US 2002/0000352 A1Published application

Damping force control type hydraulic shock absorber

AssigneeTokico Ltd.

InventorsTakuya Matsumoto, Takashi Nezu

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Abstract

A pilot chamber is formed at the back of a disk valve for each of the fluid flow systems for the extension and compression strokes. Damping force in a low piston speed region is controlled with a pressure control valve. The valve opening pressure of the disk valve is controlled by varying a pilot pressure introduced into the pilot chamber from a cylinder's hydraulic fluid chamber through a cut portion in a piston bolt and an orifice groove formed in a fixed member supporting the disk valve, thereby controlling damping force in a high piston speed region. A sharp pressure change occurring when the stroke direction of a piston rod changes is attenuated by the restricting action of the orifice groove so as not to be readily transmittable to the pilot chamber. Accordingly, it is possible to suppress a change in damping force due to the sharp pressure change and hence possible to obtain stable damping force.

Claims11

Dependent claims

A damping force control type hydraulic shock absorber comprising:

a cylinder having a hydraulic fluid sealed therein;
a piston slidably fitted in said cylinder to divide an inside of said cylinder into two chambers;
a piston rod connected at one end thereof to said piston, the other end of said piston rod extending to the outside of said cylinder;
a main passage and a sub-passage for allowing the hydraulic fluid to flow between said two chambers in response to sliding movement of said piston;
a pilot-operated damping valve for generating damping force by controlling flow of the hydraulic fluid in said main passage, said pilot-operated damping valve including a valve member and a pilot chamber provided such that the pressure of the hydraulic fluid in the pilot chamber urges the valve member to the valve closing position;
a fixed orifice provided in said sub-passage;
a regulating valve provided in said sub-passage at a position downstream of said fixed orifice;
a pilot passage for allowing a portion of said sub-passage between said fixed orifice and said regulating valve to communicate with said pilot chamber;
and
a restrictor provided in said pilot passage.

7 more elements

A damping force control type hydraulic shock absorber comprising:

a cylinder having a hydraulic fluid sealed therein;
a piston slidably fitted in said cylinder to divide an inside of said cylinder into a first chamber and a second chamber;
a piston rod assembly including a piston rod and a piston bolt for securing said piston to said piston rod at one end of the piston rod, the other end of said piston rod extending to the outside of said cylinder, said piston bolt having an axial bore;
a main passage including a fluid passage formed in said piston so as to communicate said first and second chambers;
a pilot-operated damping valve for generating damping force by controlling flow of the hydraulic fluid in said main passage, said damping valve comprising:
a valve member secured to said piston on one side thereof so that the valve member is subjected to the pressure of the hydraulic fluid which flows through said main passage from said first chamber to said second chamber,
a fixed member secured to said piston bolt on the side of said valve member remote from said piston, and
means provided on said fixed member so that a pilot chamber is formed between said valve member and said fixed member;
a sub-passage bypassing said pilot operated damping valve, a portion of said sub-passage being formed by a first passage formed in said piston and functioning as a fixed orifice and a second passage formed in said piston bolt so as to communicate said first passage with said axial bore of the piston bolt;
a regulating valve provided in said axial bore of said piston bolt;
a pilot passage for allowing a portion of said subpassage between said fixed orifice and said regulating valve to communicate with said pilot chamber;
and
a restrictor formed in said fixed member so as to provide a restriction to the flow in said pilot passage.

10 more elements

Dependencies are inferred from the claim text.