CN109631073B - Pumping pressure type water atomization mixing device and use method - Google Patents
Pumping pressure type water atomization mixing device and use method Download PDFInfo
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- CN109631073B CN109631073B CN201811343840.2A CN201811343840A CN109631073B CN 109631073 B CN109631073 B CN 109631073B CN 201811343840 A CN201811343840 A CN 201811343840A CN 109631073 B CN109631073 B CN 109631073B
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- water
- water injection
- valve
- water tank
- metering pump
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23K—FEEDING FUEL TO COMBUSTION APPARATUS
- F23K5/00—Feeding or distributing other fuel to combustion apparatus
- F23K5/02—Liquid fuel
- F23K5/08—Preparation of fuel
- F23K5/10—Mixing with other fluids
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23K—FEEDING FUEL TO COMBUSTION APPARATUS
- F23K2300/00—Pretreatment and supply of liquid fuel
- F23K2300/10—Pretreatment
- F23K2300/103—Mixing with other fluids
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Loading And Unloading Of Fuel Tanks Or Ships (AREA)
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Abstract
The invention belongs to the technical field of aviation test equipment, and particularly relates to a pumping pressure type water atomization mixing device and a use method thereof; the pump pressure formula moisture atomizing mixing device includes: the device comprises a water tank (2), a drain valve (3), an adjustable metering pump (4), a motor (5), a static mixer (6), an atomizing spray head (7), a fuel oil pipeline (8), a flowmeter I (9), a valve (10), a flowmeter II (11), a safety valve (12), an air tank (13) and a pressure gauge (14); the device is a core device for preparing oil for an aircraft fuel oil system icing test, can atomize water and uniformly mix the water into aviation fuel oil, and is not easy to generate layering, precipitation and accumulation phenomena; the device can measure, record and display parameters such as water injection quantity, water injection flow, water injection pressure and the like in real time, the water injection flow and the water injection quantity can be adjusted as required, and the device is simple in structure, reliable in function and convenient to move.
Description
Technical Field
The invention belongs to the technical field of aviation test equipment, and particularly relates to a pumping pressure type water atomization mixing device and a using method thereof.
Background
Aviation kerosene can be contaminated with moisture for a variety of reasons during storage, transportation, filling and use. If the oil storage container is not dry and has residual moisture, the sealing is not tight, rain, snow, ice and frost fall in the filling process, the condensation of water vapor and the like can cause the aviation kerosene to have some moisture, and the water exists in three possible forms of suspended water, dissolved water and free water.
The freezing point of aviation fuel is increased if the aviation fuel contains moisture. If the airplane flies in cold air temperature conditions for a long time, water in fuel oil can be frozen into ice, oil filters or filter screens can be blocked, accessories and systems can be disabled, fuel oil flowing to an engine can be slowed down or completely interrupted, and the engine can be flamed out, so that flight safety is endangered. GJB3577-99 'icing requirements and tests of aircraft fuel systems and accessories' has the following requirements on the icing of the fuel system:
the system works continuously: the fuel system should have the ability to continue operation when the fuel without the anti-icing additive is cooled to any temperature between-55 c at 27 c moisture saturation. The system works in emergency: the fuel without anti-icing additive is saturated at 27 ℃ with water, 0.2ml of free water is added per litre of fuel, and the fuel is cooled to the most critical icing conditions that may be encountered during operation, the fuel system should be able to allow the aircraft to continue flying for 30min at the minimum engine power required to not compromise flight safety. Meanwhile, the CCAR25 department requires that the fuel system for a turbine engine must be able to continue operating throughout its flow and pressure ranges when using fuel in the following conditions: the fuel was first saturated with water at 27 c and contained 2ml of free water added per 10 litres of fuel and then cooled to the most critical icing conditions likely to be encountered in operation.
Disclosure of Invention
The purpose of the invention is: in order to evaluate the low-temperature anti-icing performance of an aircraft fuel system and an engine, a set of device for adding water to aviation kerosene is required to be developed and used for preparing water-containing fuel for an icing test of the fuel system. The technical problem that water can stably exist in the kerosene in a saturated or super-saturated state cannot be solved.
