Accession Number : ADA108091
Title : Helicopter Propulsion Systems
Descriptive Note : Conference proceedings
Corporate Author : ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)
PDF Url : ADA108091
Report Date : SEP 1981
Pagination or Media Count : 279
Abstract : Helicopter propulsion systems are reviewed, and it is noted that helicopter development is paced to a major extent by the power plant. Power available, reliability, fuel consumption, power-to-weight ratio, and life-cycle costs are key parameters. The application of emerging technologies such as microelectronics, ceramics and other new materials and approaches, and the continuing refinement of the aerodynamics and dynamics of gas turbine power plants are discussed and noted to result in a significant benefit to the helicopter and its operator. Important airframe-propulsion system interface requirements are given, and the need is discussed for new innovative certification procedures that provide for emergency operation with acceptable economics. Finally, future propulsion system capabilities are projected and their dramatic benefit for the helicopter noted. Bringing this about is the challenge for propulsion system specialists.
Descriptors : *TURBOSHAFT ENGINES, *STATE OF THE ART, *GAS TURBINES, *PROPULSION SYSTEMS, *TECHNOLOGY FORECASTING, *HELICOPTER ENGINES, SYMPOSIA, ENGINE COMPONENTS, COMPATIBILITY, HELICOPTERS, FRANCE, AIRFRAMES, DRIVES, LIFE CYCLE COSTS, INLETS, TRANSMISSION GEARS, AUTOMATIC TRANSMISSIONS.
Subject Categories : Helicopters
Administration and Management
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE