Fuel supply control system for engine

Abstract

A composite control valve is constructed by a valve housing, a negative pressure working chamber defined in the valve housing to communicate with a negative pressure generating section in the engine, a first control valve operable to be opened and closed with generation and extinction of a negative pressure in the negative pressure working chamber, and a second control valve operable to be opened and closed with the generation and losing of the negative pressure in the negative pressure working chamber. The first control valve is incorporated into an air vent system which provides communication between an upper space in a fuel tank and the atmosphere, and the second control valve is incorporated into a fuel passage system which provides communication between a portion of the fuel tank below a fuel oil surface and a fuel supply section in the engine. At least a portion of the air vent system is constituted by an inner air vent pipe disposed within the fuel tank, and a gas-liquid separating device is provided in an opening of the inner air vent pipe into the upper space. Thus, upon stoppage of the operation of the engine, not only the fuel passage system but also the air vent system leading to the upper space in the fuel tank can be blocked simultaneously, to prevent release of evaporated fuel generated in the fuel tank to the atmosphere.

Description

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to a fuel supply control system for an engine, which is adapted to control opening and closing of an air vent system which provides communication between an upper space in a fuel tank and the atmosphere, and opening and closing of a fuel passage system which provides communication between a portion of the fuel tank below a fuel oil surface and a fuel supply section in the engine.

2. Description of the Related Art

Japanese Utility Model Application Laid-open No. 62-93145 discloses a conventional fuel supply control system for an engine, wherein a negative-pressure responsive type automatic fuel cock adapted to be opened by a negative pressure generated in a negative pressure generating section in the engine is incorporated in a fuel passage which provides communication between a portion of the fuel tank below a fuel oil surface and a fuel supply section in the engine, so that upon stoppage of the operation of the engine, the fuel passage is automatically blocked by the automatic fuel cock to inhibit flowing-down of a fuel from the fuel tank to the fuel supply section in the engine.

With such a conventional fuel supply control system for the engine, the flowing-down of the fuel from the fuel tank to the fuel supply section in the engine can be inhibited by the automatic fuel cock upon stoppage of the operation of the engine, but an upper space in the fuel tank is put in a state in which it is opened to the atmosphere through an air vent, so that if an evaporated fuel is produced in the fuel tank, the evaporated fuel is released into the atmosphere through the air vent.

SUMMARY OF THE INVENTION

Accordingly, it is an object of the present invention to provide a fuel supply control system of a simple construction for an engine, wherein upon stoppage of the operation of the engine, not only the fuel passage system but also the air vent system leading to the upper space in the fuel tank can be blocked simultaneously, to thereby prevent release of an evaporated fuel generated in the fuel tank to the atmosphere.

To achieve the above object, according to a first feature of the present invention, there is provided a fuel supply control system for an engine, comprising a composite control valve which is constructed by a valve housing, a negative pressure working chamber defined in the valve housing to communicate with a negative pressure generating section in the engine, a first control valve operable to be opened and closed with generation and extinction of a negative pressure in the negative pressure working chamber, and a second control valve operable to be opened and closed with the generation and extinction of the negative pressure in the negative pressure working chamber, the first control valve being incorporated into an air vent system which provides communication between an upper space in a fuel tank and the atmosphere, the second control valve being incorporated into a fuel passage system which provides communication between a portion of the fuel tank below a fuel oil surface and a fuel supply section in the engine, at least a portion of the air vent system being constituted by an inner air vent pipe disposed within the fuel tank, a gas-liquid separating means being provided in an opening of the inner air vent pipe into the upper space, the gas-liquid separating means being adapted to inhibit entrance of a fuel within the fuel tank into the inner air vent pipe and to permit the ventilation.

The negative pressure generating section and the fuel supply section correspond to a crank chamber 1a and a carburetor C respectively in the embodiments of the present invention which will be described hereinafter; the negative pressure working chamber corresponds to first and second negative pressure working chambers 44 and 45 communicating with each other; the air vent system corresponds to an inner air vent pipe 23, an outer vent pipe 24, an atmospheric air introducing pipe 49, an atmospheric air chamber 43 and an atmospheric air inlet pipe 47; and the fuel passage system corresponds to a fuel introducing pipe 70, a fuel conduit 71, a combustion chamber 46 and a float chamber 12a.

With the first feature, during operation of the engine, a negative pressure generated in the negative pressure generating section is transmitted to the negative pressure working chamber in the valve housing, and in response to this, the first and second control valves are opened. Therefore, the air vent system and the fuel passage system are opened, thereby smoothly conducting the supply of the fuel from the fuel tank to the fuel supply section.

If the operation of the engine is stopped, not only the negative pressure in the negative pressure generating section in the engine but also the negative pressure in the negative pressure working chamber in the valve housing are lost, and in response to this, the first and second control valve are closed and hence, the air vent system and the fuel passage system are closed. Therefore, it is possible not only to inhibit the supply of the fuel from the fuel tank to the fuel supply section in the engine, but also to prevent the release of the evaporated fuel generated in the fuel tank to the atmosphere.

