WO2022163220A1 - 蛍光体ホイール - Google Patents
蛍光体ホイール Download PDFInfo
- Publication number
- WO2022163220A1 WO2022163220A1 PCT/JP2021/047272 JP2021047272W WO2022163220A1 WO 2022163220 A1 WO2022163220 A1 WO 2022163220A1 JP 2021047272 W JP2021047272 W JP 2021047272W WO 2022163220 A1 WO2022163220 A1 WO 2022163220A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- substrate
- heat radiating
- radiating member
- heat dissipation
- phosphor
- Prior art date
Links
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 title claims abstract description 190
- 239000000758 substrate Substances 0.000 claims abstract description 122
- 230000017525 heat dissipation Effects 0.000 claims abstract description 111
- 230000002093 peripheral effect Effects 0.000 claims abstract description 67
- 238000005452 bending Methods 0.000 claims abstract description 18
- 239000000463 material Substances 0.000 claims description 22
- 238000012546 transfer Methods 0.000 claims description 7
- 238000010586 diagram Methods 0.000 description 45
- 239000012530 fluid Substances 0.000 description 43
- 230000000052 comparative effect Effects 0.000 description 31
- 238000012986 modification Methods 0.000 description 24
- 230000004048 modification Effects 0.000 description 24
- 238000004458 analytical method Methods 0.000 description 22
- 238000012795 verification Methods 0.000 description 15
- 230000000694 effects Effects 0.000 description 14
- 230000005855 radiation Effects 0.000 description 10
- 238000009423 ventilation Methods 0.000 description 8
- 239000002245 particle Substances 0.000 description 7
- 230000009467 reduction Effects 0.000 description 6
- 229910052782 aluminium Inorganic materials 0.000 description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 5
- 239000000470 constituent Substances 0.000 description 5
- 239000011230 binding agent Substances 0.000 description 4
- 230000005284 excitation Effects 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 3
- 229920005989 resin Polymers 0.000 description 3
- 239000011347 resin Substances 0.000 description 3
- 238000004088 simulation Methods 0.000 description 3
- 125000006850 spacer group Chemical group 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000006866 deterioration Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000000191 radiation effect Effects 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 229910052594 sapphire Inorganic materials 0.000 description 2
- 239000010980 sapphire Substances 0.000 description 2
- 238000007790 scraping Methods 0.000 description 2
- 229920002050 silicone resin Polymers 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 230000001052 transient effect Effects 0.000 description 2
- 239000013598 vector Substances 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 239000006227 byproduct Substances 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 210000003746 feather Anatomy 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000013007 heat curing Methods 0.000 description 1
- 230000020169 heat generation Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 229910010272 inorganic material Inorganic materials 0.000 description 1
- 239000011147 inorganic material Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000001678 irradiating effect Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 238000007650 screen-printing Methods 0.000 description 1
- 230000002123 temporal effect Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V29/00—Protecting lighting devices from thermal damage; Cooling or heating arrangements specially adapted for lighting devices or systems
- F21V29/50—Cooling arrangements
- F21V29/70—Cooling arrangements characterised by passive heat-dissipating elements, e.g. heat-sinks
- F21V29/83—Cooling arrangements characterised by passive heat-dissipating elements, e.g. heat-sinks the elements having apertures, ducts or channels, e.g. heat radiation holes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V29/00—Protecting lighting devices from thermal damage; Cooling or heating arrangements specially adapted for lighting devices or systems
- F21V29/50—Cooling arrangements
- F21V29/502—Cooling arrangements characterised by the adaptation for cooling of specific components
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21S—NON-PORTABLE LIGHTING DEVICES; SYSTEMS THEREOF; VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLE EXTERIORS
- F21S10/00—Lighting devices or systems producing a varying lighting effect
- F21S10/007—Lighting devices or systems producing a varying lighting effect using rotating transparent or colored disks, e.g. gobo wheels
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V29/00—Protecting lighting devices from thermal damage; Cooling or heating arrangements specially adapted for lighting devices or systems
- F21V29/50—Cooling arrangements
- F21V29/70—Cooling arrangements characterised by passive heat-dissipating elements, e.g. heat-sinks
- F21V29/74—Cooling arrangements characterised by passive heat-dissipating elements, e.g. heat-sinks with fins or blades
- F21V29/745—Cooling arrangements characterised by passive heat-dissipating elements, e.g. heat-sinks with fins or blades the fins or blades being planar and inclined with respect to the joining surface from which the fins or blades extend
-
- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B21/00—Projectors or projection-type viewers; Accessories therefor
- G03B21/14—Details
- G03B21/16—Cooling; Preventing overheating
-
- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B21/00—Projectors or projection-type viewers; Accessories therefor
- G03B21/14—Details
- G03B21/20—Lamp housings
- G03B21/2006—Lamp housings characterised by the light source
- G03B21/2033—LED or laser light sources
- G03B21/204—LED or laser light sources using secondary light emission, e.g. luminescence or fluorescence
Definitions
- the present disclosure relates to phosphor wheels.
- a phosphor wheel that emits light by laser light (excitation light) emitted from a laser light source is one of the light source devices used in laser projectors.
- the phosphor wheel is rotated about its rotation axis while the phosphor layer is being irradiated with the laser light in order to suppress deterioration caused by heat generation of the phosphor layer due to the irradiation of the laser light.
- Patent Document 1 As a technique for improving the heat dissipation performance of a phosphor wheel, a technique is disclosed in which a fin having a feather structure is formed in a gap space between two supporting members having phosphors arranged on both side surfaces facing each other (for example, Patent Document 1). According to Patent Literature 1, air as a coolant flows through the gap space, thereby promoting the discharge of the heat brought to the phosphor, so that the heat dissipation performance of the phosphor wheel can be improved.
- the present disclosure provides a phosphor wheel with improved heat dissipation performance.
- a phosphor wheel includes a substrate having a first main surface and a second main surface facing each other, and a phosphor layer provided on the first main surface. and a heat dissipating member made of a plate material arranged to face either one of the first main surface and the second main surface and rotated together with the substrate, wherein the heat dissipating member A protruding portion provided in the central portion of the heat radiating member so as to protrude toward the surface of the heat radiating member and having a contact surface in contact with any of the surfaces, and a plurality of regions in the peripheral region excluding the central portion are cut and raised.
- the projecting portion is in contact with the substrate through the contact surface to ensure a constant gap between the substrate and the heat dissipation member, and to dissipate heat from the substrate to the heat dissipation member. It conducts to said peripheral region of the member.
- the phosphor wheel of the present disclosure has improved heat dissipation performance.
- FIG. 1 is an exploded perspective view of a phosphor wheel according to Embodiment 1.
- FIG. FIG. 2 is a side view of the phosphor wheel according to Embodiment 1.
- FIG. FIG. 3 is a front view of the substrate according to Embodiment 1 when viewed from the first main surface side. 4 is an enlarged side view of the heat radiating member shown in FIG. 2.
- FIG. 5 is a front view of the heat radiating member according to Embodiment 1 when viewed from the first main surface side.
- FIG. 6 is a perspective view of the heat radiating member according to Embodiment 1 when viewed from the first main surface side.
- 7 is an exploded perspective view of a phosphor wheel according to another aspect of Embodiment 1.
- FIG. 8 is a front perspective view of the heat radiating member according to Embodiment 2 when viewed from the first main surface side.
- FIG. 9 is a rear perspective view of the heat radiating member according to Embodiment 2 when viewed from the second main surface side.
- 10 is a partially enlarged view of the heat dissipation member of FIG. 9.
- FIG. 11 is a diagram showing analysis results of fluid flow near the fins of the heat radiating member according to the second embodiment.
- FIG. 12 is a front perspective view of a heat radiating member according to a modification of Embodiment 2 when viewed from the first main surface side.
- FIG. 13 is a front perspective view of a heat radiating member according to a comparative example when viewed from the first main surface side.
- FIG. 14 is a diagram showing analysis results of fluid flow in the vicinity of the fins of the heat radiating member according to the comparative example.
- 15 is a front perspective view of the heat radiating member according to Embodiment 3 when viewed from the first main surface side.
- FIG. 16 is a partially enlarged view of the heat dissipation member of FIG. 15.
- FIG. 17A and 17B are diagrams showing verification results of the actual prototype of the phosphor wheel according to Embodiment 3.
- FIG. FIG. 18 is a diagram showing analysis results of fluid flow in the vicinity of the fins of the heat radiating member according to the comparative example.
- 19A and 19B are diagrams showing analysis results of the flow of fluid in the vicinity of the fins of the heat radiating member according to Embodiment 3.
- FIG. 20A is a diagram showing another example of the size of the notch according to Embodiment 3.
- FIG. 20B is a diagram showing another example of the size of the notch according to Embodiment 3.
