Photomultiplier tube

Abstract: A photomultiplier tube of the present invention is the one which collects the electrons, which have been multiplied by the dynodes laminated into a plurality of stages in the electron multiplier section and that have subsequently been reflected at the final-stage dynode, as an output signal. The photomultipluer tube forms the final-stage dynode as multi-stage, for example, in two layers, and has its alkali metal vapor passage holes of its first layer so arranged as to have the holes shifted with respect to the alkali metal vapor passage holes of the second layer. Furthermore, each of the dynodes, except the final-stage dynode consists of the focusing mesh electrode, the coarse mesh electrode, and the spacer electrode and the reinforcing bars are formed at identical locations in the coarse mesh electrode and the spacer electrode. Secondary electron emission sections are provided in the vicinity regions of these reinforcing bars of the focusing mesh electrodes.

Description: BACKGROUND OF THE INVENTION Field of the Invention The present invention relates to a photomultiplier tube, more particularly to a large-size photomultiplier tube that multiplies electrons incident on an electron multiplier section by laminated multi-stage dynodes. Related Background Art Conventionally, a photomultiplier tube of this kind which is described in Japanese Patent Application Laid Open No. 59-151741 has been known. This photomultiplier tube comprises a photoelectric surface formed on one end of a cylindrical blind vacuum container, an electron multiplier section that has a plurality of laminated dynodes, which multiplies the incident photoelectrons, an anode (positive electrode) of a net shape that collects the electrons multiplied by the electron multiplier section as an output signal, and a final-stage dynode (reversal dynode) of flat plate shape. Consequently, the photoelectrons emitted from the photoelectric surface are multiplied at the electron multiplier section, and are reflected at the final-stage dynode. Thereafter, the photoelectrons are collected as an output signal at the anode. A further dynode structure is disclosed in UK Patent GB 1,306,510. Japanese Patent Application No. 6-314550 also discusses dynode structures. SUMMARY OF THE INVENTION However, since the conventional photomultiplier tube has the structure as described above, there has existed the following problems in the conventional photomultiplier tube. Since the electron multiplier section tube is made up of multi-stage dynodes, when the size of the photomultiplier tubes is small, for example, in case where the diameter of the sealed container is equal to 5.08 cm (2 inches) or smaller, the diameter of each of the dynodes themselves does not become too large, and rigidity can be possessed by itself. Therefore, the desired rigidity may be obtained, even in the case of assembling each of the dynodes before the formation of the electron multiplier section tube. Nevertheless, when the diameter of the sealed container becomes larger than 7.62 cm (3 inches), each of the dynodes becomes large-sized, and dynodes themselves are prone to deformations, including twisting and bending; moreover, even for the case in which each dynode is assembled first to make the electron multiplier section, it is difficult to obtain the desired rigidity. Therefore, if left in this state, deformations due to heat are prone to occur at the time of the manufacturing of the photomultiplier tube, and there was the problem that it is difficult to ensure its characteristics constant. The present invention has been presented so as to solve the above-mentioned problems, and in particular, is aimed at preventing deformations of the electron multiplier section tube, at the same time as providing a photomultiplier tube which is made to form a secondary electron surface having uniform characteristics. A photomultiplier tube of the present invention comprises dynodes, the photomultiplier tube characterised by the dynodes comprising a focusing mesh electrode, a coarse mesh electrode with a secondary electron surface, and a spacer electrode interposed between the focusing mesh electrode and the coarse mesh electrode; reinforcing bars formed at identical locations in the coarse mesh electrode and the spacer electrode; and secondary electron emission sections provided on the focusing mesh electrodes in the vicinity of the reinforcing bars. In a further embodiment of the present invention, the dynode of each stage consists of a focusing mesh electrode of mesh shape that collects the electrons; a coarse mesh electrode having one or a plurality of first reinforcing bars bridged across the ends which become the outermost block of each dynode, the coarse mesh electrode having a secondary electron surface; and a spacer electrode having second reinforcing bars which mutually overlap with the first reinforcing bars. The focusing mesh electrodes may be such as to have a secondary electron emission section formed at the location corresponding to the