FIELD OF THE INVENTION
[0001] The present invention relates to hot air heaters, such as hair driers, desktop hot
air heaters, etc.
BACKGROUND OF THE INVENTION
[0002] Hot air heaters having a heating element such as nichrome wire, wound around an insulating,
fire-resistant substrate such as a mica plate, are generally known.
[0003] Also known are hot air heaters in which a carbon molding is additionally attached
to the hot air nozzle to thereby add far-infrared ray effects produced by the carbon
molding (e.g., Japanese Utility Model Registration Publication
No. 3011964).
[0004] Electromagnetic waves are generally classified into radio waves, infrared rays, visible
light, ultraviolet rays, X-rays and y rays, in order from the longest wavelength to
the shortest (i.e., from the lowest frequency to the highest), and the shorter the
wavelength, the larger the photon energy. When visible light or ultraviolet rays strike
a substance, such electromagnetic waves cause a chemical reaction and deteriorate
the substance. Intense ultraviolet rays, X-rays and γ-rays adversely affect the living
body. Electromagnetic waves with wavelengths longer than infrared rays generally do
not cause chemical reactions, but at high intensities, they heat substances. It has
not been clarified whether electromagnetic waves with longer wavelengths than infrared
rays (radio waves) influence the human body, but studies have been made recently in
many countries on the effects of some types of radio waves on the human body. Some
countries, for example, Sweden, restrict electric fields to a maximum of 0.025 kV/m
and magnetic fields to a maximum of 2.5 mG in the case of radio waves with wavelengths
of 2 to 2000 Hz and at a distance of 50 cm from the human body (SWEDISH BOARD FOR
TECHNICAL ACCREDITATION GUIDELINE: MPR2). Conventional hair driers are said to generate
a magnetic field of about 70 mG at a distance of 50 cm. Further, it has been reported
that electromagnetic waves have caused malfunctions in electronic devices such as
semiconductors, pacemakers, etc.
[0005] Hot air heaters having a carbon molding attached to the hot air nozzle are disadvantageous
in that carbon moldings are expensive and increase the price of the heaters.
DISCLOSURE OF THE INVENTION
[0006] An object of the invention is to provide a hot air heater capable of reducing the
emission of a certain type of electromagnetic wave.
[0007] Another object of the invention is to provide a hot air heater with enhanced infrared
radiation efficiency at low cost.
[0008] To achieve the first object, the hot air heater of the invention comprises an insulating
fire-resistant substrate and heating wires wound therearound, wherein a plurality
of wires that are connected in parallel or series between an input line and an output
line of an electric power supply line are wound around the insulating fire-resistant
substrate in such a manner that the current runs in opposite directions through the
heating wires so that the electromagnetic waves generated from the heating wires cancel
each other out.
[0009] The hot air heater of the invention may be configured in such a manner that a first
heating wire and a second heating wire are connected in parallel between the input
line and the output line of the electric power supply line and are alternatively wound
around the insulating fire-resistant substrate in the same direction and wherein the
adjacent loops of first and second heating wires have the same or substantially similar
winding diameters, in such a manner that the current runs in opposite directions through
the first and second heating wires so that the electromagnetic waves generated from
the heating wires cancel each other out.
[0010] To achieve the second object, the hot air heater of the invention is characterized
by comprising a ceramic honeycomb structure disposed downstream of the heating wire.
[0011] Preferably, the ceramic honeycomb structure has a coating containing carbon powder
and the coated ceramic honeycomb structure has an emissivity of 0.8 or more over the
entire infrared wavelength region.
[0012] More preferably, the coated ceramic honeycomb structure has an emissivity of 0.9
or more over the entire infrared wavelength region.
[0013] Preferably, the coating containing carbon powder is an impregnation coating.
[0014] Preferably, the ceramic honeycomb structure is disposed in the vicinity of the heating
wire.
[0015] Preferably, the ceramic honeycomb structure is coated with a glassy carbon. The glassy
carbon coating is preferably formed by impregnating a ceramic honeycomb structure
with a glassy carbon precursor resin, followed by calcination under a non-oxidizing
atmosphere.
