US2468768A - Means to indicate the presence of - Google Patents
Means to indicate the presence of Download PDFInfo
- Publication number
- US2468768A US2468768A US2468768DA US2468768A US 2468768 A US2468768 A US 2468768A US 2468768D A US2468768D A US 2468768DA US 2468768 A US2468768 A US 2468768A
- Authority
- US
- United States
- Prior art keywords
- vapor
- fluid
- pressure
- chamber
- chambers
- 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
Links
- 239000012530 fluid Substances 0.000 description 74
- 210000000188 Diaphragm Anatomy 0.000 description 44
- 239000007788 liquid Substances 0.000 description 44
- 230000000694 effects Effects 0.000 description 14
- 230000004048 modification Effects 0.000 description 14
- 238000006011 modification reaction Methods 0.000 description 14
- 230000015572 biosynthetic process Effects 0.000 description 12
- 238000005755 formation reaction Methods 0.000 description 12
- 239000000203 mixture Substances 0.000 description 12
- 238000005192 partition Methods 0.000 description 8
- 238000002485 combustion reaction Methods 0.000 description 6
- 238000001514 detection method Methods 0.000 description 4
- 239000000446 fuel Substances 0.000 description 4
- 238000009413 insulation Methods 0.000 description 4
- 230000001264 neutralization Effects 0.000 description 4
- 210000003141 Lower Extremity Anatomy 0.000 description 2
- 210000001364 Upper Extremity Anatomy 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000003247 decreasing Effects 0.000 description 2
- 239000011810 insulating material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000002265 prevention Effects 0.000 description 2
- 230000029058 respiratory gaseous exchange Effects 0.000 description 2
- 230000035945 sensitivity Effects 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 230000001052 transient Effects 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01H—ELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
- H01H35/00—Switches operated by change of a physical condition
- H01H35/24—Switches operated by change of fluid pressure, by fluid pressure waves, or by change of fluid flow
- H01H35/34—Switches operated by change of fluid pressure, by fluid pressure waves, or by change of fluid flow actuated by diaphragm
- H01H35/346—Switches operated by change of fluid pressure, by fluid pressure waves, or by change of fluid flow actuated by diaphragm in which the movable contact is formed or directly supported by the diaphragm
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L7/00—Measuring the steady or quasi-steady pressure of a fluid or a fluent solid material by mechanical or fluid pressure-sensitive elements
- G01L7/02—Measuring the steady or quasi-steady pressure of a fluid or a fluent solid material by mechanical or fluid pressure-sensitive elements in the form of elastically-deformable gauges
- G01L7/08—Measuring the steady or quasi-steady pressure of a fluid or a fluent solid material by mechanical or fluid pressure-sensitive elements in the form of elastically-deformable gauges of the flexible-diaphragm type
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S60/00—Power plants
- Y10S60/911—Fluid motor system incorporating electrical system
Definitions
- This invention relates to an improved method for detecting the existence of the formation of vapor in fluid conduit systems and an improved ,indicator for accomplishing the same.
- vapor shall be used generally hereinafter to indicate any compressible fluid such as gas, air, or any other substance having a density lower than that of the incompressible liquid in a fluid conduit system.
- common practice In an effort to provide, in the fluid conduitsystem, some means for prevention of failure of various parts of the system, due to these causes, which means would in turn reflect favorably upon the operation of the system, common practice ⁇ includes certain auxiliary, booster, or emergency pumps, or other known devices, which are intended to reduce or eliminate the formation of vapors. For a number of reasons, it is undesirable to operate these pumps or other devices continuously. Accordingly, the common practice is to operate or begin the operation of these devices manually, only after the presence of vapor in the system is detected by the operator, based upon the functioning of the engine.
- An object of this invention is to provide an improved indicator for thek detection of the partial formation yof vapor in uid conduit systems.
- a further object of this invention is to provide a method for the detection of the partial formation of vapor in fluid conduit systems.
- Fig. I is a cross sectional view of the device embodying this invention.
- Fig. II shows a cross sectional view of a modilcation embodied in this invention.
- Fig. III shows ⁇ a cross sectional view of a further modification embodied in this invention.
- numeral 1 of Fig. I designates a casing or housing having a covering 2 ailixed to the top of the housing in any suitable manner.