Moreover, the above-described effect is achieved by the composite control valve having the common valve housing and hence, the construction of the fuel supply control system for the engine can be simplified.

In addition, because at least a portion of the air vent system is constituted by the inner air vent pipe disposed within the fuel rank, it is unnecessary to extend the air vent pipe upwards above the fuel tank and thus, the appearance of the fuel tank can be improved, and at least the inner air vent pipe can be protected from any contact with other objects.

Further, the gas-liquid separating means is provided in the opening of the inner air vent pipe into the upper space, and hence, even when the fuel in the fuel tank is waved, such fuel can be prevented from entering the inner air vent pipe.

According to a second feature of the present invention, in addition to the first feature, an upper end of an air vent passage extending downwards through the fuel tank to communicate with the atmosphere opens into an inner wall of an oil supply port tube of the fuel tank, the oil supply port tube being tightly closed by a tank cap, and an upper end of an overflow passage extending downwards below the fuel tank opens into the inner wall of the oil supply port tube at a location below an opening in the upper end of the air vent passage.

With the second feature, when the oil surface of the fuel rises up to the inside of the oil supply port tube due to an excessive supply of the fuel oil during supplement of the fuel to the fuel tank, such fuel is allowed to overflow to the overflow passage, whereby any further rising of the oil surface of the fuel in the oil supply port tube is suppressed. Therefore, it is possible to prevent the entrance of the fuel into the air vent passage which opens into the inner wall of the oil supply port tube at the location above the overflow passage and hence, the air vent passage can constantly exhibit a good ventilating function.

The above and other objects, features and advantages of the invention will become apparent from the following description of the preferred embodiments taken in conjunction with the accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a side view of a vertical-type engine provided with a fuel tank according to a first embodiment of the present invention;

FIG. 2 is a plan view of portions around a carburetor in FIG. 1;

FIG. 3 is a sectional view taken along a line 3-3 in FIG. 2;

FIG. 4 is an enlarged vertical sectional view of essential portions of the fuel tank;

FIG. 5 is an enlarged vertical sectional view of a composite control valve in FIG. 3 (showing an operation-stopped state of the engine);

FIG. 6 is a view of the composite control valve for explaining the operation upon increase of a pressure in the fuel tank;

FIG. 7 is a view of the composite control valve for explaining the operation upon decrease of the pressure in the fuel tank;

FIG. 8 is a view of the composite control valve for explaining the operation during operation of the engine;

FIG. 9 is a sectional view taken along a line 9-9 in FIG. 5;

FIG. 10 is a sectional view taken along a line 10-10 in FIG. 2;

FIGS. 11A, 11B and 11C are views for explaining the operation of an oil flow-out preventing means in FIG. 2;

FIG. 12 is a view similar to FIG. 3, but showing a second embodiment of the present invention;

FIG. 13 is a view similar to FIG. 3, but showing a third embodiment of the present invention;

FIG. 14 is a side view of a horizontal-type engine provided with a fuel tank according to a fourth embodiment of the present invention;

FIG. 15 is an enlarged vertical sectional view of essential portions of FIG. 14;

FIG. 16 is a view similar to FIG. 4, but showing a fifth embodiment of the present invention; and

FIG. 17 is a view for explaining the overflow action of the fuel during an excessive supply of the fuel into the fuel tank shown in FIG. 16.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

The present invention will now be described by way of preferred embodiments with reference to the accompanying drawings.

A first embodiment of the present invention shown in FIGS. 1 to 11 will be described first. In FIGS. 1 and 2, reference character E denotes a general-purpose engine of a 4-cycle vertical type. A crankshaft 2 supported in a crankcase 1 of the engine E is disposed vertically with its output end protruding downward below the crankcase 1. A fuel tank T and a recoil starter 4 are mounted to an upper portion of the crankcase 1.

A cylinder block 5 having a cylinder axis disposed horizontally is connected to one side of the crankcase 1, and a carburetor C is mounted to one side of a cylinder head 6 coupled to a tip end of the cylinder block 5.

Referring to FIG. 3, the carburetor C includes a carburetor body 10 having an intake passage 11 leading to an intake port 6a in the cylinder head 6, a float chamber member 12 coupled to a lower surface of the carburetor body 10 and having a float chamber 12a, a fuel nozzle 13 which permits an area below a fuel oil surface in the float chamber 12a to communicate with a venturi portion of the intake passage 11, a choke valve 14 for opening and closing the intake passage 11 at a location upstream of the intake passage 11, a throttle valve 15 for opening and closing the intake passage 11 at a location downstream of the intake passage 11, and a float valve 17 for opening and closing an fuel inlet 16 of the float chamber member 12 to control the oil surface of a fuel stored in the float chamber 12a to be constant. The fuel nozzle 13 is supported in a nozzle support tube 10a formed at a lower portion of the carburetor body 10. A composite control valve V is mounted on one side of the float chamber member 12 for controlling the opening and closing of an air vent system for the fuel tank T as well as the opening and closing of a fuel passage system extending from the fuel tank T to the float chamber 12a depending on the operational state of the engine E. The composite control valve V will be described later.

