JPS63280600A - Composite diaphragm for speaker - Google Patents
Composite diaphragm for speakerInfo
- Publication number
- JPS63280600A JPS63280600A JP11636487A JP11636487A JPS63280600A JP S63280600 A JPS63280600 A JP S63280600A JP 11636487 A JP11636487 A JP 11636487A JP 11636487 A JP11636487 A JP 11636487A JP S63280600 A JPS63280600 A JP S63280600A
- Authority
- JP
- Japan
- Prior art keywords
- layer
- diaphragm
- resin layer
- hot
- dome
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 239000002131 composite material Substances 0.000 title claims description 19
- 239000004831 Hot glue Substances 0.000 claims abstract description 14
- 229920005992 thermoplastic resin Polymers 0.000 claims abstract description 4
- 229910052751 metal Inorganic materials 0.000 claims description 19
- 239000002184 metal Substances 0.000 claims description 19
- 229920005989 resin Polymers 0.000 abstract description 15
- 239000011347 resin Substances 0.000 abstract description 15
- 229920003002 synthetic resin Polymers 0.000 abstract description 12
- 239000000057 synthetic resin Substances 0.000 abstract description 12
- 239000000853 adhesive Substances 0.000 abstract description 8
- 230000001070 adhesive effect Effects 0.000 abstract description 8
- 239000000463 material Substances 0.000 abstract description 6
- 239000000314 lubricant Substances 0.000 abstract description 2
- 238000010030 laminating Methods 0.000 abstract 1
- 239000010410 layer Substances 0.000 description 39
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 15
- 239000010936 titanium Substances 0.000 description 14
- 229910052719 titanium Inorganic materials 0.000 description 14
- 238000003384 imaging method Methods 0.000 description 9
- 239000004743 Polypropylene Substances 0.000 description 8
- 229920001155 polypropylene Polymers 0.000 description 8
- 230000000052 comparative effect Effects 0.000 description 7
- -1 polypropylene Polymers 0.000 description 7
- 238000000034 method Methods 0.000 description 6
- 238000000465 moulding Methods 0.000 description 6
- 239000004697 Polyetherimide Substances 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 230000000704 physical effect Effects 0.000 description 4
- 229920001601 polyetherimide Polymers 0.000 description 4
- 230000037303 wrinkles Effects 0.000 description 4
- ZWEHNKRNPOVVGH-UHFFFAOYSA-N 2-Butanone Chemical compound CCC(C)=O ZWEHNKRNPOVVGH-UHFFFAOYSA-N 0.000 description 3
- XEKOWRVHYACXOJ-UHFFFAOYSA-N Ethyl acetate Chemical compound CCOC(C)=O XEKOWRVHYACXOJ-UHFFFAOYSA-N 0.000 description 3
- 239000004925 Acrylic resin Substances 0.000 description 2
- 229920000178 Acrylic resin Polymers 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 241000288673 Chiroptera Species 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000011247 coating layer Substances 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 238000007740 vapor deposition Methods 0.000 description 2
- 239000002759 woven fabric Substances 0.000 description 2
- KXGFMDJXCMQABM-UHFFFAOYSA-N 2-methoxy-6-methylphenol Chemical compound [CH]OC1=CC=CC([CH])=C1O KXGFMDJXCMQABM-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229920005549 butyl rubber Polymers 0.000 description 1
- 239000000839 emulsion Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 239000012943 hotmelt Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000011259 mixed solution Substances 0.000 description 1
- 239000004745 nonwoven fabric Substances 0.000 description 1
- 229920001568 phenolic resin Polymers 0.000 description 1
- 239000005011 phenolic resin Substances 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000003786 synthesis reaction Methods 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
Landscapes
- Diaphragms For Electromechanical Transducers (AREA)
Abstract
Description
【発明の詳細な説明】
[産業上の利用分野]
この発明はスピーカ用振動板、特に金属層と熱可塑性樹
脂層が積層された複合(騒動板の改良に関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to improvements in speaker diaphragms, particularly composite diaphragms in which a metal layer and a thermoplastic resin layer are laminated.