- a fluid inlet passage 3 is provided in the bottom or base and a fluid outlet passage 4 in the top of said housing, as shown.
- Oriflces 5 and 6 of suitable size are provided in the said fluid passages .3 and 4.
- the housing I is placed above the main conduit.
- FIG. I Within the said casing I of the modification shown by Fig. I are four expansion chambers 9, I0, II, and I2 separated by three diaphragms I3, I4, and I5, as shown,rigidly ailixed at their outer circumference to the casing 2, as by welding or in any other suitable manner.
- Communication between chambers 9 and III is provided by a plurality of passages I6 having an orifice ⁇ Il in each of the said passages.
- a baille I8 is provided, as shown, within the chamber 9 over the opening of the inlet 3 to deflect the ow of fluid away from the passages I6 nearest the said inlet 3.
- a shaft I9 is mounted on the three diaphragms I3, I4, and I5, and carries on its lower extremity in the chamber I2, a suitable electrically responsive U-shaped element 20 having a contact point 2
- Leads 24 and 25 are connected to the housing I and the arm 23, respectively, and operate a suitable electronic signal or control which may take the form of a simple battery circuit comprising, as shown, the leads 24-25, a battery l2, a lamp 44 and a solenoid coil I8 which is adapted to operate a valve or an electrical switch shown diagrammatically at 46.
- Suitable insulating material 26 is provided, as shown, between the portion of the U-shaped element 20 and the arm 23 to prevent closing of the electrical contact when the shaft I9 is moved downward.
- the upper extremity of the shaft I8 carries a biased spring 21 in the expansion chamber II, adapted to counteract the differential pressure existing across the diaphragm I4 during the flow of fluid from the chamber 9 to the chamber I0, and to provide a positive assurance of separation of contact points 2I and 22 during non-operation.
- An adjustable tension screw 28 threadedly engages cover 8 and bears on spring 21 to give control of the compression on said spring.
- Ports 29 are provided in the chambers II and I2 to permit breathing of the chambers.
- the function is the same as that shown in Fig, I, and the structure differs only in that the expansion chamber I2 and diaphragm I3 are omitted and the electrical contacts 2I and 22 are modified and located within the spring 21 in the expansion chamber Il.
- the contact point 2l iS grounded to the housing 2 and a suitable insulation 30 is provided to separate the contact point 22 from the grounding effect of the housing 2,
- a wire or open bridge 3l is provided over the inlet passage 3 to limit the downward movement of the shaft I@ and still permit the unrestricted passage of fluid and vapor into the chamber 9.
- the function is the same as the modification shown in Fig. II and the structure differs only from that modification in that the expansion chamber if and diaphragm I5 are omitted.
- the spring 2l is located in the chamber Ill and is rigidly affixed to the diaphragm lil.
- the shaft i9 is affixed to the spring 21 and the diaphragm I 4 by any suitable means, as shown.
- the adjusting screw 29 is provided with an opening 32 adapted to slidably receive, under pressure seal, a plunger 33.
- the lower end of the said plunger 33 is rigidly aflixed to the shaft I8 in any suitable manner.
- is provided at the upper end of the plunger 33 and is grounded to the housing 2 through the said plunger,
- a housing 3S carrying a second Contact point 22, suitably insulated, is provided to protect the contact points from dirt, etc.
- the circuits in modifications shown in Figs, II and III as in the modification shown in Fig. I are closed by grounding the insulated contact 22 against the grounded contact 2 I.
- the drop in pressure across orifices I1 can be made small.
- the volurne-rate of flow will increase somewhat and produce a momentary slight decrease in the volume of fluid in chamber S, which in turn will affect the differential across diaphragm I4 and thereby create adownward movement of the shaft I9; however this is not the effect which determines the operation of the indicator as embodied in this'invention but if present will not create an undesirable closing of the electrical circuit because the downward action on the diaphragm will be absorbed by the insulation 26.
- the electrical circuit can be made to start the operation of those known devices in the fuel and/or fuel metering system which are included to alleviate the formation of vapor and which do not oper-- ate continuously, or such other devices whose continuous operating characteristics differ from the characteristics desired during the presence of vapor.
