WO2005066591A1 - Fuel tank level monitoring system and method - Google Patents
Fuel tank level monitoring system and method Download PDFInfo
- Publication number
- WO2005066591A1 WO2005066591A1 PCT/US2004/040056 US2004040056W WO2005066591A1 WO 2005066591 A1 WO2005066591 A1 WO 2005066591A1 US 2004040056 W US2004040056 W US 2004040056W WO 2005066591 A1 WO2005066591 A1 WO 2005066591A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- fuel
- tank
- level
- volume
- expended
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
- G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
- G01F1/05—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects
- G01F1/20—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects by detection of dynamic effects of the flow
- G01F1/206—Measuring pressure, force or momentum of a fluid flow which is forced to change its direction
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
- G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
- G01F1/05—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects
- G01F1/20—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects by detection of dynamic effects of the flow
- G01F1/28—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects by detection of dynamic effects of the flow by drag-force, e.g. vane type or impact flowmeter
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
- G01F9/00—Measuring volume flow relative to another variable, e.g. of liquid fuel for an engine
- G01F9/008—Measuring volume flow relative to another variable, e.g. of liquid fuel for an engine where the other variable is the flight or running time
Definitions
- This disclosure generally relates to fuel delivery systems and, more particularly, to systems for monitoring a remaining fuel level in a fuel supply tank.
- the consumers are supplied propane gas from a tank of liquefied propane.
- the tank is typically isolated from any established fuel pipelines, and therefore must be periodically refilled.
- a float level sensor is used in the propane tank to monitor the liquefied propane level.
- the user periodically views the tank level sensor and then requests delivery of replacement propane as required. While such fuel level sensors which are mounted in the tank can provide a reliable indication of the liquefied propane level remaining in the tank, they are difficult to maintain and time- consuming to repair when needed in view of their placement within the tank itself.
- a propane tank level monitoring system which can not only sense and display the level liquefied propane in the tank, but which can also provide a signal to a central location to use the information to track gas usage rate and to schedule delivery of replacement fuel as needed.
- an in-line gas flow rate sensor for sensing the gas flow rate from which the level of the propane remaining in the tank can be derived.
- Fig. 1 is a schematic diagram of a propane gas tank distribution system incorporating an in-line flow rate sensor according to the present invention
- Fig. 2 is a schematic diagram illustrating an in-line flow rate sensor according to the present invention including an in-line flow tube
- Fig. 3 is a cross sectional view illustrating a gas flow rate sensor in accordance with the present invention
- Fig. 4 is a schematic diagram of an alternative gas fuel distribution system
- Fig. 1 is a schematic diagram of a propane gas tank distribution system incorporating an in-line flow rate sensor according to the present invention
- Fig. 2 is a schematic diagram illustrating an in-line flow rate sensor according to the present invention including an in-line flow tube
- Fig. 3 is a cross sectional view illustrating a gas flow rate sensor in accordance with the present invention
- Fig. 4 is a schematic diagram of an alternative gas fuel distribution system
- Fig. 1 is a schematic diagram of a propane gas tank distribution system incorporating an in-line flow rate sensor according to the present invention
- FIG. 5 is a flow chart illustrating steps for measuring gas fuel flow rate and scheduling delivery of additional gas fuel to the tank.
- a propane gas distribution system 10 which includes a tank 12 containing a supply of propane gas.
- a pressure regulator 14 regulates the gas pressure in a supply conduit 16 which is coupled to an in-line flow rate sensor 18.
- the gas flow output of the flow rate sensor 18 is coupled on an outlet conduit 20 to users 21 of the propane gas.
- the gas flow rate sensor 18 includes a communication link to provide a signal on output line 22 representing the gas flow rate which signal is coupled to a report station 24.
- the report station 24 uses the gas flow rate information to determine the level of propane remaining within the propane tank 12 and can then schedule delivery of replacement gas to the tank 12 as needed.
- Figure 2 schematically illustrates the in-line gas flow rate sensor 18 in accordance with the present invention which includes a flow tube 26 and an auxiliary housing 28 mounted on the flow tube 26:
- a movable magnet 30 is mounted within the flow tube 26 and acted upon by the gas flow from conduit 16 to provide a changing flux density in response to the changing gas flow rate.
