[Technical Field]
[0001] The present invention relates to a glow plug, particularly, a glow plug capable of
providing higher heating-up temperature.
[Background Art]
[0002] A glow plug used as an auxiliary heat source in a compression-ignition-type internal
combustion engine such as a diesel engine is required to provide higher heating-up
temperature in the situation of tightening regulations on internal combustion engines.
Patent Document 1 discloses a technique for allowing a glow plug having a coil disposed
within a tube to meet the requirement to provide higher heating-up temperature. In
the disclosed technique, a refractory metal containing W or Mo as a main component
and having a melting point higher than those of an FeCrAl alloy and an NiCr alloy
is used for the coil.
[Prior Art Document]
[Patent Document]
[0003] [Patent Document 1] International Publication No.
WO2014/206847
[Summary of the Invention]
[Problem to be Solved by the Invention]
[0004] However, since the resistance ratio of a refractory metal such as W or Mo is high
as compared with the resistance ratios of an FeCrAl alloy and an NiCr alloy, the above-mentioned
conventional technique involves a problem in that when a constant voltage is applied
to the coil for heating up to a predetermined temperature (e.g., 1,000°C), the resistance
of the coil abruptly increases, resulting in an abrupt reduction in current value.
The resistance ratio is "the ratio of a resistance of the coil at 1,000°C to a resistance
of the coil at 20°C." The larger the value of the resistance ratio, the larger the
resistance at high temperature. Since the amount of generated heat is proportional
to the square of current, difficulty is involved in heating up to the predetermined
temperature.
[0005] By contrast, it is conceived that a rearward coil formed of an FeCrAl alloy or an
NiCr alloy and lower in resistance ratio than a refractory metal is joined to the
rear end of a coil (forward coil) formed of a refractory metal. By employing such
a coil structure, when voltage is applied to a coil, the forward coil and a forward
side of a tube can be heated up to a predetermined temperature without involvement
of an excessive increase of resistance of the entire coil.
[0006] Meanwhile, the coil heated up to the predetermined temperature needs to be saturated
at around the predetermined temperature (e.g., at 1,100°C). For such saturation, the
voltage applied to the coil needs to be lowered; however, this causes transfer of
heat from the forward side of the tube toward a rearward side of the tube lower in
temperature than the forward side, potentially resulting in a transient great drop
in temperature of the forward side of the tube. As a result, the combustion in an
engine becomes unstable, and the emission of exhaust gas increases.
[0007] By contrast, by reducing the wall thickness of the entire tube, the heat capacity
of the tube can be reduced, whereby the transfer of heat from the forward side to
the rearward side of the tube can be restrained. However, reducing the wall thickness
of the entire tube causes oxidization wear, which results in both deformation of the
tube and shortening in endurance time until formation of a through hole in the tube.
As a result, durability of the tube potentially deteriorates.
[0008] The present invention has been conceived to solve the above problem, and an object
of the invention is to provide a glow plug capable of restraining a temperature drop
in the event of lowering applied voltage for saturating temperature, while ensuring
durability and provision of higher heating-up temperature.
[Means for Solving the Problem]
[0009] To achieve the object, a glow plug of the present invention comprises a closed-bottomed
tube extending in a direction of an axial line; a forward coil and a rearward coil
disposed within the tube; and an axial rod connected to a rear end of the rearward
coil. The forward coil is connected at its forward end to a forward end portion of
the tube and contains W or Mo as a main component. The rearward coil is connected
at its forward end to a rear end of the forward coil and has a resistance ratio R1
lower than a resistance ratio R2 of the forward coil, where the resistance ratio R1
is the ratio of a resistance of the rearward coil at 1,000°C to a resistance of the
rearward coil at 20°C, and the resistance ratio R2 is the ratio of a resistance of
the forward coil at 1,000°C to a resistance of the forward coil at 20°C. The tube
has a tube forward portion ranging from the forward end of the tube to a position
around a center of the forward coil with respect to the direction of the axial line,
and a tube rearward portion ranging from a position around the rear end of the rearward
coil to a position around the forward end of the rearward coil. A wall thickness A
of the tube forward portion is 0.5 mm or more; a wall thickness B of the tube rearward
portion is 0.3 mm or more; and a minimal wall thickness B1 of the tube rearward portion
is smaller than the wall thickness A of the tube forward portion.
[Effect of the Invention]
[0010] According to the glow plug described in claim 1, the forward coil containing W or
Mo as a main component is connected to the forward end portion of the tube, and the
rearward coil having a resistance ratio R1 lower than a resistance ratio R2 of the
forward coil is connected to the rear end of the forward coil. Accordingly, even in
application of a constant voltage, the forward coil containing W or Mo as a main component
and a forward portion of the tube can be heated up to a predetermined temperature,
whereby provision of higher heating-up temperature can be ensured.