- a device for sensing vapor in a liquid comprising a pair of expansion chambers in a housing adapted to receive fluid under pressure, conduit means interconnecting said chambers adapted to direct successive iluid llow therethrough, discharge orifice means in the second of said chambers adapted to effect a change of pressure in that chamber with respect to pressure in the other chamber when entrained vapor in the fluid ilows through the sensing device, and sensing means responsive to any change of pressure due to entrained vapor.
- a device for sensing vapor in a liquid comprising a pair of chambers adapted to receive the iiuid under pressure, conduit means interconnecting said chambers to direct successive iluid ilow therethrough, discharge orifice means adapted to eiIect a change of pressure in the second of said chambers with respect to the pressure in the nrst chamber when entrained vapor in the liquid flows through the device, diaphragm means positioned between the chambers responsive to said change, and a sensing device responsive to said diaphragm.
- a device i'or sensing vapor in a liquid comprising the combination of a pair of chambers in a housing adapted to receive the iluid under pressure, a movable partition wall common to both chambers, conduit means interconnecting said chambers adaptedto direct successive iluid flow therethrough and discharge conduit-means including an orifice communicating with the second chamber and effective to create a dif Schlierenbers when the fluid mixture oi' vapor and liquid flows through the device, said partition wall being movable in response to said diierential pressure, and sensing means actuated by said wall.
- a device for indicating the presence of a mixture of vapor and liquid in a fluid conduit comprising a housing connected to said conduit for fluid ow therefrom, a pair of chambers positioned in said housing adapted to receive liquid under pressure, a flexible diaphragm forming a common wall between the two chambers, conduit means provided with restrictive horrs connecting said chambers for successive fluid flow therebetween, said conduit means adapted to create a differential pressure between said chambers across said diaphragm, the pressure in the said second chamber being less than that in the ilrst chamber to thus actuate said diaphragm lsway from neutral position, resilient means positioned in said housing adapted to counteract the differential pressure to return the diaphragm to neutral position, means to limit the movement of the diaphragm when the diilerential pressure decreases, an inlet passage to the mst chamber.
- an outlet passage from the second chamber adapted to pass liquid substantially at the critical velocity thereof and to pass vapor below the critical velocity thereof whereby the pressure dierential -between the two chambers is increased when vapor alone flows through said last named orifice and means actuated by the diaphragm under the last named condition to indicate the presence of the vapor.
- a device for sensing the presence oi' vapor in a liquid system comprising a casing definingl a pair of chambers and a communicating passage for liquid under pressure, said chambers having a common yieldaible partition, an inlet oriiice for one oi' said chambers, an outlet oriilce for the other oi' said chambers calibrated at approximately the critical velocity of said liquid, whereby the relative pressure in said chambers varies upon the flow oi' vapor through said outlet orifice, and sensing means responsive to pressure din'erentials between said chambers when there is vapor in the liquid system.
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Physics & Mathematics (AREA)
- Measuring Fluid Pressure (AREA)
Description
May 3, 1949. E, A, MALICK 2,468,768
MEANS TO INDICATE THE PRESENCE OF VAPOR IN FLUID CONDUIT SYSTEMS Filed March 25, 1945 9 /7 I r l I ,l /7
22 .Q5` 2/ F/G. 3 52 33 /6' 2 /4 A|1 lf". /6 /7 '2 I y /7 'lilw 5 3/ WWW/@WWW 5% QW LWR Patented May 3, A1949 MEANS T INDICATE THE PRESENCE 0F VAPOR IN FLUID CONDUIT SYSTEMS Emil A. Malick, United states' Navy Application March 23, 1945, Serial No. 584,481
(Granted under the act of March 3, 1883, al amended April 30, 1928; 370 0. G. 757) 8 Claims.
This invention relates to an improved method for detecting the existence of the formation of vapor in fluid conduit systems and an improved ,indicator for accomplishing the same.
.In order to simplify the specification and claims which are to follow, the broad term vapor shall be used generally hereinafter to indicate any compressible fluid such as gas, air, or any other substance having a density lower than that of the incompressible liquid in a fluid conduit system.
