Stiffness enhanced electrohydrostatic actuator

Power plants – Pressure fluid source and motor – Pump means moves motive fluid from one chamber to an...

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

91415, 91420, 91436, 91465, F16D 3102, F15B 1108

Patent

active

055751504

ABSTRACT:
Disclosed is a stiffness enhanced electrohydrostatic actuator for aircraft flight controls which eliminates the requirement for a central hydraulic system. The actuator replicates the blocked port condition of the central hydraulic system to provide static and dynamic stiffness by the use of valves having a first sleeve and spool and a second sleeve and spool disposed on either side of a valve seat with the first spool biased towards the valve seat.

REFERENCES:
patent: 2657533 (1953-11-01), Schanzlin et al.
patent: 3408035 (1968-10-01), Lathrop II et al.
patent: 3747351 (1973-07-01), Wilkerson et al.
patent: 3908687 (1975-09-01), Wood
patent: 3974742 (1976-08-01), Johnson
patent: 4266464 (1981-05-01), Baatrup et al.
patent: 4286432 (1981-09-01), Burrons et al.
patent: 4293051 (1981-10-01), Nishikawa
patent: 4669494 (1987-06-01), McBeth
patent: 5136929 (1992-08-01), Kervagoret
patent: 5214997 (1993-06-01), Lebret

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

Stiffness enhanced electrohydrostatic actuator does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Stiffness enhanced electrohydrostatic actuator, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Stiffness enhanced electrohydrostatic actuator will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-532967

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