first and the second reinforcing bars or the region close to that location. This way, since each dynode is reinforced by the dynode reinforcing bars which are made up of the first and the second reinforcing bars, the structure can be preserved, which is strong against twisting and bending deformations of the dynodes due to heat and furthermore is excellent in vibration-resistance. On the other hand, furnishing dynode reinforcing bars at the dynode of each stage causes the secondary electrons not to be generated in the vicinity of the dynode reinforcing bars; and as this region would become then an insensitive region, and as a countermeasure, secondary electron emission section is provided on the focusing mesh electrodes. By taking this measure, the insensitive region is dissolved, and the output characteristics may be maintained uniform. In a further embodiment of the present invention, it is desirable that secondary electron emission surfaces be formed at each of the second reinforcing bars. By adopting such structure, the loss of the secondary electrons would not occur at the second reinforcing bars of the spacer electrodes, and electrons can be multiplied with good efficiency. Further scope of applicability of the present invention will become apparent from the detailed description given hereinafter. However, it should be understood that the detailed description and specific examples, while indicating preferred embodiments of the invention, are given by way of illustration only, since various changes and modifications within the scope of the claims will be apparent to those skilled in the art from this detailed description. BRIEF DESCRIPTION OF THE DRAWINGS The present invention will be described in further detail with reference to the accompanying drawings, in which: Fig. 1 shows a cross-sectional view indicating an embodiment of a photomultiplier tube according to the present invention; Fig. 2 is a perspective view showing the construction of each of the stages for the dynode of Fig 1; Fig. 3 is a plan view showing a focusing mesh electrode of Fig. 2; Fig. 4 is a plan view showing a coarse mesh electrode of Fig. 2; Fig. 5 is a plan view showing a spacer electrode of Fig.2; Fig. 6 is a perspective view showing a mask body for forming a secondary electron emission section for the focusing mesh electrode of Fig.3; Fig.7 is a graph showing an anode output when experiment is run with a condition in which no secondary electron emission section is formed in the focusing mesh electrodes; Fig. 8 is a graph showing the anode output when experiment is run with a condition in which secondary electron emission sections are formed in the focusing mesh electrodes; Figs. 9 and 10 are a perspective view and a plan view, respectively, of the reinforcing plate of Fig.1; Fig. 11 is a perspective view showing a final-stage dynode made up of two layers of Fig.1; and Fig.12 and Fig.13 are a cross-sectional view of Fig. 11 and a plan view of Fig. 11, respectively. Detailed Description of the preferred Embodiments Preferred embodiments of the photomultiplier tube according to the present invention will be explained in detail together with the drawings, in the following section. Fig.1 is a cross-sectional view showing the photomultiplier tube according to the present embodiment. Photomultiplier tube 1, shown in the same drawing, has a sealed container 2, and this sealed container 2 has a side tube made of a Kovar metal of cylindrical shape. A large-sized light-receiving surface plate 4 made of glass with about 20.32 cm (8 inch) diameter is fixed by means of high frequency welding, on top of this side tube 3, so as to block the upper end of side tube 3. Furthermore, in the lower section of the side tube 3, a stem 5 made of glass is fixed by high frequency welding, so as to block the lower opened end of the side tube 3. Then, a photoelectric surface 4a for generating photoelectrons by the incident light is formed on the inside surface of the light-receiving surface 4, and the tube 6 made of glass, used to inject the alkali metal vapor into the sealed container 2, is formed integrally with the stem 5 at the center of the stem 5. An electron multiplier section 7, which is used to multiply the electrons from the photoelectric surface 4a in a multi-stage manner, is arranged in the sealed container 2. The electron multiplier section 7 consists of eleven sheets of circular plate dynodes 8 that have been laminated into 11 stages, and a final-stage dynode 9 (the reversal dynode) which is provided in the lower section of the eleventh stage dynode 8. Then, a specified voltage is applied to the dynode 8 of each stage and to the final-stage dynode 9 by a plurality of pins 33a which are arranged in a circular form, the pins 33a penetrating through the stem 5. Between the final dynode 9 and the eleventh stage 8, arranged is a crossed wire-type anode (positive electrode) 10 consisting of a plurality of X-anodes 10a and a plurality of Y-anodes 10b which are arranged in a matrix form. Each X-anode 10a and each Y-anode 