CN203431068U - Hydraulic retarder oil circuit structure for reducing no-load loss - Google Patents
Hydraulic retarder oil circuit structure for reducing no-load loss Download PDFInfo
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- CN203431068U CN203431068U CN201320559513.7U CN201320559513U CN203431068U CN 203431068 U CN203431068 U CN 203431068U CN 201320559513 U CN201320559513 U CN 201320559513U CN 203431068 U CN203431068 U CN 203431068U
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Abstract
The utility model discloses a hydraulic retarder oil circuit structure for reducing no-load loss. The hydraulic retarder oil circuit structure comprises a working chamber, a heat exchanger and an oil tank which are sequentially communicated, and a bypass valve is arranged on an oil circuit between a bypass orifice of the working chamber and the heat exchanger. When a hydraulic retarder is no-load, air exists in the working chamber, the bypass valve is constantly open at the moment, the air in the working chamber is driven by a rotor impeller to flow back to the working chamber through the bypass valve and an oil inlet of the working chamber, small circulating airflow is formed, accordingly, residual torque can be reduced, the no-load loss of the hydraulic retarder is reduced, service cost is reduced, and the service performance of the hydraulic retarder is improved. When the retarder works, the bypass valve is closed, and the torque of the hydraulic retarder is greatly improved.
Description
Technical field
The utility model relates to hydrodynamic retarder, particularly a kind of hydrodynamic retarder oil channel structures that reduces open circuit loss.
Background technique
Hydrodynamic retarder is a kind of complemental brake system for motor vehicle, mainly by stator impeller, impeller of rotor, retarder housing, active chamber, heat exchanger and fuel tank, formed, its essence is a kind of rotary damping device, utilize impeller of rotor to drive working solution and stator impeller to impact, produce reverse vortex moment of torsion, the heat energy that is working solution by the kinetic transformation of vehicle, and then make vehicle deceleration.The working solution of active chamber is under the drive of impeller of rotor, through retarder oil outlet, enter heat exchanger and carry out oil water heat exchange, from filler opening, flow back to active chamber again, thereby the heat energy of working solution is taken away the heat energy of working solution by the mode of cools down by the cooling water from engine-cooling system.
Fig. 1 is the hydrodynamic retarder oil channel structures figure of current known reduction open circuit loss.As shown in Figure 1, it comprises the oil channel structures being formed by active chamber 14, heat exchanger 11 and fuel tank 51 order connections, when hydrodynamic retarder is worked, working solution enters heat exchanger 11 from active chamber 14 through the oil outlet 52 of active chamber and carries out oil water heat exchange, from the filler opening 53 of active chamber, flow back to active chamber 14 again, form a major cycle.
When hydrodynamic retarder quits work, working solution enters heat exchanger 11 from active chamber 14 through oil outlet 52 and flows back to fuel tank 51, now in heat exchanger, store working solution, make gas in active chamber 14 heat exchanger 11 of can not flowing through form recycle gas, thereby the gas that the interior gathering of active chamber 14 is a large amount of, gas in active chamber 14 impacts stator impeller under the drive of impeller of rotor, has produced higher residual torque, has improved the open circuit loss of retarder.
Summary of the invention
The purpose of this utility model is, a kind of hydrodynamic retarder oil channel structures that reduces open circuit loss is provided, the high problem of residual torque when solution hydrodynamic retarder is not worked, and reduce its open circuit loss and reduce automobile user cost.
The technological scheme that the utility model adopted is for achieving the above object:
A hydrodynamic retarder oil channel structures for open circuit loss, it comprises by active chamber, heat exchanger and fuel tank and is sequentially communicated with the oil channel structures forming, the by-pass port of this active chamber and the oil circuit between heat exchanger are provided with bypass valve.
The oil outlet of this bypass valve is connected with the filler opening of active chamber.
