Project planning data for a rotor and control system procurement and testing program for modifications to the XV-15 tilt-rotor research demonstrator aircraft is presented. The design, fabrication, and installation of advanced composite blades compatible with the existing hub, an advanced composite hub, and a nonmechanical control system are required.
Preliminary Design Study of Advanced Composite Blade and Hub and Nonmechanical Control System for the Tilt-Rotor Aircraft. Volume 2: Project Planning Data
1980
65 pages
Report
Keine Angabe
Englisch
Aircraft , Aircraft design , Composite structures , Fly by wire control , Hubs , Procurement , Project planning , Rotary wings , Rotors , Wind tunnel tests , Xv-15 aircraft , Aircraft construction materials , Cost estimates , Fabrication , Finance , Schedules , Tilt rotor research aircraft program , NTISNASA