Variable capacity type pump

Rotary expansible chamber devices – With changeable working chamber magnitude – By cylinder or cylinder portion pivotal movement

Reexamination Certificate

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Details

C418S150000, C418S031000, C418S259000, C418S269000, C417S204000, C417S220000, C417S315000

Reexamination Certificate

active

06503068

ABSTRACT:

BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to a variable capacity type pump used in a power steering apparatus for a motor vehicle or the like.
2. Description of the Related Art
Conventionally, a variable capacity type pump used in a power steering apparatus for a motor vehicle or the like, as shown in Japanese Patent Application Laid-Open (JP-A) No. 9-14155, has a structure which has a cam ring being eccentric with respect to a rotor arranged in a pump casing so as to be rotated, forms a pump chamber between a cam ring and an outer peripheral portion of the rotor, increases an eccentricity amount of the cam ring with respect to the rotor during low speed rotation of the pump, thereby increasing the capacity of the pump chamber and increasing the discharge amount of a working fluid, and reduces the eccentricity amount of the cam ring with respect to the rotor at a time of a high speed rotation of the pump, thereby reducing the capacity of the pump chamber and reducing the discharge amount of the working fluid.
In the conventional art mentioned above, in order to reduce the pressure pulsation of the variable capacity type vane pump, and the vibration and sound induced therefrom, spaces of two closed portions comprised of a first closed portion formed by closing a suction port and a discharge port at a bottom dead center and a second closed portion formed by closing the discharge port and the suction port at a top dead center, among the pump chamber surrounded by the cam ring and the rotor are both formed as a space surrounded by a concentric circle around the center of rotation of the rotor under a maximum eccentric condition of the cam ring (in other words, a dynamic radius of the vane is set to be constant). In the conventional art, since a distance between the rotor and the cam ring in the closed portion is constant, an over compression on the basis of a capacity change of the pump chamber is not generated, so that it is possible to prevent a pulsation phenomenon on the basis of moving apart of the vane.
In the conventional art, since the structure is made such that the distance between the rotor and the cam ring becomes constant (that is, concentric) in the closed portion during the maximum eccentricity of the cam ring when the pump rotates at a low speed, an inner periphery of the cam ring and an outer periphery of the rotor are not concentric when the eccentricity amount becomes small during high speed rotation, so that it is impossible to prevent the vane from moving apart, and a great pressure pulsation caused by an increase of leakage in a gap at a front end of the vane is generated. Further, in the conventional art, it is considered that the moving apart of the vane is caused by the over compression within the closed chamber. However, by right as described below, the moving apart of the vane is mainly caused by an offset load on the basis of an unbalance between pressures applied to a front surface and a back surface of the vane existing in the closed section.
In
FIG. 14
, under a state that a vane
2
received in a groove of a rotor
1
receives a force in a centrifugal direction by a back pressure Pd and a centrifugal force so as to be in contact with an inner periphery of a cam ring
3
, and the vane
2
rotates together with a rotation of the rotor
1
, in a suction section until one vane
2
A reaches an end point of a suction port
4
, since the same suction pressure is applied to a front surface and a back surface of the vane
2
A, no offset load is applied in a circumferential direction, and the front end of the vane
2
A is pressed to the inner periphery of the cam ring
3
due to the back pressure Pd and the centrifugal force and does not move apart from the inner periphery of the cam ring
3
. When the vane
2
exists in a first closed section which is not yet connected to a start point of a discharge port
5
after the vane
2
further rotates together with the rotation of the rotor
1
and the vane
2
A passes through the suction section, a high pressure in a side of the discharge port
5
and a low pressure in a side of the suction port
4
are respectively applied to the front surface of the vane
2
A and the back surface thereof. The offset load is then applied to the vane
2
A in a circumferential direction, the vane
2
A is inclined in a root portion received within the groove of the rotor
1
so as to be caught thereon. The vane
2
A can not be pressed against the inner periphery of the cam ring
3
even by the back pressure Pd and the centrifugal force so as to move apart from the inner periphery of the cam ring
3
, whereby the great leakage mentioned above from the discharge port
5
to the suction port
4
is generated with passing through the front end gap of the vane moving apart therefrom. Further, in the second closed section, the same phenomenon is generated.
A detailed description will be given below of problems in the conventional art. In the conventional art, under the maximum eccentric state (during low speed rotation), the inner periphery of the cam ring in the first closed portion and the second closed portion is formed in the concentric circle with the center of rotation of the rotor. Accordingly, since the dynamic radius of the vane in the closed section is constant at a time of the low speed rotation, the moving apart of the vane is not generated (FIGS.
15
A and
16
A), whereby it is possible to prevent the great pressure pulsation from being generated due to the moving apart. However, under the minimum eccentric state (during high speed rotation), the inner periphery of the cam ring is not the concentric circle with the center of rotation of the rotor together with the first closed portion and the second closed portion, and when the vane is caught on due to the offset load on the basis of the unbalance of pressure between the front surface and the back surface, the front end of the vane moves apart from the inner surface of the cam ring and the great pressure pulsation is generated.
That is,
FIGS. 15A and 15B
show a motion of the vane front end in the first closed portion by setting an angle of rotation of the rotor to a horizontal axis and setting a dynamic radius corresponding to a protruding radius of the vane with respect to the center of rotation of the rotor to a vertical axis, in which a solid line relates to the cam ring corresponding to the concentric circle with the center of rotation of the rotor, and a broken line relates to the cam ring formed in a completed round shape. In this case, since the distance between the rotor and the cam ring is constant as expressed by a relation Ha=Hb=Hc in
FIG. 17A
during low speed rotation in the first closed portion in
FIG. 15A
, the moving apart of the vane is hard to be generated. Since the cam ring becomes in the minimum eccentric state and the distance between the rotor and the cam ring becomes short in a center (Hb) of the first closed portion and becomes long in both sides (Ha, Hc) thereof as shown in
FIG. 17B
, at a time of the high speed rotation in the first closed portion in
FIG. 15B
, the vane is pressed in a centripetal direction in the front half of the first closed portion so as not to move apart. In a rear half, since the dynamic radius becomes a positive incline (a positive slope), the eccentric load is applied to the vane and the vane is caught on, so that the vane moves apart.
FIGS. 16A and 16B
show a motion of the vane front end in the second closed portion by setting an angle of rotation of the rotor to a horizontal axis and setting a dynamic radius corresponding to a protruding radius of the vane with respect to the center of rotation of the rotor to a vertical axis, in which a solid line relates to the cam ring corresponding to the concentric circle with the center of rotation of the rotor, and a broken line relates to the cam ring formed in a completed round shape. In this case, since the distance between the rotor and the cam ring is constant as expressed by a relation Hd=He=Hf in
F

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