Information
-
Patent Grant
-
6481530
-
Patent Number
6,481,530
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Date Filed
Monday, September 25, 200024 years ago
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Date Issued
Tuesday, November 19, 200222 years ago
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Inventors
-
-
Examiners
Agents
-
CPC
-
US Classifications
Field of Search
US
- 184 63
- 184 61
- 184 64
- 123 196 R
- 123 196 S
- 137 217
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International Classifications
-
Abstract
To be used with an internal combustion engine having a crank case wherein engine oil is contained, and an engine internal oil pressure system structured to distribute lubricating oil to moving and wearing parts of the engine from the crank case, an engine pre-lubrication system which includes an oil reservoir to contain a quantity of engine oil to be supplied through an oil flow corridor of the reservoir to the engine internal oil pressure system for pre-lubrication of the engine. The pre-lubrication system is structured to constantly maintain an acceptable supply of oil within the reservoir and will supply pre-lubricating oil upon a burst of air being initiated and directed into the oil reservoir, through an air flow corridor, so as to displace oil contained in the reservoir out through the oil flow corridor for pre-lubrication of the engine.
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to an engine pre-lubrication system to be used with an internal combustion engine, which is easy to install and operate in order to provide start up lubrication to the engine and eliminate the need for the engine to run for a period of time, without lubrication, until the normal engine operation provides lubrication.
2. Description of the Related Art
It is a known fact that a main source of the wear and tear that can affect an engine, results from a cold start up of an unlubricated engine. Specifically, after sitting for even a short period of time, the internal wearing parts within an internal combustion engine lose a substantial amount of the oil lubricant, which coats their surface, therefore requiring an initial start up with insufficient lubrication. As a result, many engine oils are being specifically manufactured with properties that will help the oil remain on the wearing parts for an extended period of time, thereby providing some lubrication for start up after the engine has been sitting idle. These improved oils, however, do not completely solve the problem, especially if the engine, such as in boats, trucks, heavy machinery, power plants, or other applications, remains idle for an extended period of time.
As a result, mechanical systems have been devised consisting of a motor and oil pump along with associated wiring, relays and controls, which start just a few seconds before starting the engine. The pump takes oil from the engine crankcase or oil reservoir and forces it into the engine internal oil pressure system such that the wearing parts are properly lubricated before the engine is started. Immediately upon starting, the internal engine oil pump starts supplying oil to all the moving and wearing parts and the pre-lubricating pump and motor is shut down. This type of system, however, is expensive, complicated, difficult to install and has many moving and wearing parts, such as the pump and motor, which are subject to maintenance and wearout. Accordingly, such systems are not widely implemented, especially in circumstances of retro-fitting existing engines.
In this regard, it is recognized that some of these problems were solved with the issue of U.S. Pat. No. 5,494,013, which provided a system that was less expensive, simpler, and more easily and economically installed. That system, however, still left room for further improvement. In particular, that system still included a number of complicated and often expensive valves to achieve the necessary function. Also, the oil reservoir was susceptible to gravitational discharge of its oil supply during engine shut down.
Accordingly, there is still a need in the art for a pre-starting lubrication system which is inexpensive and simple in design, eliminates the need for complicated, expensive mechanical parts, and retains the oil supply within the oil reservoir prior to engine start-up. The system of the present invention is designed specifically to meet these needs.
SUMMARY OF THE INVENTION
The present invention relates to a pre-starting lubrication system to be utilized primarily on an internal combustion piston engine of the type having a crankcase, wherein engine lubricating oil is contained, and an integral engine driven oil pump and pressure system are structured to distribute lubricating oil to all of the moving and wearing parts of the engine. Specifically, the pre-starting lubrication system will include an oil reservoir which will contain a quantity of engine oil therein to be utilized in the pre-lubrication process. Further included with the oil reservoir is an air flow corridor wherethrough air will enter and exit the oil reservoir and an oil flow corridor wherethrough oil will enter and exit the oil reservoir. The oil reservoir is connected in fluid flow communication with the engine internal oil pressure system through first an oil riser, and then an oil conduit, thereby allowing the oil to flow from the reservoir to lubricate the wearing parts prior to starting. The oil riser derives from the oil flow corridor and connects to the oil conduit at a point equal to generally a top portion of the oil reservoir. This, in turn, eliminates the possibility of gravitational discharge from the oil reservoir to the engine internal pressure system. Connected in fluid flow communication with the air flow corridor is an air supply assembly and an air venting assembly. The air supply assembly is connected by way of an air conduit with the air flow corridor, which is structured to supply a quantity of air under pressure into the oil reservoir through the air flow corridor. As to the air venting assembly, it is connected to the air flow corridor so as to vent pressurized air from the reservoir.
