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Advanced Environmental Control System (The 2nd Part)
Technical Paper
2007-01-3923
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
The Advanced ECS is under development for the purpose of saving fuel, improving safety, and cabin comfort. In FY2006 study, basic components (i.e. MDC, OBNOGS, desiccant units, and CO2 removers) have been improved and their performances evaluated including resistance to environmental condition (i.e. vibration). In addition, the suitable system configuration for a 90-seats aircraft has been considered to evaluate the feasibility of the system. In this paper, we show the results of the evaluated performances based on prototype components, and the analytical study of a revised system configuration.
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Authors
- Hidefumi Saito - Shimadzu Corporation
- Yukio Kamiyoshihara - Japan Aircraft Development Corporation
- Takafumi Kawadu - Japan Aircraft Development Corporation
- Kay Takao - Mitsubishi Heavy Industries, Ltd.
- Tadashi Ueda - Kawasaki Heavy Industries, Ltd.
- Masahiro Ohshima - Kawasaki Heavy Industries, Ltd.
- Toru Iwata - Tokyo Aircraft Instrument Co., Ltd.
Citation
Saito, H., Kamiyoshihara, Y., Kawadu, T., Takao, K. et al., "Advanced Environmental Control System (The 2nd Part)," SAE Technical Paper 2007-01-3923, 2007, https://doi.org/10.4271/2007-01-3923.Also In
References
- Saito Hidefumi et al. “Development of Advanced ECS” SAE 36th ICES 2006-01-2199 July 2006
- Kouzuma Mitsuyiki et al. “Development of CO2 Remover for Aircraft Advanced ECS” SAE 36th ICES 2006-01-2200 July 2006
- RTCA “Environmental Conditions and Test Procedures for Airborne Equipment” “Vibration” December 2004
- RTCA “Environmental Conditions and Test Procedures for Airborne Equipment” “Temperature and Altitude” December 2004
- “Reduction of Fuel Tank Flammability in Transport Category Airplanes” Nov. 2005