- FIG. 21A is a diagram showing another example of the shape of the notch according to the modification of Embodiment 3.
- FIG. 21B is a diagram showing another example of the shape of the notch according to the modification of Embodiment 3.
- FIG. FIG. 22A is a diagram showing an example in which a notch portion according to a modification of Embodiment 3 is formed near the rotation axis of the heat radiating member.
- FIG. 22B is a diagram showing an example of a case in which a cutout portion according to a modification of Embodiment 3 is formed near the outer peripheral edge of the heat radiating member.
- FIG. FIG. 23 is a diagram showing analysis results of the temperature reduction effect of the phosphor layer of the phosphor wheel according to the third embodiment.
- FIG. 24 is a diagram showing analysis results of fluid flow in the vicinity of the fins of the heat radiating member having cutouts formed near the rotation axis of the heat radiating member.
- 25 is a front perspective view of the heat radiating member according to Embodiment 4 when viewed from the first main surface side.
- FIG. 26 is a partially enlarged side view of the heat dissipation member and substrate of FIG. 25.
- FIG. 27 is a partially enlarged perspective view of the vicinity of the bending end shown in FIG. 26.
- FIG. FIG. 28 is a partially enlarged perspective view of the vicinity of a bent end having dimensions different from those of the bent end shown in FIG.
- FIG. 29 is a diagram showing verification results of the actual prototype of the phosphor wheel according to the fourth embodiment.
- FIG. 30A is a diagram showing analysis results of relative velocities in the vicinity of the outer peripheral edge of a heat radiating member according to a comparative example.
- 30B is a diagram showing analysis results of the relative velocity of the fluid near the bent end of the heat radiating member according to Embodiment 4.
- FIG. 31 is a partially enlarged side view of a heat dissipating member and a substrate having bent ends according to Modification 1.
- FIG. 32 is a partially enlarged perspective view of the vicinity of the bending end shown in FIG. 31.
- FIG. 33 is a partially enlarged perspective view of the vicinity of a bent end having dimensions different from those of the bent end shown in FIG.
- FIG. 34 is a diagram showing analysis results of the temperature reduction effect of the phosphor layer of the phosphor wheel according to the fourth embodiment.
- 35 is a contour diagram of the value of the time derivative of the root mean square pressure in the comparative example of FIG. 34.
- FIG. 38 is a partially enlarged side view of a heat dissipating member and a substrate having bent ends according to Modification 2.
- FIG. 39 shows a partially enlarged perspective view of the vicinity of the bending end shown in FIG. 38.
- FIG. 40 is a partially enlarged perspective view of the vicinity of a bent end portion different from the bent end portion shown in FIG. 39.
- FIG. 39 shows a partially enlarged side view of a heat dissipating member and a substrate having bent ends according to Modification 2.
- FIG. 39 shows a partially enlarged perspective view of the vicinity of the bending end shown in FIG. 38.
- FIG. 40 is a partially enlarged perspective view of the vicinity of a bent end portion different from the bent end portion shown in FIG. 39.
- each figure is a schematic diagram and is not necessarily strictly illustrated. Moreover, in each figure, the same code
- coordinate axes may be shown in the drawings used for explanation in the following embodiments.
- the Z-axis direction is described as the height direction of the phosphor wheel.
- the positive side of the Z-axis may be expressed as the upper side (upper), and the negative side of the Z-axis may be expressed as the lower side (downward).
- the X-axis direction and the Y-axis direction are directions orthogonal to each other on a plane perpendicular to the Z-axis direction.
- a front view means a drawing when viewed from the X-axis + side
- a rear view means a drawing when viewed from the X-axis - side.
- a side view means a drawing when viewed from the Y-axis direction.
- FIG. 1 is an exploded perspective view of a phosphor wheel 1 according to Embodiment 1.
- FIG. 2 is a side view of the phosphor wheel 1 according to Embodiment 1.
- FIG. 1 is an exploded perspective view of a phosphor wheel 1 according to Embodiment 1.
- FIG. 2 is a side view of the phosphor wheel 1 according to Embodiment 1.
- the phosphor wheel 1 according to Embodiment 1 is a reflective phosphor wheel, and is used for light sources such as laser projectors, lighting devices for equipment, and endoscopes.
- the phosphor wheel 1 includes a substrate 11, a phosphor layer 12 provided on the substrate 11, a heat dissipation member 30, a motor 40, and an adjustment plate 41, as shown in FIGS.
- the adjustment plate 41 is used to adjust the deviation of the center of gravity during rotation in order to transmit the rotational power of the motor 40 to the substrate 11 and the like in a well-balanced manner, but it is not an essential component.
- the adjustment plate 41 may be the hub of the motor 40 .
- FIG. 3 is a front view of the substrate 11 according to Embodiment 1 when viewed from the first main surface side.
- the substrate 11 is a disk-shaped plate member having a first main surface and a second main surface facing each other, and driven to rotate about the rotation axis J by the motor 40 .
- the shape of the substrate 11 in plan view is circular.
- the shape in plan view is the shape (that is, the front shape) when viewed from the direction perpendicular to the substrate 11 (X-axis + side).
- the diameter of the substrate 11 is, for example, about 8 cm, but is not particularly limited.
- the substrate 11 is provided with the phosphor layer 12 on the first main surface.
- An opening 33 is provided in the center of the substrate 11 for protruding a part (hub, rotor, etc.) of the motor 40 that is connected to the adjustment plate 41 .
- the substrate 11 has a rotation axis J passing through its center (center position), and is rotationally driven about the rotation axis J by the motor 40 .
- the material of the substrate 11 is not particularly limited as long as it is a metal with good thermal conductivity such as aluminum, stainless steel or sapphire.
- the substrate 11 is made of aluminum, for example. This is because aluminum has a relatively high thermal conductivity and is lightweight, so that the substrate 11 made of aluminum not only improves the heat radiation performance but also reduces the weight.
- the thickness of the substrate 11 is, for example, 1.5 mm or less.
- the phosphor layer 12 is provided on the first main surface of the substrate 11 .
- the phosphor layer 12 may be made of, for example, a resin material containing a large number of YAG-based yellow phosphor particles.
- the base material of the resin material is, for example, translucent and thermosetting silicone resin.
- the phosphor layer 12 can be provided by screen-printing such a resin material on the first main surface of the substrate 11 and then heat-curing it in a heating furnace.
- the phosphor layer 12 may be composed of, for example, YAG-based yellow phosphor particles and a binder.
- the phosphor layer 12 preferably contains a large amount of YAG-based yellow phosphor particles that contribute to the conversion of excitation light into fluorescence. That is, in the phosphor layer 12, the higher the phosphor particle content ratio, the better.
- the binder is a mixture other than the yellow phosphor particles that constitute the phosphor layer 12 .
- the binder is made of, for example, an inorganic material with high thermal conductivity such as alumina.
- the thermal conductivity of alumina is ten times or more that of silicone resin. Therefore, the phosphor layer 12 can achieve high thermal conductivity by being composed of yellow phosphor particles and a binder made of alumina.
- a reflective film may be provided between the first main surface of the substrate 11 and the phosphor layer 12.
- the phosphor layer 12 is provided in a ring shape (annular shape) along the circumferential direction ⁇ of the disk-shaped substrate 11 in plan view. More specifically, the phosphor layer 12 is provided in a ring shape (annular shape) on the circumference at equal distances from the rotation axis J that is the center of rotation of the phosphor wheel 1 . In other words, the width of the phosphor layer 12 in the radial direction r is constant. Furthermore, it is desirable that the phosphor layer 12 is provided on the periphery of the first main surface. Even if the substrate 11 is not a disk-shaped substrate, the phosphor layer 12 may be provided in an annular shape.
- the phosphor layer 12 emits light when irradiated with laser light.
- the phosphor wheel 1 is rotated by the motor 40 while the phosphor layer 12 is being irradiated with the laser light. Rotated around J. As a result, deterioration of the phosphor particles contained in the phosphor layer 12 due to heat generated by laser light irradiation is suppressed.
- the heat radiating member 30 is made of a plate material, arranged to face either the first main surface or the second main surface of the substrate 11 , and rotated together with the substrate 11 .
- the heat dissipation member 30 is arranged to face the second main surface of the substrate 11 .
- the phosphor layer 12 is provided on the first main surface of the substrate 11 .
- FIG. 4 is an enlarged side view of the heat dissipation member 30 shown in FIG.
- FIG. 5 is a front view of the heat radiating member 30 according to Embodiment 1 when viewed from the first main surface side.
- FIG. 6 is a perspective view of the heat radiating member 30 according to Embodiment 1 when viewed from the first main surface side.