Referring to FIG. 4, an oil supply port tube 20 formed on one side of a ceiling wall of the fuel tank T is tightly closed by a tank cap 21 threadedly engaged with an outer periphery of the oil supply port tube 20. A ventilation hole 22 opens into an inner surface of the oil supply port tube 20. The ventilation hole 22 extends vertically within the fuel tank T and communicates with an inner air vent pipe 23 extending through a bottom wall of the fuel tank T, and an outer air vent pipe 24 disposed below the fuel tank T is connected at one end to a lower end of the inner air vent pipe 23. The inner air vent pipe 23 is formed integrally with the fuel tank T.

The inner air vent pipe 23 disposed within the fuel tank T is protected from any contact with other objects. It is unnecessary to extend the air vent pipe upward above the fuel tank T and hence, the appearance of the fuel tank T can be maintained to be excellent.

The tank cap 21 is provided with a gas-liquid separating means 25 interposed between an upper space 3 in the fuel tank T and the ventilation hole 22. The gas-liquid separating means 25 is comprised of a partitioning member 26 and a porous member 27 made of a urethane foam having open cells. The partitioning member 26 is made of an elastic material such as rubber, and includes a cylindrical portion 28 disposed within the oil supply port tube 20 and having an upper end wall 28a recessed downwards into a cone-shape, a flange portion 29 which protrudes radially outwards from an upper end of the cylindrical portion 28 and which is clamped between an end wall of the tank cap 21 and an end face of the oil supply port tube 20. A seal bead 28b is formed at a lower end of the cylindrical portion 28 to come into close contact with an inner peripheral surface of a lower end portion of the oil supply port tube 20. Small bores 30 and 31 are provided in the upper wall 28a and the flange portion 29. The partitioning member 26 divides the inside of the oil supply port tube 20 into an inner chamber 32 leading to the upper space 3 within the fuel tank T, an outer chamber 33 which surrounds the inner chamber 32 with the cylinder portion 28 interposed therebetween, and an upper chamber 35 communicating with the inner and outer chambers 32 and 33 through the small bores 30 and 31, respectively. The ventilation hole 22 is disposed to open into the outer chamber 33.

The porous member 27 is set in the upper chamber 35 to cover the small bore 30 in the upper end wall 28a. A cylindrical wave trap protruding toward the inner chamber 32, i.e., downwards to surround the small bore 30, is connected to the upper end wall 28a.

Thus, the ventilation hole 22 and the upper space 3 within the fuel tank T communicate with each other through the outer chamber 33, the small bore 31, the upper chamber 35, the porous member 27, the small bore 30 and the inner chamber 32, thereby enabling the breathing of the inside of the fuel tank T. On the other hand, even if the fuel in the fuel tank T enters the inner chamber 32 due to waving, the entrance of the fuel into the small bore 30 can be prevented by the wave trap 34. However, when the fuel has entered the upper chamber 35 through the small bore 30, it is absorbed by the porous member 27, and if the fuel absorbing capability of the porous member 27 reaches a level corresponding to a saturated state, the fuel flows toward the small bore 30 along the cone-shaped upper end wall 28a, and is dropped into the fuel tank T. In this manner, the fuel in the fuel tank T cannot reach the outer chamber 33 through the outer small bore 31 and hence, the entrance of the fuel into the ventilation hole 22 can be prevented.

The composite control valve V will be described below with reference to FIG. 5.

The composite control valve V has a valve housing 40 which is constructed by sequentially superposing a first block 40a, a second block 40b and a third block 40c one on another and coupling them to one another. In this case, an outer peripheral edge of a first diaphragm 41 is clamped between the first block 40a and the second block 40b, and an outer peripheral edge of a second diaphragm 42 is clamped between the second block 40b and the third block 40c. An atmospheric chamber 43 is defined between the first block 40a and the first diaphragm 41; a first negative pressure working chamber 44 is defined between the first diaphragm 41 and the second block 40b, and a second negative pressure working chamber 43 is defined between the second block 40b and the second diaphragm 42. A fuel chamber 46 is defined between the second diaphragm 42 and the third block 40c.

An atmospheric air inlet pipe 47 is integrally formed on one sidewall of the first block 40a so that the atmospheric chamber 43 is always maintained under an atmospheric pressure. An atmospheric air introducing pipe 49 is integrally formed on the other sidewall of the first block 40a to open at its inner end into the atmospheric chamber 43, and the other end of the outer air vent pipe 24 is connected to an outer end of the atmospheric air introducing pipe 49.

