[0001] The present invention relates to CRT display apparatus, and more particularly relates
to apparatus for reducing unwanted magnetic radiation external to a cathode ray tube
display device without affecting the intended electron beam deflection magnetic field
within the device.
[0002] Cathode ray tube (CRT) display apparatus generally has associated coils, or yokes,
to provide a varying magnetic field for electron beam deflection, for example for
a raster scan. In addition to manifesting itself within the CRT, for beam deflection,
this magnetic field also extends around the outside of the CRT and beyond the display
apparatus. This external magnetic field serves no useful purpose and an effort is
frequently made to reduce this unwanted magnetic field. In particular the unwanted
frequency range is from 1K to 350K hertz (VLF).
[0003] A. A. Seyno Sluyterman of Phillips describes the radiated field due to the horizontal
deflection system in his paper entitled "The Radiating Fields of Magnetic Deflection
Systems and Their Compensation" presented in 1987 SID Society of Information Display
Proceedings. That paper shows that the radiated field of the horizontal magnetic circuit
of the yoke at mid-range resembles a vertically oriented dipole, whose mathematical
centre lies on the long axis slightly ahead of the yoke.
[0004] The use of Helmholtz coils to provide reduction of this radiation is proposed in
this paper. In one case the Helmholtz coils are "on top" and "below" a saddle-shaped
deflection yoke. In another case the Helmholtz coils are behind the yoke. The Helmholtz
coils are coupled to the deflection coils and an EMF is induced in the Helmholtz coils,
giving rise to a magnetic field which tends to cancel the unwanted radiated magnetic
field. However, this is a relatively expensive and bulky solution to the problem.
A similar top and bottom coil configuration is in published Finnish Patent Application
861458, April 4, 1986 of Nokia.
[0005] Another proposed solution is the placement of shielding all around the CRT, which
results in magnetic radiation reduction from the eddy currents induced in the shielding.
However, this is also an expensive solution to the problem, and results in only minimal
reduction in the magnetic field in front of the screen.
[0006] Accordingly, there is a need for means to reduce to acceptable levels the residual
magnetic field in front of the cathode ray tube display apparatus that provides an
inexpensive and compact solution to the problem.
[0007] EP-A- 302995 discloses the use of a magnetic shunt in the form of a ring of magnetic
permeable material located between the deflection coil and the viewing screen of a
CRT display apparatus in order to reduce unwanted magnetic radiation which extends
outside the CRT.
[0008] While this is acceptable for many applications other physical constraints such as
the shapes of the coils, the tube or the presence of wedges for deflection coil alignment
can prevent sufficient coupling of the ring to the coil.
[0009] The object of the present invention is to provide an improved arrangement for reducing
the unwanted magnetic radiation which extends outside a CRT display apparatus.
[0010] The present invention relates to a cathode ray tube display apparatus comprising
a cathode ray tube including a viewing screen, means for producing a charged particle
beam directed at the screen from the rear thereof and aligned with a central axis
of the apparatus, deflection coils generating a first magnetic field which extends
within the tube for deflecting the beam across the screen and a second magnetic field
which extends outside the tube, and means for reducing the second magnetic field which
extends outside the tube including a ring of magnetically permeable material centred
substantially on the central axis and positioned adjacent to the coil.
[0011] According to the invention the apparatus is characterised in that the means for reducing
the second magnetic field comprises at least one pair of wire loops extending round
and through the ring and electrically connected to the deflection coils so as to induce
a magnetic field within the ring to counteract and reduce the second magnetic field
which extends outside the tube but to have negligible effect on the first magnetic
field within the tube.