- the back surface is the side opposite to the surface (front) facing the second main surface of the substrate 11, and the direction perpendicular to the heat dissipation member 30 (that is, the X-axis ⁇ side). It is the face when you see it.
- the heat radiating member 30 is a disc-shaped plate material that is driven to rotate about the rotation axis J by the motor 40 .
- the shape of the heat radiating member 30 in plan view is circular.
- the diameter of the heat radiating member 30 is, for example, approximately 7 cm, but may be approximately 3 cm to 100 cm.
- the diameter of the heat dissipation member 30 is not particularly limited as long as it is smaller than the inner diameter of the phosphor layer 12 when the heat dissipation member 30 is arranged to face the first main surface of the substrate 11 as will be described later.
- the diameter of the heat radiating member 30 is the same as that of the fluorescent material provided on one surface of the substrate 11 in a belt-like and annular shape. It should be smaller than the inner diameter of layer 12 .
- the diameter of the heat dissipation member 30 is larger than the diameter of the substrate 11 than the inner diameter of the phosphor layer 12. may be larger than the diameter of the substrate 11 .
- the heat dissipation member 30 has a plurality of fins 31 and projections 34, as shown in FIGS. 1, 2 and 4-6.
- the heat dissipation member 30 is arranged to face the second main surface of the substrate 11 .
- the plurality of fins 31 are cut and raised toward the second main surface of the substrate 11 , and the protruding portions 34 also protrude toward the second main surface of the substrate 11 .
- the plurality of fins 31 are formed by cutting and raising a plurality of regions 32 that are a plurality of partial regions of the plate material of the heat radiating member 30 .
- the plurality of regions 32 become through holes after the plurality of fins 31 are formed. Details of the projecting portion 34, the plurality of fins 31, the region 32, etc. will be described later.
- the material of the heat radiating member 30 is not particularly limited as long as it is a metal plate material such as stainless steel, iron, copper, sapphire or aluminum.
- the protruding portion 34 is provided in the central portion of the heat dissipation member 30 so as to protrude toward either the first main surface or the second main surface of the substrate 11, and has a contact surface in contact with either surface. .
- the projecting portion 34 secures a constant space between the substrate 11 and the heat dissipation member 30 and dissipates the heat of the substrate 11 to the periphery of the heat dissipation member 30 except for the central portion. conduct to the area.
- the projecting portion 34 is a heat radiating member that protrudes from the second main surface of the substrate 11 in order to keep the distance between the substrate 11 and the heat radiating member 30 constant. 30 is provided in the central part.
- the projecting portion 34 is formed by drawing.
- the thickness of the projecting portion 34 that is, the distance between the substrate 11 and the heat dissipation member 30 is determined by the height of a plurality of fins 31 formed by cutting and raising the peripheral region of the heat dissipation member 30, which will be described later, as shown in FIGS. Anything above that is fine.
- the protruding portion 34 has a strip-shaped and ring-shaped contact surface for contacting the second main surface of the substrate 11 .
- An opening 33 is provided in the center of the protruding portion 34 and connected to the motor 40 via the adjustment plate 41 .
- the size (diameter) of the opening 33 may be of a size that allows a portion of the motor 40 to be connected to the adjustment plate 41 to protrude.
- the opening 33 may have a size that allows a gap of up to 1 mm from a portion of the motor 40 .
- the diameter of the projecting portion 34 is, for example, about 3.7 cm, but is not limited to this.
- the diameter of the projecting portion 34 is not particularly limited as long as it is smaller than the inner diameter of the heat radiating member 30 and larger than the diameter of the opening 33 .
- the protruding portion 34 is provided in the central portion of the heat radiating member 30 so as to have a strip-shaped and ring-shaped contact surface. Accordingly, the protruding portion 34 not only functions as a spacer capable of forming a gap (space) of air between the substrate 11 and the peripheral region of the heat dissipation member 30, but also functions as a spacer. It functions as a heat conduction path through which the heat generated in the substrate 11 can be transferred to the peripheral area of the heat dissipation member 30 .
- the plurality of fins 31 are formed by cutting and raising. More specifically, the plurality of fins 31 are formed by cutting and raising a plurality of regions 32 in the peripheral region of the plate material of the heat radiating member 30 excluding the central portion. Each of the plurality of fins 31 is cut and raised toward either the first main surface or the second main surface of the substrate 11 . In the present embodiment, as shown, for example, in FIGS. 1 to 3, the plurality of fins 31 are formed by cutting and raising the plurality of regions 32 toward the second main surface of the substrate 11 so as to form the second main surface of the substrate 11 . It is set up facing the main surface.
- the height of the plurality of fins 31 is smaller than the thickness of the projecting portion 34, as shown in FIGS.
- the fins 31 are formed in a peripheral region within the region of the heat dissipation member 30 corresponding to the region inside the inner diameter of the phosphor layer 12, but the present invention is not limited to this. .
- the fins 31 correspond to the region of the phosphor layer 12 when the heat dissipation member 30 is arranged to face the first main surface of the substrate 11 and the diameter of the heat dissipation member 30 is larger than the inner diameter of the phosphor layer 12 . It may be formed in a peripheral area including the area of the heat radiating member 30 .
- the fins 31 are arranged so that the heat dissipation member 30 faces the first main surface of the substrate 11 , and when the diameter of the heat dissipation member 30 is larger than the inner diameter of the phosphor layer 12 , the fins 31 It may be formed in a peripheral region including the region of the heat dissipation member 30 corresponding to the outer side.
- the plurality of fins 31 are annularly arranged along the circumferential direction ⁇ at a constant distance from the center (rotational axis J) in the peripheral region of the heat dissipation member 30 .
- the shape of the plurality of fins 31 is, for example, a substantially rectangular shape (substantially trapezoidal shape), but the tips may be rounded with rounded corners.
- each of the plurality of fins 31 is formed to have a constant angle with respect to the radial direction r in the peripheral region, and the second main portion of the substrate 11 is formed.
- each of the plurality of fins 31 may be formed in the peripheral region, and may not be formed along the radial direction r. Further, each of the plurality of fins 31 does not have to stand vertically with respect to the second main surface of the substrate 11 (or the front surface of the heat dissipation member 30).
- each of the plurality of fins 31 sends air outward (in the centrifugal direction) from the fins 31 in accordance with the rotation of the heat radiating member 30 around the rotation axis J.
- each of the plurality of fins 31 allows air (fluid) on the back side (X-axis side) of the heat dissipation member 30 to pass through the plurality of regions 32, which are through holes, between the substrate 11 and the heat dissipation member 30.
- the angle of the fins 31 with respect to the radial direction r and the angle of the fins 31 with respect to the second main surface are not limited to the examples shown in FIGS. .
- the region 32 is a partial region of the plate material of the heat radiating member 30, and becomes a through hole after the plurality of fins 31 are formed.
- the plurality of regions 32 are located in the peripheral region. Furthermore, as shown in FIG. 5 , the plurality of regions 32 are located at predetermined distances from the center of the heat radiating member 30 when viewed from the substrate 11 toward the heat radiating member 30 (viewed from the first main surface). It is located along an imaginary straight line having a predetermined angle or more with respect to the radial direction r from a position substantially equidistant in the direction ⁇ .
- the plurality of regions 32 may have similar shapes, but are not limited to similar shapes.
- the plurality of regions 32 are through holes penetrating the heat radiating member 30, and function as ventilation holes through which air generated by the plurality of fins 31 passes.
- the plurality of regions 32 are annularly positioned along the circumferential direction ⁇ at a constant distance from the center (rotational axis J) of the heat radiating member 30 in the peripheral region. If the plurality of regions 32 are arranged at random, the rotation of the heat radiating member 30 will not be stable, which may cause abnormal noise or the like.
- the shapes of the plurality of regions 32 are, for example, substantially rectangular (substantially trapezoidal), but may be rounded with rounded corners.
- each of the plurality of regions 32 is formed to have a constant angle with respect to the radial direction r, as shown in FIG. Note that each of the plurality of regions 32 does not have to be formed along the radial direction r.
- the magnitude of the angles of the plurality of regions 32 with respect to the radial direction r may be determined so that the plurality of cut-and-raised fins 31 can effectively send air to the outside. Not limited.
- the motor 40 rotates the substrate 11 and the heat radiating member 30 by being controlled by an electronic circuit (not shown) as shown in FIG. 1, for example.
- the motor 40 is, for example, an outer rotor type motor, but is not particularly limited.
- the phosphor wheel 1 includes the substrate 11 having the first main surface and the second main surface facing each other, and the phosphor layer 12 provided on the first main surface. , a heat radiating member 30 made of a plate material, arranged to face the second main surface of the substrate 11 and rotated together with the substrate 11 .
