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ECS Schemes for All Electric Airliners
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English
Abstract
This paper introduces the concepts and state-of-the-art advances on which the All-Electric Airliners will be based, discusses present practice and experience in the design of ECS and derives some ground rules and guidelines for generating new ECS schemes. Based on these, two examples of system schematic layout (Vapor Cycle and Recircair) are presented. Innovative development needed for execution of the systems is highlighted. The conclusion is that the systems are feasible and advantageous, but work on translating into practice should be started as soon as possible.
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Authors
Citation
Rosenbush, F., "ECS Schemes for All Electric Airliners," SAE Technical Paper 820870, 1982, https://doi.org/10.4271/820870.Also In
References
- Electromechanical Flight Control Actuation Bird David K. A. F. Flight Dynamics Lab. SAE Paper No. 771004
- Design Considerations of DC-Link Aircraft Generation Systems Rosswurm Mark A. Westinghouse Aerospace Electrical Division SAE Paper No. 811081
- The Effect of Critical Design Parameters on the Selection of a VSCF System Yorksie Daniel S. Hyvarinen Wayne E. Westinghouse Aerospace Electrical Div. SAE Paper No. 811086
- Evolution and Development of High Voltage (270 V) DC Aircraft Electric Systems in the United States Segrest J. D. Cloud W. W. Lockheed C. C. SAE Paper No. 811087
- Packaging the VSCF System for an Aircraft Engine Environment Pollard David D. Krojci Gary E. Westinghouse Aerospace SAE Paper No. 811088
- The All-Electric Airplane as an Energy Efficient Transport Cronin M. J. Lockheed California Co. SAE Paper No. 801131