[go: up one dir, main page]

US2627876A - Venturi control for liquid flow - Google Patents

Venturi control for liquid flow Download PDF

Info

Publication number
US2627876A
US2627876A US166511A US16651150A US2627876A US 2627876 A US2627876 A US 2627876A US 166511 A US166511 A US 166511A US 16651150 A US16651150 A US 16651150A US 2627876 A US2627876 A US 2627876A
Authority
US
United States
Prior art keywords
disc
liquid
venturi
flow
casing
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
US166511A
Inventor
Esther C Goddard
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.)
DANIEL AND FLORENCE GUGGENHEIM
DANIEL AND FLORENCE GUGGENHEIM FOUNDATION
Original Assignee
DANIEL AND FLORENCE GUGGENHEIM
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 DANIEL AND FLORENCE GUGGENHEIM filed Critical DANIEL AND FLORENCE GUGGENHEIM
Priority to US166511A priority Critical patent/US2627876A/en
Application granted granted Critical
Publication of US2627876A publication Critical patent/US2627876A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants
    • F02K9/56Control
    • F02K9/58Propellant feed valves
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D7/00Control of flow
    • G05D7/01Control of flow without auxiliary power
    • G05D7/0193Control of flow without auxiliary power using hydraulic or pneumatic amplifiers, relays or transmitters
    • 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
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S60/00Power plants
    • Y10S60/915Collection of goddard patents