- the heat dissipating member 30 is provided in the central portion of the heat dissipating member 30 so as to protrude toward the second main surface, and has a protruding portion having a contact surface in contact with the second main surface, and a plurality of protrusions in the peripheral region excluding the central portion.
- the protruding portion 34 is in contact with the substrate 11 via the contact surface, thereby securing a constant space between the substrate 11 and the heat dissipation member 30 and conducting the heat of the substrate 11 to the peripheral area of the heat dissipation member 30. .
- the phosphor wheel 1 is a reflective phosphor wheel, and includes the phosphor layer 12 only on the first main surface of the substrate 11 . Further, since the phosphor wheel 1 is provided with the heat dissipation member 30 provided with the projecting portion 34 , it is possible to form a space with a constant interval between the substrate 11 and the heat dissipation member 30 . As a result, the wind generated by the plurality of fins 31 can pass through the plurality of regions 32 (through holes) and be sent toward the outside of the space between the substrate 11 and the heat radiating member 30 . That is, the wind generated by the plurality of fins 31 can be used to cool the phosphor layer 12 .
- the heat dissipation performance of the phosphor wheel 1 can be improved.
- the contact between the substrate 11 and the protruding portion 34 of the phosphor wheel 1 can form a heat conduction path for transferring the heat generated in the phosphor layer 12 from the substrate 11 to the peripheral region of the heat dissipation member 30 . Therefore, the heat dissipation performance can be further improved.
- the phosphor wheel 1 with improved heat dissipation performance can be realized.
- the plurality of fins formed on the heat radiating member 30 are formed by cutting and raising a plurality of regions of the plate material, so that they can be formed in a simple manner. can.
- the size of the opening 33 provided in the center of the heat radiating member 30 should be such that a portion of the motor 40 for connection with the adjusting plate 41 can protrude, it is not limited to this. do not have. It may be made larger than the opening 33 and used for ventilation. That is, the heat radiating member 30 has an opening 33 formed for ventilation in the center of the heat radiating member 30, and the rotation axis J of the heat radiating member 30 rotated together with the substrate 11 passes through the opening 33. good too.
- the wind generated by the plurality of fins 31 is allowed to escape not only through the plurality of regions 32 (through holes), but also through the openings 33, and is outside the space (gap) between the substrate 11 and the heat radiating member 30.
- the amount of air passing through the space between the substrate 11 and the heat dissipation member 30, which can be used for cooling the phosphor layer 12, can be increased, so that the heat dissipation performance of the phosphor wheel 1 can be further improved. can.
- the configuration of the phosphor wheel 1 is not limited to the above-described mode, and in order to further improve the heat radiation performance, fins may be formed on the substrate 11, or openings as through holes may be formed on the substrate 11. good too.
- FIG. 7 is an exploded perspective view of phosphor wheel 1A according to another aspect of Embodiment 1.
- the heat dissipation member 30 may be arranged so as to face the first main surface of the substrate 11 on which the phosphor layer 12 is provided.
- the plurality of fins 31 may be cut and raised toward the first surface of the substrate 11
- the protruding portion 34 may also be formed so as to protrude toward the first main surface of the substrate 11 .
- the protrusion 34 may not be provided on the heat radiating member 30 and the adjustment plate 41 may also function as the protrusion 34 .
- the heat dissipation member 30 and the adjustment plate 41 that also functions as the projecting portion 34 may be integrated. As a result, the number of parts can be further reduced, and the cost can be reduced.
- FIG. 8 is a front perspective view of the heat radiating member 30B according to Embodiment 2 when viewed from the first main surface side.
- FIG. 9 is a rear perspective view of the heat radiating member 30B according to Embodiment 2 when viewed from the second main surface side.
- 10 is a partially enlarged view of the heat dissipation member 30B of FIG. 9.
- FIG. Elements similar to those in FIGS. 5 and 6, etc., are denoted by the same reference numerals, and detailed description thereof is omitted.
- a heat dissipating member 30B shown in FIGS. 8 and 9 differs from the heat dissipating member 30 shown in FIGS. 5 and 6 in that a through hole 35B is further formed in the projecting portion 34B.
- Protruding portion 34B is provided in the central portion of heat dissipation member 30 so as to protrude toward either the first main surface or the second main surface of substrate 11, as in the first embodiment.
- the projecting portion 34B has a contact surface 341 in contact with one of the surfaces and a peripheral wall 342 having the contact surface 341 as a bottom surface.
- Projecting portion 34B is provided at the center of heat radiating member 30B so as to protrude from the second main surface of substrate 11 in order to keep the distance between substrate 11 and heat radiating member 30B constant, as in the first embodiment. It is The projecting portion 34B is formed by drawing. Since the opening 33 provided in the center of the projecting portion 34B and the diameter of the projecting portion 34B are the same as those described in the embodiment, description thereof will be omitted here.
- the projecting portion 34B functions as a spacer capable of forming a constant gap (space) made of air between the substrate 11 and the peripheral region of the heat radiating member 30B, as in the first embodiment. do.
- the projecting portion 34B contacts the substrate 11 via the contact surface 341, thereby functioning as a heat conduction path that can conduct heat generated in the phosphor layer 12 from the substrate 11 to the peripheral area of the heat dissipation member 30B.
- the projecting portion 34B further has a plurality of through holes 35B formed in the peripheral wall 342 for ventilation.
- the through hole 35B is provided in the peripheral wall 342 of the projecting portion 34B. More specifically, each of the plurality of through holes 35B is formed at the boundary between the peripheral wall 342 and the contact surface 341, as shown in FIGS. 8-10. That is, each of the plurality of through holes 35B is formed across the peripheral wall 342 and the contact surface 341 .
- each of the plurality of through holes 35B is formed at a position different from the region connecting the rotation axis J of the heat radiating member 30B and each of the plurality of fins 31 . That is, the through holes 35B and the fins 31 are formed so as not to line up in the radial direction r.
- the dimensional sense of the through hole 35B will be explained using FIG.
- the outer diameter of the heat radiating member 30B is ⁇ 70 mm to 80 mm
- the length of the region 32 in the radial direction r is about 11 mm to 14 mm
- the outer diameter of the contact surface 341 is about ⁇ 35 mm to 38 mm.
- the diameter of the through hole 35B is about ⁇ 3 mm.
- the through hole 35B is provided in the boundary between the heat dissipation member 30B and the projecting portion 34B so as to straddle the peripheral wall 342 and the contact surface 341 of the projecting portion 34B. is formed.
- This configuration can further promote the flow of fluid (air) generated between the phosphor layer 12 and the heat dissipation member 30B. As a result, the temperature of the phosphor layer 12 can be further reduced, so that the heat dissipation performance of the phosphor wheels 1 and 1A can be improved.
- the temperature rise of the phosphor layer 12 was verified when the actual phosphor wheels 1 and 1A according to the present embodiment configured as described above were prototyped and operated for a predetermined time. explain. As a comparative example, verification was also conducted on actual prototypes of the phosphor wheels 1 and 1A according to Embodiment 1 that do not have the through holes 35B.
- a verification result was obtained in which the temperature rise of the phosphor layer 12 was 115.7°C.
- a verification result was obtained in which the temperature rise of the phosphor layer 12 was 119.5°C. That is, it was confirmed that the temperature rise of the phosphor layer 12 according to the present embodiment was lower than the temperature rise of the phosphor layer 12 according to the comparative example.
- FIG. 11 is a diagram showing analysis results of fluid flow near the fins 31 of the heat radiating member 30B according to the second embodiment.
- flow lines of the fluid (air) passing through the through holes 35B toward the vicinity of the fins 31 are shown.
- the streamlines shown in FIG. 11 represent the flow of fluid (air) in vectors.
- the fins 31 remove the fluid (air) present in the area (see, for example, FIGS. 1 and 8) sandwiched between the planar portions of the heat dissipating members 30 and 30B provided with the fins 31 and the substrate 11. It has a function of scraping out the heat radiating members 30 and 30B in the outer peripheral direction. This function promotes heat transfer by convection in the phosphor wheels 1 and 1A according to the first and second embodiments, so that the temperature of the phosphor layer 12 provided on the substrate 11 can be reduced.
- the phosphor wheels 1 and 1A according to the second embodiment are provided with the through holes 35B in the heat dissipation member 30B, so that when the through holes 35B are not provided (the phosphor wheel 1 according to the comparative example shown in FIG. 12). , 1A), heat transfer by convection can be promoted, and heat dissipation is considered to be improved.
- the through hole 35B is formed at the boundary between the heat radiating member 30B and the projecting portion 34B so as to straddle the peripheral wall 342 and the contact surface 341 of the projecting portion 34B. do not have. As shown in FIG. 12, the through hole 35C may be formed only in the peripheral wall 342 of the projecting portion 34B.
