The present invention will become more fully understood from the detailed description given hereinbelow and the accompanying drawings which are given by way of illustration only, and thus are not limitative of the present invention, and wherein:
The carburetor body 1 includes an air intake-system formed section la as well as a fuel system formed section 1b joined to and integrated into the bottom of the air intake-system formed section 1a. The air intake tube 6 and a guiding section 7 are formed in the air intake-system formed section 1a. The air intake tube 6 is the place where the intake air flown, through the air cleaner, into the air intake tube 6 and the fuel supplied from the fuel system 4 are blended to produce an air-fuel mixture. While the throttle valve 3 reciprocally travels as cutting across the air intake tube 6, the guiding section 7 guides the reciprocating movement of the throttle valve 3. The air-fuel mixture, let out from a downstream end 6b of the air intake tube 6, passes through the intake passage which the intake pipe and the like constitute. The air-fuel mixture is eventually taken into combustion chamber of the internal combustion engine.
The throttle valve 3 is a sliding valve that is slidably guided by the guiding section 7. The throttle valve 3 links with a control lever 8, which is controlled as swinging when the driver operates the accelerator controlling member. As the accelerator controlling means controls the throttle valve 3 with the control lever 8, the throttle valve 3 travels reciprocating up and down. The reciprocating movement is an opening-and-closing movement for the air intake tube 6, and the air intake tube 6 opens and shuts within an opening degree range from the idling opening degree to the full throttle. The intake air flowing through the air intake tube 6 is controlled in this way.
The float chamber 10 is formed by joining the float chamber body 2 to the fuel-system formed section 1b. The fuel retained in the float chamber 10 forms a liquid surface of a certain level defined by a float 12 that opens and closes a fuel-inflow-control valve 11. The fuel in the float chamber 10 is supplied to the air intake tube 6 through the fuel system 4 by a negative pressure generated in the air intake tube 6 in accordance with the opening degree of the throttle valve 3. A drain plug 13, which is a member in a shape of tube with a bottom, is screwed up to the bottom of the float chamber body 2.
The fuel system 4 is provided to the fuel-system formed section 1b, which is located under the air intake tube 6 and extends down to the underneath of the liquid surface of the fuel in the float chamber 10. A slow-speed fuel system 4s and a main fuel system 4m constitute the fuel system 4. A slow fuel jet 16, an idle port 17, a by-pass port 18 constitute the slow-speed fuel system 4s. Meanwhile the main fuel system 4m includes a needle jet 20 into which the jet needle 5 attached to the throttle valve 3 is inserted. The main fuel system also includes a main fuel jet 21 that meters the amount of fuel flowing into the needle jet 20. The fuel is supplied to the air intake tube 6 mainly through the slow-speed fuel system 4s with the throttle valve 3 being in the range of small opening degree, that is, while the internal combustion engine is operating at an idling speed or is operating with a light load. Meanwhile the fuel is supplied to the air intake tube 6 mainly through the main fuel system 4m with the throttle valve 3 being in the range of large opening degree, that is, while the internal combustion engine is operating with a heavy load. At this time, the fuel supplied to the air intake tube 6 is metered by the jet needle 5.
The main fuel pipe, that is the needle jet 20, is disposed as extending linearly in the up and down directions, and is screwed to be fixed to the fuel-system formed section 1b. The fuel, which comes from the float chamber 10 passing through the main fuel jet 21, is supplied to the air intake tube 6 through an upper end portion 20a of the needle jet 20. The upper end portion 20a is disposed inside a main nozzle 22, which is formed at an upper end portion of the fuel-system formed section 1b, and which protrudes inside the air intake tube 6. The fuel injected from the upper end portion 20a is supplied to the air intake tube 6 after the fuel is atomized, in the main nozzle 22, by the bleed air coming from a bleed air passage 23.
The needle jet 20 includes a metering portion 20c into which the jet needle 5 is inserted. The jet needle 5 and the metering portion 20c combined together form a cross section area, and the area is changed by the position of the jet needle 5 in accordance with the opening degree of the throttle valve 3. With the change, the amount of fuel corresponding to the intake air flow is supplied from the needle jet 20, and thus the output of the internal combustion engine is controlled.
Incidentally, when a running motorcycle, an off-road type motorcycle in particular, makes a relatively big jump and then lands on the ground, the fuel inside the needle jet 20, that is, the fuel-in-jet, is accelerating downward (hereinbelow, the force acting on the fuel is referred to as “downward acceleration”). The downward acceleration sometimes makes the fuel-in-jet move downward and flow out of the needle jet 20. The fuel thus flown out may possibly be flown back to the float chamber 10 through the main fuel jet 21. This reverse flow makes the air-fuel mixture lean temporarily. For the purpose of preventing the lean air-fuel mixture from being produced in this way, a valve mechanism 30 is provided to the carburetor C. The valve mechanism 30 checks the downward reverse flow of the fuel-in-jet, which may take place when the downward acceleration acts on the fuel-in-jet.