Definitions

  • This invention relates to the control of liquid flow in feed pipes and other similar conduits.
  • the invention is particularly useful in regulating the flow of a liquid combustion element to a combustion chamber of the general type used in rockets and rocket craft.
  • the invention further relates to arrangements and combinations of parts which will be hereinafter described and more particularly pointe out in the appended claims.
  • ' Fi 1 is a sectional side elevation of a Venturi tube and a preferred form of the control apparatus associated therewith;
  • Fig. 2 is a sectional side elevation of a jacketed construction
  • Fig.8 is'asectional side elevation showing a modified venting arrangement
  • Fig. 4 is a sectional side elevation of a modified control apparatusi and Fig. 5 is a sectional side elevation of a further modification.
  • a Venturi tube T which comprises an inlet section It, a contracting Venturi section II, an expending Venturi section [2, and anoutlet section I4.
  • An annular casing 16 connects the sections I0 and II and is provided with an annular recess I! which communicates with an annular slot l8 between the adjacent ends of the Venturi sections l0 and H.
  • the slot I8 is inclined in the direction of flow, as clearly indicated in Fig. 1.
  • a second annular casing 20 connects the Venturi sections H and I2 and is provided with an annular recess 2
  • the slot 22 is also inclined in the direction of flow.
  • the control apparatus shown in Fig. 1 comprises upper and lower casing members and 31, mounted in fixed spaced relation and connected by pipes 32 and 33 to the annular recesses I1 and 2i respectively.
  • a disc 35 is mounted be-. tween the casing members 20 and 3
  • the upper inner bellows member 36 connects the middle portion of the disc 35 to an upward extension 50 of the upper casing member 30, and the lower inner bellows member 31 similarly connects the disc 35 in a downward extension 4
  • the upper outer bellows member 38 connects the outer edge of the disc 35 to a peripheral upward extension 44 of the upper casing member 30, and the lower outer bellows member 39 similarly connects the edge of the disc 35 to a peripheral downward extension Q5 of the lower casing member 3
  • the middle portion of the disc 35' is connected to actuate a rod 41, which rod controls the flow of liquid through the Venturi tube T.
  • any suitable control connections may be provided between the rod 4'! and the tube T.
  • Illustrative connections as shown in Fig. l comprise an indicating lever 50 pivoted at 5
  • the lever 50 is suitably insulated from the rod d! and is connected to a line wire L.
  • the long arm of the lever'50 is adapted to engage one or the other of two contacts 52 and 53, connected by wires 54 and 55 to reverse windings in a motor M, to which a second line wire L is also connected.
  • the motor M is adapted to operate a valve V in the Venturi inlet section Ill through bevel gears 56 and 51, a worm 58 and a worm gear 59.
  • the liquid to be controlled is a very cold liquid, such as liquid oxygen
  • a suitable jacket J Fig. 2 which lined or coated with a suitable insulating material to prevent escape of heat and vaporization of the cold liquid.
  • the space S within the jacket be filled with the same or some equivalent cold liquid, so as to further reduce the tendency to form vapor within the control apparatus.
  • This cold liquid may be supplied through a pipe 60 (Fig. 2) and discharged through a pipe 61. Otherwise the construction is as shown in Fig. 1.
  • the construction shown in Fig. 4 is desirable where very high pressures are to be encountered in the Venturi tube T2.
  • the control apparatus is substantially as shown in Fig. 1, except that the disc 35b is mounted in a vertical instead of a horizontal plane, and except that the casing members 301) and 31b are enclosed within a spherical jacket J2, which is preferably made of steel or other material adapted to resist substantial pressure.
  • Vent pipes I4 and 15 may be connected into the upper parts of the casing members 301) and 31b and may be provided with suitable valves 16 and H.
  • the rod In order to balance pressures on the actuating rod 41b, the rod is extended through both sides of the jacket casing J2 and may be sealed therein by elongated bellows members 80 and 8
  • Any desired pressure may be maintained in the space S2 to selectively offset any pressures en-. countered in the tube T2 or within the casing members 38b and 31b,
  • FIG. 5 A simplified and extremely rigid construction is shown in Fig. 5, in which a corrugated disc 90 is mounted between segmental concave casing members 91 and 92 and is provided with an actuating rod 93. Pressures from spaced points in a Venturi tube are applied through pipes 94 and 95, which correspond to the pipes 32 and 33 in Fig. l.
  • Vent pipes 96 with associated valves are provided at the top of the casing members 91 and 92, and drainage pipes 91, also with associated valves, are connected into the lower portions of the casing members SI and 92.
  • This form of the invention economical to manufacture and is well adapted to handle substantial pressures in the associated Venturi tube.
  • Apparatus displaceable by differential liquid pressures comprising a diaphragm disc, upper and lower casing members providing a closed compartment at each side of said disc, said casing members each having a substantially raised edge portion and an outwardly extending middle portion substantially spaced from said edge portion, separate bellows members sealed to said disc and to the raised edge portion of each casing member, separate bellows members sealed to said disc and to the outer end of the middle portion of each casing member, means to supply liquids under differential pressures to said closed compartments, which liquids are effective to bodily displace said diaphragm disc, and a control member fixed to said disc and movable therewith,
  • Displaceable apparatus set forth in claim 1 in which said apparatus is entirely enclosed in an outer jacket, and in which mean-s is provided to supply a fluid under pressure to said jacket to partially oiiset the internal pressures in said compartments.
  • Displaceable apparatus as set forth in claim 1 in which provision is made to connect the outwardly extending edge and middle portions of one casing member to each other and to theatmosphere, whereby to vent the compartment enclosed by said member and to facilitate filling of: saidcompartment.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)