[0011] Also, the wall thickness A of the tube forward portion is 0.5 mm or more, and the
wall thickness B of the tube rearward portion is 0.3 mm or more. Accordingly, with
respect to the tube rearward portion and the tube forward portion whose temperature
increases as compared with the tube rearward portion, there can be restrained the
shortening of endurance time until formation of a through hole in the tube and the
deformation of the tube both of which are caused by oxidization wear. Therefore, durability
can be ensured.
[0012] Further, the minimal wall thickness B1 of the tube rearward portion is smaller than
the wall thickness A of the tube forward portion. Accordingly, the heat capacity per
unit length of the tube rearward portion (a portion having the minimal wall thickness
B1) can be smaller than that of the tube forward portion. As a result, when the applied
voltage is lowered, the amount of heat transfer from the tube forward portion to the
tube rearward portion can be restrained. Therefore, even in the event of lowering
voltage applied to the coil for saturating the temperature of the coil, a drop in
temperature of the forward side of the tube can be restrained.
[0013] Notably, the expression "W or Mo as a main component" means that the W or Mo content
of a coil material is 50 wt% or more.
[0014] The "tube forward portion" indicates a portion of the tube which has high temperature
as compared with the other portion in the event of the coil generating heat; specifically,
"a portion ranging from the forward end of the tube to a position around the center
of the forward coil with respect to the direction of the axial line." The "tube rearward
portion" indicates a portion of the tube which is low in temperature as compared with
the tube forward portion and to which heat is apt to transfer from the tube forward
portion; specifically, "a portion ranging from a position around the rear end of the
rearward coil to a position around the forward end of the rearward coil."
[0015] Further, "the wall thickness A of the tube forward portion" and "the wall thickness
B of the tube rearward portion" indicate "the wall thickness of the entire forward
portion" and "the wall thickness of the entire tube rearward portion," respectively.
"The minimal wall thickness B1 of the tube rearward portion" indicates "the minimal
value of the wall thickness of the entire tube rearward portion (i.e., the wall thickness
B of the tube rearward portion)."
[0016] According to the glow plug described in claim 2, the wall thickness A is 0.7 mm or
less, and the ratio of the wall thickness A to the minimal wall thickness B1; i.e.,
ratio A/B1, satisfies the relational expression A/B1 ≥ 1.11. Since the wall thickness
A is 0.7 mm or less, it is possible to prevent the heat capacity per unit length of
the tube forward portion from becoming excessively large. Accordingly, in addition
to provision of the effect of claim 1, there can be improved the performance of heating
up the tube forward portion to a predetermined temperature in a short period of time
(hereinafter, called "rapid heating-up performance").
[0017] The ratio of the wall thickness A to the wall thickness B1; i.e., A/B1, satisfies
a relational expression A/B1 ≥ 1.11. Accordingly, even when voltage applied to the
coil is lowered for saturating the temperature of the coil, a drop in temperature
of the forward side of the tube can be further restrained.
[0018] According to the glow plug described in claim 3, the wall thickness A is 0.56 mm
or more, and the ratio A/B1 satisfies a relational expression A/B1 ≥ 1.24. Accordingly,
in addition to provision of the effect of claim 2, there can be further lengthened
service life until formation of a through hole in the tube forward portion caused
by oxidization wear, and there can be further restrained a drop in temperature of
the forward side of the tube when voltage applied to the coil is lowered for saturating
the temperature of the coil.
[0019] According to the glow plug described in claim 4, the wall thickness A is from 0.58
mm to 0.64 mm, and the ratio A/B1 satisfies a relational expression A/B1 ≥ 1.29. Accordingly,
since the heat capacity per unit length of the tube rearward portion can be further
reduced as compared with that of the tube forward portion, in addition to provision
of the effect of claim 3, there can be further improved restraint of a drop in temperature
in the event of lowering applied voltage, durability, and rapid heating-up performance.
[0020] According to the glow plug described in claim 5, the wall thickness A is 0.62 mm
or less. Accordingly, in addition to provision of the effect of claim 4, rapid heating-up
performance can be further improved.
[0021] According to the glow plug described in claim 6, the tube has a wall thickness C
of 0.5 mm or more as measured at a portion ranging from the forward end of the tube
to a position around an end of a first turn starting from the forward end of the rearward
coil. Heat generated by the forward coil is easily transmitted not only to a portion
of the tube surrounding the forward coil but also to a portion of the tube surrounding
the first turn of the rearward coil. By setting the wall thickness C of the portion
of the tube to 0.5 mm or more, in addition to the provision of the effect of any one
of claims 1 to 5, durability of the portion of the tube can be ensured.
[Brief Description of the Drawings]
[0022]
[FIG. 1] Half sectional view of a glow plug.
[FIG. 2] Enlarged sectional view showing a portion of the glow plug.
[FIG. 3] Schematic diagram showing the relation between voltage applied to the glow
plug and heating-up temperature.
