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Emergency Monopropellant Auxiliary Power Units for Large Commercial Aircraft

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Stancliffe, A. Colin, author.
Conference Name:
Aeronautic and Space Engineering and Manufacturing Meeting (1969-10-06 : Los Angeles, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1969
Summary:
This paper discusses the use of liquid monopropellant powered turbopumps designed to provide emergency hydraulic power for large commercial aircraft. This type of equipment has been used in the past in missile hydraulic power supplies, and the application to aircraft emergency use represents no major changes or advances in technology. Fuel selection criteria, decomposition chamber design, turbine design, and gearbox layout are discussed as well as the control system. The integration of this type of equipment into other power producing units is briefly described
Notes:
Vendor supplied data
Publisher Number:
690659
Access Restriction:
Restricted for use by site license

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