US2938535A - Liquid supply apparatus - Google Patents
Liquid supply apparatus Download PDFInfo
- Publication number
- US2938535A US2938535A US611536A US61153656A US2938535A US 2938535 A US2938535 A US 2938535A US 611536 A US611536 A US 611536A US 61153656 A US61153656 A US 61153656A US 2938535 A US2938535 A US 2938535A
- Authority
- US
- United States
- Prior art keywords
- fuel
- valve
- pump
- line
- zone
- 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
- 239000007788 liquid Substances 0.000 title description 12
- 239000000446 fuel Substances 0.000 description 36
- 239000012530 fluid Substances 0.000 description 10
- 230000008878 coupling Effects 0.000 description 8
- 238000010168 coupling process Methods 0.000 description 8
- 238000005859 coupling reaction Methods 0.000 description 8
- 238000009434 installation Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
- 239000003502 gasoline Substances 0.000 description 1
- 239000003350 kerosene Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/28—Liquid-handling installations specially adapted for fuelling stationary aircraft
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/6851—With casing, support, protector or static constructional installations
- Y10T137/6855—Vehicle
- Y10T137/6881—Automotive
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8158—With indicator, register, recorder, alarm or inspection means
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/85978—With pump
- Y10T137/85986—Pumped fluid control
- Y10T137/85994—Manual
Definitions
- LIQUID SUPPLY APPARATUS Filed Sept. 24, 1956 16 a 11 2 $2 JO 6 15 m LIQUID SUPPLY APPARATUS Norman Humphrey Brear, London, England, asslgnor'to The British Petroleum Company Limited, London,
- This invention relates to improved liquid supply apparatus. More particularly it relates to apparatus for the metered supply of liquid both to and from a storage tank.
- Fuel tanker vehicles are known in which the fuel is supplied from a storage tank, via a four way valve, to the suction side of a fuel supply pump, the fuel thereafter being passed through a pressure control valve, microfilter, air separator and fuel supply meter and again through said four way valve to a fuel supply hose.
- a pressure control valve microfilter, air separator and fuel supply meter and again through said four way valve to a fuel supply hose.
- the figure is a schematic diagram of a fluid supply system, embodying this invention.
- the apparatus may incorporate conventional auxiliary equipment such as pressure control valves, venturis, filters and air separators.
- the apparatus of the present invention is further illustrated with reference to the accompanying drawing which is a schematic diagram of a fuel supply installation of a fuel supply tanker vehicle suitable for the fuelling of aircraft with gasoline or kerosene.
- a bulk tank 1 of the fuel supply tanker vehicle is connected by valve 19 and line 2 to the suction side of a fuel discharge pump 3.
- fuel is passed through a pressure control valve 4, micro-filter 5 and air separator 6.
- a valve 7 To the delivery side of said air separator is connected a valve 7, a fuel returned meter 8 and fuel return line 9 by which fuel may be returned to tank 1.
- a line 10 from said air separator delivery side is con- 'nected to delivery meterl'l, fuel thence passing through manual valve 12, venturi 13and hose 14.
- a line is provided to the socket 15 of a self-sealing detachable coupling, that is, a coupling such that the components thereof are constructed to ensure that, after separation one from the other, the components do not permit the flow of liquids from the ends so exposed.
- the duplicate system is indicated on the drawing by the corresponding numerals with the sufiix a.
- a coupling component 16 is connected as required to either of sockets 15 and 15a or to a blind socket 15b. Coupling component 16 is connected by hose 17 and line 18 to line 2.
- venturis 13 and 13a are employed in conventional manner to operate pressure control valve 4.
- the fuel supply installation of the fuel supply tanker vehicle is operated in the following manner.
- valve 7 For the discharge of fuel from the vehicle bulk tank 1, coupling component 16 is attached to the blind socket 15b, thereby blanking off line 18. Valve 7 is closed. Valves 12 and 19 are opened whereby, on operation of pump 3, fuel is fed from tank 1 via valve 19, line 2, pump 3, valve 4, filter 5, separator 6, line 10, meter 11, valve 12, venturi 13 to hose 14. If desired valve 12a may be opened to provide similarly a supply of fuel to hose 14a.
