US3384103A - Airline lubricator - Google Patents

Airline lubricator Download PDF

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US3384103A
US3384103A US531476A US53147666A US3384103A US 3384103 A US3384103 A US 3384103A US 531476 A US531476 A US 531476A US 53147666 A US53147666 A US 53147666A US 3384103 A US3384103 A US 3384103A
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passage
flow
fluid
feed tube
outlet
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US531476A
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Zdenek J Lansky
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Parker Hannifin Corp
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Parker Hannifin Corp
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16NLUBRICATING
    • F16N7/00Arrangements for supplying oil or unspecified lubricant from a stationary reservoir or the equivalent in or on the machine or member to be lubricated
    • F16N7/30Arrangements for supplying oil or unspecified lubricant from a stationary reservoir or the equivalent in or on the machine or member to be lubricated the oil being fed or carried along by another fluid
    • F16N7/32Mist lubrication
    • F16N7/34Atomising devices for oil
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/2931Diverse fluid containing pressure systems
    • Y10T137/3112Main line flow displaces additive from shunt reservoir
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/8158With indicator, register, recorder, alarm or inspection means
    • Y10T137/8326Fluid pressure responsive indicator, recorder or alarm

Description

May 21, 1968 z. J. LANSKY 3,384,103
AIRLINE LUBRICATOR Filed March 5, 1966 l0 f H I my Jf' INVENTOR ZDENEK J. LANS/(Y mam/mmm ATroRNEYs United States Patent O 3,384,103 AIRLINE LUBRICATOR Zdenek J. Lansky, Winnetka, lll., assignor to Parker- Hannifin Corporation, Cleveland, Ohio, a corporation of Ohio Filed Mar. 3, 1966, Ser. No. 531,476 10 Claims. (Cl. 137-2055) The present invention relates to devices for mixing two fluids by metering one into the other and has application, for example, to a lubricator for pneumatic systems in which air under pressure for operating a pneumatic unit passes through a lubricator housing and pressurizes a supply of lubricant therein to force the same into the air stream in finely divided form.
An object of the invention is to provide a visual indication of ow of the metered fiuid and to provide for instantaneous feed of such fluid when pressurization of the same is low or intermittent.
It is another object to provide a device of the character indicated in which a visual flow indicator indicates an average metered flow when the actual flow varies due to pressure fluctuations.
It is another object of the invention to provide a device of the type described in which a flow indicator is located exteriorly of the device for visual observation but has connections to the interior of the device for conducting the metered fluid from a reservoir to the point of mixture with the other fluid.
It is another object to provide a device of a type described in which there is a visual liow indicator for the metered fluid with means associated with the iiow indicator for varying the rate at which it responds to the metered fiow.
Other objects and advantages of the present invention will become apparent as the following description proceeds.
To the accomplishment of the foregoing and related ends, the invention, then, comprises the features hereinafter fully described and particularly pointed out in the claims, the following description and the annexed drawing setting forth in detail certain illustrative embodiments of the invention, these being indicative, however, of a few of the various ways in which the principle of the invention may be employed.
In said annexed drawing:
FIG. 1 is a central vertical cross-section view of one embodiment of this invention;
FIG. 2 is a fragmentary cross-section view of a modified form of oil ow indicator to extend the range of oil ow rates indicated thereby;
FIG. 3 is a cross-section view of modified form of air line lubricator embodying the present invention; and
FIG. 4 is a view showing the flow indicator located exteriorly of the device.
Referring now more particularly to the drawing, and first to FIG. 1, the lubricator 1 there shown comprises a housing 2 having a reservoir for oil in the form of a transparent bowl 3 detachably secured to the housing as by means of the clamp ring 4. The housing 2 has an inlet port 5 for connection with an air pressure source and an outlet port 6 for connection with a pneum-atically operated unit, the main air ilow being through a venturi passage 7. The throat of the venturi passage 7 is intersected by a passage 8 through which a rotary valve element 9 extends, said valve element 9 having a stem portion 10 at its upper end which is serrated and which cooperates with a spring detent member 11 which yieldably holds the valve element 9 at any desired rotatively adjusted position. The portion 12 of the valve element 9 that extends across the venturi throat is in the form of a narrow diametrically extending blade which, as apparent, increases or decreases the fiow of air through the venturi passage 7 when the valve element 9 is rotatively adjusted in one direction or the other. The lower tubular end 14 of the valve element 9 has an inner bore 15 which intersects the blade portion 12 of the valve member and opens into the venturi passage 7 for mixing of oil from the bowl 3 with airstream flowing through the venturi passage 7.
Snugly fitted in the lower tubular end 14 of the valve element 9 is a feed control element 13 of porous material which not only meters the oil through the multiple openings thereof, but additionally, breaks up the oil into tiny droplets for uniform dispersal in the airstream, thus providing improved lubricating effectiveness at the pneumatically operated unit.
