670529: Hydraulic Power Units for Supersonic Aircraft - Technical Paper

Event: Aerospace Systems Conference and Engineering Display

Authors

Vickers, Inc., Div., Sperry Rand Corp.

Abstract

Content: The requirements of hydraulic power units for the Supersonic Transport are compared with those for present commercial aircraft and with the requirements that have been met in supersonic military applications Trends in component power, speed, flow and other parameters, and their effects on component design are discussed.

Meta Tags

Topics: Hypersonic and supersonic aircraft
Commercial aircraft
Freighter aircraft
Hydraulic motors
Seals and gaskets
Hydraulic drives
Hydrostatic transmissions
Chassis
Transportation Systems
Design Engineering and Styling
Steel
Electric vehicles
Fuel economy

Affiliated or Co-Author: Vickers, Inc., Div., Sperry Rand Corp.

Details

Citation: Lambeck, R., "Hydraulic Power Units for Supersonic Aircraft," Aerospace Systems Conference and Engineering Display, Los Angeles, California, United States, June 27, 1967, .

Additional Details

Publisher: SAE International

Published: 2/1/1967

Product Code: 670529

Content Type: Technical Paper

Language: English