JP3037058B2 - Ignition mechanism of high frequency inductively coupled plasma device - Google Patents

Ignition mechanism of high frequency inductively coupled plasma device

Info

Publication number
JP3037058B2
JP3037058B2 JP6050674A JP5067494A JP3037058B2 JP 3037058 B2 JP3037058 B2 JP 3037058B2 JP 6050674 A JP6050674 A JP 6050674A JP 5067494 A JP5067494 A JP 5067494A JP 3037058 B2 JP3037058 B2 JP 3037058B2
Authority
JP
Japan
Prior art keywords
gas
nebulizer
valve
inductively coupled
plasma
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 - Fee Related
Application number
JP6050674A
Other languages
Japanese (ja)
Other versions
JPH07263182A (en
Inventor
岩永光恭
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Jeol Ltd
Original Assignee
Jeol Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Jeol Ltd filed Critical Jeol Ltd
Priority to JP6050674A priority Critical patent/JP3037058B2/en
Publication of JPH07263182A publication Critical patent/JPH07263182A/en
Application granted granted Critical
Publication of JP3037058B2 publication Critical patent/JP3037058B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Electron Sources, Ion Sources (AREA)
  • Other Investigation Or Analysis Of Materials By Electrical Means (AREA)
  • Plasma Technology (AREA)

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【産業上の利用分野】本発明は高周波誘導結合プラズマ
(ICP)装置の点火機構に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an ignition mechanism for a high frequency inductively coupled plasma (ICP) device.

【0002】[0002]

【従来の技術】図2は従来のICP装置の点火機構の例
を示す図である。ガスボンベ1からのガスを減圧弁2を
通してガスフローコントローラ3で3系統に分けてトー
チ管7に導入する。3系統の1つはプラズマガス、1つ
は補助ガス、もう1つは試料液5の霧化と搬送とに使用
するため、ネブライザー4へ流し込んでいる。ネブライ
ザー4へ導入されるガスは試料液5の霧と共に、スプレ
ーチャンバー6を経て、トーチ管7の中心軸筒へ導入さ
れる。スプレーチャンバー6には円筒形の内筒6aが設
けられ、ここで、粒径の大きい霧は内筒に接触して液化
し、霧の粒径が揃えられてキャリアガスと共にトーチ管
7へ供給される。トーチ管7にはその周囲にロードコイ
ル8が設けられており、イグナイター9で点火してロー
ドコイル8で励起してプラズマ10を形成している。
2. Description of the Related Art FIG. 2 is a view showing an example of an ignition mechanism of a conventional ICP device. The gas from the gas cylinder 1 is introduced into the torch tube 7 through the pressure reducing valve 2 and divided into three systems by the gas flow controller 3. One of the three systems is supplied to the nebulizer 4 for use in plasma gas, one for auxiliary gas, and the other for atomization and transport of the sample liquid 5. The gas introduced into the nebulizer 4 is introduced into the central barrel of the torch tube 7 through the spray chamber 6 together with the mist of the sample liquid 5. The spray chamber 6 is provided with a cylindrical inner cylinder 6a. Here, the mist having a large particle diameter comes into contact with the inner cylinder and liquefies, and the mist having a uniform particle diameter is supplied to the torch tube 7 together with the carrier gas. You. A load coil 8 is provided around the torch tube 7, and is ignited by an igniter 9 and excited by the load coil 8 to form a plasma 10.

【0003】[0003]

【発明が解決しようとする課題】ところで、プラズマ1
0を点火・形成させる際は、ネブライザー4に流すガス
をほぼ0にした状態でイグナイター9からトーチ管7に
高電圧を印加する必要がある。ネブライザー4に流すガ
スは霧化の安定性・再現性を確保するために、ガスフロ
ーコントローラ3としてマスフローコントローラ型を使
用しており、この制御器は流量が0付近では制御が難し
くトーチ管7へガスが流れ込んでしまうという問題があ
る。ガスが流れ込むと、特に、スプレーチャンバー6に
水分があるときは、この水分(水蒸気)をもトーチ内へ
運び込むため、プラズマの点火に不利な条件となり、プ
ラズマの点火が容易ではない。
However, the plasma 1
When 0 is ignited and formed, it is necessary to apply a high voltage from the igniter 9 to the torch tube 7 with the gas flowing through the nebulizer 4 being almost zero. The gas flowing into the nebulizer 4 uses a mass flow controller type as the gas flow controller 3 in order to secure the stability and reproducibility of the atomization. There is a problem that gas flows in. When the gas flows, especially when there is moisture in the spray chamber 6, this moisture (water vapor) is also carried into the torch, which is a disadvantageous condition for plasma ignition, and plasma ignition is not easy.