The housing 2 has a cap 16 removably secured thereto for periodic refilling of the bowl 3 with oil and as the cap 16 is being removed, the bowl is vented through passage 17 and a tire valve 18 engaged with the cap is permitted to be closed to maintain air pressure in the passage 7. When the cap 16 is replaced, the tire valve 18 is opened thereby and air pressure enters through the tire valve 18 and the passage 17 in the housing 2 to pressurize the oil in the bowl 3 for feeding it under pressure through the transparent feed tube 19 which is secured as by means of the rubber like O-ring 20 to the lower end 14 of the valve element 9 and extends downwardly close to the botto-m of the bowl 3.
In the lubricator 1 shown in FIG. l, the upper end of the feed tube 19 constitutes a seat for a spring biased check valve 21 which keeps the -feed tube 19 filled with oil even though the level of the oil in the -bowl 3 is below said check valve 21. Said check valve 21 also prevents pressurizing of the oil in the bowl 3 when the cap 16 is being removed.
The feed tube 19 has a check valve 22 therein which preferably comprises a lightweight ball of aluminum, for example, and the portion 23 of the bore above seat 24 is slightly tapered OA per foot, for example) so that when the lubricator 1 is in use the ball check 22 will rise in the feed tube in accordance with the rate of flow of oil upwardly through the feed tube 19. Thus, with a transparent bowl 3 and transparent feed tube 19 it is possible for the operator to visually inspect the operation of the lubricator 1 and to determine the rate of fiow of oil into the main airstream. There are provided suitable iiow indicia 25 on the feed tube such as a series of grooves which are painted black or other color so as to be clearly visible.
In View of the pressure drops across the fiow ball 22, the check ball 21, and the porous element 13, the liow ball 22 will move slowly up or down to indicate the average iiow rate of oil through the feed tube 19 and will not be subject to rapid movements as occasioned by pressure shocks, pulses or surges in the pneumatic circuit. When the pneumatically operated unit reaches the end of its stroke or its actuation is discontinued, the equalization of pressure at the venturi throat and in the bowl 3 will maintain the porous element 1S and the entire feed tube 19 filled with oil because of the seating of the check ball 21 and also of the flow ball 22.
FIG. 2 illustrates a modification in which the feed tube 30 has a flow passage 31 calibrated for high and low rates of flow. In other words, the fiow passage 31 has portions 32 and 34 of different taper and when the liow ball 3S is moved by low rates of flow it will be disposed in the portion 32 of smaller taper and each increment of movement will represent a smaller change in flow rate than when the flow ball 35 is within the portion 34 of greater taper in which case, a larger change in flow rate will be indicated by a smaller increment of movement to the flow ball 35. It is to be understood that instead of two distinct tapers 32 and 34, as shown in FIG. 2, the fiow passage 31 may be of continuously varying taper to cover a wide range of fiow rates along a relatively short length of the feed tube 30. Furthermore, if greater sensitivity is desired at the higher rates of flow than at the lower rates of flow the taper 32 may be steeper than taper 34.
As aforesaid, the flow balls 22 and 35 in FIGS. l and 2 are preferably of lightweight metal such as aluminum, and are heavier than the oil displaced thereby. As apparent, the ow rates of the lubricators shown in FIGS. l and 2 may readily be increased or decreased by substituting heavier or lighter flow balls 22 and 35. Also, the flow rates denoted by the indicia 2S may further be varied by substituting flow balls 22 and 35 of larger or smaller diameter, thus to change the radial clearances between the fiow passages and the fiow balls.
Referring now to FIG. 3, the lubricator there shown has an inverted feed tube 41 in which is disposed a flow ball 42 which is hollow and/or made of lightweight material such as plastic such that the weight thereof is less than that of the displaced lubricant. In this case, the center feed tube 41 is of transparent material and has a tapered bore 43 which is larger at its lower end than at its upper end, whereby as lubricant flows downwardly therethrough, the flow ball 42 will be forced downwardly a distance corresponding to the rate of flow of lubricant. The maximum oil level is indicated by the line 45 and therefore the flow ball 42 in FIG. 3 will be readily visible through the transparent bowl 46 and the transparent center feed tube 41. At any rate, at relatively low rates of flow of lubricant, the flow ball 42 will be disposed at a position above the maximum oil level so that it will be more readily visible than at greater rates of flow when it may be disposed below the lubricant level. When the fiow ball 42 is of effective specific gravity only slightly less than that of the lubricant and when the feed tube 41 has a long bore 43 of very slight taper, the flow characteristics are very sensitive that is, a small change in flow rate will be reflected by a relatively large change in the position of the ball 42 in said feed tube 41. Suitable ball stops 46 and 47 are provided at the upper and lower ends of said feed tube 41.
The inlet and outlet feed tubes 48 and 49 may be made of metal and at the upper end of the inlet feed tube there may be provided a lubricant fiow control valve 50 comprising, as shown a cylindrical rod 51 having a relatively close sliding fit in the bore of the body 52 and preferably formed with a plurality of metering slots 53 through which the lubricant must flow at a rate depending on the axial position of the slotted end of the rod 51 with respect to the bore 54 which intersects the bore in said body.
The outlet feed tube 49 has at its upper end a suitable check valve 56 which prevents back fiow of lubricant and thus maintains the lubricator feed tube 49, 41, and 48 filled with lubricant so that the next time there is air fiow through the lubricator, lubricant will at once be introduced into the airstream at a rate indicated by the position of the flow ball 42. The flow control valve rod 51 may be turned in either direction to increase or decrease such flow rate.