[従来の技術〕
従来の中高音再生用スピーカの振動板は、■チタン、ア
ルミニウム等の軽金属部を成形してなる振動板、
■織布又は不織布にフェノール樹脂等の熱硬化性樹脂を
含浸して成形した後、アクリル樹脂等を塗布してなる、
いわゆるソフトドーム撮動板、■ポリプロピレン、ポリ
エーテルイミド等の合成7脂を成形してなる振動板。[Conventional technology] The diaphragms of conventional speakers for medium and high frequency reproduction are: ■ A diaphragm formed by molding a light metal part such as titanium or aluminum, or ■ A diaphragm made of a woven or nonwoven fabric impregnated with a thermosetting resin such as phenolic resin. After molding, acrylic resin etc. are applied.
The so-called soft dome imaging plate ■A diaphragm made of synthetic 7 resins such as polypropylene and polyetherimide.
■合成樹脂を基体とし、当該基体に前記軽金属やカーボ
ン、ダイヤモンドライクカーボン等をイオンブレーティ
ング等の蒸着技術によりコーティングしてなる振動板、
■合成樹脂層に金属層を貼り合わせた複合(騒動板、
等が考えられ、且つ実用に供されていた。■A diaphragm made of synthetic resin as a base and coated with the light metals, carbon, diamond-like carbon, etc., using vapor deposition techniques such as ion blating; ■A composite diaphragm in which a metal layer is bonded to a synthetic resin layer (a diaphragm plate) , etc. have been considered and put into practical use.
[発明が解決しようとする問題点]
しかるに従来の上記振動板はそれぞれ長所短所を有して
おり、所望の物性を有する振動板を提供するには至って
いなかった。[Problems to be Solved by the Invention] However, each of the above-mentioned conventional diaphragms has advantages and disadvantages, and it has not been possible to provide a diaphragm having desired physical properties.
例えば、前記■の金属振動板は、材料自体のヤング率が
大きい(5〜7 x 10” dyn/cIi以上)の
で剛性が大きくピストン撮動領域が広く、高域再生限界
周波数が高い、耐熱性等の耐環境性が良好である、熱伝
導率が大きいことによりボイスコイルの放熱効果が大き
く耐入力特性が良好でおる等の利点を有する反面、内部
損失が小さい(tanδ−0,02以下)ために高域再
生限界周波数以上の周波数帯域において高域共振による
顕著なピーク・ディップが発生し高調波歪みか著しく増
大する問題を有している。For example, the metal diaphragm mentioned above has a high Young's modulus of the material itself (5 to 7 x 10" dyn/cIi or more), so it has high rigidity, a wide piston sensing area, a high high-frequency reproduction limit frequency, and heat resistance. It has advantages such as good environmental resistance such as high thermal conductivity, high heat dissipation effect of the voice coil and good input resistance characteristics, but low internal loss (tan δ - 0.02 or less). Therefore, there is a problem in that significant peak dips occur due to high-frequency resonance in a frequency band above the high-frequency reproduction limit frequency, and harmonic distortion increases significantly.
又、■のソフトドーム]騒動板は高域再生限界周波数以
上のピーク・ディップの発生に関しては前記金属撮動板
に比較すると著しく小さいが、再生帯域、耐環境性、耐
入力特性は劣る。In addition, the [Soft Dome] noise plate has a significantly smaller occurrence of peaks and dips above the high-frequency reproduction limit frequency than the metal imaging plate, but is inferior in reproduction band, environmental resistance, and input resistance characteristics.
又、■の合成樹脂振動板は、ポリプロピレン樹脂製のよ
うに内部損失が太きく(tanδ= 0.09 ”)、
高域再生限界周波数以上にあけるピーク・ディップの発
生が小さい特徴を有する撮動板や、ポリエーテルイミド
樹脂製のように耐熱性が大きい(熱変形温度150°C
)特徴を有する振動板等、所望の物性の一部については
特徴をそれぞれ有するが、総合的に考えて前記各振動板
■及び■と比べると剛性及び内部損失の値において中間
的性質を有するものであり適用範囲が制限されていた。In addition, the synthetic resin diaphragm (■) has a large internal loss (tan δ = 0.09'') like it is made of polypropylene resin.
The imaging plate has the characteristic of minimizing the occurrence of peaks and dips above the high-frequency reproduction limit frequency, and has high heat resistance such as polyetherimide resin (heat distortion temperature 150°C).
) A diaphragm with characteristics, each having its own characteristics with respect to some of the desired physical properties, but overall, compared to the above-mentioned diaphragms (■) and (■), it has intermediate properties in terms of rigidity and internal loss values. Therefore, the scope of application was limited.