【0004】本発明は上記課題を解決するためのもの
で、ICP装置のプラズマ点火を容易に行うことができ
るようにした高周波誘導結合プラズマ装置の点火機構を
提供することを目的とする。
An object of the present invention is to provide an ignition mechanism of a high-frequency inductively coupled plasma device which can easily perform plasma ignition of an ICP device.

【0005】[0005]

【課題を解決するための手段】本発明の高周波誘導結合
プラズマ装置の点火機構は、ガスフローコントローラを
介して供給されるガスにより、ネブライザーで試料液を
霧化し、点火装置およびロードコイルが設けられたトー
チ管に導入してプラズマ化させるようにした高周波誘導
結合プラズマ装置において、ガスフローコントローラか
らネブライザーへの流路にバイパス流路を設けて該流路
に弁を配置し、プラズマ点火時には前記弁を開いてネブ
ライザーへのガスをバイパス流路へ流すようにしたこと
を特徴とする。
The ignition mechanism of the high-frequency inductively coupled plasma apparatus according to the present invention atomizes a sample liquid by a nebulizer with a gas supplied through a gas flow controller, and is provided with an ignition apparatus and a load coil. In a high-frequency inductively coupled plasma apparatus which is introduced into a torch tube and turned into plasma, a bypass flow path is provided in a flow path from the gas flow controller to the nebulizer, and a valve is disposed in the flow path, and the valve is provided at the time of plasma ignition And the gas to the nebulizer is caused to flow to the bypass flow path.

【0006】[0006]

【作用】本発明はガスフローコントローラを介してネブ
ライザーに流すガスを、プラズマ点火時に弁を介して分
岐させるようにしたので、ネブライザーに流入するガス
をほぼ0にでき、プラズマの点火が極めて容易となり、
また分岐させたガスも他の用途へ利用することも可能で
ある。
According to the present invention, the gas flowing into the nebulizer through the gas flow controller is branched through the valve at the time of plasma ignition, so that the gas flowing into the nebulizer can be reduced to almost zero, and the plasma ignition becomes extremely easy. ,
The branched gas can also be used for other purposes.

【0007】[0007]

【実施例】図1は本発明の1実施例を示す図である。図
1は図2における3系統のガスフローのうち、ネブライ
ザーへ導入するガスフローを示したものであり、図2と
同一番号は同一内容を示している。図1において、図2
と相違する点はガスフローコントローラ3の後段にガス
を分岐させるための弁9が配置されている点である。即
ち、弁9は通常閉じた状態で使用し、その際の動作は図
2の場合と同様である。プラズマを点火する時はこの弁
9を開き、ガスフローコントローラ3のガス流量を最小
状態にすると、ガスフローコントローラ3を介して、な
お流れ出てくるガスは弁9を介して流路外へ逃がすよう
にする。この状態で図に示したようなイグナイター9で
点火すれば、トーチ管7へは水分が運び込まれていない
ため、容易にプラズマ点火を行うことができる。プラズ
マが点火したら弁9を閉じる。
FIG. 1 is a diagram showing one embodiment of the present invention. FIG. 1 shows the gas flow introduced into the nebulizer among the three gas flows in FIG. 2, and the same numbers as those in FIG. 2 indicate the same contents. In FIG. 1, FIG.
The difference from the first embodiment is that a valve 9 for branching the gas is provided at a stage subsequent to the gas flow controller 3. That is, the valve 9 is normally used in a closed state, and the operation at that time is the same as that in FIG. When the plasma is ignited, the valve 9 is opened, and when the gas flow rate of the gas flow controller 3 is minimized, the gas which still flows through the gas flow controller 3 is allowed to escape to the outside of the flow path via the valve 9. To In this state, if ignition is performed by an igniter 9 as shown in the figure, since no water is carried into the torch tube 7, plasma ignition can be easily performed. When the plasma ignites, valve 9 is closed.