The pre-starting lubrication is initiated by an air control assembly which initiates and maintains air flow from the air supply assembly through the air flow corridor and into the oil reservoir in such a manner as to push oil out of the oil reservoir, through the oil flow corridor, and into the engine internal oil pressure system, wherein the oil is distributed to the wearing parts for a predetermined time after which the air supply assembly is shut off and pressurized air in the oil reservoir is then vented by the air venting assembly.
Further included with the pre-starting lubrication system is an oil supply assembly. The oil supply assembly ensures that the quantity of engine oil for use in pre-starting lubrication is continuously supplied to the oil reservoir once the engine has been started and is running normally. Additionally, in order to ensure that the oil reservoir does not become overfilled or underfilled, a level maintenance assembly is included. The level maintenance assembly protect the engine by preventing total emptying of the oil reservoir and thereby ensuring that air does not exit the oil reservoir through the oil flow corridor where it can adversely affect the pressure of the engine lubricating system. The level maintenance assembly also detects and prevents overfilling of the oil reservoir, thereby ensuring that the excess oil does not adversely affect the air supply assembly and will not drain the oil system of the engine.
BRIEF DESCRIPTION OF THE DRAWINGS
For a fuller understanding of the nature of the present invention, reference should be had to the following detailed description taken in connection with the accompanying drawings in which:
FIG. 1
is a schematic view of a first embodiment of the pre-lubrication system of the present invention;
FIG. 2
is a schematic view of the junction housing of the present invention;
FIG. 3
is a schematic view of a second embodiment of the pre-lubrication system of the present invention;
FIG. 4
is a schematic view of a third embodiment of the pre-lubrication system of the present invention;
FIG. 5
is schematic partial view wherein the engine has its oil reservoir separate from the crankcase;
FIG. 6
is a schematic partial view illustrating an alternative embodiment including a locating guide for the stopper float.
Like reference numerals refer to like parts throughout the several views of the drawings.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
Shown throughout the figures, the present invention is directed towards a pre-starting engine lubrication system, generally indicated as
10
. The pre-starting lubrication system is structured for utilization with any type of internal combustion engine
80
which includes an engine oil reserve
70
, such as a reserve in the crank case of the engine
80
or in a separate oil reserve
71
, structured to contain and supply lubricating oil to all of the moving and wearing parts of the engine
80
, by way of an engine internal oil pressure system
75
. Specifically, conventional internal combustion engines
80
will draw oil from the engine oil reserve
70
only after the engine is started and operational, so as to direct the oil into the pressure system for lubrication of all moving and wearing parts to prevent breakdown. It is apparent that the engine must operate for an extended period of time without proper lubrication.
Turning specifically to the pre-starting lubrication system
10
of the present invention, it includes an oil reservoir
20
wherein a quantity of engine oil is contained for pre-starting lubrication purposes. It is noted, however, that this system may be used with any acceptable type of synthetic lubricant. This reservoir
20
can be manufactured with or separate from the engine
80
, either within or remote from the engine housing/compartment wherein the engine
80
is secured. As shown in
FIG. 1
, which illustrates a first embodiment of the pre-starting lubrication system
10
, the oil reservoir
20
includes an air flow corridor
40
and an oil flow corridor
30
. Specifically, the air flow corridor
40
is structured to allow the passage of air A in and out of the reservoir
20
therethrough. Similarly, the oil flow corridor
30
is structured to facilitate the exit and possible entry of oil B therethrough. Oil flow corridor
30
is connected to oil riser
89
which preferably terminates at a point generally equal to a top of reservoir
13
, and is then connected with the engine internal oil pressure system by oil conduit
35
. Through oil riser
89
and oil conduit
35
, oil B is provided from the oil reservoir
20
to the engine internal oil pressure system
75
for appropriate lubrication of the engine
80
. Because, however, oil riser
89
generally terminates either at or slightly above the level of the oil in reservoir
20
, the oil in the reservoir
20
will not be able to flow by gravity into the engine oil system
75
when the engine is shut down. As illustrated, oil riser
89
may, if desired, be secured to oil reservoir
20
by attachment mounts
12
, may be integrated within the reservoir, or may be separately secured.
