JPH0459023B2 - - Google Patents
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- Publication number
- JPH0459023B2 JPH0459023B2 JP61044878A JP4487886A JPH0459023B2 JP H0459023 B2 JPH0459023 B2 JP H0459023B2 JP 61044878 A JP61044878 A JP 61044878A JP 4487886 A JP4487886 A JP 4487886A JP H0459023 B2 JPH0459023 B2 JP H0459023B2
- Authority
- JP
- Japan
- Prior art keywords
- injection port
- liquid
- liquid injection
- nozzle
- gas
- 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.)
- Expired - Lifetime
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- Loading And Unloading Of Fuel Tanks Or Ships (AREA)
- Nozzles (AREA)
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は各種産業に於て、2種類以上の混合液
を微粒化し、造粒、燃焼、塗装及び窯業に於ける
釉薬の吹付け等の作業に使用されるノズルであつ
て、特願昭60−184628号(二流体ノズル)の改良
に係り、特に前出願に於ては液体送入口が一つの
ため、予め混合液を用意しなければならなかつた
が、本発明では複数個の液体送入口を介して各液
を単独で送り込める様にした二流体ノズルに関す
る。[Detailed Description of the Invention] [Field of Industrial Application] The present invention is used in various industries to atomize a mixed liquid of two or more types, and to be used in granulation, combustion, painting, spraying of glaze in the ceramics industry, etc. This is a nozzle used for work, and is related to the improvement of Japanese Patent Application No. 60-184628 (two-fluid nozzle), especially in the previous application, there is only one liquid inlet, so a mixed liquid must be prepared in advance. However, the present invention relates to a two-fluid nozzle in which each liquid can be fed individually through a plurality of liquid inlet ports.
従来のこの種のノズルでは、2種類以上の混合
した液体を予め造つておき、一つの混合液として
ノズルに送り込み微粒化していた。このため混合
液によつては沈殿を生じ均一な微粒化が困難で有
つたり、水と油の様な場合は混合する事そのもの
が不可能で有り、又複数の液体を混合した場合、
時間の経過と共に化学変化を起したり、ノズルを
小型化する場合は従来の技術では微粒化する事が
不可能に近い等の問題があつた。
In conventional nozzles of this type, a mixture of two or more types of liquids is prepared in advance and fed into the nozzle as a single mixed liquid to be atomized. For this reason, depending on the mixed liquid, precipitation may occur and it is difficult to uniformly atomize the liquid, and in cases such as water and oil, mixing itself is impossible, and when multiple liquids are mixed,
There have been problems such as chemical changes occurring over time, and when miniaturizing the nozzle, it is almost impossible to atomize the particles using conventional techniques.
本発明は前記従来技術の問題点に鑑みなされた
もので、その目的は、一つのノズルに設けた複数
の液体送入口より複数の液体をそれぞれ送り込
み、ノズルの内部で瞬間に一次混合を行つた粒子
を再び外部混合により微粒化を行い、今迄に予め
混合の出来なかつた液体や沈殿性の強い液体の微
粒化を達成できる二流体ノズルを提供することで
あり、さらに具体的には、第1には、混合する液
体によつて沈殿物を生ずる液体の場合従来のノズ
ルでは沈殿物により目詰りを起すが本発明により
解決する事、第2には、混合する事により経時的
に硬化する液体をノズルの中で瞬時に混合し微粒
化して解決する事、第3には、油と水等を混合し
て燃焼を行う場合に一つのノズルの別々の液体送
入口より送り込みノズル内で混合し微粒化し燃焼
を可能にする事である。 The present invention was made in view of the problems of the prior art, and its purpose is to feed a plurality of liquids through a plurality of liquid inlet ports provided in one nozzle, and perform primary mixing instantly inside the nozzle. The object of the present invention is to provide a two-fluid nozzle that can atomize particles by external mixing again and achieve atomization of liquids that could not be mixed in advance or liquids with strong sedimentation properties. Firstly, in the case of liquids that produce precipitates when mixed, conventional nozzles are clogged by the precipitates, but this is solved by the present invention.Secondly, by mixing, the nozzles harden over time. The solution is to instantly mix the liquid in the nozzle and atomize it. Thirdly, when mixing oil and water for combustion, the liquid is fed from separate liquid inlet ports of one nozzle and mixed in the nozzle. The goal is to atomize it and make it possible to burn it.