- valve 7 For defuelling from hose 14, valve 7 is opened, valves 12, 12a and 19 are closed and coupling component 16 is connected to socket 15. On operation of pump 3, fuel is drawn from hose 14, via venturi 13, socket 15, coupling component 16, hose 17, line 18, line 2, pump 3, valve 4, filter 5, separator 6, valve 7, fuel returned meter 8, line 9 to tank 1.
- a fluid supply system capable of metering both the flow of fluid from a first zone to a second zone and from said second zone to said first zone and whereby inaccuracy of metering due to internal leakage of fluid within the apparatus is avoided at least during fluid flow in one direction, said system comprising a pump; a feed line including a shut-off valve for feeding fluid from said second zone to the suction side of said pump; a first meter for measuring fluid supplied to said first zone from said second zone, a first valve and a first line, said first line, in operation, connecting said first zone through said first meter and through said first valve to said delivery side of said pump, said first meter being between said first valve and the delivery side of said pump; a second meter for measuring fluid supplied to said second zone from said first zone, a second valve and a second line, said second line, in operation, connecting said second zone through said second meter and through said second valve to the delivery side of said pump, said second valve being between said second meter and the delivery side of said pump; a third line I which
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Feeding And Controlling Fuel (AREA)
Description
May 31, 1960 N. H. BREAR 2,938,535
LIQUID SUPPLY APPARATUS Filed Sept. 24, 1956 16 a 11 2 $2 JO 6 15 m LIQUID SUPPLY APPARATUS Norman Humphrey Brear, London, England, asslgnor'to The British Petroleum Company Limited, London,
England, a British joint stock corporation This invention relates to improved liquid supply apparatus. More particularly it relates to apparatus for the metered supply of liquid both to and from a storage tank.
Fuel tanker vehicles are known in which the fuel is supplied from a storage tank, via a four way valve, to the suction side of a fuel supply pump, the fuel thereafter being passed through a pressure control valve, microfilter, air separator and fuel supply meter and again through said four way valve to a fuel supply hose. By manipulation of said four way valve, the overall direction of flow of the fuel can be reversed whereby fuel is drawn through said hose to the suction side of the fuel supply pump, the fuel thereafter being passed through said pressure control valve, micro-filter, air separator and fuel supply meter and again through said four way valve to said storage tank. This system while providing for the use, both in supply from and return of fuel to storage, of a single fuel supply pump, fuel meter and auxiliary equipment is open to the disadvantage that, simultaneously, two fuel streams are passed through the four way valve. Any defect in the valve which leads to internal leakage will have the effect of recycling fuel through the fuel pump and hence through the fuel supply meter, leading to inaccurate record of the amount of fuel transferred.
It is an object of the present invention to provide a liquid supply apparatus capable of metering both the flow of fluid from a zone A to a zone B and from zone B to zone A under the action of a pump whereby inaccuracy of metering due to internal leakage of fluid within the apparatus is avoided.
It is a further object of the present invention to provide apparatus for the metered supply of liquid, said apparatus being capable of use for the transference of liquid either to or from storage, which ensures that no inaccuracies of metering arise from recycle of supplied liquid through the metering stage when transferring the liquid from storage.
Further objects will appear from the following description, the accompanying drawing and the appended claims.
Of the drawing:
The figure is a schematic diagram of a fluid supply system, embodying this invention.
The apparatus may incorporate conventional auxiliary equipment such as pressure control valves, venturis, filters and air separators.
The apparatus of the present invention is further illustrated with reference to the accompanying drawing which is a schematic diagram of a fuel supply installation of a fuel supply tanker vehicle suitable for the fuelling of aircraft with gasoline or kerosene.
With reference to said drawing:
A bulk tank 1 of the fuel supply tanker vehicle is connected by valve 19 and line 2 to the suction side of a fuel discharge pump 3. From the delivery side of said nited States Patent O Patented May 31, 1960 2 pump, fuel is passed through a pressure control valve 4, micro-filter 5 and air separator 6. To the delivery side of said air separator is connected a valve 7, a fuel returned meter 8 and fuel return line 9 by which fuel may be returned to tank 1.