[0012] In order that the invention may be more readily understood an embodiment will now
be described with reference to the accompanying drawings in which:
Fig. 1 is a diagram showing pertinent portions of the deflection yoke of a CRT display
apparatus,
Fig. 2 is a simplified diagram of one winding each from the upper and lower horizontal
deflection coils of the deflection yoke shown in Fig. 1,
Fig. 3 is a computed plot showing the magnetic field intensity along the Z axis for
a typical deflection yoke such as is shown in Fig. 1,
Fig. 4 is a diagram showing a CRT yoke like that of Fig. 1, having added thereto a
radiation reducing ring 50,
Fig. 5 is a diagram like that of Fig. 2, having added thereto a radiation reducing
ring 50,
Fig. 6 is a set of curves, on the same set of axes as in Fig. 3, showing the effect
on the net field A of ring 50,
Fig. 7 is a set of curves showing the effect of ring 50 on the end turn field shown
in Fig. 3,
Fig. 8 is an expanded view of the portion of the curve shown in Fig. 6 beyond approximately
2.5 centimetres along the Z axis,
Fig. 9 is a plot like that of Fig. 8, wherein ring 50 is a slightly different distance
from the deflection yoke,
Fig. 10 is a diagram like Fig. 8, in which the inner diameter radius of ring 50 is
slightly different from that of Fig. 8,
Fig. 11 is a curve like that of Fig. 8, but wherein the distance of the ring 50 from
the end of the deflection yoke is different from that of Fig. 8 and Fig. 9,
Fig. 12 is a diagram showing a CRT display apparatus with a deflection yoke having
a ferrite core and the associated fields,
Fig. 13 illustrates the system of Fig. 12 with the radiation reducing ring 50,
Fig. 14 is a sketch of a plan view of the core and coil of the deflection yoke and
the radiation reducing ring of Fig. 13 illustrating induced magnetization currents
and magnetic fields,
Fig. 15 is a sketch of a front view of the arrangement in Fig. 14 illustrating induced
magnetization currents and magnetic fields,
Fig. 16 shows a preferred embodiment of the radiation reducing ring for colour tubes
in which the ring is split providing two portions,
Fig. 17 is a sketch of the split ring illustrated in Fig. 16 showing the shunt fields
across the base of the tube,
Fig. 18 is a cross-sectional diagram through a portion of a still further embodiment
of the radiation reducing ring, made with conventional µ metal laminates,
Fig. 19 shows a further embodiment of the ring, having a hexagonal shape,
Fig. 20 is a top view of a CRT, with deflection coils, radiation ring and additional
wire loops,
Fig. 21 is an electrical schematic diagram of the arrangement illustrated in Fig.
20,
Fig. 22 is a diagram of one winding of each of the upper and lower horizontal deflection
coils of the arrangement illustrated in Fig. 20 with the wire loops connected thereto,
Fig. 23 is an end view of the ring in Fig. 20 illustrating the pair of loops.
Fig. 24 is a sketch of a further arrangement of the ring with quadrature placed pairs
of holes through the ring through which the wire loops are passed, and
Fig. 25 is a sketch illustrating how the wire loops pass through the holes in the
ring in Fig. 24.
[0013] Fig. 1 shows the pertinent portions of the deflection yoke of a CRT display apparatus
10 which includes a CRT 12, having a front screen 14, and upper and lower horizontal
deflection coils 16, 18. The deflection coils 16, 18 generate a varying magnetic field
between them, inside CRT 12, to deflect an electron beam within the tube 12 for horizontal
sweeping across the fact of the screen 14, as is well known in the art.
[0014] Fig. 2 is a simplified diagram of one winding each from the upper and lower deflection
coils 16, 18 of Fig. 1. Thus, loop 20 is a single loop from coil 16, while loop 22
is a single loop from coil 18. As illustrated, a current i flows through each of the
coils so as to generate the above described varying magnetic field for horizontal
deflection of the electron beam.
[0015] In Fig. 2, X, Y, and Z are axes having their common origin in the plane of circumferential
coil portions 34, 38 of loops 20, 22 and centrally located between them. The X axis
coincides with the central axis of CRT 12 (Fig. 1). Note that the upper and lower
loops 20, 22 are symmetrical about the X-Z and Y-Z planes.
