improvement of spray characteristics in port injectors...generally, fuel injected by an injector...
TRANSCRIPT
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Keihin Technical Review Vol.2 (2013)
※Received28June2013,Reprintedwithpermission,fromSAEpaper2012-32-0071(JSAEpaper#20129071).Copyright©2012SAEInternationalandSAEofJapan.FurtheruseordistributionofthismaterialisnotpermittedwithoutpermissionfromSAEInternationalorSAEofJapan.
ポート噴射インジェクタより噴射される燃料噴霧は,エンジンの出力や燃焼効率に強い影響をあたえる.よって燃料を小さな油滴にする微粒化と,エンジンより受ける温度や負圧などの環境変化に依存しない正確な燃料供給が求められている.本報では,ニードルバルブとのシート部下流の徹底した圧力損失(エネルギーロス)の低減と噴孔位置の適正化による微粒化手法,及びシート部下流のデッドボリューム削減と燃料通路長短縮による温度や負圧の変化に依存しないインジェクタを紹介する.
Key Words: Fuel Injector, Atomization
Improvement of Spray Characteristics in Port Injectors※
ポートインジェクタにおける噴霧特性の向上
INTRODUCTION
Lately, there have been growing demands for
internal combustion engines for motorcycles and
other applications to have lower emissions, better fuel
economy and higher performance insusceptible to use
environments. This is because of skyrocketing fuel
prices and greater use of fuel injection systems under
stricter global-scale emission control regulations in
various countries including developing countries. As
part of such demands, injectors need to atomize fuel
spray for lower emissions and better fuel economy
and to minimize a variance in flow rate without being
susceptible to changes in temperature and negative
pressure so as to ensure a higher performance that is
unaffected by the use environments.
Our development focused on the following three
improvements for injectors.
(1) Atomization
(2) Minimization of change in temperature and flow
rate characteristics
(3) Minimization of negative pressure and under-seat
Technical paper
Junichi NAKAMURA*1 Akira AKABANE*2 Koji KITAMURA*1 Yuzuru SASAKI*1
中 村 順 一 赤羽根 明 北 村 浩 二 佐々 木 譲
flow rate characteristics
Various atomization techniques and flow rate
stabilization techniques have been developed and
put into practice. Among the currently available
techniques, this development focused on and modified
the structure located under the valve seat. Effects
of under-seat flow and pressure were clarified in
our existing injector structure so as to improve and
modify a flow path from the seat to the nozzle orifice.
1. Overview of injector for small motorcycles
Fig. 1 represents the structure of our gasoline
injector. When current flows through a coil, a core
of injector is vacuumed and a valve train integrated
with the core is lifted to open the valve as shown
in the figure. Next, fuel pressure applied by a fuel
pump delivers fuel through the opened seat and the
fuel is sprayed through multiple nozzle orifice laid
out in the plate.
On Fig. 2, the under-seat flow in the existing
*1DevelopmentDepartment3,R&DOperations *2DevelopmentDepartment1,R&DOperations
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Improvement of Spray Characteristics in Port Injectors
structure shows that fuel passes through the seat
toward the center of axis, then comes down to the
vertical hole area, and radially flows from the center
of axis to the counter bore. After entering the counter
bore, the fuel flows laterally along the plate located
under the counter bore. The plate has multiple nozzle
orifice laid out to deliver the required flow rate. At the
nozzle orifice in the plate, the laterally flowing fuel
rapidly changes its flow direction. Such rapid flow
direction change separates and pulls off the fuel from
the inner walls of nozzle orifice and forms a fuel film
with external air trapped in the space produced by
separation prior to spraying and diffusion.
Since the existing structure has a long fuel flow
path from the seat to the nozzle orifice and a large
dead volume, fuel often tends to drip out without
being atomized immediately after the valve opening
and closing stages in which a full fuel pressure is
not reached. Furthermore, fuel may be sprayed with
an improper particle size at the start of spraying
if the counter bore is filled up with fuel and fuel
separation is instable, such as when a change in fuel
temperature or negative pressure causes a variance
in dripping rate.
