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High-Efficiency Hydraulic Power Transfer Units for Multisystem Aircraft Douglas Aircraft Company, McDonnell Douglas Corporation, Lon

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Boehringer, Boehringer, author.
Conference Name:
1979 Automotive Engineering Congress and Exposition (1979-02-26 : Detroit, Michigan, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1979
Summary:
Many contemporary aircraft requiring multiple hydraulic systems for power redundancy have utilized hydraulic power transfer units to provide that service. These units, which are commonly called reversible motor pumps (RMPs), have been heavy, noisy and inefficient with generally very poor differential pressure startup characteristics. A new-generation RMP that has solved many of these problems has been developed for the Douglas DC-9 Super 80 Series aircraft. The new unit emits significantly less noise than existing comparable units and is both weight- and cost-competitive, with excellent startup and running characteristics. It will provide an excellent means of attaining pumping redundancy in future hydraulic system configurations
Notes:
Vendor supplied data
Publisher Number:
791056
Access Restriction:
Restricted for use by site license

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