[0016] According to the hot air heater of the invention, electromagnetic waves are weakened
by causing the current to run in opposite directions through adjacent heating wires.
[0017] Further, the infrared radiation efficiency can be enhanced by disposing a ceramic
honeycomb structure downstream of the heating wire.
BRIEF DESCRIPTION OF THE DRAWINGS
[0018]
FIG. 1 is a cut-away view of a first embodiment of the hot air heater of the invention.
FIG. 2 is a conceptual diagram illustrating a method of winding the heating wires
according to the first embodiment.
FIG. 3 is a conceptual diagram illustrating a method of winding the heating wires
according to the second embodiment.
FIG. 4 is a partial broken isometric projection illustrating a method of winding the
heating wire according to the third embodiment.
FIG. 5 is a schematic diagram illustrating a modification of the third embodiment.
FIG. 6 is a schematic diagram illustrating a method of winding the heating wire according
to the forth embodiment.
DETAILED DESCRIPTION OF THE INVENTION
[0019] Embodiments of a hot air heater according to the invention are described below with
reference to FIG. 1 to FIG.6. The embodiments described below illustrate examples
of hair driers. Like numerals represent like elements throughout the drawings.
[0020] A first embodiment of a hot air dryer according to the invention is described first.
As shown in FIG. 1, the hot air dryer 1 comprises an insulating fire-resistant supporter
2 that is wound with heating wires 3. The heating wires 3 are wound to form a coil
along the direction in which hot air flows from the hot air dryer 1 or in the opposite
direction.
[0021] The insulating fire-resistant supporter 2 may be made of a mica plate, a ceramic
plate, or the like. The insulating fire-resistant supporter 2 shown in FIG. 1 is made
of a crisscrossed plate-like body. The heating wires 3 may be composed of a coiled
nichrome wire or the like. In FIG. I, the numeral 4 represents a fan motor, and the
numeral 5 represents a fan.
[0022] The heating wires 3 comprise, as schematically shown in FIG. 2, two wires, a first
heating wire 3a and a second heating wire 3b which are connected in parallel between
an input line 6 and an output line 7 of a power supply line. Note that the heating
wire is shown rather than in a coil shape but by a mere solid line for the sake of
convenience.
[0023] The first heating wire 3a has its input line 6 side wound from the rear end of the
insulating fire-resistant supporter 2 toward the front end thereof, and connected
to the output line 7 at the front end of the insulating fire-resistant supporter.
[0024] In contrast, the second heating wire 3b is connected with the input line at the front
end of the insulating fire-resistant supporter, wound from the front end toward the
rear end, and connected to the output line 7 at the rear end of the insulating fire-resistant
supporter 2.
[0025] The first heating wire 3a and the second heating wire 3b are wound at a desired interval
so that they are alternately arranged. Both the heating wires 3a, 3b are wound in
the same direction. In addition, as shown in FIG.1, the adjacent first heating wire
3a and the second heating wire 3b are wound around the insulating fire-resistant supporter
2 with the same diameter.
[0026] Current flowing in the adjacent first heating wire 3a and the second heating wire
3b as described above is in opposite directions to each other. Note that the power
supply of the hot air heater is generally an alternating-current power supply. In
this case, the current flowing in adjacent heating wires has opposite phases, and
the current flowing in a given period of time is in opposite directions.
[0027] When the current flowing in the adjacent first heating wire 3a is in the opposite
direction to that of the second heating wire 3b, magnetic lines of force and electric
lines of force are cancelled out. This phenomenon is caused by phase inversion of
the electric and magnetic fields.
[0028] Next, the hot air heater according to the second embodiment of the invention is explained
with reference to the schematic diagram shown in Fig. 3.
[0029] As in the first embodiment, the hot air heater of the second embodiment comprises
a first heating wire 3a and a second electric heating wire 3b connected in parallel
between an input line 6 and an output line 7.
