Effects of injection pressure and length-diameter ratio on the velocity and cavitation inside injector nozzle

Sadhana ◽  
2021 ◽  
Vol 46 (1) ◽  
Author(s):  
Changhyuk Kim ◽  
Zhendong Liu ◽  
Jeonghoon Lee
Author(s):  
Andi Firdaus Sudarma ◽  
Hadi Pranoto ◽  
Mardani A. Sera ◽  
Amiruddin Aziz

The use of diesel engines for vehicle applications has expanded for decades. However, it produces black smoke in the form of particulate matter contains fine and invisible particles during operation. The popular method for measuring the smoke opacity is by using a smoke meter for its simplicity and less costly. Fuel injection pressure is one of the parameters that affect the emission significantly, and the proper nozzle adjustment can reduce the density of exhaust gases and improve the engine performance. The purpose of this study is to determine the optimum fuel spray pressure that produces the lowest opacity value and analyse the effect of fuel spray pressure on the opacity value at a different engine speed. The present experiment uses the Hyundai D4BB engine, and the pressure variations were implemented on the injector nozzle at 125, 130, and 135 kg/cm2. The engine was also tested with various engine idle speed, i.e., 1000, 1500, 2000, and 2500 rpm. It has been found that the optimum distance of fuel spraying is 147.679 mm with injector nozzle pressure 130 kg/cm2, and the value of opacity is 9.51%.


2020 ◽  
Vol 10 (2) ◽  
pp. 549
Author(s):  
Sang-Wook Han ◽  
Yun-Sub Shin ◽  
Hyun-Chul Kim ◽  
Gee-Soo Lee

In this paper, a nozzle flow model was used to design an injector nozzle and obtain initial spray conditions for the dimethyl ether (DME) common rail-injection system. In order to deliver the same amount of energy as that provided by diesel at a low injection pressure of 50 MPa, the injector for DME needs nozzle holes with larger diameters and a higher SAC volume for the same injection duration. In addition, the needle lift and needle seat diameter should be increased to maintain a minimum flow area ratio. Although the vapour pressure and maximum injection pressure of DME are lower than those of diesel, the nozzle in a DME system showed higher discharge coefficients and effective nozzle exit diameters for the same injection duration owing to low kinematic viscosity. However, because the maximum injection pressure in DME is lower than that with diesel, and the length of the cavitation region is narrower.


Energies ◽  
2019 ◽  
Vol 12 (3) ◽  
pp. 434 ◽  
Author(s):  
Xinhai Li ◽  
Yong Cheng ◽  
Shaobo Ji ◽  
Xue Yang ◽  
Lu Wang

The accuracy of a nozzle diameter directly affects the difference of the injection characteristics between the holes and productions of a GDI (gasoline direct injection) injector. In order to reduce the difference and guarantee uniform injection characteristics, this paper carried out a CFD simulation of the effect of nozzle diameter which fluctuated in a small range on single-cycle fuel mass. The sensitivity of the fuel injection quantity to the injector nozzle diameter was obtained. The results showed that the liquid phase ratio at the nozzle outlet decreased and the velocity of the outlet increased with the increase of the nozzle diameter. When fluctuating in a small range of nozzle diameters, the sensitivity of the single-hole fuel mass to the nozzle diameter remained constant. The increase of the injection pressure lead to the increase of the sensitivity coefficient of the single-hole fuel mass to the nozzle diameter. The development of cavitation in the nozzle and the deviation of the fuel jet from the axis were aggravated with the increase of the injection pressure. However, the fluctuation in a small range of nozzles had little effect on the near-nozzle flow.


1992 ◽  
Vol 114 (1) ◽  
pp. 97-103 ◽  
Author(s):  
S. K. Chen ◽  
A. H. Lefebvre ◽  
J. Rollbuhler

The spray cone angles produced by several simplex pressure-swirl nozzles are examined using three liquids whose viscosities range from 0.001 to 0.012 kg/ms (1 to 12 cp). Measurements of both the visible spray cone angle and the effective spray cone angle are carried out over wide ranges of injection pressure and for five different values of the discharge orifice length/diameter ratio. The influence of the number of swirl chamber feed slots on spray cone angle is also examined. The results show that the spray cone angle widens with increase in injection pressure but is reduced by increases in liquid viscosity and/or discharge orifice length/diameter ratio. Variation in the number of swirl chamber feed slots between one and three has little effect on the effective spray cone angle.