前記目的を達成するために本発明に係る二流体
ノズルにおいては、微粒化対象である液体が気体
とともに噴出する液体噴射口と、前記液体噴射口
を取り囲む位置に形成された渦流室と、渦巻状に
渦流室に延びて、渦流室に高速旋回流を発生する
べく渦流室に高速気流を導入する旋回導孔と、前
記渦流室の前記液体噴射口に臨む位置に形成され
て液体噴射口の前方に先細り円錐形の高速渦流を
噴射形成する環状噴射口と、からなる高速渦流気
体による超微粒子発生用の二流体ノズルであつ
て、前記液体噴射口及び気体噴射口の開口されて
いるノズル先端部を、液体噴射口を突出端部とす
る尖頭形状に形成し、前記旋回導孔及び液体噴射
口に単一の圧縮気体送入口からそれぞれ気流通路
を延設し、液体噴射口に延びる気流通路に複数の
送液口を開口して、各々の送液口から導かれた液
体を気流により破砕混合して液体噴射口に導くよ
うにしたものである。
In order to achieve the above object, the two-fluid nozzle according to the present invention includes a liquid injection port through which the liquid to be atomized is ejected together with gas, a swirl chamber formed at a position surrounding the liquid injection port, and a swirl-shaped a swirl guide hole extending into the swirl chamber and introducing a high-speed airflow into the swirl chamber to generate a high-speed swirl flow in the swirl chamber; and a swirl guide hole formed at a position facing the liquid injection port of the swirl chamber and facing the liquid injection port A two-fluid nozzle for generating ultrafine particles by means of a high-speed vortex gas, comprising an annular injection port that injects and forms a tapered conical high-speed vortex flow, the nozzle tip having an opening for the liquid injection port and the gas injection port. is formed into a pointed shape with a liquid injection port as a protruding end, and an air flow passage is provided extending from a single compressed gas inlet to the swirl guide hole and the liquid injection port, respectively, and an air flow passage extending to the liquid injection port. A plurality of liquid feeding ports are opened in the liquid feeding port, and the liquid introduced from each liquid feeding port is crushed and mixed by an air flow and then guided to a liquid injection port.
複数の液体送入口かたそれぞれ導かれた液体
は、圧縮気体送入口から導かれた気流により第1
の空気通路において破砕混合されて液体噴射口か
ら気液混合体として噴出される。またこの液体噴
射口周りの環状の気体噴射口からは、第2の気流
通路から導かれた気流がスパイラル状の旋回導孔
を介して渦流室に送られて先細り円錐形の高速渦
流となつて噴射される。そして液体噴射口から噴
出された気液混合体はこの高速渦流と接触して破
砕されて霧状の微粒子となる。
The liquid guided through each of the plurality of liquid inlets is transferred to the first one by the airflow led from the compressed gas inlet
The liquid is crushed and mixed in the air passage and is ejected from the liquid injection port as a gas-liquid mixture. Also, from the annular gas injection port around the liquid injection port, the airflow guided from the second airflow passage is sent to the vortex chamber via the spiral swirl guide hole and becomes a tapered conical high-speed vortex. Injected. The gas-liquid mixture ejected from the liquid injection port comes into contact with this high-speed vortex and is crushed into atomized fine particles.
また液体噴射口及びこの液体噴射口を取り囲む
環状の気体噴射口の形成されているノズル先端部
は液体噴射口を突出端部とする尖頭型で、液体噴
射口周りに負圧が生じにくい。 Further, the nozzle tip, in which the liquid injection port and the annular gas injection port surrounding the liquid injection port are formed, has a pointed shape with the liquid injection port as a protruding end, so that negative pressure is less likely to be generated around the liquid injection port.
次に本発明の実施例を図面に基づいて説明す
る。
Next, embodiments of the present invention will be described based on the drawings.
第1図〜第5図は本発明の一実施例を示すもの
で、第1図は本発明の一実施例である二流体ノズ
ルの外形平面図、第2図は正面図、第3図は第2
図A−A′断面図、第4図は第2図B−B′断面図、
第5図は第1図C−C′断面図である。 Figures 1 to 5 show an embodiment of the present invention. Figure 1 is an external plan view of a two-fluid nozzle which is an embodiment of the present invention, Figure 2 is a front view, and Figure 3 is a front view. Second
Figure A-A' sectional view, Figure 4 is Figure 2 B-B' sectional view,
FIG. 5 is a sectional view taken along the line C-C' in FIG.
