Fuel injection pump having hydraulic timer mechanism and load timer mechanism

Information

  • Patent Grant
  • 6782870
  • Patent Number
    6,782,870
  • Date Filed
    Wednesday, September 24, 2003
    21 years ago
  • Date Issued
    Tuesday, August 31, 2004
    20 years ago
Abstract
A load timer mechanism of a fuel injection pump includes a governor shaft, which is secured to a housing, and a governor sleeve, which is axially slidably supported around the governor shaft. The governor shaft includes a fuel relief passage, which is communicated with a low pressure side of the pump and has an outer opening in an outer peripheral surface of the governor shaft, and a first annular groove, which is recessed in the outer peripheral surface of the governor shaft such that the first annular groove is axially displaced from the outer opening. The governor sleeve includes a port, which extends between an outer peripheral surface and an inner peripheral surface of the governor sleeve, and a second annular groove, which is recessed in the inner peripheral surface of the governor sleeve such that the second annular groove is axially displaced from the port.
Description




CROSS REFERENCE TO RELATED APPLICATION




This application is based on and incorporates herein by reference Japanese Patent Application No. 2002-284146 filed on Sep. 27, 2002.




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates to a fuel injection pump and more particularly to a load timer mechanism of a fuel injection pump of a distributor type.




2. Description of Related Art




The emission regulation of diesel engines has become increasingly stringent due to the increasing environmental concern. In general, when the fuel injection timing of the diesel engine is retarded, the emission of NOx is reduced. However, when the fuel injection timing is retarded to reduce the emission of NOx, the engine power is disadvantageously reduced. To address such a problem, it is known to use of a load timer, which reduces the amount of timer advancement when the load of the engine is reduced to reduce the emission of NOx and noises without reducing the engine power under the high load condition where high engine power is required. Such a load timer is disclosed, for example, in Japanese Unexamined Patent Publication No. 57-119132.




In the prior art load timer, an orifice penetrates through a governor sleeve of a centrifugal governor, which is reciprocated according to the rotational speed of the engine. Furthermore, a fuel relief passage, which is communicated with a low pressure side of a fuel injection pump, is formed in a governor shaft, along which the governor sleeve is guided. Upon operation of the governor sleeve, when the orifice of the governor sleeve is communicated with the fuel relief passage of the governor shaft, fuel in a pump housing of the fuel injection pump is relieved into the low pressure side of the fuel injection pump through the orifice of the governor sleeve and the fuel relief passage of the governor shaft. When the fuel pressure in the pump housing is reduced, a timer piston of a hydraulic timer received in the pump housing is retarded. As a result, cam rollers, which are in rolling contact with a face cam of the fuel injection pump, are moved to retard the fuel injection timing.




However, in the prior art load timer, since the amount of timer advancement is reduced in the low load condition, misfire could occur to cause generation of white smoke emissions.




To address such a problem, according to the disclosure of Japanese Unexamined Patent Publication No. 57-119132, a solenoid valve, which opens and closes the fuel relief passage, is provided to limit timer retardation caused by the load timer under operating conditions where generation of white smoke is expected, for example, in a case of driving the vehicle at highlands or in a case of operating the engine at low coolant temperature conditions, such as at the time of engine cranking. However, due to the increasingly stringent emission regulation, the amount of emission of NOx needs to be further reduced. Thus, according to the disclosed technique, it is difficult to further improve, i.e., further increase the amount of timer retardation. That is, when the load timer is operated to further increase the timer retardation, the solenoid valve, which limits the timer retardation, is actuated. As a result, the amount of timer retardation is limited. In some cases, the load timer could become inoperable.




SUMMARY OF THE INVENTION




The present invention addresses the above disadvantages. Thus, it is an objective of the present invention to provide a fuel injection pump, which is capable of limiting the timer retardation in the low load range and the high load range and also capable of improving the timer retardation in the intermediate load range with a relatively simple structure.




