U.S. patent number 3,674,043 [Application Number 05/050,074] was granted by the patent office on 1972-07-04 for method of preventing vapor lock during engine operation and of fuel leakage to carburetor after engine stoppage.
Invention is credited to Neil C. Norton.
United States Patent |
3,674,043 |
Norton |
July 4, 1972 |
METHOD OF PREVENTING VAPOR LOCK DURING ENGINE OPERATION AND OF FUEL
LEAKAGE TO CARBURETOR AFTER ENGINE STOPPAGE
Abstract
Vapor lock which might otherwise occur in its fuel supply pump
during high temperature operation of a liquid-fuel engine, is
minimized or eliminated by continuously withdrawing a small
fraction of the flow liquid from the bottom level of the pump
outlet conduit and reintroducing it at the top level of the pump
inlet conduit. Also, after pump and engine stoppage, pressurized
liquid remaining in the pump to carburetor (outlet) conduit, is
prevented from dribbling into the carburetor and vaporizing into
adjacent space (and creating a fire hazard and air pollution) by
relieving the back-pressure in such conduit and then closing same
without breaking the liquid column, by valve means in the (sigmoid)
pump bypass. Such small capacity bypass may be left open during
pump and engine function, without interfering with normal
operation, and closes in response to decreased back-pressure in the
line when the pump stops.
Inventors: |
Norton; Neil C. (Gardena,
CA) |
Family
ID: |
21963236 |
Appl.
No.: |
05/050,074 |
Filed: |
June 26, 1970 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
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726308 |
May 3, 1968 |
3559680 |
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616594 |
Feb 16, 1967 |
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Current U.S.
Class: |
137/12; 137/563;
261/72.1; 123/510; 417/311; 137/565.35 |
Current CPC
Class: |
F02D
33/006 (20130101); F02M 37/0047 (20130101); F02M
37/20 (20130101); F02M 37/0023 (20130101); Y10T
137/85954 (20150401); Y10T 137/0379 (20150401); Y10T
137/86171 (20150401) |
Current International
Class: |
F02M
37/20 (20060101); F02M 37/00 (20060101); F04b
023/00 () |
Field of
Search: |
;137/12,563,569 ;417/311
;261/72 ;123/139 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Cline; William R.
Parent Case Text
This is a continuation-in-part of Ser. No. 726,308, filed May 3,
1968, now U.S. Pat. No. 3,559,680, which is a continuation-in-part
of Ser. No. 616,594, filed Feb. 16, 1967, now abandoned.
Claims
What is claimed is:
1. In a method of moving a liquid-fuel supply from a liquid-fuel
reservoir by a pump inlet stream and pumping the fuel to a
carburetor of an engine by a pump outlet stream so as to move
liquid fuel to the carburetor from the reservoir at a normal
operating pressure of the pump, the steps for restraining fuel
entrance to the carburetor from the pump outlet stream after pump
stoppage, comprising:
back-relieving substantially all pressure in the outlet stream by
reverse movement of a small stream of the liquid fuel having a very
small cross-sectional flow area in respect to an internal cross
section of the outlet stream so as to bypass the pump after
cessation of pump operation until the pressure in said outlet
stream is substantially equalized with the pressure in said inlet
stream, and then stopping said reverse movement in response to
decline of backpressure in said outlet stream so as to retain
unpressurized liquid which was in the outlet stream from draining
into the carburetor after the pump has stopped.
2. The method of the preceding claim 1 wherein continuously during
pump operation said small stream is enabled to move to a top level
of the inlet stream from a bottom level of the outlet stream,
thereby minimizing occurrance of vapor lock in said pump.
3. In a method of moving a liquid-fuel supply from a liquid-fuel
reservoir by a pump inlet stream and pumping the fuel to a
carburetor of an engine by a pump outlet stream so as to move
liquid fuel to the carburetor from the reservoir at a normal
operating pressure of the pump, the improved step comprising:
relieving potential or actual fuel vaporization in the pump or
outlet stream by continually passing a small stream of the liquid
fuel from a bottom level of the outlet stream to a top level of the
inlet stream thereby reverse bypassing the pump and enabling
purging of vapor formed therein so as to maintain a continuous
supply of liquid fuel to the carburetor and prevent severance of
such supply by occurrance of vapor lock in the pump.
4. The method of the preceding claim 3 wherein said small stream of
bypassing liquid fuel enters the pump inlet stream by a downwardly
concave segment of a sigmoid path arising from the bottom level of
the outlet stream.
5. The method of the preceding claim 3 wherein upon pump stoppage,
flow of said small stream of bypassing liquid fuel is stopped in
response to decline of backpressure of the pump outlet stream,
thereby preventing pump-pressurized liquid which was in the outlet
stream from draining into the carburetor after the pump has
stopped.