In order to solve the technical problem, the technical scheme of the invention is as follows: .
A pump pressure type moisture atomizing and blending device, comprising: the device comprises a water tank 2, a drain valve 3, an adjustable metering pump 4, a motor 5, a static mixer 6, an atomizing nozzle 7, a fuel oil pipeline 8, a flowmeter I9, a valve 10, a flowmeter II 11, a safety valve 12, an air tank 13 and a pressure gauge 14; the water tank 2, the adjustable metering pump 4, the flowmeter II 11, the valve 10 and the atomizing nozzle 7 are connected together through a pipeline to form a water injection passage; the motor 5 is arranged on the adjustable metering pump 4; the adjustable metering pump 4 can adjust the flow speed of water; the drain valve 3 is arranged at the lowest position of the horizontal height between the water tank 2 and the valve 10 of the water filling passage and is used for draining water in the pipeline; the safety valve 12 and the air tank 13 are connected together through a pipeline to form a gas passage; one end of the gas passage is connected above the water tank 2, and the other end of the gas passage is connected between the adjustable metering pump 4 and the valve 10 on the water injection passage; the safety valve 12 is arranged between the air tank 13 and the water tank 2, a safety pressure is set on the safety valve 12, and when the pressure of the air tank is higher than the pressure, the pressure is relieved to the water tank 2; the pressure gauge 14 is arranged on the air tank 13 and used for indicating the pressure of the air tank; the atomizing nozzle 7 is arranged in a fuel oil pipeline 8; the static mixer 6 is arranged on the fuel pipeline 8 and is positioned at the downstream of the atomizer 7 and is used for stirring the fuel after being mixed with water, and the static mixer 6 can enable the water to be mixed again.
Preferably, the pumping pressure type water atomization blending device further comprises a water tank cover 1, the water tank cover 1 covers the water tank 2 for preventing dust, and weighed water can be added into the water tank 2 through the water tank cover 1.
Preferably, one end of the air passage is connected to a position which is not covered by the water level above the water tank 2.
The adjustable metering pump 4 can adjust the flow speed of water; because the water needed to be injected in the fuel test is less, and the water injection flow needs to be matched with the fuel flow, the adjustable metering pump 4 is adopted. If the air tank 13 is not provided, the atomizing nozzle 7 has a pulsating water outlet phenomenon, and the water injection flow and the pressure jump are increased, so that the air tank 13 is mainly used for buffering the pressure in a water injection pipeline to achieve the purpose of stable water injection.
The use method of the pumping type water atomization blending device comprises the following steps:
firstly, draining water in a water injection passage, adding fuel oil with the volume of Q into a water tank 2, starting an adjustable metering pump 4, and opening a valve 10 when the pressure indicated by a pressure gauge 14 reaches an empirical preset value;
then, the adjustable metering pump 4 is adjusted, and when the flow is stable, the weighed pure water is added into the water tank 2;
finally, calculating water injection time according to the water injection amount and the water injection flow, adding fuel oil with the volume Q for emptying water in a water injection pipeline when the working time of the adjustable metering pump 4 is close to the calculated water injection time, closing the adjustable metering pump 4 and the valve 10 after the added fuel oil with the volume Q is completely injected, opening the drain valve 3, and discharging the fuel oil in a water injection pipeline; the volume Q is larger than the volume of other pipelines on the water injection pipeline, which do not comprise the water tank 2.
The advantage of implementing fuel → water → fuel is that all water added to the tank can be filled into the fuel line, the actual water fill being the same as the planned water fill.
The invention has the technical effects that: the pumping pressure type water atomization mixing device has the functions of atomizing a certain amount of water and uniformly mixing the water into aviation fuel oil to finish the preparation of the water-containing fuel oil. The device has stable water injection flow and is easy to control; the water injection pressure is adjustable, and the atomization effect is good; blending again through a static mixer, and uniformly distributing water in the fuel oil; through a certain water injection step, the actual total water injection amount is consistent with the planned total water injection amount, and the purpose of accurate water injection is achieved. The whole device has the advantages of simple structure, strong reliability, accurate measurement, easy operation, convenient movement and good water injection effect.