To achieve the objective of the present invention, there is provided a fuel injection pump for an internal combustion engine. The fuel injection pump includes a pump housing, a hydraulic timer mechanism and a load timer mechanism. The pump housing defines a pump chamber therein. The hydraulic timer mechanism is received in the housing and adjusts fuel injection timing based on fuel pressure of the pump chamber. The load timer mechanism is received in the housing and adjusts the fuel injection timing based on a load of the engine. The load timer mechanism includes a governor shaft and a governor sleeve. The governor shaft is secured to the housing. The governor shaft includes a fuel relief passage and a first annular groove. The fuel relief passage is communicated with a low pressure side of the fuel injection pump and has an outer opening in an outer peripheral surface of the governor shaft. The first annular groove is recessed in the outer peripheral surface of the governor shaft such that the first annular groove is axially displaced from the outer opening of the fuel relief passage. The governor sleeve is axially slidably supported around the governor shaft and is moved back and forth relative to the governor shaft based on the load of the engine. The governor sleeve includes a port and a second annular groove. The port extends between an outer peripheral surface and an inner peripheral surface of the governor sleeve and includes an outer opening placed in the outer peripheral surface of the governor sleeve and an inner opening placed in the inner peripheral surface of the governor sleeve. The port conducts the fuel pressure of the pump chamber from the outer peripheral surface to the inner peripheral surface of the governor sleeve. The second annular groove is recessed in the inner peripheral surface of the governor sleeve such that the second annular groove is axially displaced from the port. When the governor sleeve is positioned within a predetermined axial range, the first annular groove and the second annular groove are at least partially overlapped one another to define a fuel pool therebetween. When the engine is in one of a full load condition and a high load condition, the first annular groove and the second annular groove are at least partially overlapped one another, and the fuel pool is not substantially communicated with the port to prevent substantial communication between the port and the fuel relief passage. When the engine is in one of a partial load condition and an intermediate load condition, the first annular groove and the second annular groove are at least partially overlapped one another, and the fuel pool is substantially communicated with the port to substantially communicate between the port and the fuel relief passage. When the engine in one of a no load condition and a low load condition, the first annular groove and the second annular groove are not substantially overlapped one another to prevent substantial communication between the port and the fuel relief passage.











BRIEF DESCRIPTION OF THE DRAWINGS




The invention, together with additional objectives, features and advantages thereof, will be best understood from the following description, the appended claims and the accompanying drawings in which:





FIG. 1

is a cross sectional view of a fuel injection pump according to an embodiment of the present invention;





FIG. 2

is a partial cross sectional view schematically showing a load timer mechanism of the fuel injection pump;





FIG. 3

is a partial cross sectional view showing a main feature of the load timer mechanism;





FIG. 4A

is a cross sectional view schematically showing a governor sleeve in a high load condition;





FIG. 4B

is a cross sectional view schematically showing the governor sleeve in a transitional range between the high load condition and an intermediate load condition;





FIG. 4C

is a cross sectional view schematically showing the governor sleeve in the intermediate load condition;





FIG. 4D

is a cross sectional view schematically showing the governor sleeve in another transitional range between the intermediate load condition and a low load condition;





FIG. 4E

is a cross sectional view schematically showing the governor sleeve in the low load condition; and





FIG. 5

is a graph showing a relationship between the fuel injection amount and timer advancement, which correspond to the fuel injection timing.











DETAILED DESCRIPTION OF THE INVENTION




A fuel injection pump according to an embodiment of the present invention will be described with reference to the accompanying drawings.




With reference to

FIG. 1

, the fuel injection pump according to the present embodiment includes a pump housing


2


, a drive shaft


1


, a rotary feed pump


3


, a pressure regulator valve


5


, a pump chamber


6


formed in the pump housing


2


, a load timer mechanism LST and a hydraulic timer mechanism HT. The drive shaft


1


is connected to a crank shaft of a diesel engine (internal combustion engine), and rotational force is transmitted to the drive shaft


1


synchronously with rotation of the diesel engine. The drive shaft


1


rotates the feed pump


3


installed in the pump housing


2


, so that the feed pump


3


pumps fuel from a fuel tank


4


. The fuel, which is pumped by the feed pump


3


, is supplied to the pressure regulator


5


where the pressure of the fuel is adjusted. Then, the fuel is supplied from the pressure regulator


5


to a pump chamber


6


formed in the pump housing


2


. Specifically, the pressure regulator valve


5


is arranged between a pump chamber side (i.e., discharge outlet side) of the feed pump


3


and a low pressure side (i.e., the fuel tank


4


side) and adjusts the pressure of the fuel to a level that is proportional to a rotational speed of the feed pump


3


. Here, it should be noted that

FIG. 1

shows both a lateral view and a frontal view (i.e., view from the left side of

FIG. 1

) of the feed pump


3


for the sake of clarity.