[0016] In actual operation the upper and lower loops 20, 22 are interconnected to produce
a dipole field on the Z axis as is known. From the known coil shape and current, the
B field is given by:

where J is the current, R is the direction and R is the distance to a point of interest
P on the Z axis. This equation is used in computing the field distribution of Figs.
3 and 6 to 11.
[0017] A plot of the computed B field distribution of an air core horizontal deflection
coil, such as is shown in Fig. 1, without any high permeability material, like ferrite
shielding, is shown in Fig. 3. The actual B field is a directional field, and the
plot shown in Fig. 3 shows only the magnitude, or intensity, of such a magnetic field
along the Z axis. The units depicted in the horizontal axis are centimetres, while
the units in the vertical axis are gauss. The curve reflects a typical coil having
current flowing so as to produce a field which deflects a 20 kilovolt electron beam
to an angle of about 40 degrees.
[0018] Curves A, B, and C of Fig. 3 represent the total field, the partial field from the
axial wires and the partial field from the end turns, respectively. Curve A is the
magnitude along the Z axis of the vector sum of the fields represented by curves B
and C. In typical uncompensated yokes, at a distance of 55 centimetres in front of
the yoke the field can be in the range of approximately 1,000 - 2,000 nano- Tesla.
Clearly, this is not a very large magnetic field. However, in accordance with the
arrangements described herein this field can be reduced to an even smaller quantity.
In actual experiments using the arrangements described below, reduction to below 200
nano-tesla at 55 centimetres was measured.
[0019] Fig. 4 shows the apparatus 10 of Fig. 1 having added thereto a ring 50 of linear
ferrite operating as a magnetic shunt, in accordance with the arrangement described
in EP-A- 302995.
[0020] Fig. 5 shows the loops 20, 22 of Fig. 2, with the ferrite ring 50 disposed in front
thereof, to illustrate the relative shape and position of ring 50.
[0021] Ring 50, as mentioned above, is made from linear ferrite. Linear ferrite is a well
known material commonly used in transformer and yoke production. According to a preferred
embodiment the ring 50 has a relatively high magnetic permeability, (µ above 2,500).
It also has a high volume resistivity, for example 1 Meg Ohm or more per cubic centimetre.
The high resistivity value keeps eddy currents induced in the ring at a minimum. Otherwise
the loading effects on the yoke would result in a need for more energy to drive the
yoke. While embodiments could be constructed, for example out of conventional µ laminates,
having this loading effect, it was deemed desirable to keep the eddy currents low,
and avoid this loading effect in the arrangement described. The cross section of the
ring 50 is large enough to avoid saturation.
[0022] Fig. 6 is a set of curves, on the same set of axes as those of Fig. 3, showing the
effect along the Z axis on the net field A shown in Fig. 3 of a flat ring, such as
ring 50 in Fig. 4. Curve A in Fig. 6 is the same as curve A in Fig. 3. Curve D in
Fig. 6 represents the field contribution from the magnetization effect of the ring
50, while curve E represents the resultant curve from the combination of curves A
and D.
[0023] To better understand the effect of field D on the overall magnetic field A, a set
of curves is shown in Fig. 7 including curve D, and the end turn magnetic field component
C. Curve C is the same curve C as shown in Fig. 3. Curve F is a curve representing
the resultant field from the combination of curves D and C. Note that in Fig. 7 the
horizontal axis scale is the same in Figs. 3 and 7 while the vertical axis scale has
been expanded, to aid in clarity.
[0024] As mentioned above, curve D is the theoretical field produced by the ring 50 alone.
