Method of manufacturing a saddle-shaped deflection coil for a picture display tube and display tube comprising a deflection system using saddle-shaped deflection coils

Abstract: Method of continuously winding in a gap-shaped winding space a saddle-shaped, flared deflection coil having a flange-shaped connection portion at its widest end extending transversely to the longitudinal axis. Since at least one symmetrical pair of pins is introduced at the front end of the coil into the winding space transversely to the plane of the flange-shaped connection portion and at least one further symmetrical pair of pins is introduced at the front end of the coil into the winding space transversely to the plane of the longitudinal turns, the designer of the coil is given an extra modulation possibility which can be utilized, for example to further reduce the east-west raster distortion.

Description: The invention relates to a method of continuously winding a saddle shaped deflection coil, flaring out from a rear end towards a front end along a longitudinal axis, for use in a display tube which coil comprises a flange-shaped connection portion at its front end extending transversely to said longitudinal axis and longitudinal turns which are distributed over a number of sections, in which the number of turns required for a coil section are wound in a winding space, in which at least one pair of pins is introduced at the front end into the winding space along the boundary of said coil section at positions located symmetrically relative to the longitudinal axis, and in which the number of turns required for a next section are wound in said winding space and around said pins such that each turn of said next section surrounds the turns of the preceding section and both said sections are separated over part of their length by an aperture. The above-mentioned method is commonly used for winding saddle-shaped coils (see, for example, EP-A-0 159 065). In this method the properties of the coil may be influenced by determining the position of the open spaces during the design and by choosing the number of turns per section during winding. In many cases this provides the possibility of adapting the distribution of the magnetic flux generated by the coil to the requirements imposed. However, it has been found that this possibility is not adequate in all cases, particularly when more refined corrections are to be performed. Such corrections are necessary, for example, if the east-west raster error is to be reduced in colour display tubes of the in-line type. Increasingly stringent requirements are imposed on the performance of colour display tubes using electromagnetic deflection units, particularly when they are used in monitors. Stringent requirements are imposed, for example on the shape of the raster. In conventional TV receivers or in monitors a raster is constituted by causing an electron beam to scan the front plate of the display tube. The (geometrical) raster errors which may occur are north-south raster errors (errors on the upper and lower side of the raster) and east-west raster errors (errors on the left and right-hand side of the raster). In colour display tubes having an in-line arrangement of the electron guns the east-west raster error becomes manifest as a pincushion or barrel-shaped distortion of the left and right-hand boundary of the raster scanned on the display screen. It is an object of the invention to improve the method of the type described in the opening paragraph in such a way that the designer of the coil is given an extra possibility to influence the distribution of the generated magnetic flux. To this end the method according to the invention is characterized in that at least one pair of pins is introduced at the front end of the coil into the winding space in a direction which is transversely to the plane of the flange-shaped connection portion, and in that at least an additional pair of pins is introduced at the front end into winding space in a direction which is transversely to the plane of the longitudinal turns of the coil. The method according to the invention is applicable to winding field deflection coils as well as line deflection coils. At positions where pins are introduced near the front end into the winding space transversely to the plane of the flange-shaped connection portion of the coil, the transition between the longitudinal part of a turn and the flange-shaped connection portion will be at a different axial position (further to the front) in the method according to the invention than at positions where pins are introduced near the front end transversely to the plane of the longitudinal parts of the turns. This creates an extra field modulation, because a stronger deflection field component is locally produced at positions where the said transition is located further to the front. It depends on the radial position of the said transition which field component is additionally generated. This provides the possibility of giving, for example a field deflection coil of the saddle type such a distribution of turns near its front end by selectively using the directions of positioning the pins during winding that, upon energization, an extra strong positive six-pole component is generated with which the east-west raster distortion is reduced. For a setmaker this means that he can omit certain raster correction magnets or raster correction circuits hitherto required. A preferred embodiment is characterized in that the at