- a magnetic sensor is mounted within the flow tube 26 and acted upon by the gas flow from conduit 16 to provide a changing flux density in response to the changing gas flow rate.
- a pressure sensor 34 is mounted in the flow tube to detect the pressure of the gas inlet from inlet conduit 16.
- a temperature sensor 36 is mounted in the auxiliary housing 28 to detect the gas temperature.
- the respective outputs of the magnetic sensor 32, pressure sensor 34 and temperature sensor 36 are coupled to a communications link 37 for supplying the corresponding information on output line 22 to the report station 24. With this information the gas flow rate can be obtained using a well known algorithm, such as the Universal Gas Sizing Equation, and the level of gas remaining in the tank 12 also can be readily obtained.
- the flow tube 26 includes an inlet tube 38 and an outlet tube 40 which are threadably joined together by an orifice guide 42.
- the inlet tube 38, the outlet tube 40, and the orifice guide 42 are all formed of a non-magnetic metal such as brass or aluminum.
- a flow plate 44 is formed of a plastic material and includes a series of flow holes 46 to evenly distribute the inlet gas flow from inlet conduit 16.
- a tapered plug 48 is mounted to the flow plate 44 by a threaded screw 49.
- a movable orifice member 50 includes a central opening 51 surrounding the tapered plug 48 with an upstream opening 51a being smaller than a downstream opening 51b so that the central opening 51 is outwardly diverging. As shown in Fig. 3 there is an increasing space between the tapered plug 48 and the central opening 51 in the downstream flow direction.
- a magnet member 52 is mounted to the orifice member 50 with a flexible diaphragm 54 having its inner perimeter inserted therebetween, and with the outer perimeter of the diaphragm mounted between the outlet tube 40 and the orifice guide 42.
- the magnet member 52 is slidably mounted within a cavity 56 provided in the outlet tube 40, so that with changing gas flow rates, the plug holder 50 and attached magnet member 52 slidably move within the cavity 56.
- a spring 58 is captured between the outlet tube 40 and the orifice member 50 and has sufficient resiliency to move the upstream opening 51a of the orifice member 50 to one end of the plug 48 as shown in Fig. 3 when there is no gas flow.
- the orifice member 50 and associated magnet member 52 is moved away from the closed position and eventually to a position with respect to the plug 48 representing a maximum gas flow rate position.
- the tapered plug 48 and the outwardly diverging central aperture are shaped so that there is a direct linear relationship provided between the change in the flow orifice (i.e., the space between the tapered plug 48 and the central opening 51) and the flow rate change. In other words, with the flow orifice closed as shown in Fig.
- plug 48 and the shape of the central opening 51 provides a linear relationship between the change in the magnetic flux density created by the movement of magnet 52 and the output from the magnetic sensor 32.
- plug 48 and central opening 51 may be termed an "equal percent plug" which provides an equal percent flow orifice, i.e., with each uniform increment of orifice member 50 there is provided a constant percent of flow change through the flow orifice.
- a linear relationship exists between the magnetic flux density and the output of the magnetic sensor 32 in response to a changing flow rate through the flow orifice.
- the central aperture was formed outwardly diverging at an angle of about 10 degrees, and the tapered plug was formed inwardly converging at an angle of about 6 degrees.
- a mounting port 60 in the inlet tube 38 enables mounting of the pressure sensor 34. Utilizing the output of the magnetic sensor 32, as well as the information from the pressure sensor 34 and the temperature sensor 36 enables the gas flow rate to be determined using an algorithm well known in the industry. Once the gas flow rate has been determined, the amount of gas remaining within propane tank 12 can readily be determined, and delivery of any replacement fuel can be scheduled as required.
- an alternative fuel supply system 100 is shown having a tank 102 for holding fuel, such as liquefied propane.
- the tank 102 maybe positioned at a remote location or may otherwise be isolated from access to an established fuel pipeline. Consequently, the tank 102 must be periodically refilled with fuel from a distribution center.
- the tank 102 includes an outlet 104 connected to a supply line 106 for delivering gas fuel to one or more users 108, and a pressure regulator 110 regulates the gas pressure in the supply line 106.
- a flow rate sensor such as flow measurement module 112 is provided for sensing gas fuel flow and generating an output providing fuel flow information.