Additionally, an air conduit
41
is connected with the air flow corridor
40
. The air conduit
41
is structured to enable the passage of air A from the air supply
45
to the reservoir
20
. As such, when air under pressure is introduced into the reservoir
20
, the oil B is naturally forced out through the oil flow corridor
30
for lubrication of the engine
80
. Alternatively, gasses other than air can be used, including but not limited to Carbon Dioxide and Nitrogen.
Located on the upper end of the oil riser
89
is a valve assembly
87
. During the pre-lubrication process described above, the valve
87
is closed by the oil pressure in riser
89
and conduit
35
and prevents any oil from escaping out of riser
89
or oil conduit
35
. Furthermore, the valve
87
also remains closed during oil flow from the engine oil system
75
, back into the reservoir
20
until the engine is shut down. During engine shutdown, however, a siphoning effect can ensue draining the oil from reservoir
20
back into engine
80
as a result of zero oil pressure in the engine
80
and a slightly negative pressure at the top of the riser
89
and at the valve
87
. Valve
87
is structured to remain closed as long as there is oil pressure in riser
89
or conduit
35
and to open when the engine oil pressure falls to zero. Accordingly, during engine shutdown, the valve
87
is opened, and the siphoning effect will be disrupted by air at atmospheric pressure carried through the conduit
43
from the crankcase
70
and into the top of riser
89
.
Connected in fluid flow communication with the air conduit
41
so as to supply a quantity of air A under pressure into the reservoir
20
is an air supply assembly
45
. The air supply assembly
45
will preferably be an air compressor or other air source structured to supply air at a pressure approximately but not necessarily equal to the normal engine operating oil pressure. For example, the air supply
45
can be a standard vehicle air compressor, as is already present in many vehicles such as a truck, and may include an independent air compressor, or a pressurized air tank. When use of the system
10
is desired, a switching assembly to actuate a valve is positioned on, near or remote from the air supply assembly
45
to admit air from the air supply assembly
45
into the reservoir
20
. As such, the switching assembly can be manual, electric, remote, direct or even automatic; i.e., sequenced with the engine starter switch. Further, in the case of many vehicles, the switching assembly can be dash-mounted for convenience, so long as it functions to admit the air into the reservoir
20
by actuating the appropriate valve on or near the air supply assembly
45
.
When the pressurized air is admitted from the air supply assembly
45
, it will flow through the air conduit
41
and into the reservoir
20
through the air flow corridor
40
. The increased air A within the reservoir
20
will then force oil B within the reservoir
20
out of the reservoir
20
through the oil flow corridor
30
as a result of the limited volume within the reservoir
20
. As such, the oil B will flow out through the oil flow corridor
30
and through the riser
89
and oil conduit
35
to the internal engine oil pressure system
75
where it will lubricate the engine
80
. Generally, the internal engine oil pressure system
75
will include the appropriate conduits and passages to allow the oil to flow to the pistons and wearing parts of the engine where it is needed. The air flow corridor
40
is, however, interconnected with the air supply assembly
45
by way of an air conduit
41
at the junction housing
42
. Specifically, referring to
FIG. 2
, the junction housing
42
may include an at least partially hollow interior
90
and is structured to receive the open ends
92
, of the conduit
41
, the conduit
44
, and the conduit
43
such that air flow is consistently able to flow therethrough. When pressurized air from the air supply assembly
45
is introduced into the junction housing
42
through the air conduit
41
, the interior wall structures
94
of the junction housing
42
direct the pressurized air into the open ends
92
of the conduits
40
and
43
. The conduit
43
, however, contains an orifice
91
, which includes a reduced diameter structured to severely restrict the airflow therethrough. As such, a majority of the air will be directed through air flow corridor
40
, and into reservoir
20
. This will, in turn, ensure that the oil B in reservoir
20
will flow out through the oil flow corridor
30
, through the oil riser
89
, and through the oil conduit
35
into the internal engine oil pressure system
75
in the method as described above.