In the present embodiment, the fuel located on the low pressure side communicated with the fuel tank


4


is referred to as low pressure fuel, and the fuel pumped by the feed pump


3


and is supplied to the pump chamber


6


is referred to as high pressure fuel. This high pressure fuel should be distinguished from high pressure fuel (pressurized fuel), which is pressurized by a plunger


8


(described below) to supply the fuel to the engine through a fuel injection valve


20


.




As shown in

FIG. 1

, a face cam


9


is connected to the drive shaft


1


through a coupling


7


to rotate synchronously with the drive shaft


1


in an axially reciprocable manner. Furthermore, the plunger


8


is connected to an end of a base of the face cam


9


to rotate synchronously with the face cam


9


. The coupling


7


transmits rotation of the drive shaft


1


to the plunger


8


and allows axial movement of the plunger


8


.




As shown in

FIG. 1

, a cam profile


9




a


is formed in an end surface of the face cam


9


, which is opposite from the end surface of the face cam


9


, to which the plunger


8


is connected. The cam profile


9




a


of the face cam


9


includes a plurality of ridges, which are circumferentially arranged, and a number of the ridges corresponds to a number of cylinders of the engine. A plurality of cam rollers


10


are in rolling contact with the cam profile


9




a


. Through the rolling contact of the cam rollers


10


with the cam profile


9




a


, the face cam


9


and the plunger


8


reciprocate a plurality of times per rotation of the drive shaft


1


, i.e., reciprocates a plurality of times, which coincide with the number of cylinders of the engine. The shape of the cam profile


9




a


is selected to achieve the best fuel injection pressure and fuel injection timing to meet a desired engine performance.




During the intake stroke of the plunger


8


, the plunger


8


is axially moved in the left direction in FIG.


1


. At this time, when one of a plurality of intake grooves


11


, which are arranged along an outer peripheral surface of a distal end of the plunger


8


, is communicated with an intake port


12


, fuel of the pump chamber


6


is drawn into a pressurizing chamber


14


, which is defined at the distal end of the plunger


8


, through a guide passage


13


.




During compression stroke of the plunger


8


, the plunger


8


is axially moved in the right direction in FIG.


1


. When the fuel of the pressurizing chamber


14


is pressurized, the pressurized fuel is guided into a longitudinal hole


15


defined in the plunger


8


. At this time, the plunger


8


is rotated and is in sliding contact with a cylinder


2




a


formed in the housing


2


. Upon rotation of the plunger


8


, a supply port


16


, which is opened in the outer peripheral surface of the plunger


8


, is communicated with one of a plurality of discharge ports


17


, which are opened in an inner peripheral surface of the cylinder


2




a


. Thus, the pressurized fuel is supplied from an injection passage


18


to the fuel injection valve


20


through a delivery valve


19


.




A spill ring


21


is slidably fitted around the plunger


8


. The spill ring


21


opens and closes a spill port


22


formed in the plunger


8


. The spill port


22


is communicated with the longitudinal hole


15


. During the pumping operation, i.e., during the pumping of the pressurized fuel from the longitudinal hole


15


to the fuel injection valve


20


through the supply port


16


, the discharge port


17


and the injection passage


18


, when the spill port


22


is opened by the spill ring


21


, the fuel in the longitudinal hole


15


, i.e., the pressurized fuel in the pressurizing chamber


14


is relieved from the spill port


22


to the pump chamber


6


, so that the fuel pressure of the pressurized fuel is reduced. When the fuel pressure of the pressurized fuel is reduced to a level equal or below a valve closing pressure for closing the fuel injection valve


20


, the fuel supply to the fuel injection valve


20


is stopped.




