US2494124A - Alarm initiator for pumping systems - Google Patents

Alarm initiator for pumping systems Download PDF

Info

Publication number
US2494124A
US2494124A US700341A US70034146A US2494124A US 2494124 A US2494124 A US 2494124A US 700341 A US700341 A US 700341A US 70034146 A US70034146 A US 70034146A US 2494124 A US2494124 A US 2494124A
Authority
US
United States
Prior art keywords
valve
flow
switch
pipe
piston
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US700341A
Inventor
Hegy Louis
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Bendix Aviation Corp filed Critical Bendix Aviation Corp
Priority to US700341A priority Critical patent/US2494124A/en
Application granted granted Critical
Publication of US2494124A publication Critical patent/US2494124A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G08SIGNALLING
    • G08BSIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
    • G08B21/00Alarms responsive to a single specified undesired or abnormal condition and not otherwise provided for
    • G08B21/18Status alarms
    • G08B21/182Level alarms, e.g. alarms responsive to variables exceeding a threshold
    • 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
    • Y10T137/7722Line condition change responsive valves
    • Y10T137/7837Direct response valves [i.e., check valve type]
    • Y10T137/7898Pivoted valves

Definitions

  • This invention relates to systems for automatically indicating an abnormal condition in a pumping system involving a reciprocating pump, and is particularly adapted for use in systems of this type in which the pump is driven by an internal combustion engine, although it is not limited thereto.
  • An object of the invention is to provide an alarm initiator that will produce an alarm in response to a reduction in the average flow of the pumped liquid after the reduction has continued for an appreciable interval of time, but will not produce false alarms in response to momentary interruptions of flow.
  • the present invention utilizes a switch-actuating element that is movable through a path of substantial length in either direction and which actuates a switch to produce an alarm when it reaches one end of its path.
  • This movable element is periodically urged in direction away from the switch in response to the flow of pumped liquid, but is urged toward the switch in response to lack of fiow of pumped liquid. So long as the average flow approximates a predetermined value, the element will be urged away from the switch to an. equal or greater extent than it is moved toward the switch, so that no alarm will be given. Furthermore, reduction in the flow of liquid for a short period will not produce an alarm, because the element must travel a substantial distance before it reaches the switch. However if the average flow of pumped liquid falls below the predetermined value for a substantial period of time, the element will gradually move toward and finally contact the switch. thereby initiating an alarm.
  • a piston element constituted by the end wall of an expansible and contractable bellows which is connected to the intake manifold of an internal combustion engine that drives the pump.
  • a valve mechanism is provided for connecting the bellows to the engine manifold during flow of pumped liquid and for disconnecting the bellows from the manifold and connecting it to the atmosphere during intervals when there is no liquid being pumped.
  • the invention is disclosed in connection with an oil well pump for actuating a switch it and pipe 26.
  • a well casing 36 a lower portion (deep in the well) which comprises a pump cylinder containing a piston 31 which is reciprocated by a sucker rod 34 extending to the top of the well.
  • the piston 31 is shown provided with a valve 38.
  • a barrier containing an inlet valve 39 Immediately below the piston there is provided a barrier containing an outlet valve 40.
  • valve 24 is normally in closed position but is swung open each time the oil surges through the pipe 26 in response to movement of the pump piston 31.
  • This valve is caused to control the movement of a reciprocal element It so that normally this element is maintained clear of a controlled means shown as a switch H, but if the flow of oil diminishes substantially for a substantial interval of time, the reciprocal element It is permitted to move downwardly to actuate the switch, thereby initiating an alarm.
  • valve 24 has secured thereto an arm 23 which is connected by a link 22 to one end of a lever 2!.
  • is connected to a rod 20 of a slide valve l2a.