The efficiency of operation of all fluid conduit systems and particularly those systems adapted for metering fluid for an internal combustion' engine, depends to a significant extent upon the condition of the uid within the said system, e. g., whether or not the fluids are in comparatively liquid state as opposed to a combined liquid and vapor state. It is well known that existing fluid conduit systems do not function as efficiently nor as accurately when a combined liquid-vapor condition exists within the system. In less actual instances of operations, it has been demonstrated that the depreciation in performance of an internal combustion engine due to the presence of vapors often causes partial or complete failure of engine operation. In an effort to provide, in the fluid conduitsystem, some means for prevention of failure of various parts of the system, due to these causes, which means would in turn reflect favorably upon the operation of the system, common practice `includes certain auxiliary, booster, or emergency pumps, or other known devices, which are intended to reduce or eliminate the formation of vapors. For a number of reasons, it is undesirable to operate these pumps or other devices continuously. Accordingly, the common practice is to operate or begin the operation of these devices manually, only after the presence of vapor in the system is detected by the operator, based upon the functioning of the engine. Such a procedure is undesirable inasmuch as it requires a conscious effort on the part of the operator and because the outward indication of the vapor function-its effect on the systemis often times difficult to diagnose (requiring an extensive knowledge of the particular system), and also because it is undesirable to permit the vapor formation to develop to the extent where actual mal-functioning is experienced, especially in the case of an internal combustion engine for an aircraft.
An object of this invention is to provide an improved indicator for thek detection of the partial formation yof vapor in uid conduit systems.
A further object of this invention is to provide a method for the detection of the partial formation of vapor in fluid conduit systems.
.Other objects and advantages of this invention will become apparent as the discussion proceeds and is considered in connection with the claims and accompanying drawings wherein like characters of reference designate like parts in the several views and wherein:
Fig. I is a cross sectional view of the device embodying this invention.
Fig. II shows a cross sectional view of a modilcation embodied in this invention.
Fig. III shows `a cross sectional view of a further modification embodied in this invention.
Referring now to the drawings, wherein for the purpose of illustration, is shown, an embodiment of this invention, numeral 1 of Fig. I designates a casing or housing having a covering 2 ailixed to the top of the housing in any suitable manner. A fluid inlet passage 3 is provided in the bottom or base and a fluid outlet passage 4 in the top of said housing, as shown. Oriflces 5 and 6 of suitable size are provided in the said fluid passages .3 and 4. Communicating with the inlet passage 3, and affixed thereto in any suitable manner, such as by a thread joint, is a conduit 'l adapted to allow passage of iluid or fluid and vapor from a main conduit line (not shown), carrying fluid under pressure, to the lnlet 3. It is to be noted that the housing I is placed above the main conduit.
Within the said casing I of the modification shown by Fig. I are four expansion chambers 9, I0, II, and I2 separated by three diaphragms I3, I4, and I5, as shown,rigidly ailixed at their outer circumference to the casing 2, as by welding or in any other suitable manner.
Communication between chambers 9 and III is provided by a plurality of passages I6 having an orifice` Il in each of the said passages. A baille I8 is provided, as shown, within the chamber 9 over the opening of the inlet 3 to deflect the ow of fluid away from the passages I6 nearest the said inlet 3.
A shaft I9 is mounted on the three diaphragms I3, I4, and I5, and carries on its lower extremity in the chamber I2, a suitable electrically responsive U-shaped element 20 having a contact point 2| on'the inside of the U, as shown, grounded to the body of the housing adapted to close a circuit by contact with an electrical contact point 22 supported by an insulated arm 23, when the shaft I9 is moved upward. Leads 24 and 25 are connected to the housing I and the arm 23, respectively, and operate a suitable electronic signal or control which may take the form of a simple battery circuit comprising, as shown, the leads 24-25, a battery l2, a lamp 44 and a solenoid coil I8 which is adapted to operate a valve or an electrical switch shown diagrammatically at 46. Suitable insulating material 26 is provided, as shown, between the portion of the U-shaped element 20 and the arm 23 to prevent closing of the electrical contact when the shaft I9 is moved downward.
The upper extremity of the shaft I8 carries a biased spring 21 in the expansion chamber II, adapted to counteract the differential pressure existing across the diaphragm I4 during the flow of fluid from the chamber 9 to the chamber I0, and to provide a positive assurance of separation of contact points 2I and 22 during non-operation. An adjustable tension screw 28 threadedly engages cover 8 and bears on spring 21 to give control of the compression on said spring. Ports 29 are provided in the chambers II and I2 to permit breathing of the chambers.