又、■の複合振動板は、前記金属撮動板と、合成樹脂1
辰動板のそれぞれの利点を現出しようとすることを目的
として考えられたものでおるが、所望の剛性等を)qる
ためにコーティング層を厚くすると蒸着物特有の残留応
力の発生や合成樹脂層との密着不良が発生し剥離し易く
なる問題があるので、実用上では約30〜50即厚の合
成樹脂層に0.02〜0.2m程度の極薄い蒸着層をコ
ーティングすることが試みられているが、この程度の厚
さではコーティング層による前記剛性の向上等の機械的
物性の向上は充分なものではなかった。In addition, the composite diaphragm (■) includes the metal pickup plate and the synthetic resin 1.
This was designed to bring out the advantages of each of the sliding plates, but if the coating layer is made thicker to achieve the desired stiffness, etc., the generation of residual stress peculiar to the deposited material and the synthesis Since there is a problem of poor adhesion with the resin layer and easy peeling, it is practical to coat a synthetic resin layer with a thickness of about 30 to 50 mm with an extremely thin vapor deposition layer of about 0.02 to 0.2 m. Although attempts have been made, the coating layer has not been able to sufficiently improve mechanical properties such as the above-mentioned increase in rigidity with such a thickness.
更に■の複合振動板は、貼り合わせにより両層を結合し
ているので金属層の厚さの制限は減少するが、金属・合
成樹脂積層シートをプレス成形する際、両者の物性の違
い、特に延びの違いにより両層が剥離しやすく、又延び
の小さい金属層が破断しやすいためプレス成形が困難で
あり、又、成形後に両層を貼り合わせることは両者の成
形寸法精度上の問題があった。Furthermore, in the composite diaphragm described in ■, both layers are bonded together, so there are fewer restrictions on the thickness of the metal layer. Press molding is difficult because both layers tend to separate due to the difference in elongation, and the metal layer with small elongation tends to break, and bonding both layers together after molding has problems with the dimensional accuracy of both. Ta.
[問題を解決するための手段]
この発明は、金属層と熱可塑性樹脂層がホットメルト型
接着剤により積層結合されてなるスピーカ用複合撮動板
である。[Means for Solving the Problem] The present invention is a composite imaging plate for a speaker in which a metal layer and a thermoplastic resin layer are laminated and bonded using a hot-melt adhesive.
[作用]
プレス成形時にホットメルト型接着剤が軟化し、異種材
料間の潤滑材的機能を発揮して、金属層と合成樹脂層の
それぞれの延びに応じて延び、接着面の全面に作用する
粘性抵抗力により均一な緊張力を与えることにより、金
属層と合成樹脂層が接着積層された複合シートのプレス
成形を可能にして、充分な厚さの金属層と合成樹脂層よ
りなり、適値の物性が得られる振動板を提供することが
できる。[Function] During press molding, the hot melt adhesive softens and acts as a lubricant between different materials, extending in accordance with the respective extensions of the metal layer and synthetic resin layer, and acting on the entire surface of the bonded surface. By applying a uniform tension force using viscous resistance force, it is possible to press-form a composite sheet in which a metal layer and a synthetic resin layer are adhesively laminated. It is possible to provide a diaphragm that provides the following physical properties.
[実施例]
(実施例1)
600 ’Cで1時間焼鈍処理したチタン箔(JIS
TP28R,O材10朗厚>18を第2図に示すように
、その片面にメチル・エチル・ケトンと酢酸エチル混合
溶液(容量比1:1)に溶解したホットメルトタイプの
ブチルゴム系接着剤1bを乾燥厚さで約2即となるよう
にスプレー塗布し、塗布面が若干の粘着性を保持した状
態で、予め表面をコロナ放電処理等の表面活性処理を施
したポリプロピレン樹脂フィルム(25M厚>1Cと重
ね合わせローラー圧により圧接してチタン層1a(10
1II11厚)・ホットメルト接着剤層1b(2切厚)
・ポリプロピレン樹脂層1C(25N1厚)の積層複合
シート1を得た。[Example] (Example 1) Titanium foil (JIS
As shown in Figure 2, a TP28R, O material 10 thick > 18 is coated with a hot melt type butyl rubber adhesive 1b dissolved in a mixed solution of methyl ethyl ketone and ethyl acetate (volume ratio 1:1). Spray coat to a dry thickness of approximately 2 mm, and with the coated surface retaining some tackiness, prepare a polypropylene resin film (25M thick> Titanium layer 1a (10
1II11 thickness)・Hot melt adhesive layer 1b (2 cut thickness)
- A laminated composite sheet 1 having a polypropylene resin layer 1C (25N1 thickness) was obtained.