In the form of the invention as shown in FIG. 4, feed tube 19', corresponding to feed tube 19 of FIG. 1, passes through the side wall of reservoir 3 to the exterior thereof. In this case reservoir 3 need not be transparent. The portion of the feed tube in which flow indicator ball 22 is transparent and is opposite an opening 60 in a panel board through which the flow ball may be observed.
Other modes of applying the principle of the invention may be employed, change being made as regards the details described, provided the features stated in any of the following claims, or the equivalent of such, be employed.
I therefore particularly point out and distinctly claim as my invention:
1. In a device for mixing two fiuids, a housing having a first passage therethrough for flow of a first fluid under pressure, means for establishing a lower pressure of said fiuid in the outlet end of the first passage than in the inlet end, a reservoir containing a second fluid, said housing having a second passage for conducting fluid from the first passage inlet to said reservoir for pressurizing the second fluid, a feed tube having an inlet end immersed in the second fluid and an outlet end connected to the first passage outlet whereby the greater pressure in the first passage inlet forces the second fluid from the reservoir through the feed tube to said first passage outlet, said tube having a visible transparent portion, a fiow element in said transparent portion movable by the fiuid flowing through said feed tube to different positions therein according to the rate of flow through said feed tube, and a check valve adjacent the outlet end of the tube that opens under force of fluid fiowing through the tube toward the first passage outlet and that closes upon cessation of said flow through the tube to prevent draining of the second uid from the feed tube to the reservoir.
2. The device of claim 1 wherein said transparent tube portion has a tapered bore to provide changing radial clearance around said flow element as the latter is moved in said tube.
3. The device of claim 1 wherein said flow element is non-buoyant in the second fluid and is moved upwardly in said tube under the influence of increasing rate of flow of said second fluid therearound.
4. The device of claim 1 wherein said reservoir is transparent and contains the transparent portion of the feed tube and movement of said flow element occurs above the level of the second fiuid in said reservoir to facilitate viewing of the same through said reservoir.
5. In a device for mixing fluids, a housing having a first passage therethrough for flow of a first fluid under pressure, means for establishing a lower pressure of said fluid in the outlet end of said passage than in the inlet end, a reservoir containing a second uid, passage means connecting said first passage inlet end with said reservoir to pressurize the fluid therein, a feed tube having an inlet immersed in said second fiuid and having an outlet connected to said first passage outlet whereby the greater pressure in the first passage inlet forces the second fluid through the feed tube to said first passage outlet, said tube having a visible transparent portion containing a flow element movable by fluid flowing through the tube to different positions according to the rate of the flow through the feed tube, said transparent portion having bore sections of different tapers to provide different rates of change of radial clearance around said flow element as the latter is moved.
6. The device of claim 5 in which the downstream bore section has a taper greater than the taper of an upstream bore section whereby the rate of change of radial clearance around said flow element is greater than that in the upstream section.
7. In a device for mixing fluids, a housing having a first passage therethrough for flow of a first uid under pressure, means for establishing a lower pressure of said fluid in the outlet end of said passage than in the inlet end, a reservoir containing a second fiuid, passage means connecting said first passage inlet end with said reservoir to pressurize the fluid therein, a feed tube having an inlet immersed in said second fluid and having an outlet connected to said first passage outlet whereby the greater pressure in the first passage inlet forces the second fluid through the feed tube to said first passage outlet, said tube having a visible transparent portion oriented so that fiuid fiowing through said portion travels in a downward direction, a buoyant fiow element in said transparent portion movable in a downward direction by fiuid flowing through the feed tube to .different positions according to the rate of such flow through the feed tube.
8. The device of claim 7 in which said feed tube comprises three separate but connected sections each connected to the housing and extending vertically into said reservoir.
9. In a device for mixing two uids, a housing having a first passage therethrough for flow of a iirst tiuid under pressure, means for establishing a lower pressure of said rst liuid in the outlet end of said passage than in the inlet end, a reservoir containing a second fluid, passage means connecting the first passage inlet to said reservoir to pressurize the iiuid therein, duct means having an inlet immersed in the second uid and `having an outlet connected to the first passage outlet whereby the greater pressure in the rst passage inlet forces the second uid through the tube to the i-rst passage outlet, said duet means having a transparent portion located exteriorly of said reservoir for visual observation, a flow element in said transparent portion movable by fluid iiowing through said duet means to different positions according to the rate of ow through said duct means.
10. The device of claim 9 in which said duct means passes through a wall of said reservoir to the exterior thereof.
References Cited UNITED STATES PATENTS 1,889,705 11/1930 Sherwood 73-209 2,778,223 1/1957 Kmbrell 137-557 X 2,835,267 5/1958 Andresen et al. 184-55 2,878,895 3/1959 Wiley 261-'78.1 X 3,342,068 9/1967 Metzger 73-209 LAVERNE D. GEIGER, Primary Examiner.
H. S. BELL, Assistant Examiner'.