In the modification of this invention shown in Fig. II the function is the same as that shown in Fig, I, and the structure differs only in that the expansion chamber I2 and diaphragm I3 are omitted and the electrical contacts 2I and 22 are modified and located within the spring 21 in the expansion chamber Il. The contact point 2l iS grounded to the housing 2 and a suitable insulation 30 is provided to separate the contact point 22 from the grounding effect of the housing 2, A wire or open bridge 3l is provided over the inlet passage 3 to limit the downward movement of the shaft I@ and still permit the unrestricted passage of fluid and vapor into the chamber 9.
In the modication of this invention shown in Fig. III the function is the same as the modification shown in Fig. II and the structure differs only from that modification in that the expansion chamber if and diaphragm I5 are omitted. The spring 2l is located in the chamber Ill and is rigidly affixed to the diaphragm lil. The shaft i9 is affixed to the spring 21 and the diaphragm I 4 by any suitable means, as shown. The adjusting screw 29 is provided with an opening 32 adapted to slidably receive, under pressure seal, a plunger 33. The lower end of the said plunger 33 is rigidly aflixed to the shaft I8 in any suitable manner. A contact point 2| is provided at the upper end of the plunger 33 and is grounded to the housing 2 through the said plunger, A housing 3S carrying a second Contact point 22, suitably insulated, is provided to protect the contact points from dirt, etc. The circuits in modifications shown in Figs, II and III as in the modification shown in Fig. I are closed by grounding the insulated contact 22 against the grounded contact 2 I.
During normal operation in the presence of fluid flow in the main conduit, there will be a certain amount of fluid flow into the inlet passage 3 and thence through the chamber 9 into the chamber III and into the outlet L. Inasmuch as the flow into the chamber I0 from chamber 9 is controlled by orifices i1, a slight pressure differential will normally exist across the diaphragm Il which is compensated for by the spring 2'L Transient variations in the fluid pressure in the main conduit will have an inappreciable effect on the pressure in the chamber 9 due to the dampening effect of the orifice 5, and accordingly the differential pressure across the diaphragm I4 will not be markedly affected, since this is also to a large extent a function of the orifice 6.
It is a known hydraulic phenomenon that for a given pressure the volume rate of flow of a liquid through an orifice is considerably less than that of a gas. The exact magnitude of the differences in rate of flow for any given liquid and gas is a function of the size of the orifice and the pressure differential existing across it. Also, it is known that the critical velocity of flow through a given oriilce is considerably lower forA a liquid than for a gas. The relative sensitivity of the indicator can be increased or decreased by altering the ratio of the size of orifices 5 and I1 to orifice 6. For example by proper selection of the orifice 6, normal flow of liquid through said orifice 6, for the average pressure differential existing across it, can be made to flow, ff desired, at or near a critical velocity condition. Inasmuch as the greatest pressure differential will at all times exist across orifice 6, it can be made to be the only restriction which is flowing in the critical region.
Now, at the time vapor begins to form in the main conduit, it will be carried past the juncture of conduits 1 and the main conduit. Due to the form of this juncture, (not shown) and due to the fact that the vapor of lower density than the fluid, will lie above the fluid, and due to the fact that the indicator housing I is located above the level of the conduits 1 and main conduit vapor, (under the same pressure as the liquid will be carried up into the inlet passage 3 and thence into the expansible chambers 9 and I0. Inasmuch as the vapor in passing through the orifice 5 will be flowing into the chamber 9 which is a lower pressure than existing in the conduit 1, it will effect neither the volume nor the pressure of the chamber 9. inasmuch as the orifice 6 permits the passage of fluid at or near a critical velocity and is the main control of flow through the indicator, the drop in pressure across orifices I1 can be made small. As vapor passes through the said orifices I1, however. the volurne-rate of flow will increase somewhat and produce a momentary slight decrease in the volume of fluid in chamber S, which in turn will affect the differential across diaphragm I4 and thereby create adownward movement of the shaft I9; however this is not the effect which determines the operation of the indicator as embodied in this'invention but if present will not create an undesirable closing of the electrical circuit because the downward action on the diaphragm will be absorbed by the insulation 26.