Although oil B in the reservoir
20
can be supplied from an independent oil source, such as through a filler cap/plug
47
, it is preferred that the oil B within the reservoir
20
be supplied directly from the engine
80
, thereby maintaining a closed system and ensuring that pre-starting lubrication oil B will always be present, so long as the engine
80
is properly maintained and contains normal oil levels. In the preferred embodiments illustrated in
FIGS. 1 and 3
, the oil conduit
35
, will also function to supply the necessary oil to refill the reservoir
20
after each start up. Specifically, the oil conduit
35
is connected with the internal engine oil pressure system
75
in order to supply oil for pre-starting lubrication through the internal engine oil pressure system
75
. After pre-starting lubrication is performed, the oil quantities within the reservoir
20
will have decreased, however, the engine
80
is now started and running so as to pressurize its own internal oil pressure system. This pressurization results in oil being forced back through the oil conduit
35
to the reservoir
20
, thereby providing oil for a future pre-starting lubrication.
When the reservoir
20
has been vented and de-pressurized, the engine oil pressure system
75
will, as stated, be trying to force oil back to the reservoir via oil supply conduit
35
. Accordingly, to prevent the free flow of oil to the reservoir
20
, a one-way check valve
32
and a bypass orifice
33
may be included on the oil conduit
35
of some embodiments. In such an embodiment, as in
FIG. 3
, the one-way check valve
32
will be disposed in line with the oil conduit
35
such that free quantities of oil can flow therethrough only from the reservoir
20
to the engine
80
. However, so that small quantities of oil may bypass the one-way check valve
32
, and flow back to refill the reservoir
20
, a bypass orifice
33
is positioned to circumvent the one-way check valve
32
. In one embodiment, illustrated in
FIG. 3
, the one-way check valve
32
and bypass orifice
33
are separately included and connected in line with the oil conduit
35
. Alternatively, however, as illustrated in
FIG. 1
, both the one-way check valve and bypass orifice may be included in a single valve
31
positioned either directly preceding the oil flow corridor
30
, anywhere along the oil conduit
35
, or incorporated directly with the oil flow corridor
30
. Accordingly, while the engine
80
is operational, the reservoir
20
will become refilled by the engine oil in order to be ready at all times for the next engine start up. Only a very small portion of the oil output from the engine internal oil pump can bypass the check valve
32
through the bypass orifice
33
such that the engine itself will not be deprived of oil while the reservoir
20
is refilling. As such, the bypass orifice
33
is sized according to the individual engine on which the pre-starting lubrication system is used and the refilling takes place over the first few minutes of operation of the engine
80
. After the reservoir
20
is filled, the level maintenance assembly stops any further flow of oil from the engine oil pressure system
75
to the reservoir
20
.
Additionally included with the pre-lubrication system
10
of the present invention is a level maintenance assembly. The level maintenance assembly is specifically configured and disposed so as to ensure that overfilling or total emptying of the oil reservoir
20
is prevented. In the first embodiment of the level maintenance assembly, as illustrated in
FIG. 1
, they will include a stopper float
50
disposed within the reservoir
20
. When utilizing this stopper float
50
, the reservoir
20
will preferably include a tapered upper and lower surface or other means of guiding the stopper float into a flow sealing orientation, and the air flow corridor
40
will be disposed in a top surface of the reservoir
20
, while the oil flow corridor
30
is disposed in a bottom surface of the reservoir
20
. In use, the stopper float
50
floats freely within the reservoir
20
atop the oil B. As additional oil enters the reservoir
20
, the stopper float
50
will float up and be guided by the tapered upper surface until it moves into a flow sealing orientation
50
′ wherein the air flow corridor
40
is blocked off by the stopper float
50
′. When the float
50
′ is in the flow sealing orientation, no additional air or oil will exit the reservoir
20
and accordingly no additional oil will flow into the reservoir
20
and the system will not overflow or continue to take oil from the engine
80
. However, because the stopper float
50
′ is freely floating, air can still enter the reservoir
20
in order to push oil out to the engine for the next start up. Similarly, as the oil level within the reservoir drops to a reservoir empty level, the stopper float
50
will follow down into a flow sealing orientation
50
″ over the oil flow corridor
30
. This will prevent air from exiting the reservoir
20
and being introduced into the internal engine oil pressure system
75
while still allowing oil to flow into the reservoir
20
in order to refill it. Alternatively, with this embodiment, the stopper float
50
, rather than directly blocking the air flow corridor
40
or oil flow corridor
30
, may trigger the sealing off of the respective corridors
30
and
40
such as by contacting a switch or moving a stopper element into place. Furthermore, in another embodiment, as illustrated in
FIG. 6
, an alternative means to guide the stopper float into flow sealing orientation at either the oil flow corridor
30
or the air flow corridor
40
are included. In this embodiment, a locating guide
51
is suspended by brackets
49
within the reservoir
20
such that the stopper float
50
is contained and constrained within the locating guide
51
but will move freely up and down the locating guide
50
as the oil level rises and falls in the reservoir
20
. The locating guide is suspended in reservoir
20
such that neither the top nor the bottom of the guide contacts the reservoir, thereby allowing air as well as oil to flow freely in or out of the guide
51
and ensuring that the oil level within the locating guide
51
remains equal to the oil level in the rest of the reservoir
20
. Accordingly, much like the tapered upper and lower portions of the reservoir, as the oil level rises or falls, the stopper float is guided into flow sealing orientation at the air flow corridor
40
or the oil flow corridor
30
by the locating guide
51
.