Claims (1)

  1. 5. IN A DEVICE FOR MIXING FLUIDS, A HOUSING HAVING A FIRST PASSAGE THERETHROUGH FOR FLOW OF A FIRST FLUID UNDER PRESSURE, MEANS FOR ESTABLISHING A LOWER PRESSURE OF SAID FLUID IN THE OUTLET END OF SAID PASSAGE THAN IN THE INLET END, A RESERVOIR CONTAINING A SECOND FLUID, PASSAGE MEANS CONNECTING SAID FIRST PASSAGE INLET END WITH SAID RESERVOIR TO PRESSURIZE THE FLUID THEREIN, A FEED TUBE HAVING AN INLET IMMERSED IN SAID SECOND FLUID AND HAVING AN OUTLET CONNECTED TO SAID FIRST PASSAGE OUTLET WHEREBY THE GREATER PRESSURE IN THE FIRST PASSAGE INLET FORCES THE SECOND FLUID THROUGH THE FEED TUBE TO SAID FIRST PASSAGE OUTLET, SAID TUBE HAVING A VISIBLE TRANSPARENT PORTION CONTAINING A FLOW ELEMENT MOVABLE BY FLUID FLOWING THROUGH THE TUBE TO DIFFERENT POSITIONS ACCORDING TO THE RATE OF THE FLOW THROUGH THE FEED TUBE, SAID TRANSPARENT PORTION HAVING BORE SECTIONS OF DIFFERENT TAPERS TO PROVIDE DIFFERENT RATES OF CHANGE OF RADIAL CLEARANCE AROUND SAID FLOW ELEMENT AS THE LATTER IS MOVED. .
US531476A 1966-03-03 1966-03-03 Airline lubricator Expired - Lifetime US3384103A (en)