[Modes for Carrying out the Invention]
[0023] A preferred embodiment of the present invention will next be described with reference
to the drawings. A glow plug 10 according to an embodiment of the present invention
will be described with reference to FIGS. 1 and 2. FIG. 1 is a half sectional view
of the glow plug 10, and FIG. 2 is an enlarged sectional view showing a portion of
the glow plug 10. In FIGS. 1 and 2, the lower side of the sheet is called the forward
side of the glow plug 10, and the upper side of the sheet is called the rearward side
of the glow plug 10.
[0024] As shown in FIG. 1, the glow plug 10 includes an axial rod 20, a metallic shell 30,
a tube 40, and a coil 50. These members are assembled along an axial line O of the
glow plug 10. The glow plug 10 is an auxiliary heat source used in, for example, starting
up an internal combustion engine (not shown) such as a diesel engine.
[0025] The axial rod 20 is a circular columnar conductor made of metal and is adapted to
supply electric power to the coil 50. The coil 50 is electrically connected to the
forward end of the axial rod 20. The axial rod 20 is inserted into the metallic shell
30 with its rear end protruding outward from the metallic shell 30.
[0026] In the present embodiment, the axial rod 20 has an externally threaded connection
portion 21 formed at its rear end portion. An O-ring 22 made of insulation rubber,
a tubular insulator 23 made of synthetic resin, a tubular ring 24 made of metal, and
a nut 25 made of metal, from the forward side, are sequentially assembled to the rear
end portion of the axial rod 20. The connection portion 21 allows connection of a
connector (not shown) of a cable for supplying electric power from a power source
such as battery. The nut 25 fixes a connected connector (not shown).
[0027] The metallic shell 30 is an approximately cylindrical member formed of carbon steel
or the like. The metallic shell 30 has an axial hole 31 extending therethrough along
the axial line O and has a threaded portion 32 formed on an outer circumferential
surface thereof. The metallic shell 30 has a tool engagement portion 33 formed on
the rearward side of the threaded portion 32. The axial hole 31 is a through hole
through which the axial rod 20 is inserted. Since the inside diameter of the axial
hole 31 is greater than the outside diameter of the axial rod 20, a gap is formed
between the axial rod 20 and the axial hole 31. The threaded portion 32 is an external
thread to be engaged with an internal combustion engine (not shown). The tool engagement
portion 33 has such a shape (e.g., hexagonal shape) as to allow a tool (not shown)
to be engaged therewith for screwing the threaded portion 32 into or unscrewing the
threaded portion 32 from a threaded hole (not shown) of the internal combustion engine.
[0028] The metallic shell 30 holds the axial rod 20 via the O-ring 22 and the insulator
23 at a rear end portion of the axial hole 31. The ring 24 in contact with the insulator
23 is crimped to the axial rod 20, thereby fixing the axial position of the insulator
23. The insulator 23 electrically insulates the ring 24 and a rear end portion of
the metallic shell 30 from each other. The metallic shell 30 receives the tube 40
fixed into a forward end portion of the axial hole 31.
[0029] The tube 40 is made of metal and closed at a forward end 41 thereof. The tube 40
is press-fitted into the axial hole 31 to thereby be fixed to the metallic shell 30.
Examples of material for the tube 40 include heat resistant alloys such as nickel-based
alloys and stainless steels.
[0030] The tube 40 receives a forward end portion of the axial rod 20 inserted therein.
Since the inside diameter of the tube 40 is greater than the outside diameter of the
axial rod 20, a gap is formed between the axial rod 20 and the tube 40. A seal member
26 is a cylindrical electrically insulative member held between a forward end portion
of the axial rod 20 and a rear end portion of the tube 40. The seal member 26 maintains
the gap between the axial rod 20 and the tube 40 and provides a seal between the axial
rod 20 and the tube 40. The coil 50 is accommodated in the tube 40 along the axial
line O. An insulating powder 60 is charged into the tube 40.
[0031] As shown in FIG. 2, the coil 50 has a spiral form and generates heat through energization.
The coil 50 is composed of a forward coil 51 joined to a forward end 41 portion of
the tube 40, and a rearward coil 52 joined to the forward end of the axial rod 20.
[0032] The forward coil 51 is welded at a forward end 54 (the boundary between the forward
coil 51 and a weld fusion zone) to a portion of the forward end 41 of the tube 40
via the weld fusion zone (not shown). A refractory metal which contains W or Mo as
a main component is used as a material for the forward coil 51. These elements can
be used singly as a material for the forward coil 51, or an alloy which contains either
one of these elements as a main component can be used as a material for the forward
coil 51. The forward coil 51 is welded at the rear end thereof to the rearward coil
52. A weld fusion zone 53 is formed between the forward coil 51 and the rearward coil
52 as a result of solidification of a molten weld metal.
[0033] The rearward coil 52 is connected in series to the forward coil 51 via the weld fusion
zone 53. The rearward coil 52 is formed of an electrically conductive material having
a resistance ratio R2 lower than a resistance ratio R1 of the forward coil 51. Examples
of material for the rearward coil 52 include an FeCrAl alloy and an NiCr alloy. The
rearward coil 52 is accommodated in the tube 40 along the axial line O (see FIG. 1)
and is welded at a rear end 55 thereof to the forward end of the axial rod 20. The
axial rod 20 is electrically connected to the tube 40 via the rearward coil 52 and
the forward coil 51.