[0030] According to the second embodiment, the first heating wire 3a and the second heating
wire 3b are both wound around insulating fire-resistant substrates (not shown), the
second heating wire 3b being wound within the windings of the first heating wire 3a.
The first heating wire 3a and the second heating wire 3b are wound in opposite directions.
The first heating wire 3a and the second heating wire 3b are wound parallel to each
other along the hot air stream direction, forming a concentric circle when viewed
from the front.
[0031] The first heating wire 3a and the second heating wire 3b are each wound around an
insulating fire-resistant substrate (not shown) at regular intervals, preferably,
as close as possible to one another.
[0032] In the second embodiment, the first heating wire 3a and the second heating wire 3b
may be connected to the input line 6 (or output line 7) either at the front-end or
at the rear-end of the insulating fire-resistant substrates.
[0033] In the second embodiment having the above structure, as in the first embodiment,
the directions of the current running through the first heating wire 3a and the second
heating wire 3b are opposite each other, thus enabling reduction of the electromagnetic
waves.
[0034] Although the second embodiment has been described as using two heating wires, one
skilled in the art will understand that four or more even-numbered heating wires may
be employed instead. The number of heating wires can also be three or more odd numbers,
and in such a case, by applying resistance to designated heating wires and thereby
limiting the amount of current, or by other means, the electromagnetic waves generated
from the heating wires can be made to cancel each other out.
[0035] Fig. 4 is a partially broken perspective view illustrating a third embodiment. In
the third embodiment, a single heating wire 3 is connected in series between an input
line 6 and an output line 7. The heating wire 3 is wound into a concentric cylinder-like
form. The heating wire 3 is wound around the inner insulating fire-resistant substrate
2a, folded back at the end, and then wound in the opposite direction around the outer
insulating fire-resistant substrate 2b.
[0036] As schematically shown in Fig. 5, a heating wire 3 on the inner and outer sides may
be cross-wound to provide parallel connections, using the insulating fire-resistant
substrate 2b as an insulating layer. Therefore, the condition that "the current runs
in opposite directions" herein does not necessarily mean that all of the directional
components of the current are opposed each other, but means only that some of them
are opposite. For example, in Fig. 5, the directional components (3ax, 3ay) of the
current in the inner heating wire 3a and the directional components (3bx, 3by) of
the current in the outer heating wire 3b have opposite components 3ay and 3by, whereby
a weakening of the electromagnetic waves is achievable.
[0037] Fig. 6 is a schematic diagram illustrating the fourth embodiment. In the fourth embodiment,
a heating wire 3a wound in the first winding direction and a heating wire 3b wound
in the second winding direction, which is opposite to the first winding direction,
are positioned adjacently and supported by an insulating fire-resistant substrate
2. In the illustrated example, the heating wire 3a and the heating wire 3b are composed
of one heating wire and connected in series between an input line 6 and an output
line 7, and the winding direction of such a heating wire is reversed between the heating
wire 3a and the heating wire 3b. Although not illustrated, the heating wires 3a and
3b may be connected in parallel.
[0038] Further, as shown in FIG. 1, the hot-air heater of the present invention may have
a cylindrical ceramic honeycomb structure mounted in a casing 10. The ceramic honeycomb
structure 9 is disposed downstream of hot air stream from the heating wires 3 and
has a multiplicity of hexagonal apertures formed along the direction of the air stream.
[0039] The ceramic honeycomb structure 9 can be made of SiC, SiO
2, B
4C, AlN, A1
2O
3, MgO and like known ceramic materials; in light of the production costs, cordilite
can be advantageously used.
[0040] It is generally known that heated materials emit radiant energy proportional to the
fourth root of the absolute temperature. In such a case, the radiant energy varies
according to surface state. The higher the emissivity, the greater the radiant energy
will be. The radiant energy approaches a maximum the closer the emissivity of a heating
element is to 1, because an ideal blackbody has an emissivity of 1.