Description
BACKGROUND OF THE INVENTION
Motorists driving in elevated temperatures, such as the summer-time
desert, as well as in rarefied atmospheres such as high mountain
areas, have become familiar with the problem of "vapor lock." This
is caused by volatilization of liquid fuel in the pump and in its
delivery line to the carburetor. Partial vaporization cuts down the
quantity of liquid fuel being pumped to the carburetor, in part
because of a gas pocket being retained in the pump or outlet, so
that the gas reduces the area left for liquid passage. The engine
chokes or sputters. At this point, the motorist may stop the car
and throw water on the fuel pump in an effort to condense the
trapped vapor, or to try to get the pump to purge it from the
system. However if such effort is unsuccessful (or is not resorted
to), further volatilization of the fuel may substantially
completely fill the pump with vapor so that no liquid fuel at all
is passed to the carburetor and the pump is "locked"; obviously the
motor then stalls and the vehicle stops. When the vaporization has
proceeded to this extent, it may not be reversible simply by
cooling the pump since the liquid flow or column has been broken.
The pump has to be primed with liquid in order to restore its
function.
Aside from cooling the engine, this problem has been dealt with by
providing gasoline blends or the like, having a higher boiling
point; such blends are then less effective at lower temperatures.
Obviously a simpler solution of the problem would be desirable.
Still another irritating problem of long standing has been that
resulting from the column of pressurized fuel remaining in the
pump-to-carburetor conduit when the pump and engine are stopped.
Especially in the presence of a leaky needle valve in the
carburetor, this liquid dribbles into the carburetor and evaporates
into the surrounding space. Especially in a closed space such as
the engine compartment of a small boat, this concentration of
combustable gases is highly explosive upon introduction of a spark,
such as that provided by engine start-up. Many fires which
completely destroyed the marine craft or motor boat have had such
origin. Such accumulated (gasoline) vapor is also toxic to persons
(or animals) having to inhale it. Beyond that, it is a general
pollutant of the atmosphere, which when multiplied by the large
number of "wet carburetors" on both land vehicles as well as marine
craft, dumps a tremendous tonnage of contaminants into the air over
any area which contains an active concentration of internal
combustion engines. In brief, such undesirable venting of unburned
fuel vapor results both from conditions associated with vapor lock
and from carburetor needle valve leakage. Both conditions benefit
from the present invention.
BRIEF SUMMARY OF THE INVENTION
As noted in the preceding abstract, leakage from the pump to
carburetor after engine shut-down is prevented by relieving the
pressure of the trapped liquid-fuel in the pump outlet conduit,
while retaining the column of liquid unbroken in this line so that
it neither dribbles into the carburetor or drains back toward the
fuel reservoir (as it would if the latter were at a lower level).
Vapor lock of the fuel pump during operation, is prevented by
bleeding of a small line of liquid from the lower level of the pump
outlet conduit and returning it to the upper level of the pump
inlet line. Such a circulation (bypass) is in continuous operation
during operation of the pump, typically by use of an S-shaped or
sigmoid bypass conduit of small internal cross section relative to
the cross section of the pump inlet and outlet conduits. Such
bypass can additionally be used to relieve the pressure of the fuel
trapped in the outlet conduit after engine and pump shut-down, by
provision in the bypass conduit of a normally-open valve which
closes (after pump stoppage) in response to decrease of
back-pressure in the outlet line. Thus a single and
simply-installed unit or assembly will perform both functions or
method-steps in sequence, and solely in response to movement of
liquid-fuel through the pump outlet conduit.
In this connection it may not be completely understood why the
method of relieving vapor lock depends upon withdrawing the bypass
stream from the lower outlet level and reintroducing it to the
upper (pump) inlet level. However, (vertical) bypass loops from top
to top, as well as from bottom to bottom are singularly
unsuccessful; so are bypass lines disposed at the same horizontal
level; so is an S-loop from top of outlet to bottom of inlet. It
may be that withdrawal from the bottom outlet level permits bubbles
to be swept to the carburetor rather than into the bypass and by
such "fractionation" relieves vapor which has started to form in
the pump and thus prevents its accumulation in situ. In any event,
the two problems (vapor lock and wet carburetor) which were not
previously thought to be associated, are thus solved simultaneously
or at least in sequence by these two method steps.
The present method which both counteracts threatened or potential
vapor lock during engine operation, and prevents leakage of
liquid-fuel from the pump to the carburetor (and its subsequent
vaporization into the atmosphere as from a flooded carburetor)
after pump stoppage, may be effected by use of a simple pump bypass
assembly such as herein illustrated, which unit can be readily
installed on conventional internal combustion engines whether
stationary engines or those used to propel land vehicles or marine
craft (as well as airplanes).