これらの図において、符号4はノズルボデイ
で、このノズルボデイ4内において、前方に開口
して液体噴射口を形成する前後に延びる内部混合
室11と、後方に開口する圧縮気体送入口8とが
小径の一次気体噴出口9を介して連通して、圧縮
気体送入口8と液体噴射口とを連絡する第1の気
流通路が形成されている。内部混合室11の絞ら
れた一次気体噴出口9の近傍には、一対の液体送
入口10,10が対向するように配置されてい
る。また内部混合室11を挾んだ位置には、内部
混合室11に沿つて圧縮気体送入口8に連通する
第2の気流通路である二次気体通路12が延びて
いる。ノズルボデイ4の前方には内部混合室11
の前方領域を形成するとともに、液体噴射口を形
成する円筒形状のノズルチツプ5が一体に形成さ
れている。ノズルチツプ5の外側には、二次気体
通路12に連絡する空洞13、旋回導孔であるス
パイラル状の二次気体噴出溝14及び渦流室15
が形成され、渦流室15はノズルチツプ5前端部
周りに環状間隙16として開口している。そして
ノズルチツプ前端の液体噴射口周りの環状間隙1
6は液体噴射口の前方に先細り円錐形の高速渦流
を噴射形成する気体噴射口を構成している。この
ように、一次気体噴出口9と内部混合室11とか
らなり、圧縮気体送入口8から液体噴射口に延び
る第1の空気通路の外側に圧縮気体送入口8から
旋回導孔(二次気体噴出溝14)に延びる第2の
空気通路である二次気体通路12が形成されてい
る。 In these figures, reference numeral 4 denotes a nozzle body, and within this nozzle body 4, there is an internal mixing chamber 11 that opens at the front and forms a liquid injection port that extends back and forth, and a compressed gas inlet 8 that opens at the rear and has a small diameter. A first airflow passage is formed which communicates with the compressed gas inlet 8 and the liquid injection port through the primary gas injection port 9 . A pair of liquid inlet ports 10, 10 are arranged in the vicinity of the constricted primary gas outlet 9 of the internal mixing chamber 11 so as to face each other. Further, at a position sandwiching the internal mixing chamber 11, a secondary gas passage 12, which is a second airflow passage communicating with the compressed gas inlet 8, extends along the internal mixing chamber 11. An internal mixing chamber 11 is located in front of the nozzle body 4.
A cylindrical nozzle tip 5 that forms a front region of the nozzle and a liquid injection port is integrally formed. On the outside of the nozzle tip 5, there are a cavity 13 communicating with the secondary gas passage 12, a spiral secondary gas ejection groove 14 serving as a swirl guide hole, and a swirl chamber 15.
is formed, and the swirl chamber 15 opens around the front end of the nozzle tip 5 as an annular gap 16. and an annular gap 1 around the liquid injection port at the front end of the nozzle tip.
Reference numeral 6 constitutes a gas injection port that injects and forms a tapered conical high-speed vortex in front of the liquid injection port. In this way, a swirl guide hole (secondary gas inlet) is formed from the compressed gas inlet 8 to the outside of the first air passage, which consists of the primary gas outlet 9 and the internal mixing chamber 11 and extends from the compressed gas inlet 8 to the liquid injection outlet. A secondary gas passage 12, which is a second air passage, is formed extending to the ejection groove 14).
なお本実施例のノズルは、ノズルボデイ4のノ
ズルチツプ5に圧縮コイルスプリング6を介して
二次気体噴出溝14の形成されている中子2(第
7図参照)を組付け、さらに中子2を覆うように
噴板キヤツプ1を配し、噴板キヤツプ1の外周か
ら締付リング3をノズルボデイのねじ部7に螺合
させて、液体噴射口であるノズルチツプ5の周り
に空洞13、二次気体噴出溝(旋回導孔)14、
渦流室15及び環状間隙(環状の気体噴射口)1
6を一体に設けた構造となつている。 In the nozzle of this embodiment, a core 2 (see FIG. 7) in which a secondary gas ejection groove 14 is formed is assembled to the nozzle tip 5 of the nozzle body 4 via a compression coil spring 6, and the core 2 is further assembled into the nozzle tip 5 of the nozzle body 4. A spout plate cap 1 is disposed so as to cover the nozzle, and a tightening ring 3 is screwed onto the threaded portion 7 of the nozzle body from the outer periphery of the spout plate cap 1 to form a cavity 13 and a secondary gas around the nozzle tip 5, which is a liquid injection port. Ejection groove (swivel guide hole) 14,
Swirl chamber 15 and annular gap (annular gas injection port) 1
6 is integrated into the structure.
