The report includes detailed manufacturing plans for the fabrication of major structural components of the ADCA aircraft and their final assembly. A survey of existing tooling/manufacturing technology is presented to highlight areas requiring further development. A corrosion-control plan and quality-control plan are presented to show their relevance to the manufacturing plan. Based on a comparison to current metal aircraft, the design/manufacturing philosophy was established to reduce composite program costs, by striving to reduce part/fastener count. (Author)
Advanced Design Composite Aircraft (ADCA) Study. Volume 2. Manufacturing Plan
1976
105 pages
Report
Keine Angabe
Englisch
Aircraft , Composite Materials , Manufacturing Processes & Materials Handling , Airframes , Composite structures , Fiber reinforced composites , Manufacturing , Wings , Fuselages , Fabrication , Efficiency , Bonding , Attachment , Fastenings , Conformal structures , Graphite , Epoxy resins , Machine tools , Molding techniques , Joints , Sandwich construction , Sandwich panels , Honeycomb structures , Corrosion , Quality control , Feasibility studies , Cost effectiveness , Advanced design composite aircraft , Composite materials , Titanium alloys , Stainless steel , Plastics , Glass , Laminates , Boron , Cocuring
Advanced Design Composite Aircraft study
AIAA | 1977
|Advanced Design Composite Material Aircraft Study
AIAA | 1978
|Advanced Design Composite Aircraft
NTIS | 1976
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