An inner end of the atmospheric air introducing pipe 49 is formed at a first valve seat 51 protruding toward the atmospheric chamber 43. A first valve member 52 for opening and closing the atmospheric air introducing pipe 49 by cooperation with the first valve seat 51 is formed at a central portion of the first diaphragm 41. A first return spring 53 for biasing the first valve member 52 toward the first valve seat 51 is mounted under compression between the first diaphragm 41 and the second block 40b. A first control valve 50 for opening and closing the atmospheric air introducing pipe 49 is constructed by the first valve member 52 and the first valve seat 51.

A relief valve 54 is mounted on a partition wall between the first block 40a and the atmospheric air introducing pipe 49, and adapted to be opened to permit the flowing of air from the atmospheric chamber 43 to the atmospheric air introducing pipe 49, only when the pressure in the fuel tank T is dropped to a level equal to or lower than a predetermined pressure.

A negative pressure introducing pipe 55 communicating with the first negative pressure working chamber 44 is connected to the second block 40b, and the negative pressure introducing pipe 55 and a negative pressure pick-up pipe 56 formed on the crankcase 1 of the engine E to lead to a crank chamber 1a in the crankcase 1 are connected to each other by a negative pressure conduit 57.

As shown in FIGS. 5 and 9, a check valve 65 is mounted at a connection between the second block 40b and the negative pressure introducing pipe 55. The check valve 65 includes a valve seat plate 66 and a resilient valve plate 67 clamped between the second block 40b and the negative pressure introducing pipe 55. The valve plate 67 is disposed on a side of the valve seat plate 66 closer to the negative pressure introducing pipe 55, to open and close a valve bore 66a in the valve seat plate 66 in accordance with a pressure difference across the valve seat plate 66. Therefore, the check valve 65 permits only the transmission of a negative pressure from the negative pressure introducing pipe 55 to the first negative pressure working chamber 44. More specifically, when the pressure in the negative pressure introducing pipe 55 is lower than that in the first negative pressure working chamber 44, the check valve 65 is opened, and when the pressure in the negative pressure introducing pipe 55 is higher that in the first negative pressure working chamber 44, the check valve 65 is closed. A constriction bore 68 is provided in the valve seat plate 66 to permit the negative pressure introducing pipe 55 and the first negative pressure working chamber 44 to be always in communication with each other irrespective of the valve-opening/closing motion of the valve plate 67. The constriction bore 68 may be provided in a portion of the valve plate 67 facing the valve bore 66a.

An orifice 58 is provided in the second block 40b to permit the communication between the first and second negative pressure working chambers 44 and 45.

A fuel introducing pipe 70 is integrally formed on the third block 40c, and a fuel conduit 71 leading to a bottom portion (see FIG. 4) in the fuel tank T is connected to the fuel introducing pipe 70. The third block 40c is provided with a fuel outlet 72 which is connected to the fuel inlet 16 in the float chamber member 12.

An inner end of the fuel introducing pipe 70, which opens into the fuel chamber 46, is formed at a second valve seat 61 protruding toward the fuel chamber 46. A second valve member 62 for opening and closing the fuel introducing pipe 70 by cooperation with the second valve seat 61 is formed at a central portion of the second diaphragm 42, and a second return spring 63 is mounted under compression for biasing the second valve member 62 in a direction to seat it on the second valve seat 61. The second return spring has a preset load larger than that of the first return spring 53. A second control valve 60 for opening and closing the fuel introducing pipe 70 is constructed by the second valve member 62 and the second valve seat 61.

The operation of the composite control valve V will be described below.

Upon Stoppage of the Operation of the Engine E (See FIG. 5)

In an operation-stopped state of the engine E, the crank chamber 1a is in a state under an atmospheric pressure and hence, the first and second negative pressure chambers 44 and 45 communicating with the crank chamber 1a through the constriction bore 68 are also under the atmospheric pressure. As a result, the first and second diaphragms 41 and 42 are biased toward the first and second valve seats 51 and 61 by the preset loads of the first and second return springs 63, 63, respectively, and the first and second valve members 52 and 62 are seated on the first and second valve seats 51 and 61, respectively. Namely, both the first and second control valves 50 and 60 are concurrently closed to block the atmospheric air introducing pipe 49 and the fuel introducing pipe 70, respectively.

On the other hand, if the inside of the fuel tank T is substantially under the atmospheric pressure, the seating of the first valve member 52 onto the first valve seat 51 is not obstructed, and the normally-closed type relief valve 54 is closed to cut off the communication between the atmospheric air introducing pipe 49 and the atmospheric pressure chamber 43.

When the atmospheric air introducing pipe 49 and the fuel introducing pipe 70 is disconnected from each other in this manner, the wasteful downward-flowing of the fuel from the fuel tank T to the carburetor C can be prevented, and the release of the evaporated fuel generated in the fuel tank T to the atmosphere can be prevented.