A second embodiment of the level maintenance assembly, as shown in
FIG. 3
, includes a pair of float valves
52
and
53
. Specifically, each of the float valves
52
and
53
includes an individual float member
54
and
55
interconnected with a sealing mechanism which will seal off the respective valves
52
and
53
allowing no outflow therethrough. In the case of the first float valve
53
, it will be disposed at the air flow corridor
40
such that upon the oil level within the reservoir
20
rising to the reservoir full orientation, the float
55
will rise up switching the float valve
53
into an exit flow stopping orientation. Similarly, the float
54
of the second float valve
52
, will be suspended within the oil B unless the oil level drops below the float
54
to a reservoir empty level resulting in downward movement of the float
54
. Upon downward movement of the float
54
, the second float valve
52
is switched into an exit flow stopping orientation wherein no oil or air exits through the oil flow corridor
30
, but oil can still flow into the reservoir
20
via the oil flow corridor
30
to refill the reservoir
20
.
Turning to a third embodiment, illustrated in
FIG. 4
, the level maintenance assembly will merely include a mount bracket
56
structured to mount the reservoir
20
at an elevation such that the top of the reservoir
20
is at or slightly above the level of the oil in crank case
70
since gravity will not fill the reservoir higher than the level of the oil B in the crank case
70
. Although the single oil conduit
35
configuration of the previous embodiments may be employed, in this embodiment, the oil conduit
35
will merely include the one-way check valve
32
such that oil may only flow through the oil conduit
35
from the reservoir
20
to the internal engine oil pressure system
75
. Accordingly, an additional supply conduit
36
is included to supply oil to the oil reservoir
20
. The supply conduit
36
will also include a one-way check valve
37
which is disposed such that oil may flow from the crankcase
70
into the oil reservoir
20
therethrough, but no oil or air to flow will be permitted from the reservoir
20
to the crankcase
70
. In this embodiment, because the elevation of the reservoir
20
will generally be below the elevation of the crank case
70
, normal gravitational forces will maintain an oil level within the reservoir
20
equal with the oil level within the crankcase
70
.
As illustrated in
FIG. 5
, some engine oil systems include separate oil reserves
71
and do not merely utilize the crankcase
70
. In this case, a conduit
73
conducts oil from the reserve
71
to the internal engine oil system
75
and a separate conduit
72
returns the engine oil to the reserve
71
by forces of gravity or by a “scavenger” pump within the engine depending on whether the reserve
71
is disposed below or above the crankcase
70
, respectively. As such, connections previously described as being made with the crankcase
70
itself will be made with the separate reserve
71
.
Referring again to
FIG. 4
, when oil exits the reservoir
20
during pre-starting lubrication and the oil level has been lowered below that of the oil in the crankcase
70
, the forces of gravity will result in a quantity of oil exiting the crankcase
70
and entering reservoir
20
. Through air conduit
43
, the air supply in reservoir
20
is in continuous fluid communication with the air supply in crankcase
70
. Therefore, when air supply means
45
is not engaged, air pressure between reservoir
20
and crankcase
70
will remain at equilibrium. Because of this, the forces of gravity will cause oil to flow from the crankcase
70
into the reservoir
20
until equilibrium between the oil levels is reached. Regarding the mount bracket
56
, any manner of mounting, connection or placement of reservoir
20
in order to provide for the proper elevation of the reservoir is adaptable. Specifically, if the oil reservoir will preferably not be mounted within the overall engine housing, but rather it may be merely secured on a platform or other support so as to maintain proper elevation between the reservoir
20
and the crankcase
70
.
Also, in this embodiment, to prevent total emptying of the reservoir
20
and possible introduction of air into the oil system
75
, the lower portion of the reservoir
20
can be provided with tapered sides and a stopper float
50
as shown in FIG.