DESCRIPTION OF THE DRAWINGS
FIG. 1 is a side elevational view of my bypass assembly connected
to an automotive fuel pump (shown in broken lines), with the fuel
reservoir and carburetor indicated schematically; and
FIG. 2 is an axial sectional view of the bypass valve unit alone,
seen in upright, operative position.
DESCRIPTION OF A PREFERRED EMBODIMENT
As here illustrated, a conventional liquid-fuel pump P is located
intermediate the length of the fuel line L which extends from a
fuel reservoir R (i.e., gasoline tank) to the carburetor C of an
internal combustion engine (not shown) which utilizes the
carburetor-atomized fuel in the usual manner. The portion of the
fuel line extending from the reservoir to the pump may be
designated as the inlet conduit 10, and the portion from the pump
to the carburteor as the outlet conduit 12. It will be understood
that an unbroken stream or column is maintained in the line,
whether moving or not. The liquid in the reservoir R is ordinarily
under ambient atmospheric pressure, while the fuel in the outlet
conduit 12 is under the pressure added by the pump P, which is
usually on the order of about 1 to 10 p.s.i.g. with diaphragm-type
pumps.
Essentially the present assembly consists of a pair of T-fittings
14, 16, a (S-shaped) bypass conduit 18 and a valve assembly 20. One
Tee, 16, is connected between the inlet conduit 10 and the inlet
port 6 of pump P, with its upstanding nipple 7 coupled to the valve
assembly 20 above it. The other Tee, 14, is inserted between the
outlet conduit 12 and the output port 8 of the pump P with its
downturned nipple 17 joined to the downwardly concave segment 19 of
the bypass conduit 18. The successive convex segment 21 of the
bypass conduit is received in the aperture mount 9 of the upper
housing piece 24 of the valve assembly 20. Preferably the internal
diameter of bypass conduit 8 is about 1/6 or less that of the
outlet conduit 12.
The valve assembly proper 20 is formed of a longitudinally
apertured, two-piece housing shell or tube 24, 26 threadedly
coupled together at the insertion neck 27 of the lower piece 26. A
metering plug 28 is formed with an axial bore 11 which defines the
flow capacity of the bypass 18, being threadedly mounted at 25 in a
tapped end-socket 12 of the lower housing 26. A slotted end 31
enables axial adjustment of the plug 28, which at its inner end 23
forms a seat for the lower end of a compression spring 30 which is
loosely disposed within the housing chamber 29. At the upper end of
the housing 26, it is peripherally relieved at 15 and axially
drilled partway to form a restricted bore 33. At the inner end of
the bore 33 an outstepped annular shoulder 32 forms a seat for a
check ball 22, the underface of which is supported by the terminal
coil 34 of the spring 30. Below the stepped area, the channel
tapers outwardly at 36; into which tapered or conic section the
valve 22 partially projects even when seated, and into which it is
progressively thrust by increased back pressure from the passage
35. It will be seen that the ball is in a position of gravitational
descent, supported only by the weak spring 30, so that a
comparatively small back pressure (e.g. 1/8 p.s.i.g. or less) in
the line 18-35-33 will serve to open it. However, when such minimum
back pressure fails, it is immediately closed by the tension of
spring 30 (which tension can be set or adjusted by positioning the
plug 28).
Thus it will be seen that the added assembly has a dual function:
When the pump P is operating, the return flow of liquid through the
open bypass 18, which is actually metered to a small trickle by the
small diameter of the passage 33, does not appreciably curtail the
main fuel flow through the supply line L; but the bottom-level
pickup provided by the descendingly bowed segment 19 of the bypass
has been found to be particularly effective (from comparison with a
top-side pickup from the same outlet conduit location by an
over-the-top-of-pump C-shape conduit) to minimize or eliminate
vapor lock in the operating pump. Secondly, the valve 22 which is
lightly loaded by the spring 29 so as to open at a low back
pressure in the bypass 18, although continually open during normal
pump operation, is successively functional after cessation of pump
action has stopped the main fluid flow through the supply line
12-10. At such time, the still-open valve first equalizes the line
pressure of the carburetor side 12 against the unpressurized feed
line 10, and then automatically closes so as to still retain liquid
in the whole line (even in the event of a leaking carburetor needle
valve). On the other hand, if for any reason the pressure on the
reservoir side of the pump should exceed that on the opposite side
after the pump has stopped, the valve 22 would close at once so as
not to exert this additional pressure against the carburetor needle
valve. It is notable that this overall or composite result is
obtainable without any alteration of an existing or installed pump,
and merely by incorporation -- because of the Tees 14, 16 at
connections already present on the fuel pump -- of the present
simplified and highly effective, self-operating structure.
It will be clear to those skilled in the art that changes of
construction and operation may be made within the present inventive
concept, and therefore this disclosure is not to be limited to the
precise details shown in the drawings and particularly described in
the specification by way of example, but it is my intention to
claim the invention broadly as hereafter defined.
* * * * *