Drawings
FIG. 1 is a schematic diagram of a pumping type water atomization blending device;
in the figure: 1-a water tank cover, 2-a water tank, 3-a drain valve, 4-an adjustable metering pump, 5-a motor, 6-a static mixer, 7-an atomizing nozzle, 8-a fuel pipeline, 9-a flowmeter I, 10-a valve, 11-a flowmeter II, 12-a safety valve, 13-an air tank and 14-a pressure gauge.
Detailed Description
Referring to fig. 1, the technical solution of the present invention is described in detail by the following embodiments:
the pumping pressure type water atomization mixing device has the functions of atomizing a certain amount of water and uniformly mixing the water into aviation fuel oil to finish the preparation of the water-containing fuel oil. The device mainly comprises the following components: the device comprises a water tank cover 1, a water tank 2, a drain valve 3, an adjustable metering pump 4, a motor 5, a static mixer 6, an atomizing nozzle 7, a fuel oil pipeline 8, a flowmeter I9, a valve 10, a flowmeter II 11, a safety valve 12, an air tank 13 and a pressure gauge 14.
The connection relation and the function of the device components are as follows:
the water tank 2, the adjustable metering pump 4, the flowmeter II 11, the valve 10 and the atomizing nozzle 7 are connected together through a pipeline to form a water injection passage; the motor 5 is arranged on the adjustable metering pump 4; the adjustable metering pump 4 can adjust the flow speed of water; the drain valve 3 is installed at the lowest position of the horizontal height between the water tank 2 and the valve 10 of the water filling passage and is used for draining water in the pipeline; the water tank cover 1 covers the water tank 2 for preventing dust, and weighed water can be added into the water tank 2 through the water tank cover 1.
The safety valve 12 and the air tank 13 are connected together through a pipeline to form a gas passage; one end of the gas passage is connected above the water tank 2, and the other end of the gas passage is connected between the adjustable metering pump 4 and the valve 10 on the water injection passage; the safety valve 12 is arranged between the air tank 13 and the water tank 2, and a safety pressure is set on the safety valve 12, and when the pressure of the air tank is higher than the pressure, the pressure is released to the water tank 2; a pressure gauge 14 is mounted on the air tank 13 for indicating the air tank pressure.
The atomizer 7 is installed in the fuel pipeline 8; a static mixer 6 is mounted on the fuel line 8 downstream of the atomizer head 7 for stirring the water-blended fuel, the static mixer 6 allowing the water to be re-blended.
The working steps of the device are as follows:
a) opening the drain valve 3 to drain the water in the pipeline;
b) closing the drain valve 3 and the valve 10, and adding fuel oil into the water tank 2;
c) starting the adjustable metering pump 4, and observing the pressure gauge 14;
d) when the pressure reaches 0.3MPa (the pressure is obtained according to the selected atomizing nozzle, so that the atomizing effect can be optimal), opening the valve 10;
e) observing the flowmeter I9 and the flowmeter II 11, and manually finely adjusting the adjustable metering pump 4 to enable the water injection flow to reach 1/1000 of the fuel flow;
f) when the flow is stable, 5L of purified water is weighed and added into the water tank 2;
g) observing the water tank 2, and adding 0.5L of fuel oil when water is about to be injected;
h) after the 2 nd fuel oil is added, closing the adjustable metering pump 4 and the valve 10, opening the drain valve 3, and discharging the fuel oil in the water injection pipeline;
i) and finishing water injection.
The present embodiment describes an implementation form of the technical mode of the present invention, and there are other implementation forms according to the design idea of the present invention, such as: the flowmeter II 11 is arranged between the water tank 2 and the valve 10 of the water injection passage; the position of the drain valve 3 is arranged at the lowest position of the horizontal height between the water tank 2 and the valve 10 of the water filling passage; the modification of the position of these components is within the scope of the present invention.