Description

Feb. 10, 1953 R. H. GODDARD VENTURI CONTROL FOR LIQUID FLOW Filed June 6, 1950 Fig.3
INVENTOR. ROBERT H.60DDARD, DECD.
ESTHER C.GODDARD, EXECUTRIX. BY
Patented Feb. 10, 1953 VENTURI CONTROL FOR LIQUID FLOW Robert H. Goddard, deceased, late of Annapolis,
Md., by Esther C. Goddard, executrix, Worcester, Mass., assignor of one-half to The Daniel and Florence Guggenheim Foundation, New York, N. Y., a corporation of New York Application June 6, 1950, Serial No. 166,511
3 Claims.
This invention relates to the control of liquid flow in feed pipes and other similar conduits. The invention is particularly useful in regulating the flow of a liquid combustion element to a combustion chamber of the general type used in rockets and rocket craft.
It is the general object of the invention to provide apparatus efiective to control the flow of a liquid in predetermined relation to the difference in pressure found at different points in a Venturi tube through which the liquid is caused to flow. This difference inpressure increases with any increase in the rateof flow of the liquid, and it is a further object of the invention to provide improved means to varythe flow in inverse relation to the changes in pressure. Means is also provided for producing the control indication with a minimum displacement of liquid in the control apparatus.
The invention further relates to arrangements and combinations of parts which will be hereinafter described and more particularly pointe out in the appended claims.
Preferred forms of the invention are shown in the drawings, in which:
' Fi 1 is a sectional side elevation of a Venturi tube and a preferred form of the control apparatus associated therewith;
Fig. 2 is a sectional side elevation of a jacketed construction Fig.8 is'asectional side elevation showing a modified venting arrangement;
Fig. 4 is a sectional side elevation of a modified control apparatusi and Fig. 5 is a sectional side elevation of a further modification.
Referring particularlyto Fig. 1, a Venturi tube T is shown which comprises an inlet section It, a contracting Venturi section II, an expending Venturi section [2, and anoutlet section I4.
An annular casing 16 connects the sections I0 and II and is provided with an annular recess I! which communicates with an annular slot l8 between the adjacent ends of the Venturi sections l0 and H. The slot I8 is inclined in the direction of flow, as clearly indicated in Fig. 1.
A second annular casing 20 connects the Venturi sections H and I2 and is provided with an annular recess 2| communicating with an annular slot 22 between the adjacent ends of the Venturi sections H and [2. The slot 22 is also inclined in the direction of flow.
The control apparatus shown in Fig. 1 comprises upper and lower casing members and 31, mounted in fixed spaced relation and connected by pipes 32 and 33 to the annular recesses I1 and 2i respectively. A disc 35 is mounted be-. tween the casing members 20 and 3| and is supported by inner bellows members 36 and 3'! and outer bellows members 38 and 39.
The upper inner bellows member 36 connects the middle portion of the disc 35 to an upward extension 50 of the upper casing member 30, and the lower inner bellows member 31 similarly connects the disc 35 in a downward extension 4| of the lower casing member 3|. The upper outer bellows member 38 connects the outer edge of the disc 35 to a peripheral upward extension 44 of the upper casing member 30, and the lower outer bellows member 39 similarly connects the edge of the disc 35 to a peripheral downward extension Q5 of the lower casing member 3|.
The middle portion of the disc 35'is connected to actuate a rod 41, which rod controls the flow of liquid through the Venturi tube T.
Any suitable control connections may be provided between the rod 4'! and the tube T. Illustrative connections as shown in Fig. l comprise an indicating lever 50 pivoted at 5| and. having its short arm operatively connected to the rod 41. The lever 50 is suitably insulated from the rod d! and is connected to a line wire L.
The long arm of the lever'50 is adapted to engage one or the other of two contacts 52 and 53, connected by wires 54 and 55 to reverse windings in a motor M, to which a second line wire L is also connected. The motor M is adapted to operate a valve V in the Venturi inlet section Ill through bevel gears 56 and 51, a worm 58 and a worm gear 59.
With these connections, it will be evident that upward displacement of the diaphragm 35 will cause the arm 50 to engage the lower terminal 53 and cause the motor M to rotate in one direction, whereas downward displacement of the disc 35 will'c'ause the arm 50 to engage the terminal 52 and rotate the motor M in the other direction. The valve V will thus be shifted in accordance with the displacement of the disc 35, due to changes in relative pressures in the Venturi tube between the slots l8 and 22. An increase in pressure difference indicates an increase in rate of flow and acts to move the disc 35 upward and to initiate a movement of the valve V in a closing direction.
If the liquid to be controlled is a very cold liquid, such as liquid oxygen, it is desirable that the bellows-operated control apparatus be enclosed in a suitable jacket J (Fig. 2) which lined or coated with a suitable insulating material to prevent escape of heat and vaporization of the cold liquid.