Described bypass valve comprises valve seat and the valve gap being interlocked, in the valve pocket of this valve seat, be provided with spool, one end of this valve pocket is provided with bypass valve oil outlet, the other end of this valve pocket is provided with sealing surface, the corresponding sealing face of sealed end of this spool, between at least one end of this valve pocket and the sealed end of spool, be provided with a spring, described valve gap is provided with bypass valve oil inlet hole.
Described bypass valve is located in the position, chamber on hydrodynamic retarder housing, between the wall of this valve seat and position, chamber, be provided with some seal rings, described by-pass port is located on the wall of position, chamber and is communicated with this bypass valve oil inlet hole, in this position, chamber, be also provided with a fuel-displaced district being connected with bypass valve oil outlet, this fuel-displaced district is connected with heat exchanger.
On this position, chamber, be also provided with the through hole that a fuel-displaced district is connected, this through hole is connected with the filler opening of active chamber.
Described valve gap is provided with one first pilot hole, and the guide end of this spool is mounted slidably in this first pilot hole, and the end of this valve gap is provided with oil drainage hole.
In described valve pocket, be provided with one second pilot hole, the guide end of this spool is mounted slidably in this second pilot hole.
Described sealing surface is the conical surface, curved surface or plane, and described sealed end is cylindric or spherical shape, is provided with boss or the depression matching with this spring in sealing end.
The oil outlet of this active chamber and the oil circuit between heat exchanger are provided with an oil outlet one-way valve.
A hydrodynamic retarder oil channel structures for open circuit loss, it comprises by active chamber, heat exchanger, fuel tank and is sequentially communicated with the oil channel structures forming, the by-pass port of this active chamber and the oil circuit between heat exchanger are provided with bypass valve; The oil outlet of this bypass valve is connected with the filler opening of active chamber; Described bypass valve comprises valve seat and the valve gap being interlocked, in the valve pocket of this valve seat, be provided with spool, one end of this valve pocket is provided with bypass valve oil outlet, the other end of this valve pocket is provided with sealing surface, the corresponding sealing face of sealed end of this spool, between at least one end of this valve pocket and the sealed end of spool, be provided with a spring, described valve gap is provided with bypass valve oil inlet hole; Described bypass valve is located in the position, chamber on hydrodynamic retarder housing, between the wall of this valve seat and position, chamber, be provided with some seal rings, described by-pass port is located on the wall of position, chamber and is communicated with this bypass valve oil inlet hole, in this position, chamber, be also provided with a fuel-displaced district being connected with bypass valve oil outlet, this fuel-displaced district is connected with heat exchanger; On this position, chamber, be also provided with the through hole that a fuel-displaced district is connected, this through hole is connected with the filler opening of active chamber; Described valve gap is provided with one first pilot hole, and the guide end of this spool is mounted slidably in this first pilot hole, and the end of this valve gap is provided with oil drainage hole; Described sealing surface is the conical surface, curved surface or plane, and described sealed end is cylindric or spherical shape, is provided with boss or the depression matching with this spring in sealing end; The oil outlet of this active chamber and the oil circuit between heat exchanger are provided with an oil outlet one-way valve.
The beneficial effects of the utility model are:
(1) when this hydrodynamic retarder is unloaded, air in active chamber is under the drive of impeller of rotor, filler opening through bypass valve and active chamber flows back to active chamber, forms short circle air-flow, or also has part air to pass through respectively the oil outlet of bypass valve and active chamber, then through heat exchanger, flow back to active chamber, form another short circle air-flow, to reduce the effect of residual torque, reduce hydrodynamic retarder open circuit loss, reduce user's user cost, improved the usability of hydrodynamic retarder simultaneously.
(2) when retarder is worked, bypass valve is shut, and bypass valve oil circuit disconnects, and the moment of torsion of hydrodynamic retarder has been improved greatly.
(3) simplify the structure of hydrodynamic retarder oil circuit, improved retarder oil circuit realizability, and improved the overall performance of hydrodynamic retarder.