  • the slide valve l2a When the flap valve 24 is in closed position, as shown in full line, the slide valve l2a is in a lower position in which it connects a vent 12d through a passage l2c in the slide valve l2a to a valve 28 which in turn is connected by a pipe 21 and a pipe H to a bellows I5.
  • This bellows [5 has an extensible side wall I51) and a closed bottom wall I50 constituting a piston element which supports the reciprocal element IS. The upper end of the bellows is anchored, as indicated.
  • the flap valve 24 is opened into the dotted line position, in which it moves the valve slide Ha upwardly to move the passage l2c therein out of registration with the atmospheric vent lid and move another passage l2b therein into registration with a pipe H, which is connected through a valve l3 to the pipe H.
  • the pipe II is connected to the intake manifold 10 of an internal combustion engine 30 which is used to reciprocate the sucker rod 34 of the pump.
  • the engine 30 is shown connected by a belt to a pulley 3
  • the flap valve 24 is in the open or dotted line position a suflicient portion of the time to cause the reciprocal element It to be moved upwardly as much or more than it is moved downwardly during the intervals when the valve 24 is closed.
  • the switch I I will not be actuated.
  • the flow of oil can be materially reduced for a short time without actuating the switch ll because of the distance that the reciprocal element i6 must travel before it reaches the switch. Then when the normal flow of oil is restored the reciprocal element It is gradually moved back up to a position near the upper limit of its travel.
  • the source of vacuum be the intake manifold of an internal combustion engine.
  • the pressure in the manifold will rise and actuate the switch l'l even though the oil flow is normal.
  • Apparatus of the type described comprising in combination: a flow pipe; flow responsive means responsive to fluid in said pipe to move into a first position during fluid flow and into a second position during no fluid flow; a reciprocal element reciprocal between spaced apart first and second positions; controlled means responsive to movement of said reciprocal element into said second position; and means controlled by said fiow responsive means for moving said reciprocal element toward its second position at a controlled rate while said flow responsive means is in its second position and moving said reciprocal element toward its first position at a controlled rate while said flow responsive mea is in its first position.
  • said means for moving said reciprocal element comprises a piston element movable in one direction in response to application of a reduced pressure thereto and movable in the opposite direction in response to application of a higher pressure thereto; a source of fluid at said reduced pressure; a source of fluid at said higher pressure; and means for connecting one of said sources to said piston element in one position of said flow responsive means and connecting said other source to said piston element in said other position of said flow responsive means.
  • said means for moving said reciprocal member comprises a piston element movable in one direction in response to application of a reduced pressure thereto and movable in the opposite direction in response to application of a higher pressure thereto; a source of fiuid at said reduced pressure; a source of fluid at said higher pressure; means for connecting one of said sources to said piston element in one position of said flow responsive means and connecting said other source to said piston element in said other position of said flow responsive means; and means for relatively adjusting the resistance to flow of fluid from said two sources to said piston element.
  • a pumping system comprising a pump actuated by an internal combustion engine having an intake manifold, apparatus responsive to a decrease in the discharge from said pump, said apparatus comprising: flow responsive means responsive to fluid discharge from said pump to move into a first position during fluid discharge and into a second position during intervals between fluid discharge; a piston element movable between first and second positions; controlled means responsive to movement of said piston element into said second position; means including a valve actuated by said fiow responsive means for connecting said piston element to said intake manifold while said flow responsive means is in its first position; and means for connecting said piston element to the atmosphere in response to movement of said flow responsive means into its second position.