Upon Increase of Pressure in Fuel Tank T (See FIG. 6)

If the fuel tank T is heated by a solar heat or the like when the engine is in the operation-stopped state, as described above, the internal pressure in the fuel tank T is raised to a level equal to or higher than the predetermined pressure, such an internal pressure moves the first valve member 52 away from the first valve seat 51 against the preset load of the first return spring 52, i.e., the first control valve 50 is opened to open the atmospheric air introducing pipe 49 into the atmospheric air chamber 43. Therefore, the excessive increment in pressure in the fuel tank T is released into the atmosphere, and thus the expanding deformation of the fuel tank T due to the excessive raising of the internal pressure can be prevented.

Upon Decrease of Pressure in Fuel Tank T (See FIG. 7)

When the engine E is in the operation-stopped state, for example, in a cold zone, the fuel tank T is cooled by the outside air, and the pressure in the fuel tank T is reduced to a level equal to or lower than the predetermined value, the relief valve 54 is opened due to a pressure difference across the relief valve 54, to thereby permit the flowing of air from the atmospheric pressure chamber 43 to the atmospheric air introducing pipe 49. Therefore, the atmospheric air is supplemented into the fuel tank T, whereby the constricting deformation of the fuel tank T can be prevented.

During Operation of the Engine E (See FIG. 8)

During operation of the engine E, the powerful pressure pulsation, in which the positive and negative pressures are alternately generated in the crank chamber 1a with the reciprocal movement of a piston, occurs, and is transmitted through the negative pressure conduit 57 and the negative pressure introducing pipe 55 to the check valve 65. The check valve 65 is closed upon the transmission of the positive pressure and opened upon the transmission of the negative pressure. Therefore, eventually, only the negative pressure is passed through the check valve 65 and transmitted first to the first negative pressure working chamber 44 and then through the through-bore 58 to the second negative pressure working chamber 45, whereby the first and second negative pressure working chambers 44 and 45 can be maintained in equally stable high negative pressure states without being influenced by a variation in opening degree of the throttle valve 15 of the carburetor C.

In this case, there is a negative pressure which is leaked from the first and second negative pressure working chambers 44 and 45 through the constriction bore 68 into the crank chamber 1a, but the amount of negative pressure leaked is extremely small, as compared with a negative pressure introduced from the crank chamber 1a into the first and second negative pressure working chambers 44 and 45, and hence such a negative pressure can be disregarded.

When the first negative pressure working chamber 44 has been brought into a predetermined negative pressure state in this manner, the first diaphragm 41 is pulled toward the first negative pressure working chamber 44 against the preset load of the first return spring 53 to move the first valve member 52 away from the first valve seat 51, i.e., the first control valve 50 is opened to open the atmospheric air introducing pipe 49. Therefore, the upper space 3 in the fuel tank T is brought into a state in which it can freely breathe the external air. When the second negative pressure working chamber 45 has been brought into a predetermined negative pressure state, the second diaphragm 42 is pulled toward the second negative pressure working chamber 45 against the preset load of the second return spring 63 to move the second valve member 62 away from the second valve seat 61, i.e., the second control valve 60 is opened to open the fuel introducing pipe 70. Therefore, the fuel in the fuel tank T is supplied to the float chamber 12a in the carburetor C through the fuel conduit 71, the fuel introducing pipe 70 and the fuel chamber 46.

Upon the starting of the engine E, the negative pressure from the crank chamber 1a is transmitted first to the first negative pressure working chamber 44, and then from the first negative pressure working chamber 44 through the orifice 58 to the second negative pressure working chamber 45. Also, the preset load of the first return spring 53 is set at the value smaller than that of the second return spring 63. That is, the first diaphragm 41 opens the first control valve 50 to open the atmospheric air introducing pipe 49, and then the second diaphragm 42 opens the second control valve 50 to open the fuel introducing pipe 70. Therefore, the positive or negative pressure remaining in a small amount in the fuel tank T is first released to the atmosphere by the opening of the first control valve 50, and thereafter the supply of the fuel to the carburetor C is started, whereby the excessive supply or insufficient supply of the fuel due to the pressure remaining in the fuel tank T can be prevented to ensure the good startability of the engine E.

In order to control the timing for opening the atmospheric air introducing pipe 49 and the fuel introducing pipe 70 in the above-described manner, the following arrangements are provided in the present embodiment:

(1) The negative pressure introducing pipe 55 is put into communication with the first negative pressure working chamber 44, and the first and second negative pressure working chambers 44 and 45 are put into communication with each other through the orifice 58.

(2) The preset load of the first return spring 53 for biasing the first valve member 52 in a closing direction is set at a value smaller than the preset load of the second return spring 63 for biasing the second valve member 62 in a closing direction.

Both the above arrangements (1) and (2) are employed in the embodiment, but the control of the timing can be achieved by employing any one of these arrangements. When only the arrangement (2) is employed, the first and second negative pressure working chambers 44 and 45 may be formed into a single negative pressure working chamber without being divided.