This is an intrinsic field which is created by the magnetization force of the end
turn field. It should be noted that the presence of the ring attenuates the end turn
field. The degree of attenuation is controlled by the variables such as ring dimensions
and ring yoke separation, as is discussed in more detail below. It should be further
noted that the end turn field combines with the main deflection field in the area
in front of the CRT screen, to form the net measurable residual field whose reduction
is an object of this invention. At optimum attenuation, the modified end turn field
F is equal in magnitude but opposite in direction to the main deflection field, resulting
in a zero vector sum. As a practical matter, the net measurable residual field in
front of the CRT screen can never be reduced to zero. However, by application of the
principles described in EP-A- 302995, this field can be reduced to very small levels.
[0025] The portion of Fig. 6 beyond approximately 2.5 centimetres to the right thereof along
the Z axis is shown in Fig. 8. In order to see clearly the curve behaviour in that
region, the scale is expanded in the vertical direction as compared with Fig. 6. Curves
A and E are described in connection with Fig. 6. Curve D is not shown in this figure
in the interest of providing more clarity for curves A and E. Note that curve E is
very nearly at a zero field magnitude at approximately 9.5 centimetres along the Z
axis.
[0026] The compensated curve E is for a typical CRT-yoke configuration, having a ring 50
of ferrite with a permeability of 1,000 - 3,000 and high volume resistivity, and having
an inner dimension of 4 centimetres, a thickness of 0.2 centimetres, and a width of
1 centimetre, placed at a distance of 0.4 centimetres from the end of the yoke. As
illustrated herein, the term "width" of the ring refers to its radial extent from
inner surface to outer surface.
[0027] Figs. 9 - 11 are plots like the plot shown in Fig. 8, for slightly different ring
configurations from the configuration producing the curves of Fig. 8. Thus, in Fig.
9 all of the parameters for the ring 50 are the same as those corresponding to Fig.
8, except the distance of the ring from the end of the yoke. In Fig. 9 the curves
correspond to a configuration in which this dimension is 0.3 centimetres. It will
be appreciated that this reveals over-compensation, as the curve E′ is slightly above
the horizontal axis, for example at 9.5 centimetres, and slightly above curve E in
Fig. 8.
[0028] The curves of Fig. 10 are for a configuration in which the dimensions of the ring
50 are the same as those corresponding to Fig. 8, but wherein the inner surface radius
is 5 centimetres, instead of 4 centimetres. It can be seen that significantly less
compensation is provided, as curve E˝ is here below the horizontal axis.
[0029] Fig. 11 shows a curve for a configuration wherein the dimensions of ring 50 are as
in Fig. 8, but wherein the distance of the ring from the end of the yoke is 0.6 centimetres,
instead of 0.4 centimetres. It can be seen that slightly less compensation is provided,
causing curve E‴ to cross the horizontal axis at 9.5 centimetres along the Z axis.
This was deemed to represent optimum compensation.
[0030] While curves are not provided showing the effect of change of width of the ring 50
on the compensation or field reducing effect, in general decreasing the width will
tend to reduce the compensating effect, while increasing the width will tend to increase
the compensating effect.
[0031] Thus, from the above Figs. 8 - 11 it will be appreciated how changing the various
dimensional parameters of the ring 50 affects the performance of the ring in compensating
by reducing the magnetic field components on the X axis in front of the screen due
to the yoke winding and components. Through an understanding of these effects, a skilled
person practising implementing the principles described herein can provide the adjustments
deemed desirable to optimize the compensation or reduction affect.
[0032] In the above described arrangement the CRT tube 10 has air core horizontal deflection
coils without any high permeability shielding about the neck of the tube. The direction
of the horizontal deflection field to move the electron beam toward the right edge
of the screen as viewed from the front is represented by arrow 70 in Fig. 12. In common
commercial type yokes the horizontal deflection coils have ferrite shielding (ferrite
core) 68 about the horizontal deflection coils as shown in Fig. 12. There are also
vertical deflection coils (not shown) positioned about the horizontal deflection coils
and under the ferrite core. The magnetic field produced by the horizontal coils with
the end loops 32, 34, 36 and 38 extending beyond the ferrite core includes a radiated
field which is in the form of a dipole centred forward of the deflection coil loop
nearest the screen as shown by arrows 70a in Fig. 12 and this radiated field extends
outside the CRT display apparatus. Note the ferrite core 68 reverses the polarity
of the radiated field.