As shown in

FIGS. 1 and 2

, the spill ring


21


is connected to a control lever


23


and a tension lever


24


through a joint


46


. The control lever


23


and the tension lever


24


are rotatably connected to a guide lever


26


through a pin


25


.




As shown in

FIG. 1

, the guide lever


26


is rotatably connected to another pin


27


. The guide lever


26


is urged in one direction by an urging spring


28


, and a top end of the guide lever


26


is engaged with a full load stopper


29


provided for adjusting the maximum amount of fuel injection.




As shown in

FIGS. 1 and 2

, the control lever


23


and the tension lever


24


are urged by a start spring


30


and an idle spring


31


, which are provided between the control lever


23


and the tension lever


24


, in opposite directions. A projection


32


is formed in the tension lever


24


. When the projection


32


is connected with the control lever


23


, the control lever


23


and the tension lever


24


are integrally rotated about the pin


25


.




As shown in

FIGS. 1 and 2

, the control lever


23


can be pushed by a governor sleeve


33


of a centrifugal governor


50


. The governor sleeve


33


is slidably guided along a governor shaft


39


. As shown in

FIGS. 1 and 2

, the governor sleeve


33


experiences thrust upon rotation of flyweights


34


. The flyweights


34


are connected to a governor gear


35


. The governor gear


35


is meshed with a gear


36


, which is integrally connected to the drive shaft


1


. When the drive shaft


1


is rotated, the governor gear


35


is rotated through the gear


36


, and centrifuge force is generated in the rotating flyweights


34


. The generated centrifugal force of the flyweights


34


applies the thrust to the governor sleeve


33


. That is, base ends of the rotating flyweights


34


push the governor sleeve


33


in the right direction in FIG.


1


. In this way, the control lever


23


is pushed by the governor sleeve


33


according to the rotational speed of the engine. Thus, the control lever


23


is rotated about the pin


25


to axially move the spill ring


21


in the left direction in FIG.


1


. Through the axial movement of the spill ring


21


, the amount of fuel injection (hereinafter, referred to as the fuel injection amount) is adjusted. The centrifugal governor


50


includes the governor sleeve


33


, the governor shaft


39


and the flyweights


34


. A governor control means for adjusting the fuel injection amount based on the rotational speed of the engine or an amount of shift of an accelerator pedal (hereinafter, referred to as an accelerator pedal shift amount) includes the control lever


23


, the tension lever


24


, the guide lever


26


and the control spring


37


.




A load timer mechanism (load sensing timer) LST, which will be described later, is formed by the governor sleeve


33


and the governor shaft


39


. Thus, the load sensing timer LST includes the governor sleeve


33


and the governor shaft


39


. Detail of the load sensing timer LST will be described later.




One end of the control spring


37


is connected to a top end of the tension lever


24


, and the other end of the control spring


37


is connected to a manipulation lever


38


. The manipulation lever


38


is actuated by the accelerator pedal (not shown). When the manipulation lever


38


is rotated by the accelerator pedal, the tension lever


24


is rotated about the pin


25


through the control spring


37


. Thus, the spill ring


21


is axially moved. In this way, the fuel injection amount can be controlled by the accelerator pedal shift amount.




Next, the hydraulic timer mechanism HT will be described with reference to FIG.


1


. The cam rollers


10


, which are in rolling contact with the face cam


9


, are supported by a roller ring


40


. The roller ring


40


is connected to a timer piston


42


through a rod


41


. The timer piston


42


is received in a timer pressure chamber


43


defined in the pump housing


2


, and fuel pressure of the pump chamber


6


is introduced into the timer chamber


43


.




When the fuel pressure of the timer pressure chamber


43


is varied according to the fuel pressure of the pump chamber


6


, the timer piston


42


is axially displaced, and the axial displacement of the timer piston


42


causes rotation of the roller ring


40


. Thus, the cam rollers


10


are circumferentially displaced relative to the face cam


9


, so that time for initiating engagement between the cam rollers


10


and the corresponding ridges of the face cam


9


is varied accordingly. As a result, timing of fuel injection is varied.




It should be noted that although the timer piston


42


and the timer pressure chamber


43


are oriented in the left-right direction in

FIG. 1

for the sake of clarity, the timer piston


42


and the timer pressure chamber


43


are actually oriented in a direction perpendicular to the plane of FIG.


