Method for the design of laminated composite materials

• US 20060029807A1
• Filed: 08/04/2004
• Published: 02/09/2006
• Est. Priority Date: 08/04/2004
• Status: Abandoned Application

• Current Assignee: Scott Owen Peck
• Original Assignee: Scott Owen Peck
• Inventors: Peck, Scott Owen
• Application Number:
  US10/911,466
• Publication Number:
  US 20060029807A1
• Time in Patent Office: Days
• US Class Current: 428/411.100
• CPC Class Codes: B32B 37/00 Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
• CPC Class Codes: G06F 2113/26 Composites
• CPC Class Codes: G06F 2119/08 Thermal analysis or thermal optimisation
• CPC Class Codes: G06F 30/00 Computer-aided design [CAD]
• CPC Class Codes: Y10T 428/31504 Composite [nonstructural laminate]

Abstract

The fundamental premise of designing structures with laminated composite materials is that the materials can be tailored to meet requirements by choosing the materials, thicknesses or thickness fractions, and orientation angles of constituent materials. Minimum weight, dimensional stability, natural frequency, and thermal conductivity are typical goals. This invention is NOT about the analysis of laminated materials and composites, of which there is no short supply. This invention is about the design of laminated materials, which has traditionally been an iterative event between the designer and the analysis tool. These iterations, if they occur at all, are often the most time consuming aspect of design. The fundamental premise of this invention is that tensor invariants of constituent material properties coupled with a tensor description of the specified material requirements can be used together to design laminated materials. The results of this invention can be used as a stand-alone design tool or as a value-added module in finite element codes. Specifically, by specifying material requirements, designers will use the method to select from a catalog of available materials a set that will satisfy their requirements. The designer is aided in the choice of materials, how much of each material to use, the layup angle orientation of the materials, and the sequencing of those materials in the composite laminate.

Claims

1. A method for efficient design of a specified laminated composite material having tensor properties, composed of a set of candidate materials having tensor properties, each of the candidate materials having a thickness or thickness fraction, stacking sequence, and layup angle to be determined, comprising the following steps:

Calculating tensor invariants of the specified laminated composite material,

Calculating tensor invariants of the candidate materials,

Forming a set of relationships between the tensor invariants of the specified laminated composite material and the tensor invariants of the candidate materials,

Determining from the set of relationships an optimal set of candidate materials, thicknesses or thickness fractions, stacking sequence, and layup angles.