The Boeing Company

Theboeing Company

Stephen Richard Dark

Garry Anthony Booker

David John Barene

David W Foutch

Gary Alan Lipczynski

Everette Desmond Gray

Chen Chuck

Kevin O'Brien Gaw

Tunde Abiodun Olaniyan

Randy Jay Grove

Zachariah B VanDeMark

Michael H Larson

Kory Shaffer

Jeston Lingelbach

Michael Nill

Mark Steven Denman

Laura Fournier

Douglas G Cogswell

Kevin O'brien Gaw

Michael A Nill

Gary Anthony Booker

Gary A Lipczynski

Compression mold assembly for forming a preform of a cascade includes first and second die elements and an axis of alignment. Line of removal of a formed preform is positioned perpendicular to a plane perpendicular to the axis of alignment. First die portion includes first curved surface forming interior surface of first strong back and second die portion includes first curved surface forming interior surface of a second strong back of a cell of a formed preform. Second die portion includes second curved surface forming an interior surface of a first vane on forward side of the cell of the formed preform and first die portion further includes first wall member which extends along line of removal and a second wall member which extends angularly from first wall portion forming an interior surface of a second vane positioned on an aft side of the cell.

Compression molded cascades with two piece mold

A method of assembling an aircraft assembly having a first member and a second member includes drilling at least one first opening through the first member, the at least one opening having a first diameter, and drilling at least one second opening through the second member, the at least one second opening having the first diameter. The method also includes forming a chamfer on the at least one first opening and the at least one second opening, the chamfer having a chamfer diameter, and positioning the first and second members to align the at least one first opening and the at least one second opening. The method further includes drilling the at least one first opening and the at least one second opening to a second diameter, wherein the second diameter is greater than the first diameter.

Method of assembling members of an assembly

A molding system for forming a composite structure having trapped volumes is presented. The molding system comprises a plurality of removeable inserts, a bottom tool member, and a plurality of restraints. Each removeable insert of the plurality of removeable inserts comprises a plurality of pieces configured to be disassembled for removal from the composite structure. Each removeable insert is configured to be placed in contact with the bottom tool member. The plurality of restraints is configured to restrain the plurality of removeable inserts in a vertical direction relative to the bottom tool member.

Molding system with removeable inserts restrained against vertical movement

A compression molding assembly for molding a honeycomb core, including a plurality of cells defined by a plurality of walls, of a blocker door is provided. The compression molding assembly includes a ram plate comprising a plurality of openings defined therethrough and a plurality of core inserts coupled to the ram plate such that the plurality of core inserts are configured to form the honeycomb core of the blocker door. Each core insert is removably coupled with a respective opening of the plurality of openings such that each core insert is configured to form a respective cell of the plurality of cells.

Compression molding assembly and methods for molding a thermoplastic blocker door

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Lynnwood, WA, United States of America

Stephen Richard Dark