[0033] In order to reduce the radiated field which is unwanted, a ferrite ring 50 as shown
and illustrated in Fig. 13 is mounted forward of the horizontal deflection coils near
the centre of the radiated field produced by the horizontal coils. The manner in which
this ring compensates for or reduces the radiated field without measurably affecting
the deflection field is illustrated in connection with Figs. 14 and 15.
[0034] Fig. 14 is a sketch of a plan view of the deflection coil 16, ferrite core 68 and
ferrite ring 50 illustrating the deflection current in the deflection coil, the magnetization
currents induced in the ferrite components and the resulting magnetic fields. Fig.
15 is a front view of the arrangement illustrated in Fig. 14.
[0035] The counterclockwise current in the horizontal deflection coil 16 seen in the plan
view is represented by 71. The magnetic field produced by this current is represented
by O
H and is directed up out of the Figure towards the viewer. This corresponds to the
arrow 70 in Fig. 12. The ferrite core 68 is magnetically coupled to the deflection
coil 16 and there is induced in the core 68 an even stronger equivalent magnetization
current M₁ represented by the heavy lines 72. The induced current 72 circulates in
the opposite direction (clockwise in Fig. 14) with the currents along the adjacent
surfaces of the coil and the core flowing in the same direction. The result is a first
magnetic field X₁ (with a direction into the Figure as viewed) in the centre of the
core. The field X₁ combines with field O
H and produces a net radiated field O₁ equivalent to the radiated field 70a of Fig.
12 which is the vector sum of O
H and X₁ in front of the ring 50. The radiated field O₁ is a dipole field and is the
major component of the unwanted magnetic radiation extending outside the CRT display
apparatus. The exposed end turns of the deflection coils 16, 18 are also radiating
a minor quadrapole magnetic field which is designated an X
E. Symbols "X" and "O" which are consistent with the sign convention established earlier
where X means the field is pointing down into the Figure, and O means the field is
pointing up towards the viewer. The sum of X₁ and X
E is the total radiated magnetic field without considering the effect of the ring 50.
[0036] When a ferrite ring 50 is placed in front of the yoke as illustrated in Figs. 13
and 14 the ring will be magnetized as described below. Magnetization currents M₁ in
the yoke shield 68 induce equivalent magnetization currents M₂ in the ring 50 in the
counter clockwise direction. The resulting field is pointing up within the ring (O₂)
and pointing down outside the ring (X₂) as illustrated in Fig. 14. The polarization
of this field is also indicated in Fig. 15 with "N" (north) on top and "S" (south)
on the bottom of the ring.
[0037] The front end-turns of the horizontal deflection coils 16, 18 (top, bottom) induce
equivalent magnetization currents M₃ in the ring 50 in a clockwise direction. The
resulting field is pointing down within the ring X₃ and pointing up outside of the
ring O₃ as illustrated in Fig. 14. The polarization of this field is also shown in
Fig. 15 with letters "N′" (north) and "S" (south).
[0038] From the distribution and polarization of the induced magnetization current end fields
it can be concluded that the induced field X₁ in the yoke shield 68 sets up a dipole
magnetization O₂ in the ring 50 which opposes the radiated dipole field O₁. Similarly,
the quadrapole component X
E of the radiated field due to the exposed end-turns of the horizontal deflection coils
16, 18 induces a quadrapole magnetization in the ring 50 which cancels the radiated
quadrapole field.
[0039] Variables such as the thickness, inside diameter, outside diameter and permeability
of the ring 50 and yoke-ring separation can be selected so as to tune for optimum
performance (reduction of the unwanted radiated field). Naturally, the lower limits
of the ring dimensions are dictated by the given CRT and yoke combination. In practice,
the tendency is to bring the ring 50 as close to the front of the yoke as possible
without adversely effecting the deflection field within the tube. This reduces the
ring dimensions and ensures minimum cost. The ring has a lower limit of permeability
of about 1,000 with the ring placed closest to the yoke. The higher the permeability
the greater the distance the ring can be from the yoke.