Fig. 4 represents a photo of the spray at the start
of injection. This photo shows that there are large
droplets at the start of injection. And, the graph of
spray particle size vs. time plotted in Fig. 5 reveals
poor atomization caused by a large particle size
of fuel dripping out at the start of injection. Also,
the distribution curve shown in Fig. 6 signifies the
distribution of large particle sizes.
Hole
Separate In inner wallsof nozzle orifice
Low High
Counter bore
Nozzle orifice
Plate
Flow direction
Seat
DeadVolume
Fig. 2 Fuel flow direction and pressure distribution
Fig. 3 Velocity in counter bore (flowing to the nozzle orifice)Model: 10-nozzle orifice
Nozzle orifice
Fig. 4 Current dripping
Initial dripping at injection
Fig. 1 Cross-section view of current Injector
Seat, valve
Fuel pressure
Moving Core
Power Supply
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Keihin Technical Review Vol.2 (2013)
As a long fuel path from the seat to the nozzle
orifice causes severe pressure loss, as shown in Fig.
7 resulting in a drop in fuel pressure applied by a
fuel pump before reaching the nozzle orifice, the
particle size of sprayed fuel eventually becomes
large. This is due to the lower effectiveness of air
entrapment and diffusion during fuel separation from
the hole wall as a consequence of a rapid change of
flow direction in the nozzle orifice.
Fig. 5 Change in particle size over time
Part
icle
siz
e [µ
m]
Time [ms]
0
50
100
150
200
250
0 2 4 6 8 10
Current model
Fig. 6 Particle size distribution of current model
0
5
10
15
20
0 100 200 300 400 500
Freq
uenc
y [%
]
Particle size [µm]
Current modelCurrent model
Fig. 7 Pressure loss and velocity of under-seat
0
10
20
30
200
250
300
350
Vel
ocity
(m
/s)
Pres
sure
(kP
a)
measurement positionValv
e sea
t hole
abov
e hole
sSea
t
Current-Pressure
Current-Velocity
Current-Pressure
Current-Velocity
Fig. 8 Change in the temperature and flow rate characteristics
-15.0%
-10.0%
-5.0%
0.0%
5.0%
10.0%
15.0%
10°C 30°C 50°C 70°C 90°C
Flow
rat
e ch
ange
[%
]
Fuel temperature [°C]
Current modelCurrent model
Fig. 9 Change in the negative pressure and flow rate characteristics
-20%
0%
20%
40%
Flow
rat
e ch
ange
[%
]
Pb [mmHg]0 200 400 600
Current model
Meanwhile, there was an issue of a change in the
temperature and flow rate characteristics. After the
valve closes, a lower pressure in the dead volume
boils the fuel. As the fuel cubically expands it is
pushed out. At higher fuel temperatures, a large dead
volume under the seat causes a variance in injection
rate in the event of a change in temperature (Fig. 8).
A change in negative pressure could also cause
a variance in the injection rate due to the aforesaid
effects of dead volume. At a higher negative
pressure from an engine, fuel flows out from the
dead volume (Fig. 9).
2. Approach to resolve issues
In light of the existing issues described under
section 1, an approach was selected and determined
based on the three mechanisms of injectors.