(4) reduce the component of hydrodynamic retarder, made retarder compacter, alleviated weight, reduced the cost of hydrodynamic retarder.
Below in conjunction with accompanying drawing and embodiment, the utility model is further illustrated.
Accompanying drawing explanation
Fig. 1 is the hydrodynamic retarder oil channel structures schematic diagram of existing known reduction open circuit loss;
Fig. 2 is the utility model hydrodynamic retarder embodiment 1 structural representation;
Fig. 3 is the utility model hydrodynamic retarder embodiment 2,3 structural representation;
Fig. 4 is the utility model embodiment 1 structural representation;
Fig. 5 is the utility model embodiment 2 structural representation;
Fig. 6 is structural representation Fig. 1 of the utility model embodiment 3;
Fig. 7 is the sectional view of valve gap in the utility model;
Fig. 8 is the left view of valve gap in the utility model;
Fig. 9 is the first structural representation of spool in the utility model embodiment 1,3;
Figure 10 is the second structural representation of spool in the utility model embodiment 1,3;
Figure 11 is the third structural representation of spool in the utility model embodiment 1,3;
Figure 12 is the structural representation of valve seat in the utility model.
Embodiment
Embodiment 1: Fig. 2, Fig. 4 and Fig. 7 to Figure 12 show first embodiment of the present utility model, a kind of hydrodynamic retarder oil channel structures that reduces open circuit loss of the utility model, it comprises the oil channel structures being formed by active chamber 14, heat exchanger 11 and fuel tank 51 order connections, and the by-pass port 13 of this active chamber 14 and the oil circuit between heat exchanger 11 are provided with bypass valve 2.
Described bypass valve 2 comprises valve seat 24 and the valve gap 22 being interlocked, in the valve pocket 132 of this valve seat 24, be provided with spool 23, one end of this valve pocket 132 is provided with bypass valve oil outlet 1321, the other end of this valve pocket 132 is provided with sealing surface, the corresponding sealing face of sealed end 231 of this spool 23, between at least one end of this valve pocket 132 and the sealed end 231 of spool 23, be provided with a spring 6, in the present embodiment, spring 6 is connected in this valve pocket 132 and is provided with between one end of bypass valve oil outlet 1321 and the sealed end 231 of spool 23, and described valve gap 22 is provided with bypass valve oil inlet hole 224.This bypass valve oil inlet hole 224 is 4,6 or 8, and this bypass valve oil inlet hole 224 is arranged on identical graduation circle or different standard pitch circles.
Described bypass valve 2 is located in the position, chamber 52 on hydrodynamic retarder housing, between this valve seat 24 and the wall of position, chamber 52, be provided with some seal rings 25, described by-pass port 13 is located on the wall of position, chamber 52 and is communicated with this bypass valve oil inlet hole 224, in this position, chamber 52, be also provided with a fuel-displaced district 122 being connected with bypass valve oil outlet 1321, this fuel-displaced district 122 is connected with heat exchanger 11.
Described valve gap 22 is provided with one first pilot hole 225, and the guide end 232 of this spool 23 is mounted slidably in this first pilot hole 225, and the end of this valve gap 22 is provided with oil drainage hole 223.
Described sealing surface 245 is the conical surface, curved surface or plane.
Described sealed end 231 is cylindric or spherical shape, in sealing end 231, is provided with the boss 234 matching with this spring 6 or caves in 233.
As shown in Figure 9, sealing end 231 is cylindric, and sealing end 231 is provided with depression 233, as shown in figure 10, sealing end 231 is spherical shape, and sealing end 231 is provided with depression 233, as shown in figure 11, sealing end 231 is spherical shape, and sealing end 231 is provided with boss 234.
Filler opening 53 and the oil circuit between fuel tank 51 of this active chamber 14 are provided with a filler opening one-way valve 4.