1


.




Here, the hydraulic timer mechanism HT includes the timer piston


42


and the timer pressure chamber


43


.




Next, the structure of the load sensing timer LST will be described with reference to

FIGS. 1

to


5


. As shown in

FIG. 1

, the governor shaft


39


is securely supported by the pump housing


2


such that the governor shaft


39


is generally parallel to the drive shaft


1


to mesh the governor gear


35


with the gear


36


. As shown in

FIGS. 2 and 3

, a fuel relief passage


57


is defined in the governor shaft


39


. The fuel relief passage


57


includes a longitudinal hole


57




a


and two diametrically opposed radial holes


57




b


. The longitudinal hole


57




a


axially extends in the governor shaft


39


. The radial holes


57




b


radially extend from a distal end of the longitudinal hole


57




a


to an outer peripheral surface of the governor shaft


39


. With reference to

FIG. 1

, a proximal end of the longitudinal hole


57




a


is communicated with the fuel in the low pressure side, i.e., the fuel tank


4


side of the feed pump


3


. The radial holes


57




b


are not limited to the through holes shown in FIG.


3


. For example, in place of the two radial holes


57




b


, it is possible to provide a single radial hole, which radially extends from the longitudinal hole


57




a


to the outer peripheral surface of the governor shaft


39


. Further alternatively, in place of the two radial holes


57




b


, it is possible to provide more than two radial holes as long as the radial holes are placed in the same axial position along the governor shaft


39


.




In the present embodiment, an opening-side annular groove


57




c


, which can be regarded as a part of the outer opening of each radial hole


57




b


, is recessed in a portion of the outer peripheral surface of the governor shaft


39


where the outer openings of the radial holes


57




b


are located, as shown in FIG.


1


. In this case, it is not necessary to place the outer openings of the radial holes


57




b


in the same axial position of the governor shaft


39


. As long as the outer openings of the radial holes


57




b


are located within an axial extent of the opening-side annular groove


57




c


, the outer openings of the radial holes


57




b


can be displaced in the axial direction.




As described above, the governor sleeve


33


can be moved back and forth, i.e., can be reciprocated in the axial direction of the governor shaft


39


by the centrifugal force of the flyweights


34


, which varies according to the rotational speed of the engine or the load of the engine. As shown in

FIG. 3

, two diametrically opposed ports


51


are provided in the governor sleeve


33


at a predetermined axial position of the governor sleeve


33


. Each port


51


extends from an inner peripheral surface to an outer peripheral surface of the governor sleeve


33


and includes an inner opening placed in the inner peripheral surface of the governor sleeve


33


and an outer opening placed in the outer peripheral surface of the governor sleeve


33


. The ports


51


are not limited to the through holes shown in FIG.


3


. For example, in place of the two ports


51


, it is possible to provide a single port, which radially extends from the inner peripheral surface to the outer peripheral surface of the governor sleeve


33


. Further alternatively, in place of the two ports


51


, it is possible to provide more than two ports as long as the ports are placed in the same axial position along the governor sleeve


33


.




In the present embodiment, as shown in

FIG. 3

, in the portion of the inner peripheral surface of the governor sleeve


33


where the inner opening of the ports


51


are located, an opening-side annular groove


51




a


, which can be regarded as a part of the inner opening of each port


51


, is recessed in the inner peripheral surface of the governor sleeve


33


. In this case, the inner openings of the ports


51


are not necessarily located in the same axial position of the governor sleeve


33


. That is, as long as the inner openings of the ports


51


are located within an axial extent of the annular groove


51




c


, the inner openings of the ports can be axially displaced.