least one pair of said pins is introduced transverse to the plane of the flange-shaped connection portion at angular positions of approximately 30° relative to the longitudinal axis. Another preferred embodiment is characterized in that the additional pairs of said pins are introduced transverse to the plane of the longitudinal parts of the turns at angular positions of approximately 15°, 40°, 50° and 60°, respectively, relative to the longitudinal axis. Some embodiments of the invention will now be described in greater detail with reference to the accompanying drawings in which Fig. 1 is a longitudinal cross-section of a part of a picture display tube including a deflection system; Fig. 2 is a perspective elevational view of a deflection coil wound according to the invention; Fig. 3 is a perspective rear view of a deflection coil wound according to the invention; Fig. 4 is a diagrammatic rear view of a cross-section through the deflection coil of Fig. 3; Fig. 5 is a cross-section of a winding jig for use of the method according to the invention. Fig. 1 shows a colour display tube 1 comprising an electron gun system 2 for generating three electron beams directed towards a display screen 3 having a repetitive pattern with red, green and blue phosphor elements. An electromagnetic deflection system 4 is arranged coaxially with the axis of the tube around the path of the electron beams between the electron gun system 2 and the display screen 3. The deflection system 4 comprises a funnel-shaped synthetic material coil support 5 supporting on its inside a line deflection coil system 6, 7 for deflecting the electron beams generated by the electron gun system 3 in the horizontal direction. The flared line deflection coils 6, 7 are of the saddle type and have a front flange 8, 9 at their widest end, which flange is substantially transverse to the axis 10 of the display tube. At their narrowest end the coils 6, 7 comprise packets of connection wires 11, 12 interconnecting the axial conductor packets of each of the coils 6, 7 and being arranged substantially parallel to the outer surface of the display tube 1. In the case shown the coils 6, 7 thus are of the type having a "lying" rear flange and an "upstanding" front flange. Alternatively, they may be of the type having both an upstanding rear flange and an upstanding front flange. On its outer side the coil support 5 supports two saddle-shaped field deflection coils 14, 15 for deflecting electron beams generated by the electron gun system 3 in the vertical direction. A ferromagnetic annular core 13 surrounds the two coil assemblies. In the case shown the field deflection coils are of the type having an upstanding front flange 16, 17 and a lying rear flange. Alternatively, they may be of the type having both an upstanding rear flange and an upstanding front flange. Fig. 2 shows a field deflection coil in an elevational view, that is to say, viewed from the right in Fig. 1. This coil comprises a number of turns of, for example copper wire and has a rear end portion 18 and a front end portion or flange 17 between which two active portions 21, 22 extend on either side of a window 19. As is apparent from Fig. 1, the front end portion 17 is "upstanding" so that its wires are further remote from the electron beams to be deflected than in the case that it would be "lying". In the embodiment shown the rear end portion 18 "is lying". It will be clear that using a coil having an upstanding rear end portion or a lying rear end portion is a design parameter which is not connected with the measures according to the invention. All these possible embodiments are comprised under the term "saddle-shaped" deflection coils. The coil 15 flares out from the rear to the front so that it is adapted to the trumpet shape of the portion 5 of the picture display tube. The magnetic flux required for the vertical deflection of the electron beams is substantially entirely generated in the active portions 21, 22. The flux generated in the end portions 18 and 17 substantially does not contribute to the deflection. Each of the active portions 21, 22 has apertures near the front end. These apertures divide the coil 15 into a number of sections, as is even more clearly shown in Fig. 3, and the field deflection coil 15 shown by way of example has six sections. Each turn of a section surrounds the turns of the sections located more inwards (closer to the window 19). By choosing the number, the position and the shape of the apertures near the front end as well as the number of turns in each of the sections, a designer can influence the distribution of the magnetic flux generated in the active portions 21, 22 to a considerable and very accurate extent. It is very favourable that the axial position of the transition between the active turn portions and the flange can be varied. This freedom of choice gives the designer a considerably greater influence on the distribution of the generated magnetic flux during the winding operation. The winding operation itself will now be described with reference to Figs. 4 and 5. Fig. 4 is a partial rear view of a cross-section of the coil shown in Fig. 2 during the winding operation. Winding is effected in a winding space which is recessed in a jig 50 shown in Fig. 5, which forms part of a winding machine. To simplify the Figure the winding machine is not shown. The jig 50 comprises two halves 51 and 52 between which a winding space 53 is recessed and which is bounded by walls 54, 55 whose shape