It is also desirable that the space S within the jacket be filled with the same or some equivalent cold liquid, so as to further reduce the tendency to form vapor within the control apparatus. This cold liquid may be supplied through a pipe 60 (Fig. 2) and discharged through a pipe 61. Otherwise the construction is as shown in Fig. 1.
Before starting the control apparatus in operation, it is desirable to thoroughly exhaust all air or gas from between the casing members 30 and 3i and the disc 35. This may be accomplished manually by moving the rod 41 upward and downward to pump out the air or gas through the pipes 32 and 33 (Fig. l), but in the construction shown in Fig. 3, this pumping operation is rendered unnecessary, at least in part, by the provision of a vent pipe 63 having a valve 64 and connected by branch pipes 65 and 66 to the upper ends of the upward extensions 40c and 44a of the upper casing member 30a. The space below the disc 35a may be similarly vented through a pipe 66 having a valve 6'1.
The construction shown in Fig. 4 is desirable where very high pressures are to be encountered in the Venturi tube T2. The control apparatus is substantially as shown in Fig. 1, except that the disc 35b is mounted in a vertical instead of a horizontal plane, and except that the casing members 301) and 31b are enclosed within a spherical jacket J2, which is preferably made of steel or other material adapted to resist substantial pressure.
Any suitable liquid under pressure may be supplied to the jacket space S2 through a supply pipe 7'9 and valve H, and may be drawn ofi through a discharge pipe 12 and valve 73. Vent pipes I4 and 15 may be connected into the upper parts of the casing members 301) and 31b and may be provided with suitable valves 16 and H.
In order to balance pressures on the actuating rod 41b, the rod is extended through both sides of the jacket casing J2 and may be sealed therein by elongated bellows members 80 and 8|. These bellows members permit substantially free axial movement of the rod 411) and th pressures in said bellows members balance each other.
Any desired pressure may be maintained in the space S2 to selectively offset any pressures en-. countered in the tube T2 or within the casing members 38b and 31b,
A simplified and extremely rigid construction is shown in Fig. 5, in which a corrugated disc 90 is mounted between segmental concave casing members 91 and 92 and is provided with an actuating rod 93. Pressures from spaced points in a Venturi tube are applied through pipes 94 and 95, which correspond to the pipes 32 and 33 in Fig. l.
Vent pipes 96 with associated valves are provided at the top of the casing members 91 and 92, and drainage pipes 91, also with associated valves, are connected into the lower portions of the casing members SI and 92.
This form of the invention economical to manufacture and is well adapted to handle substantial pressures in the associated Venturi tube.
In all forms of the invention, it will be seen that provision made to regulate and control the flow of a liquid through a Venturi tube in accordance with the rate of flow through the tube, and to vary the supply of liquid to the tube in such manner as to maintain substantially uniform flow.
Having thus described the invention and the advantages thereof, it will be understood that the invention is not to be limited to the details herein disclosed, otherwise than as set forth in the claims, but what is claimed is:
1. Apparatus displaceable by differential liquid pressures and comprising a diaphragm disc, upper and lower casing members providing a closed compartment at each side of said disc, said casing members each having a substantially raised edge portion and an outwardly extending middle portion substantially spaced from said edge portion, separate bellows members sealed to said disc and to the raised edge portion of each casing member, separate bellows members sealed to said disc and to the outer end of the middle portion of each casing member, means to supply liquids under differential pressures to said closed compartments, which liquids are effective to bodily displace said diaphragm disc, and a control member fixed to said disc and movable therewith,
2. Displaceable apparatus set forth in claim 1 in which said apparatus is entirely enclosed in an outer jacket, and in which mean-s is provided to supply a fluid under pressure to said jacket to partially oiiset the internal pressures in said compartments.
3. Displaceable apparatus as set forth in claim 1 in which provision is made to connect the outwardly extending edge and middle portions of one casing member to each other and to theatmosphere, whereby to vent the compartment enclosed by said member and to facilitate filling of: saidcompartment.
ESTHER C. GQDDA Q. Erecutria: of the, Last Will and Testament. of
Robert H. Goddard, Deceased.
REFERENCES CITED The following references are of record, in the file of this patent:
UNITED STATES PATENTS.
Number Name Date 1,206,806 Borden Dec. 5,1915 2,446,523 Bradbury Aug. 10, 1948
US166511A 1950-06-06 1950-06-06 Venturi control for liquid flow Expired - Lifetime US2627876A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US166511A US2627876A (en) 1950-06-06 1950-06-06 Venturi control for liquid flow