10b are connected to a plurality of pins 33b which penetrate through the stem 5 and are arranged in a circular form, and by utilizing each of the pins 33b, the anode output is sent to external sections. In addition, reference numeral 34 denotes a ring-shape focusing electrode for focusing the photoelectrons which come from the photoelectric surface 4a. As shown in Fig 2, the dynode 8 of each stage consists of the focusing mesh electrode 11 that focuses the electrons, the coarse mesh electrodes 12 that has the secondary electron surfaces, and the spacer electrode 13 arranged between the focusing mesh electrode 11 and the coarse mesh electrode 12, which maintains the spatial interval between the electrodes 11 and 12. As shown in Fig.3, the focusing mesh electrode 11 has the ring-shaped flange 11a of diameter about 200 mm and thickness of about 0.15 mm in its outermost block, and eight positioning lugs 11b are formed at equal intervals in the ring-shaped flange 11a. Furthermore, inside the ring-shaped flange 11a is a mesh 11c of honeycomb shape. As shown in Fig.4, the coarse mesh electrode 12 has an ring-shaped flange 12a having diameter size identical to that of the focusing mesh electrode 11, with a thickness of about 0.2 mm, and eight positioning lugs 12b are formed at equal intervals in the flange 12a. Moreover, parallel meshes 12c are spread so as to be arranged inside the flange 12a at equal intervals. As shown in Fig.5 , the spacer electrode 13 have a ring-shaped flange 13a of the same diameter as that of the focusing mesh electrode 11 and the coarse mesh electrode 12. The ring-shaped flange 13a has a thickness of about 0.6 mm, and eight positioning lugs 13b are formed at equal intervals in the flange 13a. There may also be cases in which 2 sheets of the spacers 13 of thickness 0.3 mm are stacked. Then, the spacer electrode 13 is nipped between the focusing mesh electrode 11 and the coarse mesh electrode 12. These electrodes 11, 12, and 13 are allowed to be conductive state, whereby a set of dynodes 8 making identical potentials possible are produced. At this time however, since the dynode 8 has a thin and a large ring body, the dynode 8 has a structure which is weak with respect to twisting and bending and is liable to produce deformations. Thus, four of the first reinforcing bars 12d are provided at the coarse mesh electrode 12, and each of the first reinforcing bars 12d are stretched on the inner side of the edge 12a, at equal intervals in the direction perpendicular to the parallel meshes 12c. Furthermore, in order to increase the strength of the dynode 8, four of the second reinforcing bars 13d are provided on the spacer electrode 13 as well. Each of the second reinforcing bars 13d is arranged so as to overlap each of the first reinforcing bars 12d of the coarse mesh electrode 12, and in assembling of the dynode 8, each of the second reinforcing bars 13d is welded to the respective first reinforcing bars 12d. As shown in Fig.6, the dynode 8 of a set of three sheets which consists of the focusing mesh electrode 11, the coarse mesh electrode 12, and the spacer electrode 13 is assembled so as to align the respective lugs 11b, 12b, and 13b. Each dynode 8 is piled up in 11 stages above the anode 10, as shown in Fig. 1. In this case, by passing a connecting pin ( not shown ) through the lugs 11b, 12b and 13b of the dynodes 8, each dynode 8 is laminated in multi-stages while being positioned. Then, by interposing a ceramic cylindrical spacer 14 between each of the dynodes 8, the anodes 8 are electrically insulated from each other. Moreover, when each dynode 8 is laminated in 11 stages upon another, dynodes of identical shape are used for each of the dynodes 8 in order to achieve a reduction in cost. They are piled up so as to shift by 90 degrees from each other. As a result, the four dynode reinforcing bars 15 composed of the first and second reinforcing bars 12d and 13d are arranged so that each of the bars 15 shifts by 90 degrees from the adjacent bar, and each of bars 15 is arranged in a matrix form when vied from the above (side of the light-receiving surface 4), at the electron multiplier section 7. Also, as shown in Figs. 4 and 5, although the dynode reinforcing bars 15 are arranged at equal intervals, they are as a whole, pushed slightly to one side. Therefore, when 90 degree phase array for each dynode 8 is performed in the electron multiplier section 7, each dynode reinforcing bar 15 is orthogonal to each other, in relation to the stages that are adjacent to each other. They are parallel if compared by skipping one stage; moreover, in the case in which one stage is skipped, the reinforcing bars are separated by a specified interval when viewed from above (side of the light-receiving surface 4). Here, the previously mentioned dynode reinforcing bars 15 have been added for the reason why each of the dynodes 8 is thin and large-sized. When the secondary electrons disappear in this portion, the output of the anode 10 falls in the vicinity of each of the dynode reinforcing