以下本実施例の示すノズルの作用を説明する。
第3図、第4図に於て、ノズルボデー4の後部に
設けた圧縮体送入口8より送り込まれた高圧の気
体は小口径の一次気体噴出口9を通り噴射して内
部混合室11に入る。此の時ノズルボデー4に設
けた液体送入口10,10の附近に負圧を生じ、
各々の液体送入口から液体を内部混合室11に吸
込む。一次気体噴出口9より噴出する高速気体は
液体送入口10より入る液体を第一次破砕し広く
なつた内部混合室11の中で混合され、流速を落
してノズルチツプ5前端に形成されている液体噴
射口に向う。又一方圧縮気体送入口8より入つた
高圧気体は、第4図、第5図に示されるように、
ノズルボデー4の中に設けた外側の二次気体通路
12を通り、ノズルボデー4の前面と噴板キヤツ
プ1及び中子2、ノズルチツプ5の外周によつて
構成される空洞13に入る。そして中子2の外周
部にそつてスパイラル状に設けた二次気体噴出溝
14と噴板キヤツプ1の内面によつて形成される
隙間(旋回導孔)を通り、噴板キヤツプ1と中子
2の前面凹部及びノズルチツプ5の先端外周部に
よつて構成される渦流室15に入る。そして渦流
室15内で高速渦流となつてノズルチツプ先端部
と噴板キヤツプ1の内周縁によつて構成される気
体噴射口である狭い円環状間隙16より先細り円
錐形状の高速渦流となつて噴射し、此の時液体噴
射口である内部混合室11より流速を落してノズ
ルチツプ5の前方に噴出する混合液を二次混合し
ながら破砕微粒化して前方に噴霧する。 The operation of the nozzle shown in this embodiment will be explained below.
In FIGS. 3 and 4, high-pressure gas is sent from the compressed body inlet 8 provided at the rear of the nozzle body 4 and is injected through the small-diameter primary gas outlet 9 and enters the internal mixing chamber 11. . At this time, negative pressure is generated near the liquid inlet ports 10, 10 provided in the nozzle body 4,
Liquid is sucked into the internal mixing chamber 11 from each liquid inlet. The high-speed gas ejected from the primary gas outlet 9 first crushes the liquid entering from the liquid inlet 10 and is mixed in the enlarged internal mixing chamber 11, and the flow rate is reduced to form a liquid at the front end of the nozzle tip 5. Head towards the injection port. On the other hand, the high pressure gas entering from the compressed gas inlet 8 is as shown in FIGS. 4 and 5.
It passes through an outer secondary gas passage 12 provided in the nozzle body 4 and enters a cavity 13 formed by the front surface of the nozzle body 4, the jet plate cap 1, the core 2, and the outer periphery of the nozzle tip 5. Then, it passes through the gap (swivel guide hole) formed by the secondary gas blowout groove 14 provided in a spiral along the outer circumference of the core 2 and the inner surface of the spout plate cap 1, and the spout plate cap 1 and the core The nozzle tip 5 enters a vortex chamber 15 formed by the front recess of the nozzle tip 2 and the outer periphery of the tip of the nozzle tip 5. Then, it becomes a high-speed vortex in the vortex chamber 15 and is injected from the narrow annular gap 16, which is a gas injection port formed by the tip of the nozzle tip and the inner circumferential edge of the jet plate cap 1, as a tapered cone-shaped high-speed vortex. At this time, the mixed liquid jetted forward of the nozzle tip 5 at a reduced flow rate from the internal mixing chamber 11, which is a liquid jetting port, is crushed and atomized and sprayed forward while being subjected to secondary mixing.
第6図は本発明の二流体ノズルの第2実施例の
横断面図で、第5図に対応する図である。この実
施例では、内部混合室11に沿つて第2の気流通
路を構成する二次気体通路12が3個設けられて
いる点が前記実施例と相違している。 FIG. 6 is a cross-sectional view of a second embodiment of the two-fluid nozzle of the present invention, and corresponds to FIG. 5. This embodiment differs from the previous embodiment in that three secondary gas passages 12 are provided along the internal mixing chamber 11 to constitute a second airflow passage.