当該複合シート1を絞り成形することによりドーム状撮
動板を得る。A dome-shaped imaging plate is obtained by drawing the composite sheet 1.
すなわち複合シート1を第3a図に示す様に、チタン層
1aが凸金具2Cに対向するように上下移動が可能な上
型パット2aと下型パット2b間に挟持して固定し、先
端がドーム状に形成され、130〜140°Cに加熱さ
れた凸金型2Cの頂部に複合シート1が接触するまで前
記上下バット2a、2bを下降(第3b図)せしめる。That is, as shown in FIG. 3a, the composite sheet 1 is sandwiched and fixed between an upper mold pad 2a and a lower mold pad 2b which are vertically movable so that the titanium layer 1a faces the convex metal fitting 2C, and the tip is formed into a dome. The upper and lower butts 2a and 2b are lowered (FIG. 3b) until the composite sheet 1 comes into contact with the top of the convex mold 2C which is formed into a shape and heated to 130 to 140°C.
次に、前記上下バット2a、2bを更に降下せしめて、
複合シート1を凸金型2Cの先端形状に沿って賦形(第
3C図、第3d図)し、第1図に示すチタン層1aとポ
リプロピレン樹脂層1bがホットメルト型接着剤1Cで
接着積層された複合構成の全高6.3m、直径25#の
ドーム状振動板を得た。Next, the upper and lower bats 2a, 2b are further lowered,
The composite sheet 1 is shaped along the tip shape of the convex mold 2C (Figs. 3C and 3d), and the titanium layer 1a and polypropylene resin layer 1b shown in Fig. 1 are bonded and laminated using a hot melt adhesive 1C. A dome-shaped diaphragm having a composite structure with a total height of 6.3 m and a diameter of 25# was obtained.
上記絞り成形工程中においては、金型の熱がチタン層1
a→ホットメルト接着剤層1b−ポリプロピレン樹脂層
1Cに充分に伝達され、ホットメルト接着剤1bが軟化
し、又ポリプロピレン樹脂1Cが成形可能な温度にまで
加熱され絞り加工が達成できるような速度で上下バット
2a、2bを移動する必要があり、実施例では第1a図
の状態から第2d図の成形完了まで20秒を要した。During the above drawing process, the heat of the mold is transferred to the titanium layer 1.
a→hot melt adhesive layer 1b-polypropylene resin layer 1C at a speed such that the hot melt adhesive 1b is softened and the polypropylene resin 1C is heated to a temperature at which it can be molded and drawing processing can be achieved. It was necessary to move the upper and lower bats 2a, 2b, and in the example, it took 20 seconds to complete the molding from the state shown in FIG. 1a to the state shown in FIG. 2d.
(実施例2〉
合成樹脂層としてポリエーテルイミド樹脂フィルム(2
5萌厚)を使用して実施例1と同様の工程で複合シート
を作製、金型温度205〜215℃、成形時間40秒で
実施例1と同様の絞り成形により同形状のドーム状振動
板を得た。(Example 2) Polyetherimide resin film (2
A composite sheet was produced using the same process as in Example 1 using 5 mm thick), and a dome-shaped diaphragm of the same shape was formed by drawing in the same manner as in Example 1 at a mold temperature of 205 to 215°C and a forming time of 40 seconds. I got it.