[0041] The ceramic honeycomb structure 9, thus constructed with such an above material,
usually has an infrared radiation emissivity of 0.8 to 0.98. This, however, may be
reduced to 0.7 or lower depending of the wavelength of infrared radiation.
[0042] Carbon powder has a high emissivity over the entire wavelength range. Taking advantage
of this property, a coating containing carbon powder can be applied to the ceramic
honeycomb structure 9 to give an emissivity of preferably 0.8 or higher, and more
preferably 0.9 or higher, over the entire infrared wavelength range.
[0043] Such a coating containing carbon powder can be prepared by mixing and dispersing
carbon powder in a resin binder, applying the obtained mixture to the ceramic honeycomb
structure 9 using a sprayer, brush, etc., or by impregnating the structure with the
mixture as in a dipping method, etc., and by subsequently drying the structure with
the applied mixture coated thereon. Usable carbon powders include noncrystalline substances
such as glassy carbon in addition to crystalline substances such as black-lead. The
coating can also be applied to only one side, e.g. the hot air outlet side, of the
ceramic honeycomb structure 9.
[0044] Stated more specifically, the coating can be prepared by, for example, mixing with
stirring 5 to 30 parts by weight of carbon powder and 100 parts by weight of a room
temperature-setting inorganic/organic hybrid binder (e.g. a phosphate- and polyhydroxybenzene-based
binder: EMULSION TECHNOLOGY CO., LTD.), applying the obtained mixture to the structure
or dipping the structure in the mixture, and air drying.
[0045] The average particle diameter of the carbon powder is preferably approximately 1
to 50
µ m, more preferably approximately 1 to 30 µm, and most preferably 1 to 5 µm. The smaller
are the particles, the more homogeneously the coating can be applied to or impregnated
on the ceramic surface.
[0046] Alternatively, the infrared radiant efficiency can be enhanced without using carbon
powder in the coating. A glassy carbon coating can be formed by, for example, impregnating
the ceramic honeycomb structure with a glassy carbon precursor resin, followed by
calcining under a non-oxidizing atmosphere at a predetermined temperature (approximately
800 °C to approximately 2000 °C) for a certain necessary period of time. A glassy
carbon coating may have a thickness of 5 to 100 µm,
[0047] The glassy carbon coating, when carbonized, will have an enhanced infrared radiation
efficiency, and should exhibit an average emissivity of 0.95 or higher over the entire
infrared wavelength range. For example, such a glassy carbon coating has a radiant
emittance of 1.227 kW/m
2 at ε = 0.95 at 120 °C at the hot air outlet of the hot air heater (1.292 kW/m
2 for a blackbody of ε = 1 over the entire infrared wavelength range beyond a wavelength
of 0.7
µm) .
[0048] Preferable examples of such a ceramic honeycomb structure 9 are those made of porous
materials for better impregnation. Pore diameters are preferably approximately 1 to
50
µm. When the pore diameter of the porous material is smaller than 1 µm, carbon powder
tend to be lumpy. When the pore diameter is greater than 50 µm, inhomogeneous coating
tends to result.
[0049] The ceramic honeycomb structure 9 is positioned downstream of the heating wire 3.
In view of an infrared radiant efficiency, it is preferably disposed in the vicinity
of the heating wire 3, e.g. preferably about 0 to 2 cm from the heating wire 3. When
the heating wire 3 is disposed to wind, for example, cylindrically, the ceramic honeycomb
structure 9 can be disposed in the cylindrical space formed by the wound heating wire
3.
[0050] Measurements were made of the electromagnetic waves of a hot air dryer having the
heating wire configuration shown in Fig. 6 (Example 1) and of a commercially available
conventional hot air dryer wherein all the heating wires are coiled in the same direction
and all electric current flows in the same direction (Comparative Example 1). The
results are shown in Table 1.
[0051] The test conditions were as follows;
Heating wire: 0.3 mm
φ, nichrome wire
Power consumption: 1200 W
Power supply: AC 100 V, 60 Hz
Measuring instrument:
Electric field: ME3 electromagnetic wave measuring instrument produced by Marburg
Technic (Germany)
Magnetic field: EMS tester TES1390 produced by TES Electrical Electronic Corp.