bars 15 as shown in Fig. 7, and the uniformity deteriorates due to the insensitive region S. Thus, in order to prevent lowering of the anode output by the dynode reinforcing bars 15, a secondary electron emission section 20 is provided ( See Fig. 3) at the focusing mesh electrode 11, which corresponds the four insensitive regions S (refer to Fig.5) formed in the peripheral section along the longitudinal direction of the dynode reinforcing bar 15. The method of forming this secondary electron emission sections is as follows: first, as shown in Fig.6, by utilizing a mask body 22 having an opening 21 formed by notching the portion corresponding to the secondary electron emission section 20 by 5mm width, the mask body 22 is placed on the focusing mesh electrode 11 of a set of the dynodes 8 so as to position the mask body 22 through the opening 21, antimony is externally deposited onto the dynode 8. Thus, the antimony is deposited onto the secondary electron emission sections 20 of the focusing mesh electrodes 11 and the dynode reinforcing bars 15. The antimony deposited in the above described manner reacts with alkali metal vapor introduced from the tube 6, after the assembling of the photomultiplier tube 1, and antimony produces the secondary electron surface. Moreover, just above the dynode 8 of the first stage, auxiliary electrodes (not shown), on which antimony has been deposited previously, may also be arranged at the regions corresponding to the secondary electron emission sections 20. In this case, an internal deposition of antimony may adopted which is performed in such manner that by sending an electric current to the photomultiplier tube 1 after the assembling thereof, antimony on the auxiliary electrode is splashed to adhere it onto the secondary electron emission sections 20 of the focusing mesh electrodes 11 of the first stage. Furthermore, the focusing mesh electrodes 11 which have the secondary electron emission sections 20 may be applied to any stage of the dynode 8; for example, they may be applied to the first and the second stages which are closest to the light-receiving surface plate 4 so as to cross the secondary electron emission sections 20 at the first and the second stages, or the secondary electron emission sections 20 may be applied at the first to third stages. In this way, a suitable selection of at which focusing mesh electrodes 11 the secondary electron emission sections 20 are provided depends on the characteristics of the photomultiplier tube 1; however, as is shown in Fig. 8, it is essential that uniform output of the anode 10 be ensured. In other words, it becomes necessary that the secondary electron emission sections generate the secondary electrons of enough quantity to compensate the sink in the output at the anode 10. As is shown in Figs. 1 and 9, in the interior of the sealed container 2, provided is a heat-shielding reinforcing plate 23 made of a circular plate with diameter of about 200 mm and about 0.7 mm thickness. This reinforcing plate 23 is arranged between the final-stage dynode 9 and the stem 5, and is fixed to the electron multiplier section 7 by eight positioning lugs 23a via the connecting pins ( not shown ) and the ceramic cylindrical spacers 14. The reinforcing plate 23 is fixed to the sealed container 2, by welding a plurality of lead pins 33c which rise from the stem 5 to the stainless steel supporting pillar pipes 25, one ends of which are fixed to the reinforcing plates 23. Consequently, reinforcement of the electron multiplier section 7 is made with certainty by the reinforcing plate 23 supported by the pillar pipes 25. Thus, a structure, which has a strong resistance to vibration and is not prone to twisting and bending of the electron multiplier section 7 due to heating, can be ensured. Furthermore, as is shown in Figs. 9 and 10, in the reinforcing plate 23, the alkali metal vapor collision sections 23b of circular plate shape are formed, which face opposite to the alkali metal vapor exit 6a of the alkali metal vapor injection tube 6, the alkali metal vapor exit 6a being provided at the center of the stem 5. This alkali metal vapor collision section 23b has an area substantially equal to the area of opening of the alkali metal vapor exit 6a. Also, in the periphery of an alkali metal vapor collision section 23b, formed are alkali metal vapor dispersion holes 24 which make the alkali metal vapor flow uniformly towards the electron multiplier section 7. The alkali metal vapor dispersion holes 24 consist of first alkali metal vapor dispersion sections 24a arranged so as to enclose the alkali metal vapor collision section 23b and second alkali metal vapor dispersion holes 24b arranged radially in the outer area of the first alkali metal vapor dispersion holes 24a. The first alkali metal vapor dispersion holes 24a are divided into six equal parts, each of which is formed in a sector shape; and each of the second alkali metal vapor dispersion holes 24b has a circular hole of identical size. Then, each of the first alkali metal vapor