- the regulator 110 and flow measurement module 112 are integrated to provide an intelligent pressure regulator, as disclosed in commonly owned U.S. Patent Nos. 6,178,997 and 6,539,315, the disclosures of which are incorporated herein by reference.
- the regulator 110 and flow rate sensor may be provided as separate components.
- the flow measurement module 112 includes a processor 113, a memory 115, and a communication link 114 for providing a signal on an output line 116.
- a report station 118 which may be positioned remote from the flow measurement module 112 such as at a fuel distribution center, is communicatively coupled to the communication link 114 via the output line 116.
- the report station 118 may include a controller 120 having a memory 122.
- the report station 118 receives the fuel flow information and schedules delivery of replacement gas to the tank 102 as needed.
- the propane is stored in the tank 102 as a liquid.
- the tank may require pressurization to maintain the propane in the liquid state.
- Fig. 5 is a flow chart of a method for monitoring the level of fuel in the tank and scheduling delivery of additional fuel to the tank that may be executed by the fuel distribution system 100.
- a tank capacity is stored in memory. Where the flow rate sensor includes a processor and memory, such as with the flow measurement module 112, the tank capacity may be stored in either the flow measurement module memory 115 or the report station controller memory 122, or both.
- the rate of gas fuel flow through the supply line 106 is measured.
- the flow rate may be obtained using any known method or device.
- the flow rate is inferred using a standard flow equation and measured process parameters such as upstream and downstream fluid pressure and throttling element position.
- the report station controller 120 may be programmed with the flow equation, and the flow measurement module 112 may simply forward the measured parameters to the controller 120.
- an expended volume of fuel is calculated at block 154. Again, the expended volume may be calculated by the flow measurement module 112 or by the report station controller 120.
- the remaining fuel level in the tank is determined.
- the remaining fuel level may be calculated by subtracting the expended fuel volume from the stored tank capacity.
- the expended fuel volume may first be converted from a gas volume to a liquid volume to determine the remaining liquid volume of propane in the tank 102.
- the liquid volume capacity may be converted to a gas volume capacity, and the expended fuel volume may be subtracted from the gas volume capacity of the tank 102.
- a low fuel alarm may be generated at block 158. The low fuel alarm may be generated when the remaining fuel level corresponds to a user-entered low level limit.
- the report station 118 may schedule a delivery of additional fuel to the tank at block 160.
- the new delivery may be scheduled in response to the low fuel alarm, and will typically be prompted by the report station controller 120.
- various devices may be employed as the flow rate sensor, each of which may generate different fuel flow information.
- the flow rate sensor may simply detect upstream fluid pressure, downstream fluid pressure, and regulator throttling element position. These measured variables may then be forwarded to the report station 118, which may be programmed to calculate flow rate based on the variables. Alternatively, the flow sensor may sense the process variables and calculate the fuel flow rate, which is then forwarded to the report station 118.
- the report station 118 may calculate a total volume of expended gas fuel and a remaining fuel level in the tank. Still further, where the flow rate sensor includes a microprocessor, such as with the flow measurement module 112, it may execute each of the calculations noted above and forward only the low fuel level alarm to the report station 118. Alternatively, the flow rate sensor may calculate fuel flow and the expended fuel volume and forward the expended fuel volume to the report station 118.
- the report station may include a memory having the tank volume capacity and low fuel level stored thereon, and therefore may calculate the remaining tank volume and generate a low fuel alarm as appropriate. In addition to generating flow rate information for determining the remaining fuel level in the tank, the flow sensor may forward additional information to the report station 118 for other diagnostic purposes.
- the flow sensor may include a memory for storing high and low pressure limits, logic based alarm conditions, or other process control parameters that may indicate faulty system equipment or abnormal operating conditions, such as those disclosed in commonly owned U.S. Patent No. 6,441,744, which is incorporated herein by reference.
- the flow measurement module 112 may generate alarms based on these parameters and forward the alarms to the report station 118, which may respond by scheduling a maintenance visit for the gas fuel system.