Measurement positions: (A)-(C)
(A): about 5 cm in the blowing direction from the hot air outlet
(B) about 5 cm from the casing surface over the position of the heating wire
(C) about 5 cm from the casing surface over the position of the fan motor
[Table 1]
| |
Example 1 |
Comparative Example 1 |
| Magnetic field (measurement position: A) |
1.5 mG |
22.0 mG |
| Electric field (measurement position: A) |
30 V/m |
90 V/m |
| Magnetic field (measurement position: B) |
4.0 mG |
30 mG |
| Electric field (measurement position: B) |
80 V/m |
100 V/m |
| Magnetic field (measurement position: C) |
60. 0 mG |
6 0 mG |
| Electric field (measurement position: C) |
100 V/m |
110 V/m |
[0052] The results in Table 1 show that in Example 1, the magnetic field and electric field
decreased sharply at the measurement position (A).
[0053] Since, in a hair dryer or the like, the hot air outlet is closest to the human body,
it is important that the electromagnetic waves at the measurement position (A) be
small. Although the measurements in Table 1 were carried out without grounding, the
electric field will be further decreased if measurements are carried out with the
hot air heater grounded.
[0054] Next, comparative experiments with ceramic honeycomb structures were conducted to
compare those having a carbon powder coating with those having no carbon powder coating
in terms of infrared emissivity.
Example A of a ceramic honeycomb structure
[0055] Graphite powder (1 g) (average particle diameter: 12 µm) was mixed into a resol-type
type phenol resin methanol solution (10 g) (resin content: 50 wt%) . A ceramic honeycomb
structure (diameter: 3 cm) comprising cordierite was coated with this mixture by impregnation
and dried. The resulting product had an infrared emissivity of 0.96.
Example B of a ceramic honeycomb structure
[0056] A solution of a resol-type phenol resin in methanol was adjusted to a resin solid
content of 30 wt%, giving a glassy carbon precursor resin. A mullite honeycomb structure
was impregnated with the glassy carbon precursor resin, dried, and then cured at 150°C.
After this was calcined in nitrogen gas from room temperature to 1000°C over 12 hours,
the temperature was lowered to room temperature over 8 hours, thereby coating the
mullite honeycomb structure with glassy carbon. The resulting mullite honeycomb structure
coated with glassy carbon had an infrared emissivity of 0.95.
Example C of a ceramic honeycomb structure
[0057] A solution of resorcin (1 mol), terephthalaldehyde (1.5 mol), and curing accelerator
(p-toluenesulfonic acid) (0.01 mol) in ethanol was adjusted to a resin solid content
of 30 wt%, giving a glassy carbon precursor resin. A mullite honeycomb structure was
impregnated with the glassy carbon precursor resin, dried, and then left at room temperature
for 5 hours to be cured. After this was calcined in nitrogen gas from room temperature
to 1000°C over 12 hours, the temperature was lowered to room temperature over 8 hours,
thereby coating the mullite honeycomb structure with glassy carbon. The resulting
mullite honeycomb structure coated with glassy carbon had an infrared emissivity of
0.95.
[0058] In contrast, uncoated ceramic honeycomb structures as comparative examples of ceramic
honeycomb structures had an infrared emissivity of 0.87 to 0.89.
[0059] The measurements of infrared emissivity were carried out using an IT-540N radiation
thermometer (product of Horiba, Ltd.) in the following manner: (1) A black body spray
was applied to part of the object to be measured, and the object was then heated.
(2) The part to which the black body spray had been applied was subjected to measurement
using an IT-540N radiation thermometer with the emissivity of the black body spray
being the emissivity set value. (3) A part to which the black body spray had not been
applied was subjected to measurement, adjusting the emissivity set value such that
the measurement value was equal to the already measured temperature of the part to
which the black body spray had been applied. (4) The emissivity obtained by adjustment
was taken as the emissivity of the object.