又、比較例1として、チタン(JIS TP28R,O
材、20萌厚)箔を成形したドーム状振動板、比較例2
としてポリエステル繊維織布にアクリル樹脂エマルジョ
ンをコーティングしたコーティング布(115即厚)を
成形したドーム状振動板、比較例3としてポリプロピレ
ン樹脂フィルム(38m厚)を成形したドーム状振動板
、比較例4としてポリエーテルイミド樹脂フィルム(3
8tIIrI厚)を成形したドーム状撮動板、をそれぞ
れ作製し、前記実施例1及び2のドーム状撮動板ととも
に諸物性を測定した結果を第1第1表
但し、ヤング率: X 1010dyn / ci面密
度: g /100 crA
熱変形温度:℃
更に、比較例1及び比較例4のドーム状]辰動板及び実
施例2のドーム状撮動板を同一の部品を使用してスピー
カを組立て、各スピーカの周波数特性を測定したところ
第4図の結果を得た。In addition, as Comparative Example 1, titanium (JIS TP28R, O
Dome-shaped diaphragm made of foil (20 mm thick), Comparative Example 2
As Comparative Example 3, a dome-shaped diaphragm was molded from a polyester fiber woven fabric coated with an acrylic resin emulsion (115 thick); as Comparative Example 3, a dome-shaped diaphragm was molded from a polypropylene resin film (38 m thick); as Comparative Example 4: Polyetherimide resin film (3
Table 1 shows the results of measuring various physical properties of the dome-shaped imaging plates molded with a dome-shaped imaging plate of 8tIIrI thickness) in conjunction with the dome-shaped imaging plates of Examples 1 and 2. ci surface density: g/100 crA Heat deformation temperature: °C Furthermore, a speaker was assembled using the same parts as the dome-shaped sliding plates of Comparative Examples 1 and 4 and the dome-shaped moving plate of Example 2. When the frequency characteristics of each speaker were measured, the results shown in FIG. 4 were obtained.
[発明の効果]
以上の実施例により説明したこの発明によれば、従来の
撮動板に比較すると、ヤング率はチタン振動板に次いで
大きく、又チタン振動板に比較するとtanδが著しく
増大する。[Effects of the Invention] According to the present invention described in the above embodiments, when compared with conventional imaging plates, the Young's modulus is the second largest after that of a titanium diaphragm, and when compared with a titanium diaphragm, tan δ increases significantly.
又、熱変形温度も150℃と実用上問題のない値を有し
ている。Further, the heat deformation temperature is 150° C., which is a value that poses no practical problem.
又周波数特性から見ても本発明実施例によれば、高域共
撮によるピーク・ディップの発生が極めて小さく、高調
波歪みが小さいことが分かる。Also, when looking at the frequency characteristics, it can be seen that according to the embodiment of the present invention, the occurrence of peak dips due to high frequency co-photography is extremely small, and harmonic distortion is small.
更に、この発明はホットメルト型接着材を使用すること
により金属・合成樹脂複合シートの成形加工が可能とな
る効果を有する。Furthermore, the present invention has the effect that a metal/synthetic resin composite sheet can be formed by using a hot-melt adhesive.
すなわち、従来の複合シートの成形において、絞り工程
で凸金具に当接している面は凸金具の面に沿って賦形さ
れるが、当接していない部分には放射状のシワが発生し
、上下バットの下降に伴なって、前記シワが延ばされ凸
金具に沿っていく。In other words, in conventional composite sheet forming, the surface that is in contact with the convex metal fitting during the drawing process is shaped along the surface of the convex metal fitting, but radial wrinkles occur in the areas that are not in contact, and the upper and lower parts are As the bat descends, the wrinkles are extended and follow the convex metal fittings.
この際に、複合フィルムの各層が接着され相互に独自の
伸延が阻害されているので、延びの違いにより接着剤を
介して相互に引張り合う力が作用し、当該作用力がシワ
の発生状態により部分的に異なる結果、不均一な張力が
部分的に作用し、これにより引張り力に弱いチタン層が
破断する問題があったが、この発明においては、ホット
メルト型接着剤が絞り成形時において軟化し、チタン層
と合成樹脂層の両面に均等に粘性抵抗による緊張力を与
え、チタン層のシワの発生を抑制するような力が作用す
ると共に、チタン層と合成樹脂層の延びの差は前記接着
剤の流動変形により緩衝されるのでチタン層と合成樹脂
層の部分的に直接引張り合う張力が小さくなり、チタン
層の破断を抑制することができる。At this time, each layer of the composite film is adhered and their own stretching is inhibited, so the difference in stretching causes a mutual pulling force to act through the adhesive, and this acting force depends on the state of wrinkles. As a result, the titanium layer, which is weak in tensile force, breaks due to uneven tension acting locally.However, in this invention, the hot melt adhesive softens during drawing. However, the tension force due to viscous resistance is applied equally to both sides of the titanium layer and the synthetic resin layer, and a force that suppresses the generation of wrinkles in the titanium layer acts, and the difference in elongation between the titanium layer and the synthetic resin layer is Since it is buffered by the flow deformation of the adhesive, the tension that partially draws the titanium layer and the synthetic resin layer directly against each other is reduced, and breakage of the titanium layer can be suppressed.