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3720290A (en) * 1971-01-05 1973-03-13 Parker Hannifin Corp Supersonic lubricator
US3913843A (en) * 1974-10-30 1975-10-21 Respiratory Care Humidifier
US4007876A (en) * 1972-12-15 1977-02-15 Stevenson James S Spray equipment and method
US4094384A (en) * 1975-10-22 1978-06-13 Firma Festo-Maschinenfabrik Gottlieb Stoll Bayonet connecting system for collector bowl attachment to connecting housing of compressed air conditioning device
US4101611A (en) * 1977-02-07 1978-07-18 Amark Industries, Inc. Nebulizer
US4298496A (en) * 1980-09-19 1981-11-03 The United States Of America As Represented By The United States Department Of Energy Highly stable aerosol generator
US4373421A (en) * 1979-09-17 1983-02-15 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (S.N.E.C.M.A.) Emergency aerosol lubrication device, particularly for airborne engines
US4913188A (en) * 1986-05-20 1990-04-03 Selk Kurt M Process and apparatus for supplying additives at controlled rates
US5095932A (en) * 1990-12-21 1992-03-17 Millipore Corporation Check valve for fluid delivery system
US5213129A (en) * 1991-03-25 1993-05-25 Csb Limited Partnership Fluid mixing device
US5816504A (en) * 1993-09-24 1998-10-06 Ing. Erich Pfeiffer Gmbh Discharge apparatus for flowable media
EP2065712A2 (en) * 2007-11-29 2009-06-03 Lincoln GmbH Flow monitoring unit
US20100116357A1 (en) * 2007-03-26 2010-05-13 Uldege Lebreux Liquid distributor in pressurized fluid system

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1889705A (en) * 1931-03-16 1932-11-29 Carroll P Sherwood Flow meter
US2778223A (en) * 1953-11-02 1957-01-22 Puritan Compressed Gas Corp Flowmeter
US2835267A (en) * 1953-12-31 1958-05-20 Gits Bros Mfg Co Air line lubricator
US2878895A (en) * 1957-04-12 1959-03-24 Master Pneumatic Inc Air line lubricator
US3342068A (en) * 1964-11-18 1967-09-19 Fischer & Porter Co Flowmeter

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1889705A (en) * 1931-03-16 1932-11-29 Carroll P Sherwood Flow meter
US2778223A (en) * 1953-11-02 1957-01-22 Puritan Compressed Gas Corp Flowmeter
US2835267A (en) * 1953-12-31 1958-05-20 Gits Bros Mfg Co Air line lubricator
US2878895A (en) * 1957-04-12 1959-03-24 Master Pneumatic Inc Air line lubricator
US3342068A (en) * 1964-11-18 1967-09-19 Fischer & Porter Co Flowmeter

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3720290A (en) * 1971-01-05 1973-03-13 Parker Hannifin Corp Supersonic lubricator
US4007876A (en) * 1972-12-15 1977-02-15 Stevenson James S Spray equipment and method
US3913843A (en) * 1974-10-30 1975-10-21 Respiratory Care Humidifier
US4094384A (en) * 1975-10-22 1978-06-13 Firma Festo-Maschinenfabrik Gottlieb Stoll Bayonet connecting system for collector bowl attachment to connecting housing of compressed air conditioning device
US4101611A (en) * 1977-02-07 1978-07-18 Amark Industries, Inc. Nebulizer
US4373421A (en) * 1979-09-17 1983-02-15 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (S.N.E.C.M.A.) Emergency aerosol lubrication device, particularly for airborne engines
US4298496A (en) * 1980-09-19 1981-11-03 The United States Of America As Represented By The United States Department Of Energy Highly stable aerosol generator
US4913188A (en) * 1986-05-20 1990-04-03 Selk Kurt M Process and apparatus for supplying additives at controlled rates
US5095932A (en) * 1990-12-21 1992-03-17 Millipore Corporation Check valve for fluid delivery system
US5213129A (en) * 1991-03-25 1993-05-25 Csb Limited Partnership Fluid mixing device
US5816504A (en) * 1993-09-24 1998-10-06 Ing. Erich Pfeiffer Gmbh Discharge apparatus for flowable media
US20100116357A1 (en) * 2007-03-26 2010-05-13 Uldege Lebreux Liquid distributor in pressurized fluid system
US8371327B2 (en) * 2007-03-26 2013-02-12 Productions Dr Liquid distributor in pressurized fluid system
EP2065712A2 (en) * 2007-11-29 2009-06-03 Lincoln GmbH Flow monitoring unit
EP2065712A3 (en) * 2007-11-29 2012-01-25 Lincoln GmbH Flow monitoring unit

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