Integrated propulsion/energy transfer control systems for lift-fan V/STOL aircraftAn integrated propulsion/control system for lift-fan transport aircraft is described. System behavior from full-scale experimental and piloted simulator investigations are reported. The lift-fan transport is a promising concept for short-to-medium haul civil transportation and for other missions. The lift-fan transport concept features high cruise airspeed, favorable ride qualities, small perceived noise footprints, high utilization, transportation system flexibility, and adaptability to VTOL, V/STOL, or STOL configurations. The lift-fan transport has high direct operating costs in comparison to conventional aircraft, primarily because of propulsion system and aircraft low-speed control system installation requirements. An integrated lift-fan propulsion system/aircraft low-speed control system that reduces total propulsion system and control system installation requirements is discussed.
Document ID
19740012303
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Deckert, W. H. (NASA Ames Research Center Moffett Field, CA, United States)
Rolls, L. S. (NASA Ames Research Center Moffett Field, CA, United States)