1969-02-01

Aircraft Hydraulic Pumps for High Speed Operation 690744

An increase in pump drive speeds is desirable in order to minimize pump size and weight. This paper reviews the relationship between pump speed and power loss, as well as some of the mechanical limitations encountered at higher speeds. It also discusses the trade-offs available involving weight, performance and life. The effects of temperature and fluid selection are included.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 16% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
We also recommend:
TECHNICAL PAPER

A Forced Vortex Pump for High Speed, High Pressure, Low Flow Applications

650502

View Details

TECHNICAL PAPER

F-20 Air Turbine Cartridge Start System

841570

View Details

TECHNICAL PAPER

B-1B Secondary Power Subsystem

841607

View Details

X