[0040] Despite the effort to eliminate interference between the ring 50 and the main horizontal
deflection field, it was found that the presence of the solid ring moves the centre
of deflection of the vertical deflection field slightly back toward the electron gun.
This is not noticeable in a monochrome system. However, it causes about 10⁻⁶ metre
mis-registration in a colour system and that is detectable. This problem is avoided
by using a split ring configuration, see Fig. 16. Here, part of the radiated dipole
field which is normally conducted by the ring is forced to enter the bore as shown
in Fig. 17 and to join and strengthen the vertical deflection field, thereby causing
the centre of vertical deflection to move forward. In practice, it was found that
a 2mm air-gap can compensate for the 10⁻⁶ metre mis-registration.
[0041] In an actual prototype experiment, in conjunction with a CRT display apparatus manufactured
by Matsushita Company having a serial number of M34JDJ00X1, a ferrite ring 50 of ordinary
linear ferrite was provided, having a µ of approximately 1,000 - 3,000 and a volume
of resistivity of greater than 1 meg ohm per cc, with ring dimensions of: an inner
dimension of 4-3/8 inches (11 cms), a width of 3/8 inches (1 cm), and a thickness
of 1/8 inch (0.3 cm). This ring was found to produce excellent radiated field cancellation
effects when it was placed against the circumferential wire portions (end closest
to the screen) of the yoke provided with this CRT display apparatus with spacing resulting
only from the insulation of the yoke wires.
[0042] Embodiments of the ring 50 may be made with conventional µ metal laminates, yielding
rings having a cross-section as shown in Fig. 18.
[0043] Fig. 19 shows a hexagonally shaped ring, representing a still further embodiment
for use with, for example, a hexagonally configured yoke.
[0044] As mentioned above, the compensation effect of the ring 50 is dependent on its width
and other dimensions and on its material. These factors and the spacing of the ring
50 from the end turns of the deflection coils can be overcome by coupling a pair of
wire loops 210, 211 about the ring 50 as shown in Figs. 20 - 22. Fig. 20 is a top
view of the deflection yoke, the tube and the ring. Fig. 21 is an electrical diagram
showing the terminals. Terminal 1 is coupled to one end of the driver for the deflection
coils and terminal 4 is the return to the driver. "Upper" refers to the upper yoke
coil and "Lower" refers to the lower yoke coil. Fig. 22 illustrates an upper yoke
coil 220 and a lower yoke coil 221.
[0045] The first loop 210 begins at terminal 1 on the rear bundle terminal, passes clockwise
round and through the ring 50 and terminates at terminal 2. The upper and lower yoke
coils are connected in parallel at one end to terminal 2 and at the other end to terminal
3. The second loop 211 extends from terminal 3 and passes clockwise round and through
the ring 50 on the opposite side of the ring from loop 210 (diametrically opposite
positions in the horizontal plane) and terminates at terminal 4. In this manner the
loops 210, 211 are in series with each other and in series with the parallel yoke
coils. An end view of the ring 50 as seen from the screen with the loops 210, 211
is illustrated in Fig. 23. Note the directions of arrows 215 and 216 match in Figs.
20 and 22.
[0046] In accordance with another arrangement, compensation for the quadrapole radiated
field can be by the loops 210, 211 passing round and through the ring 50 and also
through quadrature placed holes 218 in the ring 50 as shown in Figs. 24 and 25 before
returning to the terminals 1, 2, 3, 4 illustrated in Fig. 20.
[0047] It is recognized that the ring 50 may be any of the shapes, sizes, dimensions and
material discussed herein and that the number of loop turns can be selected according
to the required coupling to achieve the desired reduced radiation.