IP Library Granted Patent US 8,418,722
Granted Patent B2
US 8,418,722 · App. 11/187,999 · Granted Apr 16, 2013

Pressure-regulator servovalve with reduced leakage rate

Inventor: Raymond Grancher (Lailly en Val, FR)
Assignee: IN-LHC
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Quick Facts
Patent No.
US 8,418,722
App. No.
11/187,999
Granted
Apr 16, 2013
Kind
B2
Abstract

The invention relates to a pressure-regulator servo-valve comprising a body having a utilization port, a pressure feed port, and a return port, a distributor spool movably mounted in the body to put the utilization port into communication either with the feed port or with the return port, the spool co-operating with the body to define at least one pilot chamber connected to a nozzle that is arranged to open out into a cavity connected to the return port, a vane extending in the cavity facing the nozzle and being mounted to be moved in controlled manner. According to the invention, the pilot chamber is connected to the utilization port.

Claims (13)

1. A pressure-regulator servo-valve for delivering an adjusted utilization pressure to a hydraulic receiver, such as a hydraulic brake, said pressure regulator comprising:

a body having:

a utilization port through which said adjusted utilization pressure is transmitted to said hydraulic receiver,

a pressure feed port through which said servo-valve is fed with pressurized fluid,

a return port through which excess fluid is returned and,

a calibrated orifice for receiving a slidable spool,

wherein said spool is movably mounted in the calibrated orifice so that a position of said spool determines said adjusted utilization pressure,

wherein said position of said spool is affected by a control pressure of fluid flowing into a pilot chamber defined in said body, said pilot chamber being permanently connected to:

a nozzle opening out into a cavity connected to said return port, and

said utilization port so that said pilot chamber is fed by said utilization port,

said pressure regulator servo-valve further comprising a vane facing said nozzle and being selectively movable for modulating said control pressure into said pilot chamber.

2. The pressure regulator servo-valve according to claim 1 , wherein said servo-valve has only one nozzle.

3. The pressure regulator servo-valve according to claim 1 , wherein said pilot chamber is connected to said utilization port via a constriction.

Assignments (5)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 17, 2024
From: SAFRAN AEROTECHNICS
To: SAFRAN AEROSYSTEMS
Reel/Frame 069715/0156 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 6, 2024
From: SAFRAN AEROSYSTEMS HYDRAULICS
To: SAFRAN AEROTECHNICS
Reel/Frame 069504/0161 →
CHANGE OF NAME Recorded Jun 9, 2021
From: IN-LHC
To: ZODIAC HYDRAULICS
Reel/Frame 056526/0449 →
CHANGE OF NAME Recorded Jun 9, 2021
From: ZODIAC HYDRAULICS
To: SAFRAN AEROSYSTEMS HYDRAULICS
Reel/Frame 056526/0466 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 25, 2005
From: GRANCHER, RAYMOND
To: IN-LHC
Reel/Frame 016812/0001 →
Priority Claims (1)
FR 04 08277 · Jul 27, 2004 · national
Continuity (1)
Related Publication 20060021663A1 · Feb 2, 2006