In the time of this hydrodynamic retarder work, working solution enters into active chamber 14 from fuel tank 51, pressure in active chamber 14 increases gradually, when leading to the working fluid pressure of bypass valve 2 while being greater than the active force of these bypass valve 2 inner springs 6, the sealed end 231 of spool 23 is closed with the sealing surface of valve seat 24, thereby bypass valve 2 is shut, now working solution is undertaken after heat exchange by the oil outlet 52 of active chamber 14 heat exchanger 11 of flowing through, from the filler opening 53 of active chamber 14, flow back to active chamber 14 formation major cycle again, the moment of torsion that now hydrodynamic retarder produces is maximum;
When this hydrodynamic retarder quits work, the working solution that active chamber is 14 li is Rapid Flow oil sump tank 51 under the drive of the impeller of rotor of hydrodynamic retarder, pressure fast-descending in active chamber 14, when leading to the working fluid pressure of bypass valve 2 while being less than the active force of these bypass valve 2 inner springs 6, bypass valve 2 is opened, now oil outlet one-way valve 3 is closed, a small amount of working solution in active chamber 14 flows back to fuel tank 51 from bypass valve 2, make hydrodynamic retarder residual torque decline rapidly, reduce the open circuit loss of this hydrodynamic retarder.
When this hydrodynamic retarder is unloaded, active chamber 14 communicates with atmosphere, now bypass valve 2 is in open mode, air in active chamber 14 is under the drive of impeller of rotor, a part of gas passes through respectively the oil outlet 52 of bypass valve 2 and active chamber 14, then through heat exchanger 11, flow back to active chamber 14, form a short circle air-flow; Thereby reduction residual torque, reduces the open circuit loss of this hydrodynamic retarder.
(1) when this hydrodynamic retarder is unloaded, air in active chamber 14 is under the drive of impeller of rotor, filler opening 53 through bypass valve 2 and active chamber 14 flows back to active chamber 14, form short circle air-flow, to reduce the effect of residual torque, reduce hydrodynamic retarder open circuit loss, reduced user's user cost, improved the usability of hydrodynamic retarder simultaneously.
(2) when retarder is worked, bypass valve 2 is shut, and bypass valve 2 oil circuits disconnect, and the moment of torsion of hydrodynamic retarder has been improved greatly.
(3) simplify the structure of hydrodynamic retarder oil circuit, improved retarder oil circuit realizability, and improved the overall performance of hydrodynamic retarder.
(4) reduce the component of hydrodynamic retarder, made retarder compacter, alleviated weight, reduced the cost of hydrodynamic retarder.
embodiment 2:fig. 2 and Fig. 5 show second embodiment of the present utility model, a kind of hydrodynamic retarder oil channel structures that reduces open circuit loss of the utility model, it comprises the oil channel structures being formed by active chamber 14, heat exchanger 11 and fuel tank 51 order connections, and the by-pass port 13 of this active chamber 14 and the oil circuit between heat exchanger 11 are provided with bypass valve 2.
Described bypass valve 2 comprises valve seat 24 and the valve gap 22 being interlocked, in the valve pocket 132 of this valve seat 24, be provided with spool 23, one end of this valve pocket 132 is provided with bypass valve oil outlet 1321, the other end of this valve pocket 132 is provided with sealing surface, the corresponding sealing face of sealed end 231 of this spool 23, between at least one end of this valve pocket 132 and the sealed end 231 of spool 23, be provided with a spring 6, in the present embodiment, spring 6 is connected in this valve pocket 132 and is provided with between one end of bypass valve oil outlet 1321 and the sealed end 231 of spool 23, and described valve gap 22 is provided with bypass valve oil inlet hole 224.This bypass valve oil inlet hole 224 is 4,6 or 8, and this bypass valve oil inlet hole 224 is arranged on identical graduation circle or different standard pitch circles.