corresponds to the outer boundaries of the coil to be wound. During the winding operation the inner coil section 27 is wound first, for example around a mandril defining the shape of the window 19. As soon as the number of turns required for the section 27 is reached, pins 37 which are approximately perpendicular to the plane of the turns are substantially simultaneously introduced into the winding space at the boundary between this section and the next section 29. The first turn of the next section 29 is now laid around the pins 37 so that the apertures 23 are created between the sections 27 and 29 in the active portion 21. After the required number of turns of the second section 29 is reached, pins 39 which are approximately perpendicular to the plane of the turns are introduced in an analogous manner into the winding space at the boundary between this section and the next section while the first turn of the third section 31 is laid around these pins. This creates the apertures 25. Winding is effected continuously, that is to say the wire runs uninterrupted from one section to the next. The apertures 23 and 25 approximately have the shape of a triangle. One side of this polygon coincides with the last turn of the section preceding the relevant aperture and the other sides coincide with the first turn of the section following the aperture. The variation of the last turn of a section is determined by the location of the preceding turns of this section and this variation will generally not be strictly rectilinear but slightly curved. In the example of Fig. 4 pins 41 which are also perpendicular to the plane of the turns are introduced into the winding space after providing section 31, whereafter section 33 is wound. The subsequent pins 43 are not introduced approximately perpendicularly to the plane of the turns but approximately perpendicularly to the plane of the flange, as will be explained with reference to Fig. 5. The transition between the axial portions of the turns to the flange portion will therefore be located further to the exterior so that a field modulation can be realised. In a field deflection coil the pins 43 may be arranged, for example in a radial position of approximately 30° so as to locally generate an extra positive six-pole component (for reducing the east-west raster distortion). In such a design of the field deflection coil the pins 37, 39, 41 and 45 (not referred to) may be located at angular positions of approximately 60°, 50°, 40° and 15° relative to the longitudinal axis. The winding method according to the invention may, however, also be used to advantage when winding line deflection coils. When magnetic fields having different properties must be generated, the pins may of course be introduced at different positions. The number of pins may differ from the number given in the example. The coil described with reference to Figs. 4 and 5 is symmetrical with respect to the x-z plane, i.e. the apertures 23, 25 located to the left and right of this plane are inverted images of each other and the number of turns in the section portions located on either side of this plane is the same.

Claims: A method of continuously winding a saddle shaped deflection coil (9, 15), flaring out from a rear end (18) towards a front end along a longitudinal axis, for use in a display tube, which coil comprises a flange-shaped connection portion (17) at its front end extending transversely to said longitudinal axis (10) and longitudinal turns which are distributed over a number of sections (27, 29, 31, 33), in which the number of turns required for a coil section (27, 29, 31, 33) are wound in a winding space (53); at least one pair of pins (37, 39, 41, 43) is introduced at the front end into the winding space along the boundary of said coil section at positions located symmetrically relative to the longitudinal axis (10); and the number of turns required for a next section (29, 31, 33) are wound in said winding space (53) and around said pins such that each turn of said next section surrounds the turns of the preceding section and both said sections are separated over part of their length by an aperture (23, 25), characterized in that at least one pair of said pins (43) is introduced at the front end of the coil into the winding space (53) in a direction which is transverse to the plane of the flange-shaped connection portion (17), and in that at least an additional pair of said pins (37, 39, 41, 45) is introduced at the front end into said winding space (53) in a direction which is transverse to the plane of the longitudinal turns (27, 29, 31, 33) of the coil. A method as claimed in Claim 1, characterized in that the at least one pair of said pins (43) is introduced transversely to the plane of the flange-shaped connection portion (17) at angular positions of approximately 30° relative to the longitudinal axis. A method as claimed in Claim 2, characterized in that the additional pairs of said pins (37, 39, 41, 45) are introduced transversely to the plane of the longitudinal parts of the turns at angular positions of approximately 15°, 40°, 50° and 60°, respectively, relative to the longitudinal axis.

Inventors: DOOMERNIK FRANSISCUS MARIA PET, JACOBS FRANSISCUS CORNELIS ADR, VINK NICOLAAS GERRIT, DOOMERNIK, FRANSISCUS MARIA PETRUS PIUS, JACOBS, FRANSISCUS CORNELIS ADRIANUS JACOBUS, VINK, NICOLAAS GERRIT
Applicants: PHILIPS ELECTRONICS NV, PHILIPS ELECTRONICS N.V.
Application year: 1989
Main classification: H01J9
IPC codes: H01J29, H01J9