Claims (2)
1. The utility model provides a pumping pressure formula moisture atomizing mixing device which characterized in that: the pumping pressure type water atomization blending device comprises: the device comprises a water tank (2), a drain valve (3), an adjustable metering pump (4), a motor (5), a static mixer (6), an atomizing spray head (7), a fuel oil pipeline (8), a flowmeter I (9), a valve (10), a flowmeter II (11), a safety valve (12), an air tank (13) and a pressure gauge (14); the water tank (2), the adjustable metering pump (4), the flowmeter II (11), the valve (10) and the atomizing nozzle (7) are connected together through pipelines to form a water injection passage; the motor (5) is arranged on the adjustable metering pump (4); the drain valve (3) is arranged at the lowest position of the horizontal height between the water tank (2) and the valve (10) on the water injection passage; the safety valve (12) and the air tank (13) are connected together through a pipeline to form a gas passage; one end of the gas passage is connected above the water tank (2), and the other end of the gas passage is connected between the adjustable metering pump (4) and the valve (10) on the water injection passage; the safety valve (12) is arranged between the air tank (13) and the water tank (2); the pressure gauge (14) is arranged on the air tank (13); the atomizing nozzle (7) is arranged in the fuel pipeline (8); the static mixer (6) is arranged on the fuel pipeline (8) and is positioned at the downstream of the atomizing nozzle (7); the pumping pressure type water atomization blending device also comprises a water tank cover (1), and the water tank cover (1) is covered on the water tank (2); one end of the gas passage is connected above the water tank (2).
2. The method of using the pump water atomization blending device of claim 1, wherein: the use method of the pumping type water atomization blending device comprises the following steps:
firstly, draining water in a water injection passage, adding fuel oil with the volume of Q into a water tank (2), starting an adjustable metering pump (4), and opening a valve (10) when the pressure indicated by a pressure gauge (14) reaches an empirical preset value;
then, adjusting an adjustable metering pump (4), and adding the weighed purified water into the water tank (2) after the flow is stable;
finally, calculating water injection time according to the water injection amount and the water injection flow, adding fuel oil with the volume of Q for emptying water in the water injection pipeline when the working time of the adjustable metering pump (4) is close to the calculated water injection time, closing the adjustable metering pump (4) and the valve (10) after the added fuel oil with the volume of Q is completely filled, opening the drain valve (3), and discharging the fuel oil in the water injection pipeline; the volume Q is larger than the volume of other pipelines on the water injection pipeline, which do not comprise the water tank (2).
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CN201811343840.2A CN109631073B (en) | 2018-11-12 | 2018-11-12 | Pumping pressure type water atomization mixing device and use method |
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Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2183211Y (en) * | 1994-03-16 | 1994-11-23 | 汤民生 | Fuel-oil water-mixed emulsifying device |
CN203610057U (en) * | 2013-12-06 | 2014-05-28 | 中航商用航空发动机有限责任公司 | Low-temperature oil-water mixing device |
CN107781838A (en) * | 2016-08-30 | 2018-03-09 | 中国飞行试验研究院 | A kind of moveable pump pressure type atomized fuel water dispensing apparatus and decreasing water distribution method |
CN107792387A (en) * | 2016-08-30 | 2018-03-13 | 中国飞行试验研究院 | A kind of double atomizer water filling devices of piston type and application method |
-
2018
- 2018-11-12 CN CN201811343840.2A patent/CN109631073B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2183211Y (en) * | 1994-03-16 | 1994-11-23 | 汤民生 | Fuel-oil water-mixed emulsifying device |
CN203610057U (en) * | 2013-12-06 | 2014-05-28 | 中航商用航空发动机有限责任公司 | Low-temperature oil-water mixing device |
CN107781838A (en) * | 2016-08-30 | 2018-03-09 | 中国飞行试验研究院 | A kind of moveable pump pressure type atomized fuel water dispensing apparatus and decreasing water distribution method |
CN107792387A (en) * | 2016-08-30 | 2018-03-13 | 中国飞行试验研究院 | A kind of double atomizer water filling devices of piston type and application method |
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