Described bypass valve 2 is located in the position, chamber 52 on hydrodynamic retarder housing, between this valve seat 24 and the wall of position, chamber 52, be provided with some seal rings 25, described by-pass port 13 is located on the wall of position, chamber 52 and is communicated with this bypass valve oil inlet hole 224, in this position, chamber 52, be also provided with a fuel-displaced district 122 being connected with bypass valve oil outlet 1321, this fuel-displaced district 122 is connected with heat exchanger 11.
In described valve pocket 132, be provided with one second pilot hole, the guide end 232 of this spool 23 is mounted slidably in this second pilot hole.
Described sealing surface 245 is the conical surface, curved surface or plane.
Described sealed end 231 is cylindric or spherical shape, in sealing end 231, is provided with the boss 234 matching with this spring 6 or caves in 233.
As shown in Figure 9, sealing end 231 is cylindric, and sealing end 231 is provided with depression 233, as shown in figure 10, sealing end 231 is spherical shape, and sealing end 231 is provided with depression 233, as shown in figure 11, sealing end 231 is spherical shape, and sealing end 231 is provided with boss 234.
Filler opening 53 and the oil circuit between fuel tank 51 of this active chamber 14 are provided with a filler opening one-way valve 4.
In the time of this hydrodynamic retarder work, working solution enters into active chamber 14 from fuel tank 51, pressure in active chamber 14 increases gradually, when leading to the working fluid pressure of bypass valve 2 while being greater than the active force of these bypass valve 2 inner springs 6, the sealed end 231 of spool 23 is closed with the sealing surface of valve seat 24, thereby bypass valve 2 is shut, now working solution is undertaken after heat exchange by the oil outlet 52 of active chamber 14 heat exchanger 11 of flowing through, from the filler opening 53 of active chamber 14, flow back to active chamber 14 formation major cycle again, the moment of torsion that now hydrodynamic retarder produces is maximum;
When this hydrodynamic retarder quits work, the working solution that active chamber is 14 li is Rapid Flow oil sump tank 51 under the drive of the impeller of rotor of hydrodynamic retarder, pressure fast-descending in active chamber 14, when leading to the working fluid pressure of bypass valve 2 while being less than the active force of these bypass valve 2 inner springs 6, bypass valve 2 is opened, now oil outlet one-way valve 3 is closed, a small amount of working solution in active chamber 14 flows back to fuel tank 51 from bypass valve 2, make hydrodynamic retarder residual torque decline rapidly, reduce the open circuit loss of this hydrodynamic retarder.
When this hydrodynamic retarder is unloaded, active chamber 14 communicates with atmosphere, now bypass valve 2 is in open mode, air in active chamber 14 is under the drive of impeller of rotor, a part of gas passes through respectively the oil outlet 52 of bypass valve 2 and active chamber 14, then through heat exchanger 11, flows back to active chamber 14, forms a short circle air-flow, thereby reduction residual torque, reduces the open circuit loss of this hydrodynamic retarder.
(1) when this hydrodynamic retarder is unloaded, air in active chamber 14 is under the drive of impeller of rotor, filler opening 53 through bypass valve 2 and active chamber 14 flows back to active chamber 14, form short circle air-flow, to reduce the effect of residual torque, reduce hydrodynamic retarder open circuit loss, reduced user's user cost, improved the usability of hydrodynamic retarder simultaneously.
(2) when retarder is worked, bypass valve 2 is shut, and bypass valve 2 oil circuits disconnect, and the moment of torsion of hydrodynamic retarder has been improved greatly.
(3) simplify the structure of hydrodynamic retarder oil circuit, improved retarder oil circuit realizability, and improved the overall performance of hydrodynamic retarder.
(4) reduce the component of hydrodynamic retarder, made retarder compacter, alleviated weight, reduced the cost of hydrodynamic retarder.
embodiment 3:fig. 3, Fig. 6 and Fig. 7 to Figure 11 show the 3rd embodiment of the present utility model, a kind of hydrodynamic retarder oil channel structures that reduces open circuit loss of the utility model, it comprises the oil channel structures being formed by active chamber 14, heat exchanger 11 and fuel tank 51 order connections, and the by-pass port 13 of this active chamber 14 and the oil circuit between heat exchanger 11 are provided with bypass valve 2.The oil outlet of this bypass valve 2 is connected with the filler opening 53 of active chamber 14.