[0034] The insulating powder 60 has electric insulation and has thermal conductivity at
high temperature. A space between the coil 50 and the tube 40, a space between the
axial rod 20 and the tube 40, and a space surrounded by the coil 50 are filled with
the insulating powder 60. The insulating powder 60 has a function of transferring
heat from the coil 50 to the tube 40, a function of preventing a short circuit between
the coil 50 and the tube 40, and a function of suppressing vibration of the coil 50,
thereby preventing breakage thereof. Examples of the insulating powder 60 include
powders of oxides such as MgO and Al
2O
3. Powder of CaO, ZrO
2, SiO
2, Si, or the like can be added to powder of oxide such as MgO, Al
2O
3, or the like. In the present embodiment, the insulating powder 60 contains MgO powder
in an amount of 85% by mass to less than 100% by mass and also contains Si powder.
[0035] The tube 40 includes a tube forward portion 43 and a tube rearward portion 46. The
tube forward portion 43 ranges from the forward end 41 of the tube 40 to a position
42 around a center 56 (the midpoint of a line segment connecting the position of the
forward end 54 and the position of the weld fusion zone 53) of the forward coil 51
with respect to the direction of the axial line O (axial direction). The tube rearward
portion 46 ranges from a position 44 around the rear end 55 of the rearward coil 52
to a position 45 around a forward end 57 (the position of the weld fusion zone 53)
of the rearward coil 52. FIG. 2 shows the range of the tube forward portion 43 (from
the forward end 41 of the tube 40 to the position 42) and the range of the tube rearward
portion 46 (from the position 44 of the tube 40 to the position 45).
[0036] In the present embodiment, the wall thickness A of the tube forward portion 43 is
0.5 mm or more; the wall thickness B of the tube rearward portion 46 is 0.3 mm or
more; and the minimal wall thickness B1 of the tube rearward portion 46 is smaller
than the wall thickness A of the tube forward portion 43.
[0037] In the present embodiment, the tube forward portion 43 and the tube rearward portion
46 have the same outside diameter, and the inside diameter of the tube forward portion
43 is smaller than the inside diameter of the tube rearward portion 46 at the rear
end side thereof, whereby the minimal wall thickness B1 of the tube rearward portion
46 becomes smaller than the wall thickness A of the tube forward portion 43. Also,
the tube 40 has a wall thickness C of 0.5 mm or more as measured at a portion 48 ranging
from the forward end 41 thereof to a position 47 around an end 58 of a first turn
starting from the forward end 57 (the weld fusion zone 53) of the rearward coil 52.
[0038] Next, with reference to FIG. 3, the relation between voltage V applied to the glow
plug 10 and heating-up temperature T of the glow plug 10 will be described. FIG. 3
is a schematic diagram showing the relation between voltage V and heating-up temperature
T of the glow plug 10. In FIG. 3, time (seconds) is plotted along the horizontal axis;
the solid line indicates heating-up temperature T; and the broken line indicates voltage
V.
[0039] When voltage V is applied between the connection portion 21 and the metallic shell
30 of the glow plug 10, current I flows through the coil 50. The value of the current
I is obtained by dividing the voltage V by the sum (i.e., R
1 + R
2) of the resistance R
1 of the forward coil 51 and the resistance R
2 of the rearward coil 52. The amount of generated heat per unit time of the forward
coil 51 is R
II
2, and the amount of generated heat per unit time of the rearward coil 52 is R
2I
2.
[0040] The coil 50 is designed such that the resistance R
2 of the rearward coil 52 at 20°C is greater than the resistance R
1 of the forward coil 51 at 20°C. The reason for such design is to ensure the current
I (inrush current) flowing through the coil 50 at room temperature to thereby cause
the coil 50 to generate heat.
[0041] Since the rearward coil 52 has the resistance ratio R2 lower than the resistance
ratio R1 of the forward coil 51, as the temperature of the coil 50 rises as a result
of generation of heat, the resistance R
1 of the forward coil 51 becomes greater than the resistance R
2 of the rearward coil 52. As a result, the amount of generated heat per unit time
R
II
2 of the forward coil 51 can be greater than the amount of generated heat per unit
time R
2I
2 of the rearward coil 52. Since the forward coil 51 is formed of a refractory metal
which contains W or Mo as a main component, the heating-up temperature T can be increased.
Accordingly, the heating-up temperature T of the forward coil 51 and the tube forward
portion 43 can be raised to a desired temperature (e.g., 1,000°C).