(1) Atomization: Shorter flow path from the seat
to nozzle orifice; minimized pressure loss and
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Improvement of Spray Characteristics in Port Injectors
facilitated separation in the nozzle orifice (liquid
film forming)
(2) Minimization of change in temperature and flow
rate characteristics: Smaller dead volume
(3) Minimization of change in negative pressure and
flow rate characteristics: Smaller dead volume
2-1. Atomization mechanism
Generally, fuel injected by an injector splits in
the process shown in Fig. 10. While the mechanism
shown in Fig. 10 is a generally known droplet
mechanism, instability of this process could be a
possible cause of failed atomization. As shown in
Fig. 2, the flow in the cylinder called a counter bore
goes into the nozzle orifice but the pattern of such
flow into the nozzle orifice varies depending on their
layout. This may prevent the optimum liquid film
from forming. As fuel separation in the nozzle orifice
depends on the intensity of the lateral flow above
the nozzle orifice, instability of one flow direction
obstructs the separation. Such instability means it is
hard to ensure a stable particle size in each nozzle
orifice as the liquid film forming is a passive process
that induces separation in the nozzle orifice and uses
air trapped in the separation area in the nozzle orifice.
As a method to ensure stable atomization, it was
determined to form an active flow that would induce
liquid film forming on the inner walls of nozzle
nozzle orifice.
2-2. Mechanisms of temperature/Negative pressure
and under-seat flow rate characteristics
Fig. 11 represents a vapor pressure curve
of gasoline. This graph signifies that gasoline
can remain in a liquid state at an atmospheric
pressure of 101.3 kPa and starts vaporizing at its
vapor pressure of 53.3 kPa or lower even under
atmospheric pressure. It is also shown that gasoline
starts vaporizing at a temperature of 38°C or higher
even in the atmosphere. This suggests that the
characteristics can be improved by setting a pre-spray
pressure under the injector valve seat through the
nozzle orifice to meet the requirement stated below.
The distribution of under-seat flow pressure in an
existing injector is shown below. As seen in Fig. 11,
the pressure decreases in the dead volume under
the seat and in the larger-diameter counter bore
to or below the aforesaid requirement. Apparently,
reducing the pressure loss through an improved dead
volume is effective as a countermeasure.
2-3. Method of approach and effectiveness
Atomization
Fig. 12 represents the improved under-seat layout
of this development. The developed layout shortens
the flow path from the seat to the nozzle orifice
and reduces the dead volume, which minimizes fuel
pressure loss before it reaches the nozzle orifice in
the plate. It also allows fuel flowing from the seat
Fig. 11 Vapor pressure curve of gasoline
0
20
40
60
80
100
-100 0 100 200
Vap
er p
ress
ure
(kPa
)
Temperature (°C)
101.3kPa
53.3kPa53.3kPa
24°C
Fig. 10 Process of atomization
Liquid filmforming(Thin film)
Liquid columnforming
Liquid dropletforming(Atomization)
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Keihin Technical Review Vol.2 (2013)
Fig. 15 Initial dripping at injection
(a) Current model (b) New model
Fig. 12 Cross-section of new injector under seat and flow direction
HighLow
Fig. 13 Comparison of layout
(a) Current model (b) New model
seat
Abovenozzle orifice
Abovenozzle orifice
seat
Valve seathole
Valve seathole
Above nozzle orifice
Table 1 Countermeasure
CURRENT1.2mm3
3.9mmDead volumeLength of flow path
NEW0.5mm3
1.2mm
Fig. 14 Comparison of pressure and velocity
0
10
20
30
200
250
300
350
Vel
ocity
(m
/s)
Pres
sure
(kP
a)
measurement position
New-PressureCurrent-PressureNew-VelocityCurrent-Velocity
New-PressureCurrent-PressureNew-VelocityCurrent-Velocity
Valve s
eat h
ole
abov
e hole
sSea
t
to meet the flow returning from the center of the
axis above the nozzle orifice, and drags fuel against
the inner wall of the nozzle orifice, forming a void
in the center of hole and facilitating liquid film
forming in the nozzle orifice. In addition, a smaller
dead volume allows for the aforesaid under-seat flow
immediately after spraying, which can minimize
initial and end dripping.
Fig. 12 illustrates a flow line of under-seat flow
as identified through fluid analysis of this layout.