Described bypass valve 2 comprises valve seat 24 and the valve gap 22 being interlocked, in the valve pocket 132 of this valve seat 24, be provided with spool 23, one end of this valve pocket 132 is provided with bypass valve oil outlet 1321, the other end of this valve pocket 132 is provided with sealing surface, the corresponding sealing face of sealed end 231 of this spool 23, between at least one end of this valve pocket 132 and the sealed end 231 of spool 23, be provided with a spring 6, in the present embodiment, spring 6 is connected in this valve pocket 132 and is provided with between one end of bypass valve oil outlet 1321 and the sealed end 231 of spool 23, and described valve gap 22 is provided with bypass valve oil inlet hole 224.This bypass valve oil inlet hole 224 is 4,6 or 8, and this bypass valve oil inlet hole 224 is arranged on identical graduation circle or different standard pitch circles.
Described bypass valve 2 is located in the position, chamber 52 on hydrodynamic retarder housing, between this valve seat 24 and the wall of position, chamber 52, be provided with some seal rings 25, described by-pass port 13 is located on the wall of position, chamber 52 and is communicated with this bypass valve oil inlet hole 224, in this position, chamber 52, be also provided with a fuel-displaced district 122 being connected with bypass valve oil outlet 1321, this fuel-displaced district 122 is connected with heat exchanger 11.
On this position, chamber 52, be also provided with the through hole 121 that a fuel-displaced district 122 is connected, this through hole 121 is connected with the filler opening 53 of active chamber 14.
Described valve gap 22 is provided with one first pilot hole 225, and the guide end 232 of this spool 23 is mounted slidably in this first pilot hole 225, and the end of this valve gap 22 is provided with oil drainage hole 223.
Described sealing surface is the conical surface, curved surface or plane.
Described sealed end 231 is cylindric or spherical shape, in sealing end 231, is provided with the boss 234 matching with this spring 6 or caves in 233.
As shown in Figure 9, sealing end 231 is cylindric, and sealing end 231 is provided with depression 233, as shown in figure 10, sealing end 231 is spherical shape, and sealing end 231 is provided with depression 233, as shown in figure 11, sealing end 231 is spherical shape, and sealing end 231 is provided with boss 234.
In the time of this hydrodynamic retarder work, working solution enters into active chamber 14 from fuel tank 51, pressure in active chamber 14 increases gradually, when leading to the working fluid pressure of bypass valve 2 while being greater than the active force of these bypass valve 2 inner springs 6, the sealed end 231 of spool 23 is closed with the sealing surface of valve seat 24, thereby bypass valve 2 is shut, now working solution is undertaken after heat exchange by the oil outlet 52 of active chamber 14 heat exchanger 11 of flowing through, from the filler opening 53 of active chamber 14, flow back to active chamber 14 formation major cycle again, the moment of torsion that now hydrodynamic retarder produces is maximum;
When this hydrodynamic retarder quits work, the working solution that active chamber is 14 li is Rapid Flow oil sump tank 51 under the drive of the impeller of rotor of hydrodynamic retarder, pressure fast-descending in active chamber 14, when leading to the working fluid pressure of bypass valve 2 while being less than the active force of these bypass valve 2 inner springs 6, bypass valve 2 is opened, now oil outlet one-way valve 3 is closed, a small amount of working solution in active chamber 14 flows back to fuel tank 51 from bypass valve 2, make hydrodynamic retarder residual torque decline rapidly, reduce the open circuit loss of this hydrodynamic retarder.
