The Boeing Company

Chris J Morrow

Dwight L Engwall

Kevin J Steen

Roger A Johnson

A method of manufacturing a composite uses a hybrid tool which serves both as a form on which constituent materials are applied for bonding or curing into a part in a desired configuration, and as a fixture for holding the bonded or cured materials in the originally applied position during subsequent machining of a peripheral edge of the part. The method includes fabricating a face sheet of composite material having a facing surface configured to the reverse of a desired shape of one surface of a part to be made on the tool. The materials for the part are applied on the face sheet, debulked, bonded or cured, and edge trimmed thereon, all while on the face sheet in the originally applied position.

Method for making a composite

A hybrid tool serves as a form on which constituent materials are applied for bonding or curing into a part in a desired configuration. It also serves as a holder for the bonded or cured materials in the originally applied position during subsequent machining. The hybrid tool is made by fabricating a face sheet of composite material having a facing surface configured to the reverse of a desired shape of one surface of a part to be made on the tool. The actual part will be laid up on the facing surface, cured while on the tool, and even trimmed before release. Base structure of the tool holds the facing surface of the face sheet in the desired shape, and includes ground-engaging pads that define an &ldquo;A&rdquo; datum plane. The tool aligns a reference plane of the face sheet parallel to the datum plane. A substantially continuous groove in the face sheet, used for trimming the part, opens in the facing surface. Edge trimming of the part on the tool is performed using a CNC machine tool following a part program to move a cutter extending into the groove to engage the full thickness of the part. The groove corresponds in space to the position represented by the cutter path of travel in the part program because of the accurate spatial relationship of the face sheet reference plane and the datum plane. One embodiment of the invention includes filling the groove in the facing surface with a foaming, self-skinning sacrificial material and covering the facing surface of the tool with a caul sheet. The tool is heated to cure the foaming material, which fills the groove and forms a hard, smooth surface skin, flush with the facing surface of the tool to support the part during lay up. A series of skin plies are laid-up to form a tool-side skin, and other components of the part are laid-up on the tool-side skin. A vacuum bag is sealed to peripheral regions of the facing surface of the tool around the laid-up skin and components. An adhesive/resin matrix in the skin and components is bonded/cured in the conventional manner within the vacuum bag to produce a rigid integral assembly. The vacuum bag is removed, uncovering the rigid integral assembly for trimming. A cutter of a machine tool is guided on a predetermined path around the facing surface of the tool, running in the foam-filled groove below the facing surface of the tool and cutting a peripheral edge around the rigid integral assembly. After trimming, the rigid integral assembly is removed from the facing surface of the tool.

Hybrid lay-up tool

A hybrid tool serves as a form on which constituent materials are applied for bonding or curing into a part in a desired configuration. It also serves as a holder for the bonded or cured materials in the originally applied position during subsequent machining. The hybrid tool is made by fabricating a face sheet of composite material having a facing surface configured to the reverse of a desired shape of one surface of a part to be made on the tool. The actual part will be laid up on the facing surface, cured while on the tool, and even trimmed before release. Base structure of the tool holds the facing surface of the face sheet in the desired shape, and includes ground-engaging pads that define an 'A' datum plane. The tool aligns a reference plane of the face sheet parallel to the datum plane. A substantially continuous groove in the face sheet, used for trimming the part, opens in the facing surface. Edge trimming of the part on the tool is performed using a CNC machine tool following a part program to move a cutter extending into the groove to engage the full thickness of the part. The groove corresponds in space to the position represented by the cutter path of travel in the part program because of the accurate spatial relationship of the face sheet reference plane and the datum plane. One embodiment of the invention includes filling the groove in the facing surface with a foaming, self-skinning sacrificial material and covering the facing surface of the tool with a caul sheet. The tool is heated to cure the foaming material, which fills the groove and forms a hard, smooth surface skin, flush with the facing surface of the tool to support the part during lay up. A series of skin plies are laid-up to form a tool-side skin, and other components of the part are laid-up on the tool-side skin. A vacuum bag is sealed to peripheral regions of the facing surface of the tool around the laid-up skin and components. An adhesive/resin matrix in the skin and components is bonded/cured in the conventional manner within the vacuum bag to produce a rigid integral assembly. The vacuum bag is removed, uncovering the rigid integral assembly for trimming. A cutter of a machine tool is guided on a predetermined path around the facing surface of the tool, running in the foam-filled groove below the facing surface of the tool and cutting a peripheral edge around the rigid integral assembly. After trimming, the rigid integral assembly is removed from the facing surface of the tool.

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Wichita, KS, United States of America

Chris J Morrow