As vapor-'passes through the orice 6, however, there will exist a very marked increase in rate of volume flow through that orifice due to the fact that the differential across this orifice is high. This will result in an immediate pronounced reduction of pressure in the expansive chamber I0 only, due to the reduction in volume of fluid in this chamber. Under the set of circumstances which will then exist, when the first flow of vapor taires place through the orifice 6, i. e. when all buta small portion of the fluid contained in the chamber I0 consists of a relatively incompressible fluid, the release of vapor through the orifice 6 will cause the pressure in chamber I0 to reach a value nearly that of the pressure in conduit l. The result will be a pressure in chamber I0 considerably less than that in chamber 9 forcing the diaphragm and consequently the shaft I9 upward thereby closing the contacts 2| and 22.
With closure of' the contact points, the electrical circuit can be made to start the operation of those known devices in the fuel and/or fuel metering system which are included to alleviate the formation of vapor and which do not oper-- ate continuously, or such other devices whose continuous operating characteristics differ from the characteristics desired during the presence of vapor.
It is to be understood that the form of this invention, herewith shown and described, is to be taken as a preferred example of the same, and that various changes in the shape, size, and arrangement of the parts may be resorted to without departing from the spirit of this invention or the scope of the subjoined claims.
'I'he invention described herein may be manui'actured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
What I claim is:
1. A device for sensing vapor in a liquid comprising a pair of expansion chambers in a housing adapted to receive fluid under pressure, conduit means interconnecting said chambers adapted to direct successive iluid llow therethrough, discharge orifice means in the second of said chambers adapted to effect a change of pressure in that chamber with respect to pressure in the other chamber when entrained vapor in the fluid ilows through the sensing device, and sensing means responsive to any change of pressure due to entrained vapor.
2. In a device for sensing vapor in a liquid the combination comprising a pair of chambers adapted to receive the iiuid under pressure, conduit means interconnecting said chambers to direct successive iluid ilow therethrough, discharge orifice means adapted to eiIect a change of pressure in the second of said chambers with respect to the pressure in the nrst chamber when entrained vapor in the liquid flows through the device, diaphragm means positioned between the chambers responsive to said change, and a sensing device responsive to said diaphragm.
3. A device i'or sensing vapor in a liquid comprising the combination of a pair of chambers in a housing adapted to receive the iluid under pressure, a movable partition wall common to both chambers, conduit means interconnecting said chambers adaptedto direct successive iluid flow therethrough and discharge conduit-means including an orifice communicating with the second chamber and effective to create a difierenbers when the fluid mixture oi' vapor and liquid flows through the device, said partition wall being movable in response to said diierential pressure, and sensing means actuated by said wall.
4. A device as set forth in claim 3, wherein the movable partition wall is constructed in the tial pressure between the second and nrst cham-A' said housing adapted to receive the fluid under pressure in sequential ilow, a flexible diaphragm forming a common wall between said chambers, conduit means provided with restrictive orifices interposed between the two chambers adapted to create a pressure differential therebetween when the fluid is in motion, an inlet passage in said housing connected to one of the chambers, a discharge passage provided with a restrictive orifice connected to the other chamber adapted to discharge liquid at or near its critical velocity and to thereby create a greater pressure differential between said chambers when a mixture of vapor and liquid passes through said last named oriiice and means responsive to the movement of the diaphragm under said greater pressure differential adapted to indicate the presence of said mixture.
7. A device for indicating the presence of a mixture of vapor and liquid in a fluid conduit comprising a housing connected to said conduit for fluid ow therefrom, a pair of chambers positioned in said housing adapted to receive liquid under pressure, a flexible diaphragm forming a common wall between the two chambers, conduit means provided with restrictive orices connecting said chambers for successive fluid flow therebetween, said conduit means adapted to create a differential pressure between said chambers across said diaphragm, the pressure in the said second chamber being less than that in the ilrst chamber to thus actuate said diaphragm lsway from neutral position, resilient means positioned in said housing adapted to counteract the differential pressure to return the diaphragm to neutral position, means to limit the movement of the diaphragm when the diilerential pressure decreases, an inlet passage to the mst chamber. an outlet passage from the second chamber adapted to pass liquid substantially at the critical velocity thereof and to pass vapor below the critical velocity thereof whereby the pressure dierential -between the two chambers is increased when vapor alone flows through said last named orifice and means actuated by the diaphragm under the last named condition to indicate the presence of the vapor.