Author(s):  
Christopher P. Kolodziej ◽  
Stephen A. Ciatti

Gasoline Compression Ignition (GCI) is a promising single-fuel advanced combustion concept for increased efficiency and reduced emissions in comparison with current conventional combustion modes. Gasoline fuels are advantageous in premixed combustion concepts because of their increased volatility and reduced reactivity compared to diesel. These qualities help reduce emissions of particulate matter (PM) and oxides of nitrogen (NOx), while making combustion phasing (and therefore combustion noise reduction) easier to manage. One of the challenges of using a gasoline with an anti-knock index (AKI) of 87 in a premixed combustion concept is being able to achieve stable low load operation. (Note that AKI is equivalent to (RON + MON)/2.) With such small injection quantities of a relatively more volatile and less reactive fuel than diesel, the injection timing of minimum load fueling needs to be early enough to allow the auto-ignition chemistry enough time, but late enough to keep the fuel from over-mixing and losing ignition propensity. The objective of this study was to investigate the advantages and disadvantages of reducing the injector nozzles’ inclusion angle from 148° to 120° on the combustion and emissions performance of GCI at 850 RPM and low load. To assess these effects, minimum fueling injection timing sweeps were performed with a 3% coefficient of variance of indicated mean effective pressure with each injector nozzle angle at 500 and 250 bar injection pressure. The results from these experiments revealed that both reduced injector nozzle angle and reduced injection pressure increased ignition propensity and allowed for reduced fueling and stable low load extension to 1 bar brake mean effective pressure using 87 AKI gasoline without any external boosting or heating. Combustion characteristics (such as noise) and emissions are discussed.


2016 ◽  
Vol 18 (8) ◽  
pp. 824-836 ◽  
Author(s):  
Janardhan Kodavasal ◽  
Christopher P Kolodziej ◽  
Stephen A Ciatti ◽  
Sibendu Som

In this work, we study the effects of injector nozzle inclusion angle, injection pressure, boost, and swirl ratio on gasoline compression ignition combustion. Closed-cycle computational fluid dynamics simulations using a 1/7th sector mesh representing a single cylinder of a four-cylinder 1.9 L diesel engine, operated in gasoline compression ignition mode with 87 anti-knock index (AKI) gasoline, were performed. Two different operating conditions were studied—the first is representative of idle operation (4 mg fuel/cylinder/cycle, 850 r/min), and the second is representative of a low-load condition (10 mg fuel/cylinder/cycle, 1500 r/min). The mixture preparation and reaction space from the simulations were analyzed to gain insights into the effects of injection pressure, nozzle inclusion angle, boost, and swirl ratio on achieving stable low-load to idle gasoline compression ignition operation. It was found that narrower nozzle inclusion angles allow for more reactivity or propensity to ignition (determined qualitatively by computing constant volume ignition delays) and are suitable over a wider range of injection timings. Under idle conditions, it was found that lower injection pressures helped to reduce overmixing of the fuel, resulting in greater reactivity and ignitability (ease with which ignition can be achieved) of the gasoline. However, under the low-load condition, lower injection pressures did not increase ignitability, and it is hypothesized that this is because of reduced chemical residence time resulting from longer injection durations. Reduced swirl was found to maintain higher in-cylinder temperatures through compression, resulting in better ignitability. It was found that boosting the charge also helped to increase reactivity and advanced ignition timing.


2015 ◽  
Vol 2015.68 (0) ◽  
pp. 223-224
Author(s):  
Sho MATSUDA ◽  
Noritsune KAWAHARADA ◽  
Daisaku SAKAGUCHI ◽  
Hironobu UEKI ◽  
Masahiro ISHIDA

1993 ◽  
Vol 115 (3) ◽  
pp. 447-452 ◽  
Author(s):  
S. K. Chen ◽  
A. H. Lefebvre ◽  
J. Rollbuhler

Measurements of circumferential liquid distribution are carried out over ranges of injection pressure from 0.34 to 1.72 MPa (50 to 250 psi) using five different simplex nozzles to achieve variations in the discharge orifice length/diameter ratio from 0.5 to 4.0. Two additional simplex nozzles of the same flow number are also examined in order to ascertain the effect of variations in the number of swirl chamber feed slots on circumferential liquid distribution. Mixtures of water and glycerine are used to provide a twelve to one variation in liquid viscosity. The results obtained show that spray uniformity improves markedly at higher injection pressures. Increase in liquid viscosity also has a beneficial effect on spray uniformity. The most uniform circumferential liquid distributions are obtained with nozzles having a discharge orifice length/diameter ratio of between 1 1/2 and 2.


2010 ◽  
Vol 97-101 ◽  
pp. 2925-2928 ◽  
Author(s):  
Zhi Xia He ◽  
Qing Mu Mu ◽  
Qian Wang ◽  
Jian Ping Yuan

The presence of cavitation and turbulence in a diesel injector nozzle has significant effect on the subsequent spray characteristics. However, the mechanism of the cavitating flow and its effect on the subsequent spray is unclear. The initiation, development and collapse of the cavity are strongly influenced not only by the injection pressure and back pressure but also by the nozzle geometry. The numerical simulation of cavitating flow in nozzle holes of a vertical multi-hole injector with mixture multi-phase cavitating flow model was carried out. The effects of sac geometry, hole entrance curvature radius and hole inclination angle on the cavitating flow in nozzle holes were investigated. It is finally concluded that the performance of IMPROVED nozzle is better than that of STD nozzle and VCO nozzle and small inlet turning angle of the orifice can enhance the atomization of the spray.


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