As seen in Fig. 12, liquid-film-formed fuel at the
entrance to the nozzle orifice can actively form a
liquid film of fuel sprayed and induce atomization.
Temperature/Negative pressure and under-seat
flow rate characteristics
And as shown in Fig. 13, 14, the developed
injector can keep the under-seat pressure at a vapor
pressure of gasoline or higher and thus neither a
pressure decrease nor boiling occurs in the injector.
In addition, the pressure decrease point is located at
a post-spray point. These achievements minimize the
effects of variance in gasoline remaining in the dead
volume, which results in minimization of any change
or variance in the flow rate in comparison with the
currently achievable level even at high temperature
and/or negative pressure.
Moreover, a smal ler dead volume reduces
the time required to fill the dead volume with
fuel and contributes to both minimum (Table 1)
initial dripping and better injection responsiveness
(Fig. 15).
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Improvement of Spray Characteristics in Port Injectors
Table 2 Result of countermeasure
NEW CURRENT RESULT
64µm 85µm Improvement25%Atomization (S.M.D)
2% 9% Improvement77%
Temperature flow rate characteristics
+11.7% +28% Improvement58%
Negative pressure flow rate characteristics
Fig. 16 Comparison of change in particle size over time
0
50
100
150
200
250
0 2 4 6 8 10
Part
icle
siz
e [µ
m]
Time [ms]
New model
Current model
Fig. 17 Comparison of change in Particle size distribution
0
5
10
15
20
0 100 200 300 400 500
Freq
uenc
y [%
]
Particle size [µm]
New modelCurrent modelNew modelCurrent model
Fig. 18 Comparison of change in the temperature and flow rate characteristics
-15.0%
-10.0%
-5.0%
0.0%
5.0%
10.0%
15.0%
10°C 30°C 50°C 70°C 90°C
Flow
rat
e ch
ange
[%
]
Fuel temperature [°C]
New model
Current model
New model
Current model
Fig. 19 Comparison of Change in the negative pressure and flow rate characteristics
-20%
0%
20%
40%
0 200 400 600
Flow
rat
e ch
ange
Pb [mmHg]
New model
Current model
New model
Current model
3. Result of countermeasures
This section describes the Result of countermeasures
incorporated in the developed injector. The developed
layout was more effective in the areas listed below
(Table 2).
This can a lso be observed in d is t r ibut ion
(Fig. 16, 17).
Temperature/Negative pressure and under-seat
flow rate characteristics improvements also minimize
changes in temperature and flow rate characteristics,
CONCLUSIONS
This developed injector can reduce any variance
in flow rate in the event of a change in temperature
in different engine use environments or a change
in negative pressure in different engine running
modes and can improve the atomization of fuel
to be sprayed. Under changing market situations
in the future, manufacturers will need to develop
and offer environmentally friendly products at a
moderate price particularly in developing countries
where sales of motorcycles and automobiles are
expanding. And along with a full-fledged growth
of FI for motorcycles, these advantages can make
a great contribution to lower emissions and better
fuel economy, not only in developed but also in
developing countries.
and in negative pressure and under-seat flow rate
characteristics (Fig. 18, 19).
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Keihin Technical Review Vol.2 (2013)
We sincerely appreciate all support we recieved
from everyone. We continue challenging the further
new technology so that it can contribute to lower
emissions and better fuel economy. (NAKAMURA)
Authers
Junichi NAKAMURA Akira AKABANE Koji KITAMURA
Yuzuru SASAKI
REFERENCES
(1) Daisuke Matsuo, Akihiko Haramai, Kazuhiko
Sato, Minoru Ueda: Development of a Small
L ow - c o s t F u e l I N J E C TO R t o O ve r c o m e
Diversificat ion of Requirements in Global
Markets, SETC Paper 20097055
(2) Mitsutomo Kawahara, Kenichi Saitoh, Kazuhiko
Sato: Reduction of operation noises of Injector
for small motorcycle. SETC Paper 20119625