8. A device for sensing the presence oi' vapor in a liquid system, comprising a casing definingl a pair of chambers and a communicating passage for liquid under pressure, said chambers having a common yieldaible partition, an inlet oriiice for one oi' said chambers, an outlet oriilce for the other oi' said chambers calibrated at approximately the critical velocity of said liquid, whereby the relative pressure in said chambers varies upon the flow oi' vapor through said outlet orifice, and sensing means responsive to pressure din'erentials between said chambers when there is vapor in the liquid system.
EMIL A. MALICK. REFERENCES CITED The following references are of record in the die of this patent:
UNITED STATES PATENTS Number Name Date 492,710 Carpenter Feb. 28, 1893 2,334,220 Samiran Nov. 16,
Publications (1)
Publication Number | Publication Date |
---|---|
US2468768A true US2468768A (en) | 1949-05-03 |
Family
ID=3436370
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US2468768D Expired - Lifetime US2468768A (en) | Means to indicate the presence of |
Country Status (1)
Country | Link |
---|---|
US (1) | US2468768A (en) |
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2672602A (en) * | 1950-09-28 | 1954-03-16 | Westinghouse Air Brake Co | Apparatus for measuring rate of flow of fluid |
US2697764A (en) * | 1950-06-17 | 1954-12-21 | Burgua Corp | Pressure-responsive switch |
US2739201A (en) * | 1953-11-16 | 1956-03-20 | Alfred A Muller | Pressure responsive signal device |
US2772409A (en) * | 1952-01-22 | 1956-11-27 | Smiths Jacking Systems Ltd | Pressure responsive flow indicator |
US2788063A (en) * | 1952-08-02 | 1957-04-09 | Pratt & Whitney Co Inc | Fluid flow controls |
US2827526A (en) * | 1954-12-10 | 1958-03-18 | Gen Motors Corp | Pressure actuated switch |
US2853880A (en) * | 1954-03-10 | 1958-09-30 | Westinghouse Electric Corp | Absolute pressure sensing device |
US2923926A (en) * | 1960-02-02 | wright | ||
US2984719A (en) * | 1953-08-20 | 1961-05-16 | Paul M Higgs | Shock and pressure sensitive switch |
US2993970A (en) * | 1958-05-23 | 1961-07-25 | Allis Chalmers Mfg Co | Vacuum switch structure using sylphon and slotted diaphragm |
US3042769A (en) * | 1960-10-13 | 1962-07-03 | Norman Products Company | Fluid fuel flow control system for forced draft heating units |
US3056278A (en) * | 1960-02-17 | 1962-10-02 | Phillips Petroleum Co | Flow controller for chromatographic analyzer |
US3120171A (en) * | 1958-01-28 | 1964-02-04 | Acme Steel Co | Automatic strapping machine |
US3225340A (en) * | 1961-09-26 | 1965-12-21 | Combustion Eng | Self-compensating low velocity trip or alarm device |
US3407277A (en) * | 1965-10-22 | 1968-10-22 | Controls Co Of America | Pressure switch |
US3505791A (en) * | 1968-07-01 | 1970-04-14 | Beamco Inc | Vacuum cleaner filter condition sensing system |
US4233597A (en) * | 1977-03-19 | 1980-11-11 | Gerhard Kurz | Device indicating a state due to the pressure modification |
US4468170A (en) * | 1980-07-11 | 1984-08-28 | Beta Technology, Inc. | Low level indicator |
US4654643A (en) * | 1985-07-22 | 1987-03-31 | Meisenheimer Jr Daniel T | Pressure sensor-monitor and excessive pressure level indicator |
EP1318536A1 (en) * | 2001-12-05 | 2003-06-11 | Beru AG | Differential pressure switch |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US492710A (en) * | 1893-02-28 | Magdebtjrg | ||
US2334220A (en) * | 1940-12-13 | 1943-11-16 | Samiran David | Fuel system |
-
0
- US US2468768D patent/US2468768A/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US492710A (en) * | 1893-02-28 | Magdebtjrg | ||