To the delivery side of said air separator is also connested in duplicate the following system:
A line 10 from said air separator delivery side is con- 'nected to delivery meterl'l, fuel thence passing through manual valve 12, venturi 13and hose 14. Between valve 12 and venturi 13 a line is provided to the socket 15 of a self-sealing detachable coupling, that is, a coupling such that the components thereof are constructed to ensure that, after separation one from the other, the components do not permit the flow of liquids from the ends so exposed.
The duplicate system is indicated on the drawing by the corresponding numerals with the sufiix a.
A coupling component 16 is connected as required to either of sockets 15 and 15a or to a blind socket 15b. Coupling component 16 is connected by hose 17 and line 18 to line 2.
The venturis 13 and 13a are employed in conventional manner to operate pressure control valve 4.
With further reference to the drawing, the fuel supply installation of the fuel supply tanker vehicle is operated in the following manner.
For the discharge of fuel from the vehicle bulk tank 1, coupling component 16 is attached to the blind socket 15b, thereby blanking off line 18. Valve 7 is closed. Valves 12 and 19 are opened whereby, on operation of pump 3, fuel is fed from tank 1 via valve 19, line 2, pump 3, valve 4, filter 5, separator 6, line 10, meter 11, valve 12, venturi 13 to hose 14. If desired valve 12a may be opened to provide similarly a supply of fuel to hose 14a.
Since no physical connection exists at 15 or 15a it is impossible for fuel, once metered to recycle to the pump 3.
For defuelling from hose 14, valve 7 is opened, valves 12, 12a and 19 are closed and coupling component 16 is connected to socket 15. On operation of pump 3, fuel is drawn from hose 14, via venturi 13, socket 15, coupling component 16, hose 17, line 18, line 2, pump 3, valve 4, filter 5, separator 6, valve 7, fuel returned meter 8, line 9 to tank 1.
For defuelling from hose 14a, similar procedure is followed except that coupling component 16 is attached to socket 151:.
I claim:
1. A fluid supply system capable of metering both the flow of fluid from a first zone to a second zone and from said second zone to said first zone and whereby inaccuracy of metering due to internal leakage of fluid within the apparatus is avoided at least during fluid flow in one direction, said system comprising a pump; a feed line including a shut-off valve for feeding fluid from said second zone to the suction side of said pump; a first meter for measuring fluid supplied to said first zone from said second zone, a first valve and a first line, said first line, in operation, connecting said first zone through said first meter and through said first valve to said delivery side of said pump, said first meter being between said first valve and the delivery side of said pump; a second meter for measuring fluid supplied to said second zone from said first zone, a second valve and a second line, said second line, in operation, connecting said second zone through said second meter and through said second valve to the delivery side of said pump, said second valve being between said second meter and the delivery side of said pump; a third line I which, in operation, is connected to the suction side of 2. A liquid supply installation comprising the apparams according to claim 1 wherein said second zone is massest 5.
2. storage tank, said storage being connected to said second line downstream of said secondmentand to the suction side of said Qump.