Abstract
Description
Claims
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA2546993A CA2546993C (en) | 2003-12-22 | 2004-12-01 | Fuel tank level monitoring system and method |
EP04812552A EP1697701A1 (en) | 2003-12-22 | 2004-12-01 | Fuel tank level monitoring system and method |
AU2004312759A AU2004312759B2 (en) | 2003-12-22 | 2004-12-01 | Fuel tank level monitoring system and method |
BRPI0417642-1A BRPI0417642A (en) | 2003-12-22 | 2004-12-01 | method of monitoring a liquid fuel level in a tank and fuel tank system to store a fuel in a liquid state and provide the fuel in a gaseous state |
JP2006547025A JP2007518943A (en) | 2003-12-22 | 2004-12-01 | Fuel tank level monitoring system and method |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/743,212 US7197407B2 (en) | 2001-02-02 | 2003-12-22 | Fuel tank level monitoring system and method |
US10/743,212 | 2003-12-22 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2005066591A1 true WO2005066591A1 (en) | 2005-07-21 |
Family
ID=34749208
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2004/040056 WO2005066591A1 (en) | 2003-12-22 | 2004-12-01 | Fuel tank level monitoring system and method |
Country Status (10)
Country | Link |
---|---|
US (1) | US7197407B2 (en) |
EP (1) | EP1697701A1 (en) |
JP (2) | JP2007518943A (en) |
CN (1) | CN1890539A (en) |
AR (1) | AR046896A1 (en) |
AU (1) | AU2004312759B2 (en) |
BR (1) | BRPI0417642A (en) |
CA (1) | CA2546993C (en) |
RU (1) | RU2427806C2 (en) |
WO (1) | WO2005066591A1 (en) |
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US20060243347A1 (en) * | 2005-04-02 | 2006-11-02 | Humphrey Richard L | System for monitoring propane or other consumable liquid in remotely located storage tanks |
US7937216B2 (en) * | 2004-04-03 | 2011-05-03 | Humphrey Richard L | System for monitoring propane or other consumable liquid in remotely located storage tanks |
US7295919B2 (en) * | 2004-04-03 | 2007-11-13 | Nas Corp. | System for delivering propane or other consumable liquid to remotely located storage tanks |
JP4619685B2 (en) * | 2004-05-07 | 2011-01-26 | 矢崎総業株式会社 | Liquid level sensor using float and liquid level detection method using float |
US20060272405A1 (en) * | 2005-06-07 | 2006-12-07 | Lajos Feher | Casing for in-tank hall effect sensor used for fuel level sensing |
US7581516B2 (en) * | 2005-11-18 | 2009-09-01 | Matthew Snow | Water/alcohol injection flow switch safety device |
US20070181126A1 (en) * | 2006-02-08 | 2007-08-09 | Tolmie Craig R | Method and apparatus for ventilating a patient with a breathing gas mixture formed from nitric oxide, air, and oxygen |
US9035781B2 (en) | 2007-12-29 | 2015-05-19 | Waterstrike Incorporated | Apparatus and method for automatically detecting and alerting of gas-out conditions for a gas appliance during operation |
US8442783B2 (en) * | 2008-08-15 | 2013-05-14 | Peter Piszko | Method of and apparatus for recording fuel supplied to a vehicle |
US8249829B2 (en) * | 2009-05-20 | 2012-08-21 | Honeywell International Inc. | Online condition-based monitoring for tank farms |
US8653979B2 (en) * | 2010-04-13 | 2014-02-18 | Valerie A. Obenchain | Gas flow and pressure error alarm |
US10821243B2 (en) | 2010-04-13 | 2020-11-03 | Advanced Interactive Response Systems, LLC | Gas supply warning and communication system |
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US8984934B2 (en) * | 2013-03-13 | 2015-03-24 | Ford Global Technologies, Llc | Method and system to validate a fuel level indicator in a vehicle |
US9454856B2 (en) * | 2014-01-21 | 2016-09-27 | GM Global Technology Operations LLC | Liquefied petroleum gas tank leak detection systems and methods |
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CN104482982A (en) * | 2014-12-27 | 2015-04-01 | 中航电测仪器股份有限公司 | Method and device for detecting capacity of cryogenic liquid gas storage tank or gas cylinder |