As shown in

FIG. 3

, each radial hole


57




b


of the fuel relief passage


57


and each port


51


can be communicated one another and can be discommunicated from one another by the reciprocal movement of the governor sleeve


33


induced by the centrifugal force of the flyweights


34


, which varies according to the load of the engine. As a result, based on the operational state of the engine, it is possible to relieve the high pressure fuel of the pump chamber


6


to the low pressure side through the port


51


and the radial hole


57




b


upon communication between the port


51


and the radial hole


57




b


, and it is also possible to stop the relief of the high pressure fuel of the pump chamber


6


to the low pressure side upon discommunication between the port


51


and the radial hole


57




b


. Through the communication and discommunication between the radial hole


57




b


and the port


51


, which are achieved according to the operational state of the engine, the fuel pressure of the pump chamber


6


, which acts as a drive source of the timer mechanism HT for adjusting the fuel injection timing, is reduced and is maintained. As a result, through the communication and discommunication between the radial hole


57




b


and the port


51


, i.e., through the actuation of the load sensing timer LST, the fuel injection timing (specifically, the fuel injection timing controlled based on the high pressure fuel, which is adjusted to the pressure that is proportional to the rotational speed of the engine by actuation of the pressure regulator valve


5


) is controlled based on the load condition of the engine.




Furthermore, in the present embodiment, a first annular groove


55


is formed in the outer peripheral surface of the governor shaft


39


at an axial position that is displaced from the axial position of the outer opening of each radial hole


57




b


, as shown in

FIG. 3. A

second annular groove


53


is formed in the inner peripheral surface of the governor sleeve


33


at an axial position that is displaced from the axial position of the inner opening of each port


51


, as shown in FIG.


3


. When the governor sleeve


33


is placed within a predetermined axial range through the reciprocal movement of the governor sleeve


33


, the first annular groove


55


and the second annular groove


53


are at least partially overlapped one another to communicate between the port


51


and the radial hole


57




b


through a fuel pool


56


defined between the first annular groove


55


and the second annular groove


53


(

FIG. 1 and a

point “c” in FIG.


5


). Detail of the communication and discommunication between the radial hole


57




b


and the port


51


, i.e., the actuation of the load sensing timer LST will be described later.




Next, operation of the fuel injection pump, particularly of the load sensing timer will be described with reference to

FIGS. 1

,


4


and


5


.

FIG. 5

shows a relationship between the fuel injection amount and timer advancement, which correspond to the fuel injection timing.




In a high load condition or a full load condition of the engine, the accelerator pedal is operated to rotate the manipulation lever


38


(

FIG. 1

) forward, so that the tension lever


24


is rotated or pivoted through the control spring


37


in a counterclockwise direction (in the left direction in FIG.


1


). As a result, the spill ring


21


is axially moved toward the right side in

FIG. 1

, and thereby the fuel injection amount is increased. In this case, the axial position of the governor sleeve


33


is limited by the control lever


23


and is thus axially positioned leftward in

FIG. 1

, as shown in FIG.


4


A. At this time, the first annular groove


55


and the second annular groove


53


are overlapped one another. Furthermore, the governor sleeve


33


is axially held relative to the governor shaft


39


such that the fuel pool


56


, which is at least partially defined by the first annular groove


55


and the second annular groove


53


, is not communicated with the port


51


. Thus, the port


51


and the radial hole


57




b


are not communicated one another, and thus the fuel pressure of the pump chamber


6


is not reduced. Therefore, the fuel pressure of the pump chamber


6


is maintained at the relatively high pressure. As a result, the timer piston


42


of the timer mechanism HT is pushed toward the timer advance side by the pressure of the timer pressure chamber


43


, which is exerted by the maintained fuel pressure of the pump chamber


6


, so that the amount of timer advancement is increased, i.e., the fuel injection timing is advanced (this state corresponds to a point “a” in FIG.


5


).




When the accelerator pedal is operated to slightly rotate the manipulation lever


38


backward to reduce the load of the engine, the tension lever


24


is rotated or pivoted by the control spring


37


in a clockwise direction (in the right direction in FIG.


1


). As a result, the spill ring


21


is moved in the left direction in

FIG. 1

, so that the fuel injection amount is reduced accordingly. In this state, the governor sleeve


33


is released from the control lever


23


. The centrifugal force of the flyweights


34


of the governor


50


causes the governor sleeve


33


to move from the position of

FIG. 4A

in the right direction, as shown in FIG.


4


B. At this time, the first annular groove


55


and the second annular groove


53


are still at least partially overlapped one another like the state of FIG.