Description

Jan. 10, 1950 L. HEGY 2,494,124
ALARM INITIATOR FOR PUMPING SYSTEMS Filed Sept. 30, 1946 INVENTORA LOUIS HEGY ATTORNEY Patented Jan. 10, 1950 ALARM INITIATOR FOR PUMPING SYSTEMS Louis Hegy, Glendale, Calii'., assignor to Bendix Aviation Corporation, South Bend, Ind., a corporation of Delaware Application September 30, 1946, Serial No. 700,341
4 claims. (01. 177-311) This invention relates to systems for automatically indicating an abnormal condition in a pumping system involving a reciprocating pump, and is particularly adapted for use in systems of this type in which the pump is driven by an internal combustion engine, although it is not limited thereto.
An object of the invention is to provide an alarm initiator that will produce an alarm in response to a reduction in the average flow of the pumped liquid after the reduction has continued for an appreciable interval of time, but will not produce false alarms in response to momentary interruptions of flow.
Other more specific objects and features of the invention will become apparent from the detailed description to follow.
The present invention utilizes a switch-actuating element that is movable through a path of substantial length in either direction and which actuates a switch to produce an alarm when it reaches one end of its path. This movable element is periodically urged in direction away from the switch in response to the flow of pumped liquid, but is urged toward the switch in response to lack of fiow of pumped liquid. So long as the average flow approximates a predetermined value, the element will be urged away from the switch to an. equal or greater extent than it is moved toward the switch, so that no alarm will be given. Furthermore, reduction in the flow of liquid for a short period will not produce an alarm, because the element must travel a substantial distance before it reaches the switch. However if the average flow of pumped liquid falls below the predetermined value for a substantial period of time, the element will gradually move toward and finally contact the switch. thereby initiating an alarm.
Various methods can be employed to move the switch-actuating element in each direction. In accordance with the present invention it is urged away from the switch by a piston element constituted by the end wall of an expansible and contractable bellows which is connected to the intake manifold of an internal combustion engine that drives the pump. A valve mechanism is provided for connecting the bellows to the engine manifold during flow of pumped liquid and for disconnecting the bellows from the manifold and connecting it to the atmosphere during intervals when there is no liquid being pumped.
A thorough understanding of the invention may be had from the following detailed description when read in conjunction with the drawing, the single figure of which discloses schematically one embodiment of the invention.
The invention is disclosed in connection with an oil well pump for actuating a switch it and pipe 26.
2 when the delivery of pumped oil falls below a predetermined average value.
Referring to the drawing: There is shown a well casing 36, a lower portion (deep in the well) which comprises a pump cylinder containing a piston 31 which is reciprocated by a sucker rod 34 extending to the top of the well. The piston 31 is shown provided with a valve 38. Immediately below the piston there is provided a barrier containing an inlet valve 39 and above the piston there is provided a barrier containing an outlet valve 40. It will be apparent from the structure disclosed that in response to reciprocation of the piston 31, liquid will be drawn in through the valve 39, then passed through the valve 38 in the piston and thereafter discharged through the valve 40 into the casing 36, where it is gradually raised to the surface and discharged through a As long as there is an ample supply of oil in the casing below the valve 39, a predetermined value of liquid will be discharged through the pipe 26 on each upward stroke of the piston 31. If the oil supply is insuflicient to satisfy the demand of the pump, or if the amount of gas increases, then the quantity of liquid discharged through the pipe 26 will decrease. Whenever oil is being pumped it will be discharged in surges through the pipe 26.
The surging of the oil is caused to actuate a flap valve 24 which is provided in the pipe 26. Valve 24 is normally in closed position but is swung open each time the oil surges through the pipe 26 in response to movement of the pump piston 31. This valve is caused to control the movement of a reciprocal element It so that normally this element is maintained clear of a controlled means shown as a switch H, but if the flow of oil diminishes substantially for a substantial interval of time, the reciprocal element It is permitted to move downwardly to actuate the switch, thereby initiating an alarm.
Thus the valve 24 has secured thereto an arm 23 which is connected by a link 22 to one end of a lever 2!. The other end of lever 2| is connected to a rod 20 of a slide valve l2a. When the flap valve 24 is in closed position, as shown in full line, the slide valve l2a is in a lower position in which it connects a vent 12d through a passage l2c in the slide valve l2a to a valve 28 which in turn is connected by a pipe 21 and a pipe H to a bellows I5.
This bellows [5 has an extensible side wall I51) and a closed bottom wall I50 constituting a piston element which supports the reciprocal element IS. The upper end of the bellows is anchored, as indicated.
It will be apparent that with the flap valve 24 closed as shown in full line, atmospheric air is admitted through the valve 28 to the interior of the bellows l5, and the bellows will be permitted to slowly expand and lower the reciprocal element It (by its own weight) toward the switch IT. The rate of downward movement of reciprocal element It under these conditions can be regulated by means of the valve 28.
