Aircraft split hydraulic system

Power plants – Pressure fluid source and motor – Apparatus having means responsive to or ameliorating the...

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60420, 60430, F15B 1116

Patent

active

044281960

ABSTRACT:
A hydraulic system having two pumps, typically driven by two independent prime movers, a primary and secondary reservoir and associated valving to permit the system to run as one system or two independent systems, all for the purpose of redundancy and safety. The system senses fluid level in the primary reservoir and actuates the valves to establish two independent hydraulic systems, each with its own reservoir, when the fluid level drops below a predetermined level. The system is particularly advantageous in twin-engine aircraft where three hydraulic systems are employed, one off of each engine, and the third system uses two pumps, one driven by each engine.

REFERENCES:
patent: 2745357 (1956-05-01), Strayer
patent: 3138002 (1964-06-01), Ernst et al.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Aircraft split hydraulic system does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Aircraft split hydraulic system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft split hydraulic system will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-2340041

All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.