US2334220A (en) * | 1940-12-13 | 1943-11-16 | Samiran David | Fuel system |
Cited By (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2923926A (en) * | 1960-02-02 | wright | ||
US2697764A (en) * | 1950-06-17 | 1954-12-21 | Burgua Corp | Pressure-responsive switch |
US2672602A (en) * | 1950-09-28 | 1954-03-16 | Westinghouse Air Brake Co | Apparatus for measuring rate of flow of fluid |
US2772409A (en) * | 1952-01-22 | 1956-11-27 | Smiths Jacking Systems Ltd | Pressure responsive flow indicator |
US2788063A (en) * | 1952-08-02 | 1957-04-09 | Pratt & Whitney Co Inc | Fluid flow controls |
US2984719A (en) * | 1953-08-20 | 1961-05-16 | Paul M Higgs | Shock and pressure sensitive switch |
US2739201A (en) * | 1953-11-16 | 1956-03-20 | Alfred A Muller | Pressure responsive signal device |
US2853880A (en) * | 1954-03-10 | 1958-09-30 | Westinghouse Electric Corp | Absolute pressure sensing device |
US2827526A (en) * | 1954-12-10 | 1958-03-18 | Gen Motors Corp | Pressure actuated switch |
US3120171A (en) * | 1958-01-28 | 1964-02-04 | Acme Steel Co | Automatic strapping machine |
US2993970A (en) * | 1958-05-23 | 1961-07-25 | Allis Chalmers Mfg Co | Vacuum switch structure using sylphon and slotted diaphragm |
US3056278A (en) * | 1960-02-17 | 1962-10-02 | Phillips Petroleum Co | Flow controller for chromatographic analyzer |
US3042769A (en) * | 1960-10-13 | 1962-07-03 | Norman Products Company | Fluid fuel flow control system for forced draft heating units |
US3225340A (en) * | 1961-09-26 | 1965-12-21 | Combustion Eng | Self-compensating low velocity trip or alarm device |
US3407277A (en) * | 1965-10-22 | 1968-10-22 | Controls Co Of America | Pressure switch |
US3505791A (en) * | 1968-07-01 | 1970-04-14 | Beamco Inc | Vacuum cleaner filter condition sensing system |
US4233597A (en) * | 1977-03-19 | 1980-11-11 | Gerhard Kurz | Device indicating a state due to the pressure modification |
US4468170A (en) * | 1980-07-11 | 1984-08-28 | Beta Technology, Inc. | Low level indicator |
US4654643A (en) * | 1985-07-22 | 1987-03-31 | Meisenheimer Jr Daniel T | Pressure sensor-monitor and excessive pressure level indicator |
EP1318536A1 (en) * | 2001-12-05 | 2003-06-11 | Beru AG | Differential pressure switch |
US6621021B2 (en) | 2001-12-05 | 2003-09-16 | Beru Ag | Differential pressure switch and sensor |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2468768A (en) | Means to indicate the presence of | |
US2244373A (en) | Fluid flow responsive switching device | |
US2582483A (en) | Pressure sensitive switch | |
US2402355A (en) | Dispensing system | |
US2112664A (en) | Control mechanism | |
US2495299A (en) | Charge forming device | |
GB1076568A (en) | Fluid control device | |
US2988099A (en) | Fluid-operated control device | |
US2501709A (en) | Automatic cutoff for damaged radiator sections | |
EP0095840A3 (en) | A mechanical engine protection system | |
US2600073A (en) | Pressure regulator | |
US2220496A (en) | Flowmeter | |
US2856167A (en) | Electrically actuated fuel shut-off apparatus | |
US2873756A (en) | Device for controlling an actuator by the translation of a shock wave | |
US2810034A (en) | Filter signal | |
US2788063A (en) | Fluid flow controls | |
US2456994A (en) | Fluid pressure switch | |
US2873104A (en) | Fluid governors | |
US3009631A (en) | Control devices for fluid pressure systems | |
US2966668A (en) | Pressure switch | |
US2763286A (en) | Automatic valve control mechanism | |
US2685302A (en) | Diaphragm valve | |
US2641277A (en) | Fluid system damage control | |
US3158708A (en) | Icing detection apparatus and system | |
US2349775A (en) | Fuel regulator for aircraft carburetors |