US10060781B2 (en) * | 2015-08-05 | 2018-08-28 | The Boeing Company | Methods and systems for direct fuel quantity measurement |
CN105715423A (en) * | 2016-01-27 | 2016-06-29 | 郭一凡 | Marine ship fuel management system |
US11017344B2 (en) | 2016-09-12 | 2021-05-25 | Ecolab Usa Inc. | Method and apparatus for predicting depletion of deionization tanks and optimizing delivery schedules |
WO2018051159A1 (en) * | 2016-09-16 | 2018-03-22 | Carrier Corporation | Fuel system control for refrigeration unit engine |
CN106370267A (en) * | 2016-11-10 | 2017-02-01 | 歌思(天津)低温设备有限公司 | Gasification device |
WO2018156699A1 (en) | 2017-02-23 | 2018-08-30 | Carrier Corporation | Fuel leak detection in a gaseous fueled transportation refrigeration unit |
CN107339607A (en) * | 2017-08-31 | 2017-11-10 | 王翔鹏 | A kind of fuel delivery mode |
EP3720807A4 (en) * | 2017-12-08 | 2021-07-14 | Klatu Networks, Inc. | Monitoring and predicting failures of specialty equipment including liquid gas storage systems |
GB2572536A (en) * | 2018-03-08 | 2019-10-09 | Linde Ag | Gas cylinder flow monitoring |
US11209852B2 (en) * | 2018-03-20 | 2021-12-28 | Steffes Corporation | Flow-based energy management |
EP3833572B1 (en) * | 2018-08-10 | 2023-03-29 | Carrier Corporation | Crash detection system for transport refrigeration units |
RU198459U1 (en) * | 2019-12-09 | 2020-07-10 | Александра Валерьевна Паршина | DEVICE FOR CONTROL AND MONITORING OF PROCEDURES FOR DRAINING AND FILLING OF LIQUID PRODUCTS IN THE TANK RESERVOIRS |
US11859767B2 (en) * | 2020-05-04 | 2024-01-02 | Centri Group Inc. | Method and system for remotely monitoring fluid levels |
US11841138B2 (en) | 2021-03-01 | 2023-12-12 | Fivovos, LLC | Fuel tank monitoring systems and methods |
US11820221B2 (en) * | 2021-06-29 | 2023-11-21 | Nissan North America, Inc. | Vehicle fuel level estimation |
CN113551149A (en) * | 2021-07-26 | 2021-10-26 | 上海中船船舶设计技术国家工程研究中心有限公司 | Local monitoring system and method for marine mobile fuel tank |
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2003
- 2003-12-22 US US10/743,212 patent/US7197407B2/en not_active Expired - Lifetime
-
2004
- 2004-12-01 CA CA2546993A patent/CA2546993C/en active Active
- 2004-12-01 EP EP04812552A patent/EP1697701A1/en not_active Ceased
- 2004-12-01 JP JP2006547025A patent/JP2007518943A/en active Pending
- 2004-12-01 BR BRPI0417642-1A patent/BRPI0417642A/en not_active Application Discontinuation
- 2004-12-01 AU AU2004312759A patent/AU2004312759B2/en active Active
- 2004-12-01 CN CNA2004800363809A patent/CN1890539A/en active Pending
- 2004-12-01 RU RU2006126629/28A patent/RU2427806C2/en not_active IP Right Cessation
- 2004-12-01 WO PCT/US2004/040056 patent/WO2005066591A1/en active Application Filing
- 2004-12-15 AR ARP040104676A patent/AR046896A1/en not_active Application Discontinuation
-
2011
- 2011-09-15 JP JP2011201783A patent/JP2012017856A/en active Pending
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US6441744B1 (en) * | 1999-06-29 | 2002-08-27 | Fisher Controls International, Inc. | Regulator diagnostics system and method |
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Also Published As
Publication number | Publication date |
---|---|
US20040204870A1 (en) | 2004-10-14 |
EP1697701A1 (en) | 2006-09-06 |
CA2546993C (en) | 2011-04-19 |
JP2007518943A (en) | 2007-07-12 |
US7197407B2 (en) | 2007-03-27 |
CN1890539A (en) | 2007-01-03 |
RU2006126629A (en) | 2008-01-27 |
JP2012017856A (en) | 2012-01-26 |
RU2427806C2 (en) | 2011-08-27 |
AR046896A1 (en) | 2005-12-28 |
CA2546993A1 (en) | 2005-07-21 |
AU2004312759A1 (en) | 2005-07-21 |
AU2004312759B2 (en) | 2010-03-25 |
BRPI0417642A (en) | 2007-03-27 |
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