References Cited in the file of this patent UNITED STATESv PATENTS' 1,522,752 ishicld ;.;.,'.;T1an. 13, 1925 505 911 H V May 9, 1950 "2,507,597 -Mayf16, 1950 2,525,074 Qct. -10, 1,950 2,537,266 -4 J'ali.'9, 1951 2,747,733 wOO1dridge May 29, 1956 2,781,798 McGovern .Feb, 19, 1951
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2938535X | 1955-09-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2938535A true US2938535A (en) | 1960-05-31 |
Family
ID=10918181
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US611536A Expired - Lifetime US2938535A (en) | 1955-09-28 | 1956-09-24 | Liquid supply apparatus |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2938535A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3111968A (en) * | 1960-07-11 | 1963-11-26 | Richard T Headrick | Apparatus for transporting fluids |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1522752A (en) * | 1923-01-19 | 1925-01-13 | Augustine Davis Sr | Pumping apparatus for tanks |
| US2506911A (en) * | 1945-08-03 | 1950-05-09 | Phillips Petroleum Co | Pump for tractor-drawn trailer tanks |
| US2507597A (en) * | 1945-01-22 | 1950-05-16 | Erie Meter Systems Inc | Airport fueling system |
| US2525074A (en) * | 1945-09-14 | 1950-10-10 | Esso Exp Corp | Airport fueling system |
| US2537266A (en) * | 1947-01-18 | 1951-01-09 | Albert J Granberg | Airplane fueling system |
| US2747783A (en) * | 1951-07-12 | 1956-05-29 | Shell Dev | Liquid dispensing and withdrawing apparatus |
| US2781798A (en) * | 1953-04-10 | 1957-02-19 | Mojonnier Bros Co | Milk pumping apparatus |
-
1956
- 1956-09-24 US US611536A patent/US2938535A/en not_active Expired - Lifetime
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1522752A (en) * | 1923-01-19 | 1925-01-13 | Augustine Davis Sr | Pumping apparatus for tanks |
| US2507597A (en) * | 1945-01-22 | 1950-05-16 | Erie Meter Systems Inc | Airport fueling system |
| US2506911A (en) * | 1945-08-03 | 1950-05-09 | Phillips Petroleum Co | Pump for tractor-drawn trailer tanks |
| US2525074A (en) * | 1945-09-14 | 1950-10-10 | Esso Exp Corp | Airport fueling system |
| US2537266A (en) * | 1947-01-18 | 1951-01-09 | Albert J Granberg | Airplane fueling system |
| US2747783A (en) * | 1951-07-12 | 1956-05-29 | Shell Dev | Liquid dispensing and withdrawing apparatus |
| US2781798A (en) * | 1953-04-10 | 1957-02-19 | Mojonnier Bros Co | Milk pumping apparatus |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3111968A (en) * | 1960-07-11 | 1963-11-26 | Richard T Headrick | Apparatus for transporting fluids |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| DE69834336T2 (en) | TRANSMISSION DEVICE FOR CRYOGENEOUS LIQUIDS | |
| US2487863A (en) | Tank car unloading system | |
| CN208087218U (en) | A kind of oil pumping system for large aircraft pot type tank service truck | |
| US11554948B2 (en) | Fuel control and distribution system and methods thereof | |
| US3392753A (en) | Apparatus for blending of additives into fluid streams | |
| DE102011117158A1 (en) | Tank system for a motor vehicle and operating method therefor | |
| CN110030488A (en) | A kind of transfusion system between LNG ship oceangoing ship and LNG tank case (or tank car) | |
| US2938535A (en) | Liquid supply apparatus | |
| CN104445038A (en) | Small underground oil depot | |
| DE19546659C2 (en) | Device for refueling a vehicle | |
| CN209761596U (en) | Fuel oil system with fault diagnosis and detection functions | |
| US2145132A (en) | Apparatus for blending liquids | |
| CN207178075U (en) | A kind of oil pump oil circuit and diesel car | |
| GB930166A (en) | Fueling system for transferring fuel between reservoir means and vehicle fuel tanks | |
| US2459807A (en) | Multiple tank fuel system with emergency pump to maintain required discharge pressure | |
| DE102016226316B4 (en) | LPG tank cooling system of a dual fuel vehicle | |
| DE112019004631B4 (en) | Ventilation system for a vehicle with liquefied natural gas cryogenic tanks | |
| US3319645A (en) | Bottom loading system for tank trucks and trailers | |
| CN206191269U (en) | Immersed pump supercharging device of LNG gas station | |
| US2864410A (en) | Tandem valve arrangement for use with an eductor defueling system | |
| DE69003982T2 (en) | System for filling vehicles with petroleum products. | |
| CN207005721U (en) | Two-way gas pressure regulating station | |
| US11111126B2 (en) | Methods and systems for on demand fuel supply | |
| CN109826711A (en) | Aero-engine fuel oil supply system | |
| DE2946176A1 (en) | METHOD AND DEVICE FOR DISTRIBUTING NATURAL GAS |