Engine pre-lubrication system

Information

  • Patent Grant
  • 6481530
  • Patent Number
    6,481,530
  • Date Filed
    Monday, September 25, 2000
    24 years ago
  • Date Issued
    Tuesday, November 19, 2002
    22 years ago
  • Inventors
  • Examiners
    • Kim; Chong H.
    Agents
    • Malloy & Malloy, P.A.
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.
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Number Name Date Kind
4061204 Kautz, Jr. Dec 1977 A
4199950 Hakanson et al. Apr 1980 A
4453511 Pluequet Jun 1984 A
5014820 Evans May 1991 A
5197424 Blum Mar 1993 A
5348121 McLaughlin Sep 1994 A
5494013 Helbig Feb 1996 A