The composite control valve V for controlling the opening and closing of the air vent system for the fuel tank T and the opening and closing of the fuel supply system extending from the fuel tank T to the carburetor C, as described above, is constructed by the single valve housing 40, and the first and second diaphragms 41 and 42 mounted within the valve housing 40, as well as the first and second control valves 50 and 60. Therefore, the composite control valve V obtains a simple structure and can be provided at a relatively low cost. Moreover, the first and second diaphragms 41 and 42 are disposed to be opposed to each other with the first and second negative pressure working chambers 44 and 45 defined therebetween and hence, the compactness of the composite control valve V can be achieved.

In addition, the check valve 65 is clamped at the fitting connection between the second block 40b and the negative pressure introducing pipe 55 and hence, the check valve 65 is also incorporated into the composite control valve V. Thus, it is possible to provide a further simplification with the fuel supply control system for the engine and moreover, the assemblability of the check valve 65 is improved.

Referring to FIGS. 2, 10 and 11, a connecting tube 57a is integrally formed at an upstream end of the negative pressure conduit 57 and fitted to an inner peripheral surface of the negative pressure pick-up pipe 56, and the negative pressure pick-up pipe 56 and the connecting tube 57a are usually retained at horizontal orientation. The connecting tube 57a is provided with an oil flow-out preventing means 80 for preventing a lubricating oil from flowing out of the crank chamber 1a to the negative pressure conduit 57 in any attitude of the engine E during transportation or storage of the engine E.

The oil flow-out preventing means 80 is fitted and fixed to the inner peripheral surface of the negative pressure conduit 57 and disposed at a central portion of the connecting tube 57a, and includes an inner tube 81 which opens at opposite ends, and an outer tube 82 disposed concentrically between the inner tube 81 and the connecting tube 57a. The outer tube 82 has an end wall 82a opposed at a distance to a tip end of the inner tube 81. A cross-shaped or radial rib 83 is formed to extend from an outer surface of the end wall 82a to an outer peripheral surface of the outer tube 82. The outer tube 82 is retained at a bottom of the connecting tube 57a by the engagement of the rib 83 with an inward facing shoulder 87 of an inner periphery of an open end of the connecting tube 57a. In addition, an outer ventilation clearance 84 is defined between the connecting tube 57a and the outer tube 82 by the abutment of the rib 83 against an inner peripheral surface of the connecting tube 57a. An inner ventilation clearance 85 is also defined between the outer tube 82 and the inner tube 81 to communicate with the inner tube 81. Further, a plurality of notches 86 are provided at a tip end of the outer tube 82 to provide communication between the ventilation clearances 84 and 85.

During operation of the engine E, as shown in FIG. 11A, the negative pressure pick-up pipe 56 is normally retained substantially horizontally, and the crank chamber 1a and the negative pressure conduit 57 are in communication with each other through the ventilation clearances 84 and 85 between the outer tube 82 and the inner tube 81 and through the notches 86, thereby enabling the transmission of the pressure pulsation to the negative pressure conduit 57. In this state, even when a small amount of the mist of the lubricating oil 0 in the crank chamber 1a enters and is accumulated in lower portions of the ventilation clearances 84 and 85, the communication between the crank chamber 1a and the negative pressure conduit 57 cannot be cut off by the accumulation of the mist.

When the engine E is inclined at a given angle or more during transportation or storage of the engine E, the negative pressure pick-up pipe 56 is also inclined or turned upside down, as shown in FIGS. 11B and 11C, whereby the lubricating oil O in the crank chamber 1a flows into the connecting tube 57a and fills the outer ventilation clearance 84. When the lubricating oil O further fills a lower portion of the inner ventilation clearance 85, the communication between the inner tube 81 and the crank chamber 1a is cut off by such oil and moreover, the first and second negative pressure working chambers 44 and 45 with which the inner tube 81 communicates through the negative pressure conduit 57 are tightly-closed chambers isolated from the atmosphere, so that the air is not moved within the negative pressure conduit 57. Therefore, the oil filling the lower portion of the inner ventilation clearance 85 cannot be raised up to an opening at an upper end of the inner tube 81, and thus the flowing-out of the oil to the inner tube 81 and the negative pressure conduit 57 can be prevented.

Moreover, the oil flow-out preventing means 80 including the inner tube 81 and the outer tube 82 has a simple structure, and can be produced at a low cost.

A second embodiment of the present invention shown in FIG. 12 will now be described.

In a carburetor C, a small fuel chamber 75 is defined in a nozzle-supporting tube 10a of a carburetor body 10 for supporting a fuel nozzle 13, so that a lower end of the fuel nozzle 13 faces the small fuel chamber 75, and a valve tube 76 interconnecting a float chamber 12a and the small fuel chamber 75 is connected to one side of a nozzle support tube 10a.