[0042] Since the wall thickness A of the tube forward portion 43 to be heated by the forward
coil 51 is 0.5 mm or more, there can be restrained the shortening of endurance time
until formation of a through hole in the tube forward portion 43 caused by oxidization
wear. Since the tube rearward portion 46 located rearward of the tube forward portion
43 is lower in heating-up temperature than the tube forward portion 43, by setting
the wall thickness B of the tube rearward portion 46 to 0.3 mm or more, it is possible
to restrain the shortening of endurance time until formation of a through hole in
the tube rearward portion 46 and the deformation of the tube rearward portion 46 both
of which are caused by oxidization wear. Since the forward coil 51 formed of a refractory
metal which contains W or Mo as a main component is apt to be oxidized, if a through
hole is formed in the tube 40, the forward coil 51 is highly likely to be broken as
a result of oxidation. By restraining formation of a through hole in the tube forward
portion 43 and in the tube rearward portion 46 while restraining deformation of the
tube rearward portion 46, breaking of the forward coil 51 caused by oxidation can
be restrained, whereby durability can be improved.
[0043] After the heating-up temperature T reaches a desired temperature (herein 1,000°C),
the voltage V applied to the glow plug 10 is lowered such that the heating-up temperature
T becomes a saturation temperature (e.g., 1,100°C) in a stable state. Since the rearward
coil 52 is smaller in the amount of generated heat than the forward coil 51, in the
transition period in which the voltage V is lowered, heat moves from the forward coil
51 and the tube forward portion 43 to the rearward coil 52 and the tube rearward portion
46. As a result, the heating-up temperature T highly dependent on the forward coil
51 transiently drops by a temperature D. When the heating-up temperature T drops greatly
as a result of an increase in the temperature D, combustion in an engine becomes unstable,
and emission of exhaust gas increases.
[0044] In order to prevent such a problem, in the glow plug 10, the minimal wall thickness
B1 of the tube rearward portion 46 is rendered smaller than the wall thickness A of
the tube forward portion 43. Accordingly, the heat capacity per unit length of the
tube rearward portion 46 (a portion having the minimal wall thickness B1) can be smaller
than the heat capacity per unit length of the tube forward portion 43. As a result,
when the voltage V is lowered for transition of the heating-up temperature T of the
tube 40 to the saturation temperature, heat moving from the tube forward portion 43
to the tube rearward portion 46 can be restrained. Therefore, it is possible to restrain
a temperature drop (temperature D) in the transition period during which the voltage
V is lowered for saturating the heating-up temperature T. As a result, while durability
and provision of higher heating-up temperature T are ensured, there can be restrained
a temperature drop when the voltage V is lowered for saturating the heating-up temperature
T. Therefore, the glow plug 10 assists combustion in an engine, whereby an idling
operation of the engine after startup can be stabilized, and emission of exhaust gas
can be reduced.
[0045] Further, preferably, the wall thickness B of at least half of the tube rearward portion
46 is smaller than the wall thickness A of the tube forward portion 43 (see FIG. 2).
As a result, there can be further restrained a temperature drop when the voltage V
is lowered for saturating the heating-up temperature T.
[0046] Since the glow plug 10 is designed such that the tube 40 has a wall thickness C of
0.5 mm or more as measured at the portion 48 ranging from the forward end 41 thereof
to the position 47 around the end 58 of the first turn starting from the forward end
(the weld fusion zone 53) of the rearward coil 52, in spite of transmission of heat
generated by the forward coil 51 to the portion 48 of the tube 40, durability of the
tube 40 can be ensured at the portion 48.
[0047] Since the insulating powder 60 contains Si powder, as compared with the case where
the whole insulating powder 60 is MgO powder, the thermal conductivity of the insulating
powder 60 can be deteriorated. As a result, since heat dissipation from the forward
coil 51 resulting from heat conduction of the insulating powder 60 can be restrained,
the insulating powder 60 promotes ensuring of rapid heating-up performance in inrush
of current and restraint of a temperature drop in the temperature transition in heating-up
of the tube forward portion 43.
[0048] The glow plug 10 is manufactured, for example, as follows. First, resistance heating
wires having respective predetermined compositions are coiled to form the forward
coil 51 and the rearward coil 52. Next, the forward coil 51 and the rearward coil
52 are welded together at their ends to form the coil 50. Next, the rear end 55 of
the rearward coil 52 of the coil 50 is joined to the forward end of the axial rod
20.
[0049] A steel pipe having a predetermined composition is subjected to forming so as to
have a diameter greater than the finished diameter of the tube 40 and to has a reduced
diameter at its forward end as compared with the remaining portion, thereby yielding
a tube precursor having a tapered open forward end. The coil 50 joined to the axial
rod 20 is inserted into the tube precursor such that the forward end 54 of the forward
coil 51 is disposed in the tapered opening portion of the tube precursor. The opening
portion of the tube precursor and the forward end 54 of the forward coil 51 are fused
together by welding, thereby closing a forward end portion of the tube precursor and
thus yielding a heater precursor which accommodates the coil 50 therein.
[0050] Next, after the insulating powder 60 is charged into the tube 40 of the heater precursor,
the seal member 26 is inserted between the axial rod 20 and a rear end opening portion
of the tube 40 to seal the tube 40. Then, the tube 40 is swaged until the tube 40
has a predetermined outside diameter.