第8図は前記した第1の実施例の二流体ノズル
を用いて混合噴霧を行う場合の基本的な説明図で
有る。コンプレツサーEより送られた気体はレギ
ユレーターDにより調圧されバルブCを通り、パ
イプBを通り本発明の二流体ノズルAに入る。一
方液剤タンクGより、自吸、加圧、又は液剤ポン
プHにより送出された液体は液剤バルブIを通り
液剤調量弁Jにより、各液の量を調節した後液剤
パイプFを通り、ノズルの二箇の液体送入口より
別々に入り前述の作用により、ノズルAにより混
合噴霧されるもので有る。 FIG. 8 is a basic explanatory diagram when mixed spraying is performed using the two-fluid nozzle of the first embodiment described above. The gas sent from the compressor E is pressure regulated by the regulator D, passes through the valve C, passes through the pipe B, and enters the two-fluid nozzle A of the present invention. On the other hand, the liquid sent from the liquid tank G by self-priming, pressurization, or liquid pump H passes through the liquid valve I, adjusts the amount of each liquid by the liquid metering valve J, and then passes through the liquid pipe F to the nozzle. The two liquids enter separately from the two liquid inlets and are mixed and sprayed by the nozzle A by the above-mentioned action.
以上の説明から明らかなように、本発明によれ
ば、二種類以上の液体の超微粒化が達成でき、微
粒化対象の粘度が高い液体であつても目詰まりや
前ダレやボタ落ちといつた液体粒子の液体噴射口
周辺への付着によるトラブルの発生もない。従つ
て今迄混合する原液の性質によつては沈殿を生じ
たり、混合する事により硬化したり、又水と油の
様に混合しない液体の混合微粒化が可能となるた
め、スプレードライヤー等に於ける混合液体の造
粒、燃焼工程に於ける燃料と補助剤を用いての燃
焼、窯業に於ける釉薬等の吹付工程等混合液の微
粒化を必要とする多くの産業に寄与する所大であ
る。
As is clear from the above explanation, according to the present invention, it is possible to achieve ultra-atomization of two or more types of liquids, and even if the liquid to be atomized has a high viscosity, there will be no clogging, dripping, or dripping. There is no problem caused by liquid particles adhering to the vicinity of the liquid injection port. Therefore, depending on the nature of the stock solution being mixed, precipitation may occur, or it may harden by mixing, or it may be possible to mix and atomize liquids that do not mix, such as water and oil, so it is difficult to use with a spray dryer, etc. It contributes to many industries that require atomization of mixed liquids, such as granulation of mixed liquids, combustion using fuel and auxiliary agents in the combustion process, and spraying processes such as glazes in the ceramics industry. It is.
第1図は本発明の第1の実施例である二流体ノ
ズルの外形平面図、第2図は正面図、第3図は第
2図A−A′断面図、第4図は第2図B−B′断面
図、第5図は第1図C−C′断面図、第6図は本発
明の第2の実施例である二流体ノズルの横断面
図、第7図は中子の説明図、第8図は本発明のノ
ズルを用いての基本的な説明図である。
1……噴板キヤツプ、2……中子、3……締付
リング、4……ノズルボデー、5……ノズルチツ
プ、6……圧縮スプリング、7……ネジ部、8…
…圧縮気体送入口、9……一次気体噴出口、10
……液体送入口、11……第1の空気通路及び液
体噴射口を形成する内部混合室、12……第2の
空気通路である二次気体通路、13……空洞、1
4……旋回導孔である二次気体噴出溝、15……
渦流室、16……気体噴射口である環状間隙。
Fig. 1 is an external plan view of a two-fluid nozzle according to a first embodiment of the present invention, Fig. 2 is a front view, Fig. 3 is a cross-sectional view taken along line A-A' in Fig. 2, and Fig. 4 is a cross-sectional view of Fig. 2. FIG. 5 is a sectional view taken along line C-C' in FIG. The explanatory diagram, FIG. 8, is a basic explanatory diagram using the nozzle of the present invention. DESCRIPTION OF SYMBOLS 1... Spray plate cap, 2... Core, 3... Tightening ring, 4... Nozzle body, 5... Nozzle tip, 6... Compression spring, 7... Threaded part, 8...
