JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER
Vol. 17, No. 1, January–March 2003
Application of Magnetic Fluid Membrane for Flow Control
H. Yamaguchi,¤ Y. Suzuki,† and S. Shuchi‡
Doshisha University, Kyoto 610-0321, Japan
To study the application of a magnetic uid membrane for ow rate control, an experimental investigation was
conducted to obtain the basic characteristics and to verify the feasibility of practical use. The working principle of
a magnetically controlled magnetic uid membrane is based on the magnetic attraction body force exerted on the
magnetic uid, which is sustained in the cross-sectional area of a pipe. In the experiments, rupture pressure was
–
obtained at various conditions for an oil magnetic uid interface. Also, from the results obtained for the ow rate
ontrol characteristics, it was found that the magnetically controlled membrane has a function similar to that of an
ordinary butter y valve, and it was shown that the membrane would be feasible for controlling lower ow rates at
lower driving pressure gradients.
Nomenclature
posed to date, such as magnetic seals, dampers, bearings, etc.1¡3
Among the many promisingtechnologicalapplicationsof magnetic
uids are those devices that use surface deformationwith magnetic
attraction force.
A unique application for an aperture control, which is derived
from the interfacial formation of magnetic uid, was proposed in
our previous research work.4 The basic results were presented for
a sustained magnetic uid membrane in a pipe section under an
appliedmagnetic eld. In viewof possibleengineeringapplications,
detailed characteristics were reported in Ref. 4 for the formation
process and the aperture variation in terms of imposed magnetic
eld intensity.
D
D0
d
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
=
circular valve diameter of butter y valve, m
pipe diameter of buttery valve, m
pipe diameter of test section, m
magnetic eld intensity, A/m
magnetic eld vector
intensity of magnetic eld in direction, A/m
H
H
Hr
Hz
r
z
intensity of magnetic eld in direction, A/m
H
H
.
I
l
/
maximum of z , A/m
z
max
applied dc current, A
pipe length, m
effective length, m
le
In the present study, which proceeds from our previous study,4 a
newmethodof ow ratecontrolthatusessustainedmagnetic uid in
a pipe under an appliedmagnetic eld is proposed.The basicideaof
using the sustainedmagnetic uid in a sectionofa pipeis to form the
membrane and block the passage of ow by controlling magnetic
eldintensity.Inthepresentinvestigation,therupturepressureofthe
membrane(whichisanalogoustotheholdingpressureofanordinary
mechanical ow controlvalve)is investigatedexperimentally,using
a water-basedmagnetic uid (W-40)with a working uid of mineral
oil. In the experiment, the rupture pressure of the magnetic uid
membrane for varying magnetic eld intensity is recorded for a
given volume of magnetic uid sustainedin the pipe section.While
controllingthe volume ow rate of the working liquid (oil), the ow
characteristics (the pressure loss coef cient across the membrane)
are also recorded and examined to simulate a ow control valve.
lm
M
M
P
length covered by magnetic uid, m
magnetization,Wb/m2
magnetizationvector, Wb/m2
¢
pressure loss, Pa s
rupture pressure, Pa s
loss
P
¢
r
Re
Reynolds number
r
z
, µ,
cyclindricalcoordinates(see Fig. 6)
volume of sustained magnetic uid, m3
area mean velocity, m/s2
measured pressure difference, Pa
valve opening angle of butter y valve, rad
pressure loss coef cient
Vm
v
P
1
±
"
¢
´
¸
½
test uid viscosity, Pa s
friction loss coef cient (¸ 64=
D
Re
)
working uid density, kg/m3
II. Experimental Apparatus and Procedure
I. Introduction
Figure 1 is a schematic diagram of the experimental apparatus.
In the present investigation,oil, whose physical properties are pre-
sentedin Table1, isusedas a testworking uid.Todrivetheworking
uid into the test section, the working uid, which is contained in
the cylinder, is forced to ow by inward pushing of the piston with
driving units that consist of an electric motor, speed controller,and
other mechanical parts, as shown in Fig. 1. In this investigation,
the pressure and volumetric ow rate are kept constant throughout
the experiments.The volumetric ow rate of the working uid was
obtained by knowing the speed and area of the piston. Differen-
tial pressure across the test section, which is used to obtain to the
pressure loss coefcient, was measured by the differential pressure
gauge, as indicatedin Fig. 1. The inlet length to the test section was
taken suf ciently long so that the ow coming into the test section
was a fully developed steady laminar pipe ow. The test section is
made of acrylic pipe with an inner diameter of 12 mm and total
length of 800 mm, where a given volume of magnetic uid is sus-
tained by a magnetic eld forming a membrane. A cylindrical coil
electromagnet is placed around the test section, and it is cooled by
circulating water from a cooler unit. The electromagnetis powered
by a dc power supply unit, capable of producing a magnetic eld
MAGNETIC uid is a colloidal suspension of 10-nm ferro-
magneticparticlesthatare suspendedwith a surfactantcoating
A
in a carrier liquid such as hydrocarbon,ester, or water.1¡3 Magnetic
uid behaves as an electrically nonconducting homogeneous me-
dia in which single-domain magnetic particles are stabilized even
in strong magnetic elds. Because magnetic uids have magnetic
properties along with uidity, many applications have been pro-
Received 12 April 2002; revision received 22 July 2002; accepted for
°c
publication 24 July 2002. Copyright
2002 by the American Institute of
Aeronautics and Astronautics, Inc. All rights reserved. Copies of this paper
may be made for personal or internal use, on condition that the copier pay
the $10.00 per-copy fee to the Copyright Clearance Center, Inc., 222 Rose-
wood Drive, Danvers, MA 01923; include the code 0887-8722/03 $10.00 in
correspondence with the CCC.
¤Professor, Department of Mechanical Engineering; hyamaguc@mail.
doshisha.ac.jp.
†Research Student, Department of Mechanical Engineering; eta1305@
mail4.doshisha.ac.jp.
‡Research Student, Department of Mechanical Engineering; dta0379@
mail4.doshisha.ac.jp.
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