[0051] Next, the swaged tube 40 is fixedly press-fitted into the axial hole 31 of the metallic
shell 30, and the O-ring 22 and the insulator 23 are fitted between the metallic shell
30 and the axial rod 20 from the rear end of the axial rod 20. The ring 24 is crimped
to the axial rod 20, thereby yielding the glow plug 10.
[Examples]
[0052] The present invention will be described further in detail by way of example; however,
the present invention is not limited to the example.
<Preparation of samples>
[0053] The forward coils 51 were prepared by use of wire having a diameter of 0.20 mm and
formed of an alloy containing W as a main component. Similarly, the rearward coils
52 were prepared by use of wire having a diameter of 0.38 mm and formed of an NiCr
alloy. The rearward coils 52 were welded to the respective forward coils 51, thereby
preparing the coils 50 in which the rearward coils 52 and the forward coils 51 are
connected respectively in series. The coils 50 had a resistance of 0.33 Ω at 20°C
as measured by a 4-terminal method.
[0054] By use of the coils 50, glow plugs having a structure substantially the same as that
of the glow plug 10 shown in FIG. 1 were manufactured by the aforementioned method,
thereby yielding glow plug samples 1 to 11 shown in Table 1. Table 1 shows parameters
of the samples; specifically, the maximal and minimal values of the wall thickness
A of the tube forward portion 43, the maximal value and the minimal value (i.e., the
minimal wall thickness B1) of the wall thickness B of the tube rearward portion 46,
and the range of the ratio of the wall thickness A to the wall thickness B1.
[0055] Glow plug samples 1 to 11 had an outside diameter of the tube forward portion 43
of 3.2 mm and an outside diameter of the tube rearward portion 46 of 4.0 mm and differed
in the wall thickness A of the tube forward portion 43 and the wall thickness B of
the tube rearward portion 46 as a result of adjusting a swaging rate of swaging to
be conducted on the tube forward portion 43 and the tube rearward portion 46. In glow
plug samples 1 to 11, the insulating powder 60 was MgO powder which contained Si powder
in an amount of 0.2% by mass.
[Table 1]
No. |
Tube |
Rating |
Wall thickness A (mm) |
Wall thickness B (mm) |
A/B1 |
Temp. drop in temp. transition |
Durability |
Rapid heating-up performance |
Comprehensive |
Minimal value |
Maximal value |
Minimal value (B1) |
Maximal value |
1 |
0.40 |
0.45 |
0.45 |
0.50 |
0.89 - 1.00 |
D |
D |
A |
D |
2 |
0.50 |
0.55 |
0.45 |
0.50 |
1.11 - 1.22 |
C |
C |
A |
C |
3 |
0.56 |
0.61 |
0.45 |
0.56 |
1.24 - 1.36 |
B |
B |
A |
B |
4 |
0.58 |
0.60 |
0.45 |
0.58 |
1.29 - 1.33 |
A |
A |
A |
A |
5 |
0.59 |
0.62 |
0.45 |
0.59 |
1.31 - 1.38 |
A |
A |
A |
A |
6 |
0.59 |
0.64 |
0.45 |
0.59 |
1.31 - 1.42 |
A |
A |
B |
B |
7 |
0.65 |
0.70 |
0.45 |
0.65 |
1.44 - 1.56 |
A |
A |
C |
C |
8 |
0.75 |
0.80 |
0.45 |
0.75 |
1.67 - 1.78 |
A |
A |
D |
D |
9 |
0.58 |
0.62 |
0.45 |
0.58 |
1.29 - 1.38 |
A |
A |
A |
A |
10 |
0.58 |
0.62 |
0.30 |
0.58 |
1.93 - 2.07 |
A |
A |
A |
A |
11 |
0.58 |
0.62 |
0.25 |
0.58 |
2.32 - 2.48 |
A |
D |
A |
D |
[0056] A PR thermocouple was joined to the surface of the tube 40 of each sample at a position
located 2 mm away in the direction of the axial line O from the forward end 41 of
the tube 40 to measure temperature in the vicinity of the forward end 41 of the tube
40. In place of the PR thermocouple, a radiation thermometer may be used.
[0057] The wall thickness A of the tube forward portion 43 and the wall thickness B of the
tube rearward portion 46 were measured by observing, through a microscope, the sections
(containing the axial line O) of the tubes 40 of samples swaged at the same swaging
rates as those of samples 1 to 11.
[0058] The wall thickness A was measured at five points equally spaced along the entire
length of the tube forward portion 43 in the direction of the axial line (the axial
direction) (the five points consist of the position of the forward end 41, the position
42 around the center 56 of the forward coil 51 with respect to the axial direction,
and three other points), thereby obtaining the maximal and minimal values of the wall
thickness A from the measured values of the wall thickness A.
