Pilot actuator and spool valve assembly

Valves and valve actuation – Fluid actuated or retarded – Pilot or servo type motor

Reexamination Certificate

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Details

C239S091000, C239S093000, C239S095000, C239S096000

Reexamination Certificate

active

06283441

ABSTRACT:

TECHNICAL FIELD
The present invention relates generally to control valves, and more particularly to pilot actuated spool valve assemblies.
BACKGROUND ART
In many hydraulically actuated devices, such as hydraulically actuated fuel injectors, a three way valve assembly controls the operation of the device. In general, the valve assembly opens an internal work flow passage to a high pressure passage when the device is operating, such as to hydraulically move a piston. Between operation events, the work flow passage is opened to a low pressure passage or drain so that the used fluid in the flow passage can be removed, and the device reset for its next operation event. In the case of a hydraulically actuated fuel injector, high pressure fluid acts on a pumping element to pressurize fuel during an injection event, and the pumping element retracts and resets between injection events. In some cases, the control valve assembly consists essentially of a poppet valve member that is moved between a pair of conical valve seats by a solenoid actuator.
Although the relatively simple solenoid actuated poppet valves have performed well for many years, engineers are always seeking ways to improve performance, increase reliability and reduce costs. In addition, there is often a trend to add additional functions to the control valve assembly to perform additional functions, such as controlling a direct control needle valve in a fuel injector. One response to these trends is to substitute a pilot actuated valve that utilizes a relatively small solenoid to move a small pilot member, which in turn controls the positioning of a relatively larger spool valve that opens and closes the high and low pressure passages. These pilot actuated valves can come in a variety of designs, including those in which the pilot member is a ball, or is a relatively small poppet valve member that moves between conical valve seats. While these newer pilot valve assemblies have performed well, there still remains room for improvement in areas such as reducing part count, improving concentric alignment between valve components, integrating the valve assembly in a relatively small package, and improving the ability of the valve assembly to simultaneously control two or more functions, such as fuel pressurization and injection timing.
The present invention is directed to improving upon these and other aspects of pilot actuated valve assemblies, especially as they relate to fuel injectors.
DISCLOSURE OF THE INVENTION
A pilot actuated spool valve assembly includes a valve body the defines a first passage, a second passage and a flow passage. A unitary pilot body is at least partially positioned in the valve body and has a first valve seat and a second valve seat. A pilot member is moveable in the pilot body between an up position in which the pilot member closes the first valve seat, and a down position in which the pilot member closes the second valve seat. A spool valve member has a control hydraulic surface and is positioned in the valve body. It is moveable between a first position in which the first passage is open to the flow passage, and a second position in which the second passage is open to the flow passage. At least one of the valve body, the pilot body, the pilot member and the spool valve member define a control volume fluidly connected to the first passage when the pilot member is in one of its up position and down position. The control hydraulic surface of the spool valve member is exposed to fluid pressure in the control volume.


REFERENCES:
patent: 1707541 (1929-04-01), Roth
patent: 2479359 (1949-08-01), Holt
patent: 2622618 (1952-12-01), Ghormley
patent: 2629401 (1953-02-01), Miller
patent: 2799466 (1957-07-01), Hickerson
patent: 2977984 (1961-04-01), Barnes
patent: 3312445 (1967-04-01), Trombatore et al.
patent: 3351316 (1967-11-01), Lewis et al.
patent: 3405906 (1968-10-01), Keller
patent: 3529628 (1970-09-01), Cummins
patent: 3802626 (1974-04-01), Regneault et al.
patent: 4155535 (1979-05-01), Seamone
patent: 4544096 (1985-10-01), Burnett
patent: 4585030 (1986-04-01), Fox
patent: 4618095 (1986-10-01), Spoolstra
patent: 4746093 (1988-05-01), Scanderbeg
patent: 4779837 (1988-10-01), Mito et al.
patent: 4938450 (1990-07-01), Tripp et al.
patent: 5113908 (1992-05-01), Steinke
patent: 5323964 (1994-06-01), Doszpoly et al.
patent: 5332003 (1994-07-01), Nikolayczik
patent: 5339777 (1994-08-01), Cannon
patent: 5669355 (1997-09-01), Gibson et al.
patent: 5682858 (1997-11-01), Chen et al.
patent: 5685483 (1997-11-01), Ganser
patent: 5687693 (1997-11-01), Chen et al.
patent: 5697342 (1997-12-01), Anderson et al.
patent: 5720318 (1998-02-01), Nagarajan et al.
patent: 5738075 (1998-04-01), Chen et al.
patent: 5803119 (1998-09-01), Steinke
patent: 5803429 (1998-09-01), Tsuzuki et al.
patent: 5826562 (1998-10-01), Chen et al.
patent: 5833146 (1998-11-01), Hefler
patent: 5893350 (1999-04-01), Timms
patent: 5975139 (1999-11-01), Carroll et al.
patent: 6119960 (2000-09-01), Graves
patent: 26 02 844 A1 (1977-08-01), None
patent: 1 328 959 (1973-09-01), None

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