4


A. However, in this state, the opening-side annular groove


51




a


and the first annular groove


55


can be slightly overlapped one another without causing substantial communication between the inner opening of the port


51


(specifically, the opening-side annular groove


51




a


) and the first annular groove


55


. Even in such a case, the port


51


and the first annular groove


55


are not substantially communicated one another due to characteristics (such as viscosity) of the fuel as long as an opening area at the overlapped region between the opening-side annular groove


51




a


and the first annular groove


55


is sufficiently small. The axial position of the governor sleeve


33


shown in

FIG. 4B

corresponds to a transitional point (a point “b” in

FIG. 5

) from the highly advanced state of the fuel injection timing, which is achieved under the high load condition, to a retarded state of the fuel injection timing, which is achieved under an intermediate load condition (or partial load condition) and is retarded from the fuel injection timing achieved under the high load condition.




When the load of the engine is further reduced to achieve the intermediate load condition of the engine, the governor sleeve


33


is moved from the position of

FIG. 4B

in the right direction, as shown in

FIG. 4C

, due to the centrifugal force of the flyweights


34


. At this time, similar to the states of

FIGS. 4A and 4B

, the first annular groove


55


and the second annular groove


53


are still at least partially overlapped one another. Furthermore, the fuel pool


56


and the port


51


(specifically, the first annular groove


55


and the opening-side annular groove


51




a


) are overlapped one another. Thus, a decrease of the fuel pressure can be achieved in the pump chamber


6


, and a rate of the decrease of the fuel pressure depends on a cross sectional area of the opening of the port


51


. Therefore, the fuel injection timing under the intermediate load condition can be retarded from the fuel injection timing under the high load condition.




Furthermore, when the load of the engine is further reduced to achieve a low load condition (or no load condition) of the engine, the governor sleeve


33


is moved from the position of

FIG. 4C

in the right direction, as shown in

FIG. 4E

, due to the centrifugal force of the flyweights


34


of the governor


50


. At this time, the first annular groove


55


and the second annular groove


53


are slightly overlapped one another or are not overlapped one another. Thus, the port


51


and the radial hole


57




b


are not substantially communicated one another. As a result, the fuel injection timing can be substantially returned from the retarded state, which is achieved under the intermediate load condition, to the fuel injection timing similar to one achieved under the high load condition.




In this way, it is possible to communicate between the port


51


and the radial hole


57




b


only under the intermediate load condition to retard the fuel injection timing in comparison to the fuel injection timing under the high load condition. Furthermore, this can be achieved by providing the first annular groove


55


and the second annular groove


53


in addition to the fuel relief passage


57


(i.e., the longitudinal hole


57




a


and radial holes


57




b


) and the ports


51


. Thus, with the simple structure achieved by the slight structural modification of a previously proposed structure, the fuel injection timing under the low load condition is limited, and the timer retardation in the intermediate load range can be improved.




Furthermore, in the present embodiment, the opening of each port


51


and the opening of each radial hole


57




b


are formed by the opening-side annular groove


51




a


and the opening-side annular groove


57




c


, respectively. Thus, the variation in the cross sectional area of the opening formed in the overlapped region between the opening-side annular groove


51




a


and the opening-side annular groove


57




c


upon reciprocal movement of the sleeve


30


can be increased in comparison to the circular hole or rectangular hole (see the transitional region from the high load condition to the intermediate load condition located in the point “b” of FIG.


5


and the transitional region from the intermediate load condition to the low load condition in the point “d” of FIG.


5


). As a result, with respect to the desired intermediate load range, the movable range of the governor sleeve


33


, which allows the communication between the port


51


and the radial hole


57




b


, is increased. Thus, the timer retardation in the desired intermediate load range, i.e., the retardation of the fuel injection timing in the desired intermediate load range is further improved.




Furthermore, in the present embodiment, as shown in FIG.