[0059] The wall thickness B was measured at ten points equally spaced along the entire length
of the tube rearward portion 46 (the ten points consist of the position 45 around
the forward end 57 of the rearward coil 52, the position 44 around the rear end 55
of the rearward coil 52, and eight other points), thereby obtaining the maximal and
minimal values of the wall thickness B from the measured values of the wall thickness
B.
<Temperature drop in temperature transition>
[0060] After DC voltage was applied for two seconds between the connection portion 21 and
the metallic shell 30 of each sample in such a manner that the temperature of the
tube 40 in the vicinity of the forward end 41 after elapse of two seconds after the
application of the voltage became 1,000°C, the applied voltage was lowered. The applied
voltage was a rated voltage at which the temperature of the tube 40 in the vicinity
of the forward end 41 is saturated to 1,100°C. When the applied voltage was lowered,
the temperature of the tube 40 transiently dropped and then increased toward the saturation
temperature of 1,100°C with time (see FIG. 3). The temperature difference (temperature
D shown in FIG. 3) between the highest temperature of the tube 40 and the temperature
of the tube 40 in the temperature transition resulting from the lowering of applied
voltage.
[0061] The samples having a temperature difference of less than 30°C were evaluated as "A:
particularly excellent;" the samples having a temperature difference of 30°C to less
than 50°C were evaluated as "B: excellent;" the samples having a temperature difference
of 50°C to less than 80°C were evaluated as "C: good;" and the samples having a temperature
difference of 80°C or more were evaluated as "D: poor." Table 1 shows the results
in the column "Temperature drop in temperature transition."
<Rapid heating-up performance>
[0062] DC voltage of 11 V was applied between the connection portion 21 and the metallic
shell 30 of each sample, and two seconds later, the temperature of the tube 40 in
the vicinity of the forward end 41 was measured. The samples having a temperature
of 950°C or higher were evaluated as "A: particularly excellent;" the samples having
a temperature of 900°C to less than 950°C were evaluated as "B: excellent;" the samples
having a temperature of 850°C to less than 900°C were evaluated as "C: good;" and
the samples having a temperature of less than 850°C were evaluated as "D: poor." Table
1 shows the results in the column "Rapid heating-up performance."
<Durability>
[0063] After DC voltage was applied for two seconds between the connection portion 21 and
the metallic shell 30 of each sample in such a manner that the temperature of the
tube 40 in the vicinity of the forward end 41 after elapse of two seconds after the
application of the voltage became 1,000°C, the applied voltage was lowered to a rated
voltage, and the rated voltage was applied for 180 seconds. The rated voltage is a
voltage at which the temperature of the tube 40 in the vicinity of the forward end
41 is saturated to 1,100°C. Subsequently, the tube 40 was air-cooled for 120 seconds
until the temperature of the tube 40 in the vicinity of the forward end 41 lowered
to room temperature. A test taking this procedure as one cycle was conducted for 500
hours (about 6,000 cycles). The samples were evaluated for the occurrence of breaking
of the coil 50 caused by formation of a through hole in the tube 40 and for the occurrence
of deformation of the tube 40.
[0064] The samples free from the occurrence of breaking of the coil 50 after the elapse
of 500 hours after start of the test were evaluated as "A: particularly excellent."
The samples which suffered the occurrence of breaking of the coil 50 after the elapse
of 300 hours (about 3,600 cycles) to less than 500 hours after start of the test were
evaluated as "B: excellent." The samples which suffered the occurrence of breaking
of the coil 50 after the elapse of 100 hours (about 1,200 cycles) to less than 300
hours after start of the test were evaluated as "C: good." The samples which suffered
the occurrence of breaking of the coil 50 before the elapse of 100 hours after start
of the test or the occurrence of deformation of the tube 40 before elapse of 10 hours
(about 120 cycles) after start of the test were evaluated as "D: poor." Table 1 shows
the results in the column "Durability."
<Comprehensive evaluation>
[0065] Desirably, the glow plug satisfies high "durability," small "temperature drop in
temperature transition," and high "rapid heating-up performance." Therefore, the column
"Comprehensive" in Table 1 shows the lowest evaluation result of "durability" evaluation,
"temperature drop in temperature transition" evaluation, and "rapid heating-up performance"
evaluation.
<Results>
[0066] As shown in Table 1, sample 1 in which the wall thickness A of the tube forward portion
43 was less than 0.5 mm and sample 11 in which the minimal value (B1) of the wall
thickness B of the tube rearward portion 46 was less than 0.3 mm exhibited poor durability.
Since in sample 1 the wall thickness A of the tube forward portion 43 was less than
0.5 mm, a through hole was early formed in the tube forward portion 43 due to oxidization
wear, resulting in breaking of the coil 50. Since in sample 11 the minimal value (B1)
of the wall thickness B of the tube rearward portion 46 was less than 0.3 mm, the
tube rearward portion 46 was early deformed. By contrast, samples 2 to 10 in which
the wall thickness A was 0.5 mm or more and the wall thickness B was 0.3 mm or more
exhibited rating A to C with respect to durability. Therefore, by setting the wall
thickness A of the tube forward portion 43 to 0.5 mm or more and setting the wall
thickness B of the tube rearward portion 46 to 0.3 mm or more, durability is ensured.