dispersion holes 24a has larger area of opening, compared to each of the second alkali metal vapor dispersion holes 24b. This is due to the annular gap B formed between the side tube 3, the reinforcing plate 23, and the electron multiplier section 7, in the sealed container 2. This is, therefore, a result of considering the fact that the alkali metal vapor injected into the evacuated sealed container 2 passes through the annular gap B, in order to squirt the alkali metal vapor uniformly out of the alkali metal vapor dispersion holes 24 of the reinforcing plate 23. Thereupon, the alkali metal vapor is injected into the evacuated sealed container 2, in the direction of the arrow C via the tube 6, when the secondary electron surface is formed in the electron multiplier section 7; however, at this time, the alkali metal vapor spreads dispersing outwards along the plane of the reinforcing plate 23 because the alkali metal vapor injected via the tube 6 has a nature to advance straight, by once hitting the alkali metal vapor collision section 23b of the reinforcing plate 23. Then, while the alkali metal vapor spreads along the plane of the reinforcing plate 23, the alkali metal vapor squirts uniformly so as to diffuse from the first and second alkali metal vapor dispersion holes 24a and 24b, respectively, towards the electron multiplier section 7; and by a cooperative effect between the alkali metal vapor passage holes 30b and 31b ( See Fig. 11 ) of the final-stage dynode 9, later described, the alkali metal vapor circulates uniformly inside the electron multiplier section 7. As a result, the alkali metal vapor and the antimony previously deposited on the electron multiplier section 7 react, resulting in formation of a uniform secondary electron surface at the electron multiplier section 7 as well as a uniform photoelectric surface 4a at the light-receiving plate 4. Thus, such a reinforcing plate 23 serves as a baffle plate by utilizing tube 6 at the time when the alkali metal vapor is injected into the sealed container 2. Uniform dispersion of the alkali metal vapor is achieved by providing alkali metal vapor dispersion holes 24a and 24b on this reinforcing plate 23. Photomultiplier tube 1 having such a structure is optimal for large-sized photomultiplier tube of size 12.7 or 20.32 cm (5 or 8 inches), and photographing of organs such as heart can be made at a sitting with a single large-size photomultiplier tube 1, by utilizing the large-sized photomultiplier tube 1 in a gamma camera for medical use, without arranging numerous multiplier tubes side by side. Also, when utilizing the reinforcing plate 23 in combination with the metallic side tube 3, joining of the metallic side tube 3 and the stem 5 can be achieved by high frequency welding at the time of assembling the sealed container 2. High heat is never generated during the welding operation; and no adverse effect is made on the electron multiplier section 7 inside the sealed container, even when the stem 5 and the reinforcing plate 23 are allowed to come close to each other. Hence, the side tube 3 may be shortened in proportion to that amount which permits the stem 5 and the reinforcing plate 23 to come closer, thus promoting the compactness for the photomultiplier 1. Furthermore, by bestowing heat shielding property to the reinforcing plate 23, the heat generated at the time of joining the metallic side tube 3 and the stem 5 can be shielded by the reinforcing plate 23, and efficient shielding of heat to be conducted to the electron multiplier section 7 is provided. Next, the final-stage dynode 9 will be explained. As shown in Figs. 11 and 12, the final-stage dynode 9 consists of the two layers: the final-stage dynode 9A of the upper layer (the first layer) and a final-stage dynode 9B of the lower layer (the second layer), and these are separated by a ceramic cylindrical spacers 14 ( See Fig. 1 ). As shown in Fig. 13, the final-stage dynode 9A of the upper layer has an ring-shaped flange 9Aa having substantially the same diameter size as that of the focusing mesh electrode 11 and a thickness of about 0.3 mm. Eight positioning lugs 9Ab are formed at equal intervals in the ring-shaped flange 9Aa. Furthermore, parallel meshes 30 of rectangular cross section are stretched inside the ring-shaped flange 9Aa. Since the final-stage dynode 9A of the upper layer is thin and of a large ring-shape body, it is thus weak against twisting and bending and prone to deformations. Hence, four pieces of reinforcing bars 9Ad are provided at the final-stage dynode 9A, and each reinforcing bar 9Ad is stretched at equal intervals in a direction orthogonal with respect to the parallel meshes 30, inside the ring-shaped flange 9Aa. Similarly, the final-stage dynode 9B of the lower layer has the same shape as that of the final-stage dynode 9A of the upper layer, as well as an ring-shaped flange 9Ba, positioning lugs 9Bb, parallel meshes 31, and reinforcing bars 9Bd. There, as shown in Figs. 11 and 12, on the surface of the parallel meshes 30 which are located