When this hydrodynamic retarder is unloaded, active chamber 14 communicates with atmosphere, now bypass valve 2 is in open mode, air in active chamber 14 is under the drive of impeller of rotor, a part of gas passes through respectively the oil outlet 52 of bypass valve 2 and active chamber 14, then through heat exchanger 11, flow back to active chamber 14, form a short circle air-flow; Also have another part gas filler opening 53 by active chamber 14 after bypass valve 2 to flow back to active chamber 14, form another short circle air-flow, thereby reduce residual torque, reduce the open circuit loss of this hydrodynamic retarder.
(1) when this hydrodynamic retarder is unloaded, air in active chamber 14 is under the drive of impeller of rotor, filler opening 53 through bypass valve 2 and active chamber 14 flows back to active chamber 14, form short circle air-flow, also have part air to pass through respectively the oil outlet 52 of bypass valve 2 and active chamber 14, then through heat exchanger 11, flow back to active chamber 14, form another short circle air-flow, to reduce the effect of residual torque, reduce hydrodynamic retarder open circuit loss, reduce user's user cost, improved the usability of hydrodynamic retarder simultaneously.
(2) when retarder is worked, bypass valve 2 is shut, and bypass valve 2 oil circuits disconnect, and the moment of torsion of hydrodynamic retarder has been improved greatly.
(3) simplify the structure of hydrodynamic retarder oil circuit, improved retarder oil circuit realizability, and improved the overall performance of hydrodynamic retarder.
(4) reduce the component of hydrodynamic retarder, made retarder compacter, alleviated weight, reduced the cost of hydrodynamic retarder.
The foregoing is only preferred embodiment of the present utility model, all equalizations of doing according to the utility model claim scope change and modify, and all should belong to the covering scope of the utility model claim.
Claims (10)
1. reduce a hydrodynamic retarder oil channel structures for open circuit loss, it comprises by active chamber, heat exchanger, fuel tank and is sequentially communicated with the oil channel structures forming, and it is characterized in that: the by-pass port of this active chamber and the oil circuit between heat exchanger are provided with bypass valve.
2. the hydrodynamic retarder oil channel structures that reduces according to claim 1 open circuit loss, is characterized in that, the oil outlet of this bypass valve is connected with the filler opening of active chamber.
3. according to the hydrodynamic retarder oil channel structures that reduces open circuit loss described in claim 1 or 2, it is characterized in that, described bypass valve comprises valve seat and the valve gap being interlocked, in the valve pocket of this valve seat, be provided with spool, one end of this valve pocket is provided with bypass valve oil outlet, and the other end of this valve pocket is provided with sealing surface, the corresponding sealing face of sealed end of this spool, between at least one end of this valve pocket and the sealed end of spool, be provided with a spring, described valve gap is provided with bypass valve oil inlet hole.
4. reduce according to claim 3 the hydrodynamic retarder oil channel structures of open circuit loss, it is characterized in that, described bypass valve is located in the position, chamber on hydrodynamic retarder housing, between the wall of this valve seat and position, chamber, be provided with some seal rings, described by-pass port is located on the wall of position, chamber and is communicated with this bypass valve oil inlet hole, in this position, chamber, be also provided with a fuel-displaced district being connected with bypass valve oil outlet, this fuel-displaced district is connected with heat exchanger.
5. the hydrodynamic retarder oil channel structures that reduces according to claim 4 open circuit loss, is characterized in that, is also provided with the through hole that a fuel-displaced district is connected on this position, chamber, and this through hole is connected with the filler opening of active chamber.
6. the hydrodynamic retarder oil channel structures that reduces according to claim 3 open circuit loss, is characterized in that, described valve gap is provided with one first pilot hole, and the guide end of this spool is mounted slidably in this first pilot hole, and the end of this valve gap is provided with oil drainage hole.
7. the hydrodynamic retarder oil channel structures that reduces according to claim 3 open circuit loss, is characterized in that, is provided with one second pilot hole in described valve pocket, and the guide end of this spool is mounted slidably in this second pilot hole.