Now, refer to
An upper holder 31 and a lower holder 32 constitute the valve holder H. The upper holder 31 is joined to a female-threaded portion 20e, which is formed in a bottom portion of the needle jet 20, and which is a portion for screw fixation. The lower holder 32 is screwed to be detachably joined to the upper holder 31. A space is formed by joining together the upper holder 31, the lower holder 32 and the main fuel jet 21. Part of the space constitutes a fuel retention chamber 33. Precisely, it is the part located on a downstream side of the fuel flow from the valve body 40 in a state where the valve of the valve mechanism 30 is closed.
The cylindrical upper holder 31 is disposed immediately above the valve body 40. Formed in the upper holder 31 is an over-valve passage 34, extending in the up and down directions and communicating to a fuel passage 25 inside the needle jet 20. In addition, formed in an upper end portion 31a of the upper holder 31 is a male threaded portion 31e, as a screw-fixation portion to be screwed into the female-threaded portion 20e. Moreover, formed at a bottom end portion 31b of the upper holder 31 are: a protrusion 37 where the valve body can be seated; and a pair of fuel entrances 34a through which the fuel that has passed through the main fuel jet 21 is led to the over-valve passage 34. Furthermore, formed between the upper end portion 31a and the lower end portion 31b is a male threaded portion 31c to which the lower holder 32 is joined.
The protrusion 37 is formed in a lower end surface 31b1 of the lower end portion 31b. The protrusion 37 is an open-valve seat portion that the valve body 40 is seated on when the fuel is supplied to the air intake tube 6 from the float chamber 10. The protrusion 37 protrudes downward in a position facing, in the up and down directions, an upper end portion 21a of the main fuel jet 21. The protrusion 37 is composed of a pair of arc-shaped ridges that an annular ridge interrupted by fuel entrances 34a is formed into. For the purpose of preventing the valve body 40 from adhering to the lower end portion 31b, the protrusion 37 has a shape such that the contact area with the valve body 40 can be as small as possible. For this reason, a width t in the radial direction of the protrusion 37 is approximately equal to the thickness of the valve body 40, and, as a result, the valve body has a smaller contact area with the lower end portion 31b than that with the upper end portion 21a. In a state where the valve body 40 is seated on the protrusion 37, the protrusion 37, which serves as adherence prevention means, forms a gap 38 between the valve body 40 and the lower end portion 31b. Through the gap 38, the fuel flows into the over-valve passage 34 in that state. Part of each fuel entrance 34a constitutes the gap 38 in this embodiment. Thanks to the fuel flow through the gap 38, the gap 38 also contributes to the prevention of the adherence of the valve body 40.
The cylindrical lower holder 32 has a female-threaded portion 32c formed in the upper end portion 32a and screwed onto the male-threaded portion 31c of the upper holder 31. The cylindrical lower holder 32 also has a female-threaded portion 32e formed in the lower end portion 32b, which is a screw-fixation portion into which a screw-fixation portion of the main fuel jet 21, that is, the male-threaded portion 21e, is screwed. The main fuel jet is disposed immediately below the valve body 40. The upper end portion 21a of the main fuel jet 21 faces the fuel retention chamber 33, and constitutes close-valve seat portion. The valve body 40 can be seated on an upper end surface 21a1 of the upper end portion 21a. The passage for the fuel formed inside the main fuel jet 21 constitutes the under-valve passage 35 of the valve mechanism 30.
As has been described above, the upper holder 31 and the main fuel jet 21 constitute the upper valve seat and the lower valve seat, respectively. The over-valve passage 34 and the under-valve passage 35 are positioned with the valve body 40 and a part of the fuel retention chamber 33 placed in between. There, the over-valve passage 34 and the under-valve passage 35, together with the fuel passage 25 of the needle jet 20, are arranged to form a straight line. Additionally, in the valve mechanism 30, the lower end portion 31b and the upper end portion 21a, which face each other with the valve body 40 located in between in the up and down directions, constitute, respectively, an upper facing portion and an lower facing portion.
Furthermore, the male-threaded portion 31e of the upper holder 31 has the same structure as that of the male-threaded portion 21e of the main fuel jet 21. With this configuration, the valve mechanism 30 is also provided to an existing carburetor which has neither the valve holder H nor the valve body 40, that is, no valve mechanism 30, and in which the needle jet 20 and the main fuel jet 21 are directly screwed together.