[0067] Sample 1 in which the wall thickness A of the tube forward portion 43 was smaller
than the minimal value (B1) of the wall thickness B of the tube rearward portion 46
(i.e., A/B1 < 1) exhibited a large temperature drop in temperature transition. By
contrast, samples 2 to 11 in which the minimal value (B1) of the wall thickness B
of the tube rearward portion 46 was smaller than the maximal and minimal values of
the wall thickness A of the tube forward portion 43 exhibited rating A to C with respect
to a temperature drop in temperature transition. Therefore, by setting the minimal
value (B1) of the wall thickness B to be smaller than the wall thickness A (maximal
value), a temperature drop in temperature transition can be reduced.
[0068] Samples 1 to 7 and 9 to 11 in which the wall thickness A of the tube forward portion
43 was 0.7 mm or less were superior in rapid heating-up performance to sample 8 in
which the wall thickness A was greater than 0.7 mm. Therefore, by setting the wall
thickness A to 0.5 mm to 0.7 mm and setting the wall thickness B to 0.3 mm or more
as in the case of samples 2 to 7, 9, and 10, rapid heating-up performance can be improved
while durability is ensured. The improvement of rapid heating-up performance is conceivably
for the following reason: as a result of reduction of the wall thickness A of the
tube forward portion 43, the heat capacity per unit length of the tube forward portion
43 reduced; accordingly, the tube forward portion 43 was easily heated up by heating
up of the forward coil 51.
[0069] Samples 2 to 7, 9, and 10 evaluated as A to C with respect to a temperature drop
in temperature transition satisfied the relational expression A/B1 ≥ 1.1. Therefore,
by satisfying the relational expressions 0.5 mm ≤ A ≤ 0.7 mm, B ≥ 0.3 mm, and A/B1
≥ 1.1, durability, a small temperature drop in temperature transition, and rapid heating-up
performance can be ensured.
[0070] Of samples 2 to 7, 9, and 10, samples 3 to 7, 9, and 10 in which the wall thickness
A of the tube forward portion 43 was 0.56 mm to 0.7 mm and which satisfied the relational
expression A/B1 ≥ 1.24 were evaluated as A or B with respect to a temperature drop
in temperature transition and durability. Therefore, by satisfying the relational
expressions 0.56 mm ≤ A ≤ 0.7 mm and A/B1 ≥ 1.24, durability can be improved while
a temperature drop in temperature transition is further restrained.
[0071] Of samples 3 to 7, 9, and 10, samples 4 to 6, 9, and 10 in which the wall thickness
A of the tube forward portion 43 was 0.58 mm to 0.64 mm and which satisfied the relational
expression A/B1 ≥ 1.29 were evaluated as A with respect to a temperature drop in temperature
transition and durability and evaluated as A or B with respect to rapid heating-up
performance. Therefore, by satisfying the relational expressions 0.58 mm ≤ A ≤ 0.64
mm and A/B1 ≥ 1.29, durability can be improved while a temperature drop in temperature
transition is further restrained, and rapid heating-up performance can be improved.
[0072] Of samples 4 to 6, 9, and 10, samples 4, 5, 9, and 10 in which the wall thickness
A of the tube forward portion 43 was 0.58 mm to 0.62 mm and which satisfied the relational
expression A/B1 ≥ 1.29 were evaluated as A with respect to all of a temperature drop
in temperature transition, durability, and rapid heating-up performance. Therefore,
by satisfying the relational expressions 0.58 mm ≤ A ≤ 0.62 mm and A/B1 ≥ 1.29, durability
can be improved while a temperature drop in temperature transition is restrained,
and rapid heating-up performance can be further improved.
[0073] While the present invention has been described with reference to the above embodiment
and examples, the present invention is not limited to the above embodiment and examples,
but may be embodied through various improvements or modifications without departing
from the spirit and scope of the invention. For example, the shape of the tube 40
is not particularly limited so long as the tube 40 assumes the form of a tube, and
the section of the tube 40 taken orthogonally to the axial line O may be circular,
elliptic, polygonal, or the like.
[0074] According to the above embodiment, the tube forward portion 43 and the tube rearward
portion 46 have the same outside diameter, and the tube forward portion 43 is smaller
in inside diameter than the tube rearward portion 46, whereby the wall thickness A
of the tube forward portion 43 becomes larger than the wall thickness B of the tube
rearward portion 46. However, the present invention is not limited thereto. Needless
to say, the tube forward portion 43 can be smaller in outside diameter than the tube
rearward portion 46 as in the case of the above examples, or the tube forward portion
43 can be greater in outside diameter than the tube rearward portion 46.
[Description of Reference Numerals]
[0075]
10: glow plug
20: axial rod
40: tube
41: forward end
43: tube forward portion
46: tube rearward portion
51: forward coil
52: rearward coil
O: axial line