3


and the point “C” of

FIG. 5

, the axial extent (width) of the first annular groove


55


is larger than an axial extent (width) of a protrusion


58


formed between the inner opening (specifically, the opening-side annular groove


51




a


) of the port


51


and the second annular groove


53


. With this arrangement, it is possible to maintain the discommunication between the port


51


and the fuel pool


56


from the position (high load condition) of

FIG. 4A

to the position (transitional point) of

FIG. 4B

, at which a left end wall of the first annular groove


55


is overlapped with a left end wall of the protrusion


58


. Furthermore, it is possible to maintain the discommunication between the first annular groove


55


and the second annular groove


53


from the position (transitional point) of

FIG. 4D

to the position (low load condition) of

FIG. 4E

, at which a right end wall of the first annular groove


55


is overlapped with a right end wall of the protrusion


58


. As a result, by setting the axial extent of the first annular groove


55


, which is formed in the outer peripheral surface of the governor shaft


39


, larger than the axial extent of the protrusion


58


, which is formed in the inner peripheral surface of the governor sleeve


33


, it is possible to provide the load sensing timer LST, which limits the timer retardation in the low load range and improves the timer retardation in the intermediate load range, without causing a substantial increase in the manufacturing costs.




Additional advantages and modifications will readily occur to those skilled in the art. The invention in its broader terms is therefore not limited to the specific details, representative apparatus, and illustrative examples shown and described.



Claims
  • 1. A fuel injection pump for an internal combustion engine, the fuel injection pump comprising:a pump housing that defines a pump chamber therein; a hydraulic timer mechanism that is received in the housing and adjusts fuel injection timing based on fuel pressure of the pump chamber; and a load timer mechanism that is received in the housing and adjusts the fuel injection timing based on a load of the engine, wherein the load timer mechanism includes: a governor shaft that is secured to the housing, wherein the governor shaft includes: a fuel relief passage that is communicated with a low pressure side of the fuel injection pump and has an outer opening in an outer peripheral surface of the governor shaft; and a first annular groove that is recessed in the outer peripheral surface of the governor shaft such that the first annular groove is axially displaced from the outer opening of the fuel relief passage; and a governor sleeve that is axially slidably supported around the governor shaft and is moved back and forth relative to the governor shaft based on the load of the engine, wherein the governor sleeve includes: a port that extends between an outer peripheral surface and an inner peripheral surface of the governor sleeve and includes an outer opening placed in the outer peripheral surface of the governor sleeve and an inner opening placed in the inner peripheral surface of the governor sleeve, wherein the port conducts the fuel pressure of the pump chamber from the outer peripheral surface to the inner peripheral surface of the governor sleeve; and a second annular groove that is recessed in the inner peripheral surface of the governor sleeve such that the second annular groove is axially displaced from the port, wherein: when the governor sleeve is positioned within a predetermined axial range, the first annular groove and the second annular groove are at least partially overlapped one another to define a fuel pool therebetween; when the engine is in one of a full load condition and a high load condition, the first annular groove and the second annular groove are at least partially overlapped one another, and the fuel pool is not substantially communicated with the port to prevent substantial communication between the port and the fuel relief passage; when the engine is in one of a partial load condition and an intermediate load condition, the first annular groove and the second annular groove are at least partially overlapped one another, and the fuel pool is substantially communicated with the port to substantially communicate between the port and the fuel relief passage; and when the engine in one of a no load condition and a low load condition, the first annular groove and the second annular groove are not substantially overlapped one another to prevent substantial communication between the port and the fuel relief passage.
  • 2. The fuel injection pump according to claim 1, wherein at least one of the inner opening of the port and the outer opening of the fuel relief passage is formed as an annular groove.
  • 3. The fuel injection pump according to claim 1, wherein:the governor sleeve further includes a protrusion, which is formed in the inner peripheral surface of the governor sleeve between the inner opening of the port and the second annular groove; and an axial extent of the first annular groove is larger than an axial extent of the protrusion of the governor sleeve.
Priority Claims (1)
Number Date Country Kind
2002-284146 Sep 2002 JP
US Referenced Citations (7)
Number Name Date Kind
4334514 Konrath et al. Jun 1982 A
4469066 Yuzawa Sep 1984 A
4483297 Eheim et al. Nov 1984 A
4548184 Laufer et al. Oct 1985 A
4819606 Kawano Apr 1989 A
5105786 Kato Apr 1992 A
5161509 Krieger et al. Nov 1992 A
Foreign Referenced Citations (1)
Number Date Country
57-119132 Jul 1982 JP