- FIG. 12 is a front perspective view of a heat radiating member 30C according to a modification of Embodiment 2, viewed from the first main surface side. Elements similar to those in FIGS. 8 and 9, etc. are denoted by the same reference numerals, and detailed description thereof will be omitted.
- a heat dissipation member 30C shown in FIG. 12 differs from the heat dissipation member 30B shown in FIGS. 8 and 9 in the positions of a plurality of through holes 35C formed for ventilation in the projecting portion 34C. Others are the same as those of the through hole 35B described above.
- the through hole 35C is provided in the peripheral wall 342 of the projecting portion 34C.
- each of the plurality of through holes 35C is formed only in the peripheral wall 342 and is formed in the center of the peripheral wall 342 when viewed in the direction from the heat dissipation member 30C toward the contact surface 341.
- each of the plurality of through holes 35C is formed at a position different from the region connecting the rotation axis J of the heat radiating member 30C and each of the plurality of fins 31, similarly to each of the plurality of through holes 35B. That is, the through holes 35C and the fins 31 are formed so as not to line up in the radial direction r.
- FIG. 13 is a front perspective view of a heat radiating member 90 according to a comparative example when viewed from the first main surface side. Elements similar to those in FIG. 12 are denoted by the same reference numerals, and detailed description thereof will be omitted.
- FIG. 14 is a diagram showing analysis results of fluid flow in the vicinity of the fins 31 of the heat radiating member 90 according to the comparative example. FIG. 14 also shows the flow of fluid (air) through the through-holes 95 toward the fins 31 by streamlines.
- a heat radiating member 90 according to the comparative example has a through hole 95 provided in the projecting portion 34, which is different from the heat radiating member 30B shown in FIGS. 8 and 9 and the heat radiating member 30C shown in FIG. position is different. More specifically, the through hole 95 provided in the protruding portion 34 is formed at the boundary between the peripheral wall 342 and the heat radiating member 90 in the protruding portion 34 as shown in FIG. It is formed across the
- a notch portion may be further formed in the region 32 to increase the area of the region 32 where the plurality of fins 31 of the heat dissipation member 30 provided in the phosphor wheel 1 are cut and raised. This case will be described below as a third embodiment. Differences from the heat dissipation member 30 described in the first embodiment will be mainly described below.
- FIG. 15 is a front perspective view of a heat radiating member 30D according to Embodiment 3 when viewed from the first main surface side.
- FIG. 16 is a partially enlarged view of the heat dissipation member 30D of FIG. 15.
- FIG. Elements similar to those in FIGS. 5 and 6, etc., are denoted by the same reference numerals, and detailed description thereof is omitted.
- a heat radiating member 30D shown in FIGS. 15 and 16 differs from the heat radiating member 30 shown in FIGS. 5 and 6 in that a notch 321 is further formed in the region 32D.
- the region 32D is a partial region of the plate material of the heat radiating member 30D, as in the first embodiment, and becomes a through hole after the plurality of fins 31 are formed. 15, the plurality of regions 32D function as ventilation holes through which air generated by the plurality of fins 31 passes.
- the position and shape of the region 32D in the heat radiating member 30D are the same as those described in the first embodiment, so description thereof will be omitted here.
- each of the plurality of regions 32D further has a cutout portion 321 formed by cutting out a part of the side facing the side connecting to the fins 31 .
- the notch portion 321 is formed by notching a part of the side of the region 32D. More specifically, as shown in FIG. 16, for example, the notch portion 321 is formed by cutting out a portion of the side of the region 32D that is opposite to the side that continues to the fin 31 .
- the shape of the notch portion 321 is, for example, a semicircular notch shape as shown in FIG. In the example shown in FIG. 16, the notch 321 is positioned at the center of the side facing the side connecting to the fins 31 in the region 32D.
- the dimensional sense of the notch portion 321 in the example shown in FIG. 16 will be described.
- the outer diameter of the heat dissipation member 30D is ⁇ 70 mm to 80 mm
- the length of the radial direction r of the region 32D is about 11 mm to 14 mm
- the length R1 of the radial direction r of the notch 321 is about 2 mm.
- the notch portion 321 is further formed in the region 32D where the plurality of fins 31 of the heat dissipation member 30D are cut and raised.
- FIG. 17 is a diagram showing verification results for actual prototypes of the phosphor wheels 1 and 1A according to the third embodiment.
- FIG. 17 shows, as verification results, the temperature rise of the phosphor layer 12 when operating for a predetermined time and the noise level during operation for a predetermined time.
- FIG. 17 also shows, as a comparative example, verification results for actual prototypes of the phosphor wheels 1 and 1A having no notch 321, that is, the phosphor wheels 1 and 1A according to the first embodiment.
- FIG. 18 is a diagram showing analysis results of fluid flow near the fins 31 of the heat radiating member 30 according to the comparative example.
- FIG. 19 is a diagram showing analysis results of fluid flow near the fins 31 of the heat radiating member 30D according to the third embodiment.
- FIGS. 18 and 19 show streamlines of fluid (air) flowing toward the fins 31 through the regions 32 and 32D functioning as vent holes.
- the vector lines shown in FIGS. 28 and 19 indicate the flow of fluid (air).
- the fins 31 remove fluid (air) existing in a region sandwiched between the plane portion of the heat dissipation member 30 provided with the fins 31 and the substrate 11 (for example, see FIGS. 1 and 8). , has a function of scraping out the heat radiating member 30 in the outer peripheral direction.
- This function promotes heat transfer by convection in the phosphor wheels 1 and 1A according to the first and second embodiments, so that the temperature of the phosphor layer 12 provided on the substrate 11 can be reduced.
- the fluid flowing from the region 32 functioning as a vent hole toward the fins 31 hits the fins 31 and is then swept out to the outer circumference of the heat radiating member 30 . This also helps facilitate heat transfer.
- the area of the ventilation hole as a function of the region 32 can be increased.
- the flow rate through the ventilation holes which is the function of the region 32 and the notch 321, increases, so heat transfer due to convection can be promoted, and heat dissipation is considered to be improved. .
- FIGS. 20A and 20B are diagrams showing another example of the size of the notch 321 according to the third embodiment.
- FIGS. 20A and 20B show a notch 321 formed in a larger size than the example shown in FIG.
- the length R1 in the radial direction r of the notch 321 shown in FIG. 16 is set to about 2 mm
- the length r in the radial direction (length in the long direction) of the region 32D is set to about 11 mm to 14 mm.
- the length R3 in the radial direction r of the notch 321 shown in FIG. 20A may be about 6 mm, for example.
- the length R5 in the radial direction r of the notch portion 321 shown in FIG. 20B may be, for example, about 10 mm.
- 21A and 21B are diagrams showing another example of the shape of the notch 321A according to the modified example of the third embodiment.
- 21A and 21B show a notch 321A formed in a shape different from the example shown in FIG. More specifically, the notch portion 321A is formed in a V-shaped notch shape at the central portion of the side of the region 32D that faces the side connecting to the fins 31 .
- the notch 321A may be small or large in size as shown in FIGS. 21A and 21B.
- the shape of the notch 321A may be a V-shaped notch.
- the V-shaped notch shape may be expressed as a triangular shape.
- the cutout portion 321 is formed so as to be positioned at the center of the side facing the side connecting to the fins 31 in the region 32D, but the present invention is not limited to this. Variations in the position where the notch 321 is formed will be described below with reference to FIGS. 22A and 22B.
- FIG. 22A is a diagram showing an example in which a notch portion 321B according to a modification of Embodiment 3 is formed near the rotation axis J of the heat radiating member 30D. More specifically, as shown in FIG. 22A, the notch 321B may be formed closer to the rotation axis J of the heat radiating member 30D than the central portion of the side facing the side connecting to the fins 31 in the region 32D. .
- FIG. 22B is a diagram showing an example in which a notch portion 321C according to a modification of Embodiment 3 is formed near the outer periphery of the heat radiating member 30D. More specifically, as shown in FIG. 22B, the notch portion 321B may be formed closer to the outer peripheral edge of the heat dissipation member 30D than the central portion of the side facing the side connecting to the fins 31 in the region 32D.
- notch 321B shown in FIG. 22A and the notch 321C shown in FIG. 22B have a semicircular notch shape, but may have a V-shaped notch shape.
- FIG. 23 is a diagram showing analysis results of the temperature reduction effect of the phosphor layers 12 of the phosphor wheels 1 and 1A according to the present embodiment.
- the results shown in FIG. 23 are analytical results obtained from thermal fluid simulation.
- a notch 321 having a semicircular cutout shape with a length R1 in the radial direction r shown in FIG. 15 is indicated as 321 (R1), and a length R3 in the radial direction r shown in FIG. 20A.
- a notch 321 having a semicircular notch shape is shown as 321 (R3).