Whenever an outward surge of oil occurs in the pipe 16 the flap valve 24 is opened into the dotted line position, in which it moves the valve slide Ha upwardly to move the passage l2c therein out of registration with the atmospheric vent lid and move another passage l2b therein into registration with a pipe H, which is connected through a valve l3 to the pipe H. The pipe II is connected to the intake manifold 10 of an internal combustion engine 30 which is used to reciprocate the sucker rod 34 of the pump. Thus the engine 30 is shown connected by a belt to a pulley 3| which is connected by a connecting rod 32 to one end of a walking beam 33, the other end of which is connected to the upper end of the sucker rod 34.
As long as the engine 30 is operating under normal conditions a low pressure or partial vacuum is maintained in the intake manifold l and the pipe ll. Therefore with the valve slide I2a in the upper position as last described, air is sucked from the interior of the bellows l5 through the pipe M, the valve [3, and the pipe H to the intake manifold l0.
Whenever the bellows I5 is connected to the pipe II, and the engine 30 is operating, air is drawn out of the bellows and the piston element I50 and the reciprocal element 16 are slowly raised.
During normal operation of the system, the flap valve 24 is in the open or dotted line position a suflicient portion of the time to cause the reciprocal element It to be moved upwardly as much or more than it is moved downwardly during the intervals when the valve 24 is closed. Hence the switch I I will not be actuated. Furthermore the flow of oil can be materially reduced for a short time without actuating the switch ll because of the distance that the reciprocal element i6 must travel before it reaches the switch. Then when the normal flow of oil is restored the reciprocal element It is gradually moved back up to a position near the upper limit of its travel.
However, if the flow of oil ceases entirely for a predetermined length of time, the reciprocal element it will be lowered into contact with the switch I! and will actuate it. Likewise, if the flow of oil is materially reduced, but not fully stopped, it will eventually permit the reciprocal element It to reach and actuate the switch II.
It is not essential that the source of vacuum be the intake manifold of an internal combustion engine. However it has the additional advantage that if the engine is greatly overloaded, the pressure in the manifold will rise and actuate the switch l'l even though the oil flow is normal.
For the purpose of explaining the invention one embodiment thereof has been disclosed in the drawing in highly schematic form and its operation described herein. However various changes and modifications can be made in the particular system shown and the invention is therefore to be limited only to the extent set forth in the appended claims.
I claim:
1. Apparatus of the type described comprising in combination: a flow pipe; flow responsive means responsive to fluid in said pipe to move into a first position during fluid flow and into a second position during no fluid flow; a reciprocal element reciprocal between spaced apart first and second positions; controlled means responsive to movement of said reciprocal element into said second position; and means controlled by said fiow responsive means for moving said reciprocal element toward its second position at a controlled rate while said flow responsive means is in its second position and moving said reciprocal element toward its first position at a controlled rate while said flow responsive mea is in its first position. i
2. Apparatus as described in claim 1 in which said means for moving said reciprocal element comprises a piston element movable in one direction in response to application of a reduced pressure thereto and movable in the opposite direction in response to application of a higher pressure thereto; a source of fluid at said reduced pressure; a source of fluid at said higher pressure; and means for connecting one of said sources to said piston element in one position of said flow responsive means and connecting said other source to said piston element in said other position of said flow responsive means.
3. Apparatus as described in claim 1 in which said means for moving said reciprocal member comprises a piston element movable in one direction in response to application of a reduced pressure thereto and movable in the opposite direction in response to application of a higher pressure thereto; a source of fiuid at said reduced pressure; a source of fluid at said higher pressure; means for connecting one of said sources to said piston element in one position of said flow responsive means and connecting said other source to said piston element in said other position of said flow responsive means; and means for relatively adjusting the resistance to flow of fluid from said two sources to said piston element.
4. In a pumping system comprising a pump actuated by an internal combustion engine having an intake manifold, apparatus responsive to a decrease in the discharge from said pump, said apparatus comprising: flow responsive means responsive to fluid discharge from said pump to move into a first position during fluid discharge and into a second position during intervals between fluid discharge; a piston element movable between first and second positions; controlled means responsive to movement of said piston element into said second position; means including a valve actuated by said fiow responsive means for connecting said piston element to said intake manifold while said flow responsive means is in its first position; and means for connecting said piston element to the atmosphere in response to movement of said flow responsive means into its second position.
LOUIS HEGY.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,967,018 Bohner July 17, 1934 1 2,347,830 Kiburz et al. May 2, 1944 2,421,768 Voliazzo et a1. June 10, I947
US700341A 1946-09-30 1946-09-30 Alarm initiator for pumping systems Expired - Lifetime US2494124A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US700341A US2494124A (en) 1946-09-30 1946-09-30 Alarm initiator for pumping systems