8. reduce according to claim 3 the hydrodynamic retarder oil channel structures of open circuit loss, it is characterized in that, described sealing surface is the conical surface, curved surface or plane, and described sealed end is cylindric or spherical shape, is provided with boss or the depression matching with this spring in sealing end.
9. the hydrodynamic retarder oil channel structures that reduces according to claim 1 open circuit loss, is characterized in that, the oil outlet of this active chamber and the oil circuit between heat exchanger are provided with an oil outlet one-way valve.
10. reduce a hydrodynamic retarder oil channel structures for open circuit loss, it comprises by active chamber, heat exchanger, fuel tank and is sequentially communicated with the oil channel structures forming, and it is characterized in that: the by-pass port of this active chamber and the oil circuit between heat exchanger are provided with bypass valve; The oil outlet of this bypass valve is connected with the filler opening of active chamber; Described bypass valve comprises valve seat and the valve gap being interlocked, in the valve pocket of this valve seat, be provided with spool, one end of this valve pocket is provided with bypass valve oil outlet, the other end of this valve pocket is provided with sealing surface, the corresponding sealing face of sealed end of this spool, between at least one end of this valve pocket and the sealed end of spool, be provided with a spring, described valve gap is provided with bypass valve oil inlet hole; Described bypass valve is located in the position, chamber on hydrodynamic retarder housing, between the wall of this valve seat and position, chamber, be provided with some seal rings, described by-pass port is located on the wall of position, chamber and is communicated with this bypass valve oil inlet hole, in this position, chamber, be also provided with a fuel-displaced district being connected with bypass valve oil outlet, this fuel-displaced district is connected with heat exchanger; On this position, chamber, be also provided with the through hole that a fuel-displaced district is connected, this through hole is connected with the filler opening of active chamber; Described valve gap is provided with one first pilot hole, and the guide end of this spool is mounted slidably in this first pilot hole, and the end of this valve gap is provided with oil drainage hole; Described sealing surface is the conical surface, curved surface or plane, and described sealed end is cylindric or spherical shape, is provided with boss or the depression matching with this spring in sealing end; The oil outlet of this active chamber and the oil circuit between heat exchanger are provided with an oil outlet one-way valve.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320559513.7U CN203431068U (en) | 2013-09-10 | 2013-09-10 | Hydraulic retarder oil circuit structure for reducing no-load loss |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320559513.7U CN203431068U (en) | 2013-09-10 | 2013-09-10 | Hydraulic retarder oil circuit structure for reducing no-load loss |
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| Publication Number | Publication Date |
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| CN203431068U true CN203431068U (en) | 2014-02-12 |
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|---|---|---|---|
| CN201320559513.7U Withdrawn - After Issue CN203431068U (en) | 2013-09-10 | 2013-09-10 | Hydraulic retarder oil circuit structure for reducing no-load loss |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103671637A (en) * | 2013-09-10 | 2014-03-26 | 深圳市特尔佳科技股份有限公司 | Oil circuit structure of hydrodynamic retarder and method for lowering no-load loss of hydrodynamic retarder |
| CN114321222A (en) * | 2021-12-31 | 2022-04-12 | 富奥汽车零部件股份有限公司 | Retarder oil supply method and retarder oil supply system |
-
2013
- 2013-09-10 CN CN201320559513.7U patent/CN203431068U/en not_active Withdrawn - After Issue
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103671637A (en) * | 2013-09-10 | 2014-03-26 | 深圳市特尔佳科技股份有限公司 | Oil circuit structure of hydrodynamic retarder and method for lowering no-load loss of hydrodynamic retarder |
| CN114321222A (en) * | 2021-12-31 | 2022-04-12 | 富奥汽车零部件股份有限公司 | Retarder oil supply method and retarder oil supply system |
| CN114321222B (en) * | 2021-12-31 | 2023-07-04 | 富奥汽车零部件股份有限公司 | Retarder oil supply method and retarder oil supply system |
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Granted publication date: 20140212 Effective date of abandoning: 20170503 |