- a notch 321 having a semicircular notch shape with a length R5 in the radial direction r shown in FIG. 20B is indicated as 321 (R5).
- the small V-shaped cutout portion 321A shown in FIG. 21A is shown as 321A (small)
- the large V-shaped cutout shown in FIG. Part 321A is shown as 321A (Large).
- FIG. 23 also shows, as a comparative example, a result of a configuration having no notch, such as the region 32 of the first embodiment.
- FIG. 24 is a diagram showing analysis results of fluid flow in the vicinity of the fins 31 of the heat radiating member 30D having the notch 321B formed near the rotation axis J of the heat radiating member 30D.
- the state of the flow of fluid (air) flowing from the notch 321B is shown by streamlines.
- the fluid (air) flowing from the notch 321B formed near the rotation axis J hits the fins 31 and flows out from the rotation axis J side toward the outer peripheral edge of the heat radiating member 30D. It can be seen that the fluid repeatedly contacts the fins 31 and flows out to the outer peripheral edge of the heat radiating member 30D. That is, the cutout portion 321B formed near the rotation axis J can bring more fluid into contact with the fins 31 over a longer period of time than the cutout portion 321 formed in the central portion. Therefore, the fluid can be made to perform more heat exchange with the fins 31 .
- the cutout portion 321B formed near the rotation axis J has a higher effect of reducing the temperature of the phosphor layer 12 and improves heat dissipation compared to the cutout portion 321 formed in the central portion. be done.
- the speed of the phosphor wheels 1 and 1A of Embodiment 3, which are axially rotating bodies, increases as they approach the outer periphery. Therefore, the fluid flowing through the notch 321C formed near the outer periphery is faster than the fluid flowing through the notch 321 formed in the center.
- the cutouts 321C formed near the outer periphery are replaced by the cutouts 321C formed near the outer periphery.
- the effect of reducing the temperature of the phosphor layer 12 is higher, so it is considered that the heat dissipation is improved.
- FIG. 25 is a front perspective view of the heat radiating member 30E according to Embodiment 4 when viewed from the first main surface side.
- 26 is a partially enlarged side view of the heat dissipation member 30E and the substrate 11 of FIG. 25.
- FIG. FIG. 26 shows, for example, the heat radiating member 30E encircled by the dotted line in FIG. Elements similar to those in FIGS. 5 and 6, etc., are denoted by the same reference numerals, and detailed description thereof is omitted.
- a heat dissipation member 30E shown in FIGS. 25 and 26 differs from the heat dissipation member 30 shown in FIGS.
- the heat dissipation member 30E is made of a plate material, is arranged to face either the first main surface or the second main surface of the substrate 11, and is rotated together with the substrate 11, as in the first embodiment. Further, the heat radiation member 30E is a disk-shaped plate material that is rotationally driven about the rotation axis J by the motor 40. As shown in FIG. In other words, the shape of the heat radiating member 30E in plan view is circular. As shown in FIG. 25, the heat dissipation member 30E has a plurality of fins 31, regions 32, and projections 34, and openings 33 are provided. Since the size and material of the heat radiating member 30E are the same as those described in the first embodiment, the description thereof is omitted here.
- the heat dissipating member 30E is formed by bending the outer peripheral edge portion of the heat dissipating member 30E in the same direction as the direction in which the plurality of fins 31 are cut and raised when viewed from the heat dissipating member 30E, and is formed at an obtuse angle. It has a bend edge 301 with a bend angle.
- the bent end portion 301 is formed using a portion of the heat dissipation member 30E. More specifically, as shown in FIG. 25, for example, the bent end portion 301 bends the outer peripheral edge portion of the heat radiating member 30E in the same direction as the direction in which the plurality of fins 31 are cut and raised when viewed from the heat radiating member 30E. It is processed and formed.
- the shape of the bent end portion 301 when the heat radiating member 30E is cut along a straight line along the radial direction r is, for example, an R-bent shape as shown in FIG.
- FIG. 27 is a partially enlarged perspective view of the vicinity of the bending end portion 301 shown in FIG.
- FIG. 28 is a partially enlarged perspective view of the vicinity of a bent end portion 301A having dimensions different from those of the bent end portion 301 shown in FIG.
- the bent end portion 301 shown in FIG. 27 has a length and height of about 1.0 mm, and is bent at an obtuse angle.
- the dimensional feeling of the R bending of the bent end portion 301 is not limited to this case.
- the bent end portion 301A may have a length of about 0.5 mm, a height of about 1 mm, and be bent at an obtuse angle.
- it may also be a bent end having a length of about 1.5 mm, a height of about 1.0 mm, and an R-bend at an obtuse bending angle.
- the outer peripheral edge of the heat radiating member 30E forms an obtuse angle in the same direction as the direction in which the plurality of fins 31 are cut and raised when viewed from the heat radiating member 30E. It has bent ends 301 and 301A that are rounded at a bend angle. As a result, wind noise can be suppressed.
- FIG. 29 is a diagram showing verification results for actual prototypes of the phosphor wheels 1 and 1A according to the fourth embodiment.
- FIG. 29 shows, as verification results, the temperature rise of the phosphor layer 12 when operating for a predetermined time and the noise level during operation for a predetermined time.
- FIG. 29 also shows, as a comparative example, verification results for actual prototypes of the phosphor wheels 1 and 1A having no bent end portion 301, that is, the phosphor wheels 1 and 1A according to the first embodiment.
- FIG. 30A is a diagram showing analysis results of the relative velocity near the outer peripheral edge of the heat radiating member 30 according to the comparative example.
- FIG. 30B is a diagram showing analysis results of the relative velocity of the fluid near the bent end 301 of the heat radiating member 30E according to the fourth embodiment.
- the relative velocity in FIG. 30A is the relative velocity of the fluid in the vicinity of the surface of the substrate 11 and in the vicinity of the outer peripheral edge of the heat radiating member 30 .
- the relative velocity in FIG. 30B is the relative velocity of the fluid near the surface of the substrate 11 and near the bent end 301 of the heat dissipation member 30E.
- the outer peripheral edge portion of the heat radiating member 30E is R-bent in the same direction as the direction in which the plurality of fins 31 are cut and raised when viewed from the heat radiating member 30E. , 301A are formed.
- the verification result shown in FIG. 29 can be obtained that the noise level of phosphor wheels 1 and 1A according to Embodiment 4 is lower than the noise level of phosphor wheels 1 and 1A according to the comparative example.
- FIG. 31 and 32 are diagrams showing another example of the shape of the bent end formed on the heat radiating member 30E according to the fourth embodiment.
- FIG. 31 shows a partially enlarged side view of a heat dissipation member 30E having a bent end portion 301B and a substrate 11 according to Modification 1, and FIG. An enlarged perspective view is shown.
- FIG. 33 is a partially enlarged perspective view of the vicinity of a bent end portion 301C having dimensions different from those of the bent end portion 301B shown in FIG.
- the shape of the bent end portion 301B when the heat radiating member 30E is cut along a straight line along the radial direction r may be a bent shape.
- the bent end portion 301B shown in FIG. ).
- the dimensional feeling of bending the bent end portion 301B is not limited to this case.
- a bent end portion 301C having a length of about 1.5 mm, a height of about 1 mm, and bent at an obtuse angle may be used.
- it may also be a bent end having a length of about 1.0 mm, a height of about 0.5 mm, and being bent at an obtuse angle.
- FIG. 34 is a diagram showing analysis results of the temperature reduction effect of the phosphor layers 12 of the phosphor wheels 1 and 1A according to the present embodiment.
- the results shown in FIG. 34 are analytical results obtained from thermal fluid simulation.
- the distance between the substrate 11 and the heat radiation members 30 and 30E in the phosphor wheels 1 and 1A is 2 mm
- the outer diameter of the heat radiation members 30 and 30E is, for example, about ⁇ 70 mm
- the contact surface diameter of the protrusion 34 is ⁇ is 37 mm
- the length of the fin 31 in the short direction is about 1.7 mm.
- R shown in FIG. 34 means that the outer peripheral edge is R-bent in the direction of the substrate 11, and C shown in FIG. ) means that Also, after R or C shown in FIG. 34, the length and height of the outer peripheral edge are indicated as 1*1, for example.
- R1*1 has a length of about 1.0 mm and a height of about 1.0 mm shown in FIG. 27, and is bent at an obtuse angle.
- a case is shown in which the heat radiating member 30E has a bent end portion 301 that “R1*0.5” is, for example, a bent end portion 301A having a length of about 1.0 mm and a height of about 0.5 mm shown in FIG. 30E has.
- “R1.5*1” means that the heat dissipating member 30E has a bent end that is about 1.5 mm long, about 1.0 mm high, and is bent at an obtuse bending angle. is shown.