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US166511A US2627876A (en) 1950-06-06 1950-06-06 Venturi control for liquid flow

Publications (1)

Publication Number Publication Date
US2627876A true US2627876A (en) 1953-02-10

Family

ID=22603621

Family Applications (1)

Application Number Title Priority Date Filing Date
US166511A Expired - Lifetime US2627876A (en) 1950-06-06 1950-06-06 Venturi control for liquid flow

Country Status (1)

Country Link
US (1) US2627876A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3304722A (en) * 1965-02-16 1967-02-21 James L Culpepper Means for supplying cold gas to a propulsion jet in outer space
US3805612A (en) * 1971-02-08 1974-04-23 Oval Eng Co Ltd Orifice flow meter
US5718160A (en) * 1995-01-31 1998-02-17 Kyocera Corporation Positioning device

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1206806A (en) * 1915-03-03 1916-12-05 Simplex Valve & Meter Company Liquid-rate controller.
US2446523A (en) * 1944-01-31 1948-08-10 Westinghouse Electric Corp Fuel control apparatus for liquid fuel burners

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1206806A (en) * 1915-03-03 1916-12-05 Simplex Valve & Meter Company Liquid-rate controller.
US2446523A (en) * 1944-01-31 1948-08-10 Westinghouse Electric Corp Fuel control apparatus for liquid fuel burners

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3304722A (en) * 1965-02-16 1967-02-21 James L Culpepper Means for supplying cold gas to a propulsion jet in outer space
US3805612A (en) * 1971-02-08 1974-04-23 Oval Eng Co Ltd Orifice flow meter
US5718160A (en) * 1995-01-31 1998-02-17 Kyocera Corporation Positioning device

Similar Documents

Publication Publication Date Title
US2238905A (en) Gas turbine plant
US3212280A (en) Volatile liquid pumping system
US2870599A (en) Temperature responsive rocket nozzle
US2627876A (en) Venturi control for liquid flow
US2526221A (en) Gas-operated apparatus for pumping very cold liquids
US2247989A (en) Motor speed governor
US2670185A (en) Heat exchange apparatus provided with thermal compensating device
US1631262A (en) Variable-pressure-operated expansion device
US1394955A (en) Apparatus for filling oxygen-cylinders
US2468489A (en) Hydraulic apparatus
US1306865A (en) Prime moveb
US3724751A (en) Disc-type steam trap
US2988075A (en) Combined pressure regulator and fuel heater and vaporizer
US3344979A (en) Diffusion-pump construction
US2955649A (en) Ullage compensators for pressurizing systems
US2555445A (en) Pump control means
US2466415A (en) Pressure sensitive capsule and mixture control device embodying the same
US3266212A (en) Method and apparatus for filling bellows
US2548430A (en) Sleeve valve for resonance combustion apparatus
US1340846A (en) Feed-water-regulator system
US1807514A (en) Radiator actuating mechanism
US2314524A (en) Cooling system
US2244418A (en) Fluid engine
US1794448A (en) Heating system
SU752109A1 (en) Balanced compensator