The valve body 40 is a member which has a roughly circular shape, and which is made of a synthetic resin. The center portion of the valve body 40 constitutes a blockage portion 40c. When the valve body 40 is seated on the protrusion 37, or on the upper end portion 21a, the blockage portion 40c blocks the fuel flowing though the valve body 40, while the fuel is allowed to pass through a fuel entrance 41 formed in the valve body 40. At least one opening, formed near the perimeter of the valve body 40 constitutes the fuel entrance 41. Three cutaways 40a, which are formed in an outer peripheral portion of the valve body 40, and which are located equidistantly in the circumferential direction, correspond to the fuel entrance in this embodiment.
Flared portions 40b are formed in the valve body 40 by the formation of the cutaways 40a. When the valve body 40 is placed in the fuel retention chamber 33, the flared portions 40b are brought into contact with the inner peripheral surface of the lower holder 32. Thus, the movement of the valve body 40 in the radial direction of the two valve passages 34 and 35 is restricted. Thanks to the lower holder 32, the blockage portion 40c is seated, without failure, on the protrusion 37 to allow the fuel flow, while the blockage portion 40c is seated, without failure, on the upper end portion 21a to block the reverse flow of the fuel-in-jet.
In addition, the fuel retention chamber 33 has an annular chamber 33a, formed by the lower holder 32 and the upper holder 31 and surrounding the lower end portion 31b. The width of each fuel entrance 34a in the up and down directions is approximately equal to the width of the annular chamber 33a in the up and down directions. The fuel in the fuel retention chamber 33, mostly, passes through the annular chamber 33a, and then enters, through the fuel entrances 34a, the over-valve passage 34. After that, the fuel flows into the needle jet 20.
In the carburetor C with a configuration described above, the fuel having flown out of the float chamber 10 and through the main fuel jet 21, is then supplied from the needle jet 20 to the air intake tube 6. Incidentally, the fuel flows out of the float chamber 10, then passes through the main fuel jet 21 and the fuel retention chamber 33, and then flows into the needle jet 20. When the fuel is supplied to the air intake tube 6, the fuel thus flowing moves the valve body 40. The valve body 40 is seated on the protrusion 37 (see
On the other hand, when downward acceleration acts on the fuel-in-jet, the downward acceleration forces the fuel-in-jet to flow slightly downward, and the fuel-in-jet moves the valve body 40 until the valve body 40 is seated on the upper end portion 21a to block the under-valve passage 35 (see
As seen from above, the valve mechanism 30 constitutes a check valve. The check valve allows the flow of the fuel, which enables the supplying of the fuel from the float chamber 10 to the air intake tube 6, while the reverse flow of the fuel-in-jet is blocked by the check valve.
While the valve body 40 is seated on the upper end portion 21a, the fuel that is flown out of the fuel retention chamber 33 flows, through the fuel entrances 34a and the over-valve passage 34, into the needle jet 20. Then, the fuel is metered by the jet needle 5, and thereafter, is supplied to the air intake tube 6. The air-fuel mixture is thus prevented from becoming lean. At this time, since the fuel retention chamber 33 has the annular chamber 33a, extra fuel—precisely, the amount equivalent to the capacity of the annular chamber 33a—is retained in the fuel retention chamber 33. Consequently, even when the valve mechanism 30 is in the closed-valve state, the amount of fuel that exists in the fuel retention chamber 33 is sufficient. As a result, a shortage of fuel, which may possibly take place when the valve mechanism 30 is in the closed-valve state, is prevented without failure. The fuel in the fuel retention chamber 33 is then supplied, with no interruption, to the needle jet 20 through the fuel entrances 34a, each of which has a width in the up and down directions being approximately equal to that of the annular chamber 33a.
Subsequently, description will be given of advantages and effects of the embodiment with a configuration described thus far.
The carburetor C equipped with the needle jet 20, into which the jet needle 5 is inserted, is provided to an internal combustion engine. A motorcycle equipped with such an internal combustion engine including the carburetor C jumps while running and lands on the ground. At that moment, downward acceleration acts on the fuel-in-jet. Since the valve-mechanism 30 is provided to the carburetor C to prevent the downward reverse flow of the fuel-in-jet, the valve mechanism 30 actually prevents the downward reverse flow of the fuel-in-jet, which may possibly be caused by the downward acceleration acting on the fuel-in-jet. As a result, even under the downward acceleration, the fuel-in-jet is supplied to the air intake tube 6, and the production of a lean air-fuel mixture that may possibly be produced temporarily is prevented.