in the upper side, the electron reflecting surfaces 30a are formed to reflect the secondary electrons towards the anode 10. Alkali metal vapor passage holes 30b are formed between the parallel meshes 30, the holes 30b serving to pass the secondary electrons and the alkali metal vapor. Similarly, electron reflecting surfaces 31a are formed on the surface of the parallel meshes 31 located on the lower side, the electron reflecting surfaces 31a serving to reflect the secondary electrons towards the anode 10. Alkali metal vapor passage holes 31b are formed between the parallel meshes 31, in order to pass the alkali metal vapor. The alkali metal vapor passage holes 30 of the final-stage dynode 9A of the upper layer and the electron reflecting surfaces 31a of the final-stage dynode 9B of the lower layer are placed facing opposite each other. In addition, the pitch between the adjacent electron reflecting surfaces 30a, formed on the final-stage dynode 9A of the upper layer is set to be equal to the pitch between the adjacent electron reflecting surfaces 31a, formed on the final-stage dynode 9B of the lower layer. Moreover, the width Z of the alkali metal vapor passage holes 30b and 31b is made slightly smaller than the width W of the electron reflecting surfaces 30a and 31a. Therefore, by shifting the final-stage dynode 9B of the lower layer with respect to the final-stage dynode 9A of the upper layer by half a pitch, the secondary electrons which have been multiplied by the dynodes 8 of the electron multiplier section 7 can be reflected towards the anode 10, without leaks. Furthermore, by separating the final-stage dynode 9A of the upper layer and the final-stage dynode 9B of the lower layer with the spacer 14, the alkali metal vapor flowing holes are not blocked so that they communicate. This results in formation of uniform alkali metal vapor flowing holes. As a consequence, the alkali metal vapor squirt out of the first and second alkali metal vapor passage holes 24a and 24b, respectively, of the reinforcing plate 23, whereby the alkali metal vapor can be uniformly sent into towards the dynodes 8 of eleven stages. It is sufficient that the electron reflecting surfaces 31a of the final-stage dynode of the lower layer 9B have at least the width Z for capturing the electrons passing through the alkali metal vapor passage holes 30b of the final-stage dynode 9A of the upper layer. The pitch between the adjacent electron reflecting surfaces 30a formed on the final-stage dynode 9A of the upper layer need not be equal to the pitch between the adjacent electron reflecting surfaces 31a formed on the final-stage dynode 9B of the lower layer. In addition, although the shape of the cross-sectional plane of the parallel meshes 30 and 31 may be either trapezoidal or triangular, it is necessary that the anode 10 be arranged parallel, with respect to the electron reflecting surfaces 30a and 31a. The case with two layers was explained in the above explanation, however, a structure having three or more layers may be made as well. In this case, it is sufficient that either of the layers beyond the second layer be arranged so as to block the holes of the first layer, and that either or more than two layers becoming identical in arrangement is not hindered. Furthermore, the electron reflecting surfaces beyond the second layer need not completely block the alkali metal vapor holes of the first layer, but it is then desirable that a greater part be blocked. And the final-stage dynode may be a transmitting type rather than the reflecting type, which has an anode arranged in the back of the dynode, the anode having a structure similar to the above-described final-stage dynode. It will be understood that embodiments of the present invention are described herein by way of example only, and that modifications may be made without departing from the scope of the invention. Further details of aspects of the invention can be found in Japanese Application Nos. 8-255067 (255067/1996), 8-255074 (255074/1996) and 8-255078 (255078/1996).

Claims: A photomultiplier tube (1) comprising dynodes (8) the photomultiplier tube characterised by the dynodes comprising a focusing mesh electrode (11), a coarse mesh electrode (12) with a secondary electron surface, and a spacer electrode (13) interposed between the focusing mesh electrode and the coarse mesh electrode (12); reinforcing bars (12d, 13d) formed at identical locations in the coarse mesh electrode (12) and the spacer electrode (13); and secondary electron emission sections (20) provided on the focusing mesh electrodes (11) in the vicinity of the reinforcing bars (12d, 13d). The photomultiplier according to claim 1, wherein a secondary electron emission surface is formed on the reinforcing bars of the spacer electrode.

Inventors: MURAMATSU SHINICHI, TAKAYAMA FUMIHIRO, TERADA TOYOHIKO, MURAMATSU, SHINICHI, TAKAYAMA, FUMIHIRO, TERADA, TOYOHIKO
Applicants: HAMAMATSU PHOTONICS KK, HAMAMATSU PHOTONICS K.K.
Application year: 1997
Main classification: H01J43
IPC codes: H01J43