Course III: Aircraft Composite Tooling
Course Outline
Tooling Module
- 1. Introduction and Background
- 1.1 The Functionality of & Requirements for LMs
- 1.2 Developing a Tooling Concept
- 1.3 Terminology
- 1.4 The Autoclave Environment and its Effects - Temperature & Pressure
- 1.5 Tooling Materials
- 1.6 General Design Considerations
- 2. Metal Panel Layup Tooling (Tools made of Invar, Steel, etc.)
- 2.1 Invar Materials and Invar Tooling Fabrication Processes
- 2.2 Other Historical Tooling Materials - Aluminum, Steel and Nickel
- 2.3 Thermal Correction Factors
- 2.4 Castings
- 2.5 Design Criteria and Typical Tool Features
- 2.6 Eggcrate Design
- 2.7 Tool Repairs
- 2.8 Multi-stage/Multi-Purpose Tools - Bond Assembly Jigs and Tools with Trim/Drill Features
- 2.9 General Design Considerations
- 3. Composite Panel Layup Tooling (Tools made of composite materials)
- 3.1 Material Selection Criteria
- 3.2 Design Criteria and Typical Tool Features
- 3.3 Tool Coordination
- 3.4 Tool Face Sheet Fabrication Methods
- 3.5 Substructure Design Alternatives
- 3.6 Eggcrate Substructure Design
- 3.7 Tool Failure Modes
- 3.8 Composite Tooling Materials and Sources
- 3.9 Part Models
- 4. Layup Tools used for Automated Layup (Automated Fiber Placement and Automated Tape Laying)
- 4.1 Unique Design Requirements
- 4.2 Tool / Machine Interface Requirements
- 4.3 Seals
- 4.4 Tool Assembly/Disassembly
- 4.5 Caul Sheets
- 5. Layup Tools for Internal Composite Structural Parts
- 5.1 General Design Considerations
- 5.2 Tool/Part Orientation
- 5.3 Tool Mistake-proofing
- 5.4 Tool Removal for "Locked" Tools
- 5.5 Index Pins
- 5.6 Rib and Spar Tools
- 5.7 Resin Transfer Molds and Related Tools
- 5.8 Molds for Thermoplastic Reinforced Thermoplastic Molding (RTL)
- 6. Layup Tools for Dealing with Trapped Volume Conditions
- 6.1 General Design Considerations
- 6.2 Bladders
- 6.3 Plaster Mandrels
- 6.4 Salt Mandrels
- 6.5 Reconfigurable Mandrels
- 6.6 "Fly Away" Tools
- 6.7 Segmented Tools
- 6.8 Rubber/Elastomeric-Faced Tools
- 7. Interiors Tooling
- 7.1 Interiors-Unique Processes
- 7.2 Compression Molds
- 7.3 Mold Die Design Requirements
- 7.4 Typical Features
- 7.5 Vacuum Form Molds
- 7.6 VFM Design Requirements
- 7.7 Typical Features
- 7.8 Interiors Assembly Operations
- 8. Trim Tooling for Composite Parts
- 8.1 General Design Considerations
- 8.2 Hand Router Fixtures
- 8.3 Shaper Fixtures
- 8.4 NC Mill Fixtures for Laminated Parts
- 8.5 NC Mill Fixtures for Core Details or Subassemblies
- 8.6 Universal Holding Fixtures
- 9. Assembly Tooling for Composite Structural Assemblies
- 9.1 Assembly Basics - Indexing, Clamping, Fasteners, etc.
- 9.2 Removable Tool Parts
- 9.3 Determinant Assembly vs Tooled Assembly
- 9.4 Reference Systems and Computer-Aided Measurement Systems (CAMS)
- 9.5 Applied Drilling Tools
- 9.6 Applied Locating Tools
- 9.7 Portable Tools - Drilling Equipment
- 9.8 Drilling Setup Sheets
- 9.9 Scaffolding and Floor Mounted Equipment
- 10. Handling Equipment for Composite Parts and Assemblies
- 10.1 General Design Considerations
- 10.2 What's Different for Handling Composite Parts
- 10.3 Protective Equipment
- 10.4 Transportation Dollies
- 10.5 Overhead Handling
- 10.6 Shipping Equipment
- 11. Module Review & Wrap-up
- Mid-term and Evaluation
Instructors
Tooling: Prof. M. Ramulu and Mr. David Dickson
Repair: Prof. Brian Flinn and Dr. Gary Oakes
Questions
If you have questions about this program, please call UW Educational Outreach Advising at 206-685-8936 in the greater Seattle area or 1-800-543-2320. If you have questions about registration for this program, please call the UW Educational Outreach Registration Department at 206-543-2310 or 1-800-543-2320.
For more information about Boeing initiatives in composites education,email Michael Richey, Boeing Learning Training and Development, Engineering & Operations Group.