The valve mechanism 30 includes the valve body 40, which has a plate-like shape moved by the flow of the fuel. The valve mechanism 30 also includes the upper holder 31, which serves as an upper valve seat disposed immediately above the valve body 40, and in which the protrusion 37 is formed to allow the valve body 40 to be seated thereon. The valve mechanism 30 also includes the main fuel jet 21, which serves as a lower valve seat disposed immediately below the valve body 40 and on which the valve body 40 can be seated. When the fuel is supplied from the float chamber 10 to the air intake tube 6, the valve body 40 is seated on the protrusion 37 to prevent the adherence of the valve body 40 to the upper holder 31. When downward acceleration acts on the fuel-in-jet, the valve body 40 is seated on the main fuel jet 21 to prevent the downward reverse flow of the fuel-in-jet. The plate-like shape of the valve body 40 facilitates the movement of the valve body 40 caused by the flow of the fuel. Accordingly, a subtle downward flow of the fuel-in-jet, which takes place when the downward acceleration acts on the fuel-in-jet, causes the valve body 40 to be seated on the main fuel jet 21. In addition, the valve body 40 has such a structure including the protrusion 37 that the valve body 40 and the upper holder 31 cannot adhere to each other so easily. As a result, the reverse flow of the fuel-in-jet is prevented quickly, while the valve mechanism 30 prevents, more effectively, the air-fuel mixture from being lean.
The upper holder 31, the lower holder 32 and the main fuel jet 21 form the fuel retention chamber 33, in which the valve body 40 is housed. The fuel retention chamber 33 has the annular chamber 33a surrounding the lower end portion 31b of the upper holder 31. Accordingly, the fuel retention chamber 33 retains an extra amount of fuel—the amount equivalent to the capacity of the annular chamber 33a. While the valve body 40 is seated on the main fuel jet 21, the valve mechanism 30 is in the closed-valve state. Even in the case of the closed-valve state continuing for a little longer time, the fuel in the fuel retention chamber 33 is supplied to the needle jet 20. As a result, no fuel shortage occurs even when the valve mechanism 30 is in the closed-valve state. Thus, the valve mechanism 30 prevents, more effectively, the air-fuel mixture from being lean.
The upper holder 31 of the valve holder H is screwed into and is fixed to the needle jet 20, while the male-threaded portion 31e of the upper holder 31 and the male-threaded portion 21e of the main fuel jet 21 have the same structures. Accordingly, to an existing carburetor in which the needle jet 20 is screwed to be fixed to the main fuel jet 21, the valve mechanism 30 can be added by screwing to fix the upper holder 31 to the needle jet 20. As a result, existing carburetors can be used for the present invention.
Next, a second embodiment of the present invention will be described by referring to
The valve mechanism 30 includes a valve body 40 and a valve holder H to which a needle jet 20 is joined. A jet needle 5 is inserted into the needle jet 20. An upper holder 31 and the lower holder 32 constitute the valve holder H.
An under-valve passage 35 is formed in the lower holder 32 in a position further upstream of the fuel flow than the valve body 40 at the time when the valve body 40 is in the closed-valve state. A female-threaded portion 32c screwed onto a male-threaded part 31c of the upper holder 31 is formed in an upper end portion 32a while a female-threaded portion 32e screwed onto a male-threaded portion 21e of a main fuel jet 21 is formed in an lower end portion 32b. A close-valve seat portion 38 on which the valve body 40 can be seated is formed between the upper end portion 32a and the lower end portion 32b.
As seen from the above, the upper holder 31 and the lower holder 32 constitute the upper valve seat and the lower valve seat, respectively. The upper holder 31 and the lower holder 32 are joined together to form a space. Part of the space located on the further downstream side of the fuel flow than the valve body 40 positioned at the time when the valve mechanism 30 is in the closed-valve state constitutes a fuel retention chamber 33. A lower end portion 31b and the seat portion 38 constitute an upper facing portion and a lower facing portion, respectively. The upper and the lower facing portions face each other with the valve body 40 in between in the up and down directions.
When the fuel is supplied from a float chamber 10 to an air intake tube 6 (see
On the other hand, when downward acceleration acts on the fuel-in-jet, the downward acceleration forces the fuel-in-jet to flow slightly downward, and the fuel-in-jet moves the valve body 40 until the valve body 40 is seated on the seat portion 38 to block the under-valve passage 35 (as indicated by a two-dot chain line in
According to the second embodiment, the same advantages and effects can be obtained as those obtained according to the first embodiment.
Hereinbelow, a description will be given of an embodiment in which a part of configurations of the embodiments described above is modified. The description will be given of the part of the configuration that is modified.
In a valve mechanism 30, a valve holder H may be attached to a needle jet 20, and the needle jet 20 may constitute an upper valve sheet.
The invention being thus described, it will be obvious that the same may be varied in many ways. Such variations are not to be regarded as a departure from the spirit and scope of the invention, and all such modifications as would be obvious to one skilled in the art are intended to be included within the scope of the following claims.
Number | Date | Country | Kind |
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2006-120930 | Apr 2006 | JP | national |