insert for a composite material with a number of layers for a release system. The folding section is capable of folding a number of layers around the elongate insert to cover the elongate insert as the elongate insert is moved through the folding unit. The tape application system is capable of applying a tape to the number of layers for covering the elongate insert to form the release system.

US Patent:

8540921, Sep 24, 2013

Filed:

Nov 25, 2008

Appl. No.:

12/277483

Inventors:

Simon D. Senibi - Covington WA, US
Barry P. Van West - Bellevue WA, US
Juan Carlos Guzman - Seattle WA, US
Douglas A. McCarville - Orting WA, US
Daniel M. Rotter - Lake Forest Park WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

B29C 67/20
B32B 3/00

US Classification:

264321, 264257, 264316, 264324, 428 71

Abstract:

A method and apparatus for manufacturing a composite stringer. A composite material and foam are laid up onto a tool in the form of a stringer. The foam has a plurality of structural members within the foam. The plurality of structural members has a number of orientations to resist a number of loads. The composite material, the foam in the form of the stringer, and the plurality of structural members are cured to form the composite stringer.

US Patent:

8617687, Dec 31, 2013

Filed:

Aug 3, 2009

Appl. No.:

12/534356

Inventors:

Douglas A. McCarville - Orting WA, US
Juan C. Guzman - Seattle WA, US
Daniel M. Rotter - Lake Forest Park WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

B64C 1/00
B64C 1/06
B64C 3/34
B64C 3/18
G02B 6/036

US Classification:

428117, 244117 R, 2441235, 2441239, 244128, 428116, 428158, 385126

Abstract:

A method and apparatus for manufacturing a composite structure. A filler material with a barrier material for a channel in the filler material is formed. A composite material and the filler material with the barrier material are laid up onto a tool in a shape of the composite structure. The composite material and the filler material in the shape of the composite structure are cured.