【0008】なお、上記実施例において、弁9のさらに
後段に流路抵抗の小さい管を接続しておき、弁9を切り
換え弁として使い、他用途へネブライザーガスを利用す
るための弁としても良い。また、弁9は当然、手動、自
動どちらでも良い。
In the above-described embodiment, a pipe having a small flow resistance may be connected downstream of the valve 9 so that the valve 9 may be used as a switching valve, and may be used as a valve for utilizing nebulizer gas for other purposes. . Also, the valve 9 may be manually or automatically.

【0009】[0009]

【発明の効果】以上のように本発明によれば、ネブライ
ザーに流入するガスをほぼ0にすることができるため、
プラズマの点火が容易となり、さらにプラズマ点火時に
分岐させる弁を切り換え弁として使用することもでき、
容易に他用途へネブライザーガスの利用を行うことが可
能となる。
As described above, according to the present invention, the gas flowing into the nebulizer can be reduced to almost zero.
Plasma ignition is facilitated, and a valve that branches at the time of plasma ignition can be used as a switching valve.
The nebulizer gas can be easily used for other purposes.

【図面の簡単な説明】[Brief description of the drawings]

【図1】 本発明の1実施例を示す図である。FIG. 1 is a diagram showing one embodiment of the present invention.

【図2】 従来のICP装置の点火機構の例を示す図で
ある。
FIG. 2 is a diagram showing an example of an ignition mechanism of a conventional ICP device.

【符号の説明】[Explanation of symbols]

1…ガスボンベ、2…減圧弁、3…ガスフローコントロ
ーラ、4…ネブライザー、5…試料液、9…弁。
DESCRIPTION OF SYMBOLS 1 ... gas cylinder, 2 ... pressure reducing valve, 3 ... gas flow controller, 4 ... nebulizer, 5 ... sample liquid, 9 ... valve.

フロントページの続き (58)調査した分野(Int.Cl.7,DB名) G01N 27/62 - 27/70 H05H 1/24 - 1/52 H01J 49/00 - 49/48 G01N 21/73 Continuation of the front page (58) Field surveyed (Int.Cl. 7 , DB name) G01N 27/62-27/70 H05H 1/24-1/52 H01J 49/00-49/48 G01N 21/73

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 ガスフローコントローラを介して供給さ
れるガスにより、ネブライザーで試料液を霧化し、点火
装置およびロードコイルが設けられたトーチ管に導入し
てプラズマ化させるようにした高周波誘導結合プラズマ
装置において、ガスフローコントローラからネブライザ
ーへの流路にバイパス流路を設けて該流路に弁を配置
し、プラズマ点火時には前記弁を開いてネブライザーへ
のガスをバイパス流路へ流すようにしたことを特徴とす
る高周波誘導結合プラズマ装置の点火機構。
1. A high-frequency inductively coupled plasma in which a sample liquid is atomized by a nebulizer by a gas supplied through a gas flow controller, and introduced into a torch tube provided with an ignition device and a load coil to generate plasma. In the apparatus, a bypass flow path is provided in a flow path from the gas flow controller to the nebulizer, and a valve is disposed in the flow path. At the time of plasma ignition, the valve is opened to flow gas to the nebulizer through the bypass flow path. An ignition mechanism for a high-frequency inductively coupled plasma device.
JP6050674A 1994-03-22 1994-03-22 Ignition mechanism of high frequency inductively coupled plasma device Expired - Fee Related JP3037058B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6050674A JP3037058B2 (en) 1994-03-22 1994-03-22 Ignition mechanism of high frequency inductively coupled plasma device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6050674A JP3037058B2 (en) 1994-03-22 1994-03-22 Ignition mechanism of high frequency inductively coupled plasma device

Publications (2)

Publication Number Publication Date
JPH07263182A JPH07263182A (en) 1995-10-13
JP3037058B2 true JP3037058B2 (en) 2000-04-24

Family

ID=12865495

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6050674A Expired - Fee Related JP3037058B2 (en) 1994-03-22 1994-03-22 Ignition mechanism of high frequency inductively coupled plasma device

Country Status (1)

Country Link
JP (1) JP3037058B2 (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6879663B2 (en) * 2014-12-25 2021-06-02 株式会社日立ハイテクサイエンス Charged particle beam device

Also Published As

Publication number Publication date
JPH07263182A (en) 1995-10-13

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