On the other hand, in a valve housing of a composite control valve V, a third block 40 as in the first embodiment is not used, and a second diaphragm 42 is clamped between a second block 40b and an outer side of a float chamber member 12 to which the second block 40b is coupled. A piston-shaped second valve member 62 is mounted to the second diaphragm 42 and slidably fitted in the valve tube 76. The second valve member 62 has an axial communication groove 77 provided in an outer peripheral surface of a tip end thereof. A second control valve 60 for opening and closing the communication between the float chamber 12a and the fuel nozzle 13 is constructed by the second valve member 62 and the valve tube 76.

In the second embodiment, a negative pressure introducing pipe 49 is adapted to communicate equally with the first and second negative pressure working chambers 44 and 45. Therefore, in order to open the first control valve 50 prior to the second control valve 60 at the start of the engine E, as described above, the above-described arrangement (2), i.e., the arrangement in which the preset load of the first return spring 53 is set at the value smaller than the preset load of the second return spring 63, may be employed.

A fuel conduit 71 is connected directly to the fuel inlet 16 adapted to be opened and closed by the float valve 17.

When a negative pressure is introduced into the second negative pressure working chamber 45, whereby the second diaphragm 42 is advanced toward the second negative pressure working chamber 45, the second valve member 62 is also advanced to expose a portion of the communication groove 77 to the float chamber 12a, whereby the float chamber 12a and the fuel nozzle 13 are brought into communication with each other through the communication groove 77. Therefore, the flowing of the fuel from the float chamber 12a into the fuel nozzle 13 is permitted. When the negative pressure is extinguished from the second negative pressure working chamber 45, whereby the second diaphragm 42 is returned toward the float chamber 12a, the communication groove 77 in the second valve member 62 returning along with the second diaphragm 42 is withdrawn into the valve tube 76, whereby the communication between the float chamber 12a and the fuel nozzle 13 is cut off.

The arrangement of the other components is basically not different from that in the first embodiment and hence, portions or components corresponding to those in the first embodiment are designated by the same reference symbols and numerals in FIG. 12 and the description of them is omitted.

A third embodiment of the present invention shown in FIG. 13 will now be described.

A composite control valve V is mounted to a bottom surface of a float chamber member 12 in a carburetor C. A second valve seat 61 is formed on a lower end face of a nozzle support tube 10a of a carburetor body 10, and a second valve member 62 cooperating with the second valve seat 61 is connected to a second diaphragm 42 through a collar 78. A second control valve 60 for opening the closing the communication between a small fuel chamber 75 in a lower portion of the nozzle support tube 10a and the float chamber 12a is constructed by the second valve member 62 and the second valve seat 61.

A diaphragm 74 clamped between the second valve member 62 and the collar 78 has an outer peripheral portion clamped between the bottom surface of the float chamber member 12 and a third block 40c of a valve housing 40, whereby the communication between the float chamber 12a and the third block 40c is cut off. However, this diaphragm 74 may be disused, whereby the second diaphragm 42 can be exposed to the fuel in the float chamber 12a.

Also in the third embodiment, a fuel conduit 71 is connected directly to a fuel inlet 16 adapted to be opened and closed by a float valve 17.

When a negative pressure is introduced into the second negative pressure working chamber 45, whereby the second diaphragm 42 is advanced toward the second negative pressure working chamber 45, the second valve member 62 is also advanced away from the second valve seat 61, whereby the float chamber 12a and the fuel nozzle 13 are brought into communication with each other. Therefore, the flowing of the fuel from the float chamber 12a into the fuel nozzle 13 is permitted. When the negative pressure from the second negative pressure working chamber 45 is lost, whereby the second diaphragm 42 is returned toward the float chamber 12a, the second valve member 62 returning along with the second diaphragm 42 is seated on the second valve seat 61 and hence, the communication between the float chamber 12a and the fuel nozzle 13 is cut off.

The arrangement of the other components is basically not different from that in the first embodiment and hence, portions or components corresponding to those in the first embodiment are designated by the same reference symbols and numerals in FIG. 13 and the description of them is omitted.

Next, a fourth embodiment of the present invention shown in FIG. 14 will be described below.

An engine E is constructed into a horizontal type with a crankshaft 2 disposed horizontally. A cylinder block 5 connected to one side of a crankcase 1 supporting the crankshaft 2 is disposed in such a manner that it is inclined at an angle which is nearly horizontal, and a carburetor C is mounted to one side of a cylinder head 6 coupled to the cylinder block 5.

A fuel tank T is mounted on an upper portion of the crankcase 1, and a composite control valve V is mounted to a bottom surface of the fuel tank T. In this composite control valve V, a fuel strainer 79 projectingly mounted on an internal bottom surface of the fuel tank T is connected directly to a fuel introducing pipe 70. An inner air vent pipe 23 extending vertically through the fuel tank T opens at its lower end directly into an atmospheric air introducing recess 49′ which corresponds to the atmospheric air introducing pipe 49 in the first embodiment and which is formed in a valve housing 40.