又、前述のように絞り成形時においてホットメルト型接
着剤が軟化して流動するので接着剤の欠膠部分の発生が
なく接着強度が大ぎい。Further, as mentioned above, the hot melt adhesive softens and flows during drawing, so no adhesive portions are formed and the adhesive strength is high.
又、接着剤の欠膠部分の発生がないことにより接着剤は
必要最小限の厚さに制限することができるので軽母な振
動板を提供することができる。In addition, since there is no non-glue portion of the adhesive, the thickness of the adhesive can be limited to the minimum necessary thickness, so a lightweight diaphragm can be provided.
更に本発明に使用するホットメルト型接着剤は拘束型振
動抑制効果が大きく得られるように金属層及び樹脂層よ
りも内部損失の大きい材料を使用するのが好ましい。Further, the hot melt adhesive used in the present invention is preferably made of a material having a larger internal loss than the metal layer and the resin layer so as to obtain a large restraint type vibration suppressing effect.
第1図はこの発明実施例の振動板の断面図、第2図はこ
の発明実施例における複合シー1ル作製工程図、第3図
は同絞り成形工程図、第4図は本発明実施例及び比較例
の振動板を使用したそれぞれのスピーカの周波数特性図
である。
特許出願人 オンキヨー株式会社
第? +”L
巻取0−1し
牟乙1月Fig. 1 is a cross-sectional view of a diaphragm according to an embodiment of the present invention, Fig. 2 is a process diagram for manufacturing a composite seal in an embodiment of this invention, Fig. 3 is a drawing process diagram of the same, and Fig. 4 is a diagram of an embodiment of the present invention. and FIG. 7 is a frequency characteristic diagram of each speaker using a diaphragm of a comparative example. Patent applicant: Onkyo Co., Ltd. +”L Winding 0-1 and January
Claims (1)
接着積層されてなることを特徴とするスピーカ用複合振
動板A composite diaphragm for speakers characterized by a metal layer and a thermoplastic resin layer bonded and laminated using a hot-melt adhesive.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11636487A JPS63280600A (en) | 1987-05-12 | 1987-05-12 | Composite diaphragm for speaker |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11636487A JPS63280600A (en) | 1987-05-12 | 1987-05-12 | Composite diaphragm for speaker |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS63280600A true JPS63280600A (en) | 1988-11-17 |
Family
ID=14685133
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP11636487A Pending JPS63280600A (en) | 1987-05-12 | 1987-05-12 | Composite diaphragm for speaker |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS63280600A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2007322589A (en) * | 2006-05-31 | 2007-12-13 | Nisshin Steel Co Ltd | Precoated steel sheet for diaphragm of electric horn |
US20150075900A1 (en) * | 2011-11-03 | 2015-03-19 | Shunming Yuen | Loudspeaker diaphragm and loudspeaker using same |
US9173033B1 (en) * | 2014-08-08 | 2015-10-27 | Merry Electronics (Suzhou) Co., Ltd. | Composite vibration diaphragm and its fabrication method |
US10598408B2 (en) | 2014-02-17 | 2020-03-24 | Savo-Solar Oy | Solar thermal absorber element |
-
1987
- 1987-05-12 JP JP11636487A patent/JPS63280600A/en active Pending
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2007322589A (en) * | 2006-05-31 | 2007-12-13 | Nisshin Steel Co Ltd | Precoated steel sheet for diaphragm of electric horn |
US20150075900A1 (en) * | 2011-11-03 | 2015-03-19 | Shunming Yuen | Loudspeaker diaphragm and loudspeaker using same |
US9324315B2 (en) * | 2011-11-03 | 2016-04-26 | Innovation Sound Technology Co., Ltd. | Loudspeaker diaphragm and loudspeaker using same |
US10598408B2 (en) | 2014-02-17 | 2020-03-24 | Savo-Solar Oy | Solar thermal absorber element |
US9173033B1 (en) * | 2014-08-08 | 2015-10-27 | Merry Electronics (Suzhou) Co., Ltd. | Composite vibration diaphragm and its fabrication method |
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