...Compressed gas inlet, 9...Primary gas outlet, 10
...Liquid inlet, 11...Internal mixing chamber forming a first air passage and liquid injection port, 12...Secondary gas passage which is a second air passage, 13...Cavity, 1
4...Secondary gas ejection groove which is a turning guide hole, 15...
Whirlpool chamber, 16...An annular gap that is a gas injection port.
Claims (1)
る液体噴射口と、前記液体噴射口を取り囲む位置
に形成された渦流室と、渦巻状に渦流室に延び
て、渦流室に高速旋回流を発生するべく渦流室に
高速気流を導入する旋回導孔と、前記渦流室の前
記液体噴射口に臨む位置に形成されて液体噴射口
の前方に先細り円錐形の高速渦流を噴射形成する
環状噴射口と、からなる高速渦流気体による超微
粒子発生用の二流体ノズルであつて、前記液体噴
射口及び気体噴射口の開口されているノズル先端
部が液体噴射口を突出端部とする尖頭形状に形成
され、前記旋回導孔及び液体噴射口には単一の圧
縮気体送入口からそれぞれ気流通路が延びてお
り、液体噴射口に延びる気流通路には複数の送液
口が開口されて、各々の送液口から導かれた液体
が気流により破砕混合されて液体噴射口に導かれ
ることを特徴とする二流体ノズル。1. A liquid injection port through which the liquid to be atomized is ejected together with gas, a vortex chamber formed at a position surrounding the liquid injection port, and a vortex chamber that extends into the vortex chamber in a spiral shape to generate a high-speed swirling flow in the vortex chamber. a swirl guide hole that introduces a high-speed airflow into the vortex chamber; an annular injection port that is formed at a position facing the liquid injection port of the vortex chamber and that injects and forms a tapered conical high-speed vortex in front of the liquid injection port; A two-fluid nozzle for generating ultrafine particles using a high-speed eddying gas comprising: a nozzle tip where the liquid injection port and the gas injection port are opened; , air flow passages extend from a single compressed gas inlet to the swirl guide hole and the liquid injection port, respectively, and a plurality of liquid feed ports are opened in the air flow passage extending to the liquid injection port, and each liquid feed A two-fluid nozzle characterized in that the liquid guided from the mouth is crushed and mixed by airflow and then guided to the liquid injection port.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4487886A JPS62201665A (en) | 1986-03-01 | 1986-03-01 | Two-liquid nozzle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4487886A JPS62201665A (en) | 1986-03-01 | 1986-03-01 | Two-liquid nozzle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS62201665A JPS62201665A (en) | 1987-09-05 |
| JPH0459023B2 true JPH0459023B2 (en) | 1992-09-21 |
Family
ID=12703746
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4487886A Granted JPS62201665A (en) | 1986-03-01 | 1986-03-01 | Two-liquid nozzle |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62201665A (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH05309314A (en) * | 1992-05-07 | 1993-11-22 | Sumitomo Pharmaceut Co Ltd | Coating method |
| DE69534151T2 (en) * | 1994-02-22 | 2006-01-12 | Nippon Telegraph And Telephone Corp. | Freeze-dried blood cells, stem cells and platelets and process for their preparation |
| JP4047635B2 (en) * | 2002-06-13 | 2008-02-13 | 芝浦メカトロニクス株式会社 | Substrate processing equipment |
| CA2606868C (en) * | 2005-05-06 | 2013-10-29 | Dieter Wurz | Spray nozzle, spray device and the operation method thereof |
| JP5021925B2 (en) * | 2005-09-29 | 2012-09-12 | 株式会社アトマックス | Vortex atomization nozzle capable of various mixed atomization of powder and liquid |
| FR3020578B1 (en) * | 2014-05-05 | 2021-05-14 | Total Raffinage Chimie | INJECTION DEVICE, ESPECIALLY FOR INJECTING A LOAD OF HYDROCARBONS IN A REFINING UNIT. |
| KR102649621B1 (en) * | 2015-09-09 | 2024-03-19 | 사솔 (유에스에이) 코포레이션 | How to make magnesium aluminate spinel |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5926348A (en) * | 1982-08-06 | 1984-02-10 | Nissan Jidosha Hanbai Kk | Washer for back of bottom of automobile |
-
1986
- 1986-03-01 JP JP4487886A patent/JPS62201665A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS62201665A (en) | 1987-09-05 |
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