- R2*2 indicates the case where the heat radiating member 30E has a bent end that is about 2.0 mm long and about 2.0 mm high and that is R-bent at an obtuse bending angle.
- R2*1.5 indicates that the heat dissipating member 30E has a bent end that is about 2.0 mm long, about 1.5 mm high, and bent at an obtuse angle.
- C1*1 has a length of about 1.0 mm and a height of about 1.0 mm shown in FIG. 32, and is bent at an obtuse angle (C-bend).
- the heat radiating member 30E has a bent end portion 301B which "C1.5*1" is, for example, a bent end that has a length of about 1.5 mm, a height of about 1.0 mm, and is bent at an obtuse angle (C-bend) as shown in FIG.
- the case where the heat radiating member 30E has 301C is shown.
- "C1*0.5” is, for example, a bend of about 1.0 mm in length and about 0.5 mm in height shown in FIG.
- a case where the heat radiating member 30E has the end portion is shown.
- FIG. 34 also shows, as a comparative example, the results of a configuration that does not have a bent end like the heat radiating member 30 of Embodiment 1, for example.
- Turbulent noise is the sound produced by turbulent eddies existing in the flow field. When the vortexes collide and collapse, a sound is generated. Since the phosphor wheels 1 and 1A according to the present disclosure rotate at high speed as shaft rotating bodies, there are many turbulent eddies.
- the sound pressure caused by vortices generated around the object can be calculated from the time derivative of the object surface pressure according to the Lighthill-Curle theory. Therefore, based on the Lighthill-Curle theory, the root mean square value of the time differential of pressure can be used as an index that indicates the size of a noise source. Therefore, the value of the time derivative of the root-mean-square pressure obtained from the fluid analysis was used as an index for determining the magnitude of fluid noise generated when the phosphor wheels 1 and 1A rotate.
- the time derivative of the root-mean-square pressure can be derived by fluid analysis, it can be said that the pressure fluctuation on the surface of the phosphor wheels, which changes due to the rotation of the phosphor wheels 1 and 1A, is quantified.
- transient response is calculated in order to grasp the amount of pressure fluctuation over time, and the method of evaluating the flow field that takes the time average is often used as a method of considering the results obtained by the transient response calculation. .
- the object surface pressure is differentiated with time, the values fluctuate positively and negatively, and the normal average cancels them out to 0 (zero), so the root mean square value is used. This makes it possible to evaluate (verify) the noise level with one contour diagram (a diagram like a contour line) of the magnitude of temporal positive and negative fluctuations.
- FIG. 35 is a contour diagram of the value of the time derivative of the root-mean-square pressure in the comparative example of FIG.
- FIG. 36 is a contour diagram of the value of the time derivative of the root-mean-square pressure at "R1*1" in FIG. That is, FIG. 36 shows a contour diagram of the value of the time derivative of the root-mean-square pressure when the heat radiating member 30E has the bent end portion 301.
- FIG. 37 is a contour diagram of the value of the time derivative of the root-mean-square pressure at "C1.5*1" in FIG. 34.
- the heat radiation performance of the phosphor wheels 1 and 1A is not hindered, and the airflow generated by the plurality of fins 31 is prevented. Noise can be suppressed.
- the shape of the bent end portion formed on the heat radiating member 30E is not limited to the above-described R-bend shape or degree-bend shape, and may be a Z-bend shape.
- FIG. 38 and 39 are diagrams showing still another example of the shape of the bent end formed on the heat radiating member 30E according to the fourth embodiment.
- FIG. 38 shows a partially enlarged side view of a heat dissipation member 30E having a bent end 301D and a substrate 11 according to Modification 2
- FIG. 39 shows a part near the bent end 301D shown in FIG. An enlarged perspective view is shown.
- FIG. 40 is a partially enlarged perspective view of the vicinity of a bent end portion 301D different from the bent end portion 301D shown in FIG.
- the shape of the bent end portion 301D when the heat radiating member 30E is cut along a straight line along the radial direction r may be a Z-bent shape.
- the bent end portion 301D shown in FIG. there is The length L1 is the length from the outer peripheral edge, and the length L2 is the length of the raised portion of the bent end portion 301D.
- the Z-bent portion of the bent end portion 301D is L-shaped, but is not limited to this case.
- the Z-bent portion of the bent end portion 301D may be R-shaped.
- the dimensional feeling of the bent end portion 301D shown in FIG. 40 is the same as that of the bent end portion 301D shown in FIG. That is, the bent end portion 301D shown in FIG. 40 may be Z-bent with a length L1 and a length L2 of 1.0 mm and a height of about 2 mm.
- the configuration shown in the second embodiment may be added to the heat dissipating member having the bent ends shown in the fourth embodiment. That is, a through hole may be further provided in the peripheral wall of the projecting portion of the heat radiating member having the bent end shown in the fourth embodiment.
- the configuration shown in the second embodiment may be added to the heat dissipating member having the bent ends shown in the third embodiment. That is, a notch portion may be further formed in the region of the heat radiating member having the bent end shown in the fourth embodiment.
- the configuration shown in the second and third embodiments may be added to the heat dissipating member having the bent ends shown in the fourth embodiment. That is, a notch portion may be further formed in the area of the heat radiating member having the bent end shown in the fourth embodiment, and a through hole may be provided in the peripheral wall of the projecting portion of the heat radiating member.
- the present disclosure further includes a light source device or laser projector configured with a phosphor wheel as follows.
- the present disclosure also includes a light source device including the phosphor wheel shown in the above-described embodiments and modifications, an excitation light source such as a laser light source, and an optical system for guiding the light emitted from the excitation light source to the phosphor wheel. included.
- the phosphor wheel shown in the above-described embodiment and modifications, the motor for rotating the phosphor wheel, the laser light source for irradiating the phosphor layer with laser light, and the laser light emitted from the laser light source The present disclosure also includes a projection-type image display device including a light modulation element that modulates light emitted from the phosphor layer based on a video signal, and a projection lens that projects the light modulated by the light modulation element.
- the phosphor wheel of the present disclosure can be applied as a reflective phosphor wheel to a laser projector, a lighting device for facilities, a projection image display device such as a light source such as an endoscope, and the like.