1
. Alternatively the reservoir
20
could be provided with the locating guide
51
and stopper float
50
as shown in
FIG. 5
, or the float valve as shown in FIG.
3
. All three of these aforesaid alternatives would function in exactly the same manner as previously described.
As an alternative, in
FIGS. 1
,
3
,
4
and
6
, a filler cap/plug
47
has been provided to fill the reservoir manually for initial installation and start up of the pre-starting lubrication system and/or when the engine oil B is to be routinely changed and both the crankcase
70
and the reservoir
20
have been drained of oil.
While this invention has been shown and described in what is considered to be a practical and preferred embodiment, it is recognized that departures may be made within the spirit and scope of this invention which should, therefore, not be limited except as set forth in the claims which follow and within the doctrine of equivalents.
Now that the invention has been described,
Claims
- 1. A pre-starting lubrication system to be used on an engine having an oil reserve, wherein engine lubricating oil is contained, and an engine internal oil pressure system structured to distribute lubricating oil to wearing parts of the engine from the oil reserve, said pre-starting lubrication system comprising;an oil reservoir structured to contain a quantity of engine oil therein; said oil reservoir including an air flow corridor wherethrough air enters and exits said oil reservoir, and an oil flow corridor, wherethrough oil enters and exits said oil reservoir; said oil flow corridor being connected in fluid flow communication with an oil riser, said oil riser being in fluid flow communication with the engine internal oil pressure system; a valve assembly structured to at least selectively close and thereby prevent said oil from exiting said oil riser; said valve assembly further structured to at least selectively allow air to enter said oil riser; said air flow corridor being connected in fluid flow communication with an air supply assembly by an air conduit, said air supply assembly being structured to selectively supply a quantity of air under pressure; an air control assembly structured to maintain bi-directional airflow into said oil reservoir, and restricted airflow out of said oil reservoir; and a conduit extension connected in fluid flow communication between said air conduit and said oil riser, said valve assembly being disposed on said conduit extension; and a level maintenance assembly structured to prevent overfilling or total emptying of said oil reservoir, and accordingly preventing the oil from exiting said reservoir through said air flow corridor and the air from exiting, said reservoir through said oil flow corridor.
- 2. A pre-starting lubrication system as recited in claim 1 wherein said level maintenance assembly includes a stopper float disposed in said reservoir so as to float on the oil contained therein, said stopper float being structured to seal off said air flow corridor upon an oil level in said reservoir rising to a reservoir full level, and to seal off said oil flow corridor upon said oil level in said reservoir dropping to a reservoir empty level.
- 3. A pre-starting lubrication system as recited in claim 2 wherein said reservoir further includes a tapered upper surface which tapers inwardly to said air flow corridor so as to guide said stopper float into its flow sealing orientation over said air flow corridor.
- 4. A pre-starting lubrication system as recited in claim 2 wherein said reservoir includes a tapered lower surface which tapers inwardly to said oil flow corridor so as to guide said stopper float into its flow sealing orientation over said oil flow corridor.
- 5. A pre-starting lubrication system as recited in claim 1 wherein said level maintenance assembly includes a mount bracket structured to mount said reservoir at an elevation equal to an elevation of the oil reserve of the engine such that gravitational forces will maintain an oil level in said reservoir equal to an oil level in the oil reserve of the engine, said oil level in said reservoir being a reservoir full level in said reservoir.
- 6. A pre-starting lubrication system as recited in claim 1 wherein said oil conduit includes a one way check valve structured and disposed to prevent oil from flowing therethrough from the engine internal oil pressure system to said reservoir.
- 7. pre-starting lubrication system as recited in claim 1 wherein said oil riser terminates at a point equal to the top of said oil reservoir.
- 8. A pre-starting lubrication system as recited in claim 7 wherein said oil riser is secured to said oil reservoir.
- 9. A pre-starting lubrication system as recited in claim 1 wherein said valve assembly remains closed during the pre-lubrication process.
- 10. A pre-starting lubrication system as recited in claim 9 wherein said valve assembly remains open during engine shutdown.
- 11. A pre-starting lubrication system as recited in claim 1 wherein said air control assembly includes a restrictive air flow orifice.
- 12. A pre-starting lubrication system as recited in claim 11 wherein said air control assembly ensures a majority of air flow into said oil reservoir.
US Referenced Citations (7)