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Propulsion System Requirements for Advanced Technology Air Transports
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English
Abstract
This paper endeavors to identify some of the requirements for the propulsion system of the advanced technology transport. These requirements lie in the areas of design, material selections, accessibility and maintainability of the system, and noise and emission control. The design should provide for adequate stall margins for the compressor, maximum reliability, mechanical and operational simplicity whenever possible, and a modular type of assembly to facilitate on-line and on-wing maintenance. The airframe manufacturer must engineer the powerplant installation to provide maximum accessibility to the engine gas path hardware and the engine accessories. The engine designers must strive for noise levels within the state-of-the-art and preferably below the FAR 36 compliance requirements. The engine should be optimized to produce the minimum possible amount of noxious gases, particulates, and unburned hydrocarbons.
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Citation
Schwartz, M., "Propulsion System Requirements for Advanced Technology Air Transports," SAE Technical Paper 710761, 1971, https://doi.org/10.4271/710761.Also In
References
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- Sallee G. P. “Design Requirements and Objectives for Commercial Aircraft Propulsion Systems.” Paper 69-GT-57 ASME Gas Turbine Conference and Products Show Cleveland March 1969
- Searls F. “An Airline View of SST Powerplants.” SAE Transactions 76 paper 670865
- Lennard D. J. “Design Features of the CF6 Thrust Reverser and Spoiler.” Paper 690411 SAE National Air Transportation Meeting New York April 1969
- Taylor H. N. “Maintenance Trends for New Air Transport Powerplants.” Paper 700316 SAE National Air Transport Meeting New York April 1970