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US700341A US2494124A (en) 1946-09-30 1946-09-30 Alarm initiator for pumping systems

Publications (1)

Publication Number Publication Date
US2494124A true US2494124A (en) 1950-01-10

Family

ID=24813134

Family Applications (1)

Application Number Title Priority Date Filing Date
US700341A Expired - Lifetime US2494124A (en) 1946-09-30 1946-09-30 Alarm initiator for pumping systems

Country Status (1)

Country Link
US (1) US2494124A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2654879A (en) * 1950-04-17 1953-10-06 Combustion Eng Flow stoppage detector for fuel supply lines
US2697984A (en) * 1949-12-08 1954-12-28 Phillips Petroleum Co Well control device
US2698929A (en) * 1952-01-25 1955-01-04 Combustion Eng Flow stoppage indicator for mill fuel supply
US2844029A (en) * 1954-11-03 1958-07-22 Jesse D Leonard Apparatus for producing stripper wells
US2853575A (en) * 1955-05-09 1958-09-23 Phillips Petroleum Co Flow-responsive device
US2953659A (en) * 1955-05-16 1960-09-20 Phillips Petroleum Co Shut-down device
US3039811A (en) * 1958-11-20 1962-06-19 Atomic Energy Authority Uk Lifting devices
US3050003A (en) * 1960-10-21 1962-08-21 Jack L Edwards Pump alarm and control device
US4885984A (en) * 1988-09-19 1989-12-12 Franceus Paul E Radon removal apparatus

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1967018A (en) * 1931-12-02 1934-07-17 Wired Radio Inc Fluid flow indicator
US2347830A (en) * 1942-01-10 1944-05-02 John Kiburz Pattern Company Flow indicator
US2421768A (en) * 1945-06-29 1947-06-10 Voliazzo Jesse Fuel flow warning device

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1967018A (en) * 1931-12-02 1934-07-17 Wired Radio Inc Fluid flow indicator
US2347830A (en) * 1942-01-10 1944-05-02 John Kiburz Pattern Company Flow indicator
US2421768A (en) * 1945-06-29 1947-06-10 Voliazzo Jesse Fuel flow warning device

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2697984A (en) * 1949-12-08 1954-12-28 Phillips Petroleum Co Well control device
US2654879A (en) * 1950-04-17 1953-10-06 Combustion Eng Flow stoppage detector for fuel supply lines
US2698929A (en) * 1952-01-25 1955-01-04 Combustion Eng Flow stoppage indicator for mill fuel supply
US2844029A (en) * 1954-11-03 1958-07-22 Jesse D Leonard Apparatus for producing stripper wells
US2853575A (en) * 1955-05-09 1958-09-23 Phillips Petroleum Co Flow-responsive device
US2953659A (en) * 1955-05-16 1960-09-20 Phillips Petroleum Co Shut-down device
US3039811A (en) * 1958-11-20 1962-06-19 Atomic Energy Authority Uk Lifting devices
US3050003A (en) * 1960-10-21 1962-08-21 Jack L Edwards Pump alarm and control device
US4885984A (en) * 1988-09-19 1989-12-12 Franceus Paul E Radon removal apparatus

Similar Documents

Publication Publication Date Title
US3559731A (en) Pump-off controller
US3327635A (en) Pumps
US1635524A (en) Method of and means for cooling compressors
US3851995A (en) Pump-off control apparatus for a pump jack
US2494124A (en) Alarm initiator for pumping systems
US2635546A (en) Pump control
US3212406A (en) Pumping systems
US3918843A (en) Oil well pumpoff control system utilizing integration timer
US2953659A (en) Shut-down device
US2286613A (en) Liquid supply system
US3105443A (en) Automatic shut-off device for pumping wells
US2853575A (en) Flow-responsive device
US3434430A (en) Self-priming pump system with external actuating means
US2405734A (en) Pumping apparatus
US2426369A (en) Sampler
US1980374A (en) Valve
US3251534A (en) Compressor control system
US2732804A (en) Automatic pressure liquid supply system
US2564528A (en) Monitor for pumping systems
US2254539A (en) Fluid pump
US2851957A (en) Diaphragm pump
US2348282A (en) Fuel injection apparatus
US3276380A (en) Oil well shut-down device
US2420409A (en) Multiple pressure pump
US2301916A (en) Fuel pump