The inner air vent pipe 23 also opens at its upper end into a threadedly engaged portion between a tank cap 21 and an oil supply port tube 20 of the fuel tank T, and the inner air vent pipe 23 communicates with an upper space 3 in the fuel tank T through a spiral clearance existing at such a threadedly engaged portion. The spiral clearance functions as a gas-liquid separating means to inhibit the entrance of a waved fuel in the fuel tank T into the inner air vent pipe 23.

A fuel conduit 71 leading to a fuel chamber 46 in the composite control valve V is connected directly to a fuel inlet in the carburetor C.

The arrangement of the other components is similar to that in the first embodiment and hence, portions and components corresponding to those in the first embodiment are designated by the same reference symbols and numerals in FIG. 14 and the description of them is omitted.

Finally, a fifth embodiment of the present invention shown in FIGS. 16 and 17 will be described.

A ventilation bore 22 leading to the inner air vent pipe 22 opens into an inner surface of an oil supply port tube 20, as in the first embodiment. An overflow bore 36 is provided below the ventilation bore 22 to extend through a sidewall of the oil supply port tube 20 and opens into an inner face of the sidewall. An overflow pipe 37 extending downwards below the engine E is connected to an outer end of the overflow bore 36. Therefore, when the tank cap 21 is removed from the oil supply port tube 20 as shown in FIG. 17 to resupply the fuel into the fuel tank T through the oil supply port tube 20, if the oil surface of the fuel rises up to the inside of the oil supply port tube 20 to reach a location of the overflow bore 36 due to an excessive resupply, such fuel overflows from the overflow bore 36 into the overflow pipe 37, whereby any further rising of the fuel oil surface in the oil supply port tube 20 can be suppressed. Therefore, it is possible to prevent the entrance of the fuel into the ventilation bore 22 which opens into the inner wall of the oil supply port tube 20 at a location above the overflow bore 36 and thus, the intrinsic ventilating function of each of the ventilation bore 22, the inner air vent pipe 23 and the outer air vent pipe 24 is ensured.

On the other hand, a pair of upper and lower annular seal lips 28b and 28c are integrally formed at a lower end of a cylindrical portion 28 of a partitioning member 26 in a gas-liquid separating means 25 of a tank cap 21, to come into close contact with an inner peripheral surface of a lower end of an oil supply port tube 20. The seal lips 28b and 28c are disposed at locations where they sandwich from above and below the overflow bore 36 at a position below the ventilation bore 22. Therefore, in a state in which the tank cap 21 has been mounted to the oil supply port tube 20, the overflow bore 36 is closed by the pair of the seal lips 28b and 28c, so that the communication of the overflow bore 36 with the inside of the fuel tank T is cut off.

In this way, the partitioning member 26 is adapted to close the overflow bore 36 by the pair of the seal lips 28b and 28c to cut off the communication of the overflow bore 36 with the inside of the fuel tank T. Therefore, even if the waving of the fuel occurs within the fuel tank T, the flow-out of the fuel into the overflow bore 36 can be prevented.

A strap 38 extending through the through-bore 30 and the porous member 27 is connected to a ceiling wall of the tank cap 21, and the strap 38 is provided at its lower end with a removal-preventing member 39 which cannot easily pass through the oil supply port tube 20. Therefore, when the tank cap 21 has been removed from the oil supply port tube 20, the removal-preventing member 39 is caught at the lower end of the oil supply port tube 20, whereby the disengagement of the tank cap 21 can be prevented.

The arrangement of the other components is the same as that in the first embodiment and hence, portions or components corresponding to those in the previous embodiment are designated by the same reference symbols and numerals in FIGS. 16 and 17 and the description of them is omitted.

The present invention is not limited to the above-described embodiments, and various modifications in design maybe made without departing from the subject matter of the invention.

Claims

1. A fuel supply control system for an engine, comprising a composite control valve which is constructed by a valve housing, a negative pressure working chamber defined in the valve housing to communicate with a negative pressure generating section in the engine, a first control valve operable to be opened and closed with generation and extinction of a negative pressure in the negative pressure working chamber, and a second control valve operable to be opened and closed with the generation and extinction of the negative pressure in the negative pressure working chamber, the first control valve being incorporated into an air vent system which provides communication between an upper space in a fuel tank and the atmosphere, the second control valve being incorporated into a fuel passage system which provides communication between a portion of the fuel tank below a fuel oil surface and a fuel supply section in the engine, at least a portion of the air vent system being constituted by an inner air vent pipe disposed within the fuel tank, a gas-liquid separating means being provided in an opening of the inner air vent pipe into the upper space, the gas-liquid separating means being adapted to inhibit entrance of a fuel within the fuel tank into the inner air vent pipe and to permit the ventilation.

2. A fuel supply control system for an engine according to claim 1, wherein an upper end of an air vent passage extending downwards through the fuel tank to communicate with the atmosphere opens into an inner wall of an oil supply port tube of the fuel tank, the oil supply port tube being tightly closed by a tank cap, and wherein an upper end of an overflow passage extending downwards below the fuel tank opens into the inner wall of the oil supply port tube at a location below an opening in the upper end of the air vent passage.