- Reference Signs List 1 1A Phosphor wheel 11 Substrate 12 Phosphor layer 30, 30B, 30C, 30D, 30E, 90 Heat dissipation member 31 Fins 32, 32D Region 33 Opening 34, 34B, 34C Projection 35B, 35C, 95 Through hole 40 Motor 41 Adjusting plate 301, 301A, 301B, 301C, 301D Bent end 321, 321A, 321B, 321C Notch 341 Contact surface 342 Peripheral wall
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Abstract
Description
[蛍光体ホイール1]
以下、実施の形態1に係る蛍光体ホイール1の構成について、図1及び図2を用いて説明する。図1は、実施の形態1に係る蛍光体ホイール1の分解斜視図である。図2は、実施の形態1に係る蛍光体ホイール1の側面図である。
図3は、実施の形態1に係る基板11を第1主面側から見たときの正面図である。
蛍光体層12は、基板11の第1主面に設けられる。
放熱部材30は、板材からなり、基板11の第1主面及び第2主面のいずれかの面に対向して配置され、かつ、基板11とともに回転される。図1及び図2に示す例では、放熱部材30は、基板11の第2主面に対向して配置されている。ここで、基板11の第1主面は、蛍光体層12が設けられている。
突出部34は、基板11の第1主面及び第2主面のいずれかの面に向かって突出するように放熱部材30の中央部に設けられ、当該いずれかの面と接する接触面を有する。突出部34は、接触面を介して基板11に接することにより、基板11と放熱部材30との間に一定の間隔を確保し、かつ、基板11の熱を放熱部材30の中央部を除く周辺領域まで伝導する。
複数のフィン31は、切り起こし加工により形成される。より具体的には、複数のフィン31は、放熱部材30の板材のうち中央部を除く周辺領域における複数の領域32を切り起こして形成される。複数のフィン31のそれぞれは、基板11の第1主面及び第2主面のいずれかの面に向かって切り起こされている。本実施の形態では、例えば図1~図3に示されるように、複数のフィン31は、複数の領域32が基板11の第2主面に向かって切り起こされることで、基板11の第2主面に向かって立設されている。
領域32は、上述したように、放熱部材30の板材のうちの一部領域であり、複数のフィン31が形成された後には貫通孔となる。
モータ40は、例えば図1に示すように、電子回路(不図示)に制御されることにより、基板11及び放熱部材30を回転駆動する。モータ40は、例えば、アウターロータ型のモータであるが、特に限定されない。
以上説明したように、本実施の形態に係る蛍光体ホイール1は、互いに背向する第1主面及び第2主面を有する基板11と、第1主面に設けられた蛍光体層12と、基板11の第2主面に対向して配置され、かつ、基板11とともに回転される、板材からなる放熱部材30とを備える。放熱部材30は、当該第2主面に向かって突出するように放熱部材30の中央部に設けられ、当該第2主面と接する接触面を有する突出部と、中央部を除く周辺領域における複数の領域を切り起こして形成される複数のフィンと、を有する。突出部34は、接触面を介して基板11に接することにより、基板11と放熱部材30との間に一定の間隔を確保し、かつ、基板11の熱を放熱部材30の周辺領域まで伝導する。
上記の実施の形態1では、放熱性能が向上した蛍光体ホイール1等について説明したが、上述した態様に限らない。放熱性能をさらに向上させるために、蛍光体ホイール1が備える放熱部材の突出部にさらに貫通孔を形成してもよい。この場合の放熱部材を実施の形態2として以下説明する。以下では、実施の形態1で説明した放熱部材30と異なる点を中心に説明する。
図8は、実施の形態2に係る放熱部材30Bを第1主面側から見たときの正面斜視図である。図9は、実施の形態2に係る放熱部材30Bを第2主面側から見たときの背面斜視図である。図10は、図9の放熱部材30Bの一部拡大図である。なお、図5及び図6等と同様の要素には同一の符号を付しており、詳細な説明は省略する。
突出部34Bは、実施の形態1と同様に、基板11の第1主面及び第2主面のいずれかの面に向かって突出するように放熱部材30の中央部に設けられている。また、突出部34Bは、当該いずれかの面と接する接触面341と接触面341を底面とする周壁342とを有する。
貫通孔35Bは、突出部34Bの周壁342に設けられる。より具体的には、複数の貫通孔35Bのそれぞれは、図8~図10に示されるように、周壁342と接触面341との境界部に形成される。つまり、複数の貫通孔35Bのそれぞれは、周壁342と接触面341とに跨って形成されている。
以上説明したように、本実施の形態に係る蛍光体ホイール1、1Aでは、放熱部材30Bと突出部34Bとの境界部に、突出部34Bの周壁342と接触面341とに跨って貫通孔35Bが形成される。
上述した実施の形態2では、放熱部材30Bと突出部34Bとの境界部に、突出部34Bの周壁342と接触面341とに跨って貫通孔35Bが形成されるとして説明したが、これに限らない。図12に示すように、突出部34Bの周壁342のみに貫通孔35Cが形成されるとしてもよい。
上記の実施の形態1、2では、放熱性能が向上した蛍光体ホイール1等について説明したが、上述した態様に限らない。放熱性能をさらに向上させるために、蛍光体ホイール1が備える放熱部材30の複数のフィン31が切り起こされる領域32の面積を広げるよう領域32にさらに切り欠き部を形成してもよい。この場合を実施の形態3として以下説明する。以下では、実施の形態1で説明した放熱部材30と異なる点を中心に説明する。
図15は、実施の形態3に係る放熱部材30Dを第1主面側から見たときの正面斜視図である。図16は、図15の放熱部材30Dの一部拡大図である。なお、図5及び図6等と同様の要素には同一の符号を付しており、詳細な説明は省略する。
領域32Dは、実施の形態1と同様に、放熱部材30Dの板材のうちの一部領域であり、複数のフィン31が形成された後には貫通孔となる。また、複数の領域32Dは、図15に示すように、複数のフィン31によって生じる風の通る通気孔として機能する。放熱部材30Dにおいて領域32Dが設けられる位置、形状は、実施の形態1で説明した通りであるためここでの説明を省略する。
切り欠き部321は、領域32Dの辺の一部を切り欠いて形成される。より具体的には、切り欠き部321は、例えば図16に示すように、領域32Dにおける辺の一部であってフィン31と連なる辺と対向する辺の一部を切り欠いて形成される。
以上説明したように、本実施の形態に係る蛍光体ホイール1、1Aでは、放熱部材30Dの複数のフィン31が切り起こされる領域32Dにおいてさらに切り欠き部321が形成される。
なお、切り欠き部321のサイズと形状とは、図16で示した例に限らない。切り欠き部321のサイズ(大きさ)と形状のバリエーションについて図20A~図21Bを用いて説明する。
上記の実施の形態1~3では、蛍光体ホイール1、1Aの放熱性能を向上させるための構成等について説明した。以下の実施の形態4では、風切り騒音を抑制できる蛍光体ホイール1、1Aの構成について説明する。以下では、実施の形態1で説明した放熱部材30と異なる点を中心に説明する。
図25は、実施の形態4に係る放熱部材30Eを第1主面側から見たときの正面斜視図である。図26は、図25の放熱部材30E及び基板11の一部拡大側面図である。図26には、例えば図25の点線丸囲いの部分の放熱部材30Eが示されている。なお、図5及び図6等と同様の要素には同一の符号を付しており、詳細な説明は省略する。
曲げ端部301は、放熱部材30Eの一部を用いて形成される。より具体的には、曲げ端部301は、例えば図25に示すように、放熱部材30Eの外周縁端部を、放熱部材30Eから視て複数のフィン31が切り起こされる向きと同じ向きに曲げ加工されて形成される。
以上説明したように、本実施の形態に係る蛍光体ホイール1、1Aでは、放熱部材30Eの外周縁端部が放熱部材30Eから視て複数のフィン31が切り起こされる向きと同じ向きに鈍角の曲げ角度でR加工された曲げ端部301、301Aを有する。これにより、風切り騒音を抑制できる。
なお、放熱部材30Eに形成される曲げ端部の形状は、図27及び図28で示した例に限らない。以下、放熱部材30Eに形成される曲げ端部の形状のバリエーションについて図31~図33を用いて説明する。
なお、放熱部材30Eに形成される曲げ端部の形状は、上述したR曲げ形状または度曲に限らず、Z曲げ形状であってもよい。
上述した実施の形態及び変形例は一例にすぎず、各種の変更、付加、省略等が可能であることは言うまでもない。
11 基板
12 蛍光体層
30、30B、30C、30D、30E、90 放熱部材
31 フィン
32、32D 領域
33 開口
34、34B、34C 突出部
35B、35C、95 貫通孔
40 モータ
41 調整板
301、301A、301B、301C、301D 曲げ端部
321、321A、321B、321C 切り欠き部
341 接触面
342 周壁
Claims (7)
- 互いに背向する第1主面及び第2主面を有する基板と、
前記第1主面に設けられた蛍光体層と、
前記第1主面及び第2主面のいずれかの面に対向して配置され、かつ、前記基板とともに回転される、板材からなる放熱部材と、を備え、
前記放熱部材は、
前記いずれかの面に向かって突出するように前記放熱部材の中央部に設けられ、前記いずれかの面と接する接触面を有する突出部と、
前記中央部を除く周辺領域における複数の領域を切り起こして形成される複数のフィンと、
前記放熱部材から視て前記複数のフィンが切り起こされる向きと同じ向きに前記放熱部材の外周縁端部を曲げて形成され、かつ、鈍角の曲げ角度を有する曲げ端部とを有し、
前記突出部は、前記接触面を介して前記基板に接することにより、前記基板と前記放熱部材との間に一定の間隔を確保し、かつ、前記基板の熱を前記放熱部材の前記周辺領域まで伝導する、
蛍光体ホイール。 - 前記放熱部材を径方向に沿う直線で切断したときの前記曲げ端部の形状は、R曲げ形状である、
請求項1に記載の蛍光体ホイール。 - 前記放熱部材を径方向に沿う直線で切断したときの前記曲げ端部の形状は、Z曲げ形状である、
請求項1に記載の蛍光体ホイール。 - 前記放熱部材を径方向に沿う直線で切断したときの前記曲げ端部の形状は、度曲げ形状である、
請求項1に記載の蛍光体ホイール。 - 前記複数のフィンのそれぞれは、前記いずれかの面に向かって切り起こされている、
請求項1~4のいずれか1項に記載の蛍光体ホイール。 - 前記蛍光体層は、前記基板の一方の面において帯状かつ円環状に設けられており、
前記放熱部材の直径は、前記蛍光体層の内径よりも小さい、
請求項1~5のいずれか1項に記載の蛍光体ホイール。 - 前記基板は、円盤状であり、
前記蛍光体層は、前記基板の周方向に沿う帯状に形成されている、
請求項1~6のいずれか1項に記載の蛍光体ホイール。
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US18/260,750 US20240060636A1 (en) | 2021-01-26 | 2021-12-21 | Phosphor wheel |
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JP5661947B2 (ja) | 2011-01-21 | 2015-01-28 | オスラム ゲーエムベーハーOSRAM GmbH | 内側冷却部を備えた蛍光体装置、および、当該蛍光体装置を備えた反射照明装置 |
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