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JP3569769B2 - Igniter plug - Google Patents
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JP3569769B2 - Igniter plug - Google Patents

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Publication number
JP3569769B2
JP3569769B2 JP24838095A JP24838095A JP3569769B2 JP 3569769 B2 JP3569769 B2 JP 3569769B2 JP 24838095 A JP24838095 A JP 24838095A JP 24838095 A JP24838095 A JP 24838095A JP 3569769 B2 JP3569769 B2 JP 3569769B2
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JP
Japan
Prior art keywords
igniter plug
metal shell
distal end
insulator
protector
Prior art date
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Expired - Fee Related
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JP24838095A
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Japanese (ja)
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JPH0973972A (en
Inventor
永五 後藤
幸彦 伊藤
隆博 鈴木
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Niterra Co Ltd
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NGK Spark Plug Co Ltd
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Priority to JP24838095A priority Critical patent/JP3569769B2/en
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  • Spark Plugs (AREA)

Description

【0001】
【発明の属する技術分野】
本発明は、主に地上用発電機のガスタービンに使用されるイグナイタプラグに関するものである。
【0002】
【従来の技術】
従来、ガスタービンエンジンに使用されるイグナイタプラグ1は、図4に示す如く、通常、エンジン内への突き出し面積低減のため先端部2が径小となっている主体金具3を備える。この主体金具3内に、軸孔4に中心電極5が突き出して嵌挿された絶縁体6をはめ込み、前記絶縁体6の先端面を主体金具3の先端面31より若干引き込め、セミ沿面放電面61を形成している。また、主体金具3の略中央部にはガスタービンエンジンに装着するための取付ネジ部34が形成されている。取付ネジ部34よりも後端側には六角ボルト状の六角部35が設けられ、取付ネジ部34と先端部2の間には先端部2よりも径の大きい径大部33が設けられている。主体金具3の先端部2の後端側には冷却用の通気孔32が形成されている。
【0003】
そして、図4及び図5の如く、ガスタービンエンジン9の燃焼チャンバー91にイグナイタプラグ1が装着されている。
該燃焼チャンバー91は、外壁912と内壁911とが設けられており、外壁912と内壁911との間には冷却のため及び燃焼に必要な空気を供給するための二次空気93が送り込まれる。
また、内壁911には各所に複数の通気孔9111が開けられ、燃焼の促進及び内壁材の冷却を行っている。かかる内壁911の側面の頂部近傍にイグナイタプラグ1が位置しており、二次空気93によってイグナイタプラグ1の主体金具3、絶縁体6及び中心電極5が冷却され、電極消耗の増加、酸化腐食の増加を抑制する働きがある。
一方、二次空気93はイグナイタプラグに設けられた通気孔32を通じて放電間隙63を通過することから電極間に生じた電気火花が二次空気93の流入によって前記燃焼チャンバー91の内部方向に移動し、燃料への着火性の向上にも寄与している。
【0004】
そして、内壁911の頂部には燃料噴射ノズル95が設けられ、燃料噴射ノズル95は微粒化した燃料951を噴射する。燃料への点火は、ガスタービンエンジンの始動時にイグナイタプラグ1に最大20kV、1〜2ジュールの蓄積エネルギを持った点火電源から、高エネルギの電気火花を毎秒2〜5回発火することにより行っている。この点火の際に、プラグの通気孔32に風速2〜3m/sの二次空気93が送り込まれる。そして、点火することにより発生する高圧縮燃焼ガスによりタービン(図示せず)が駆動される。
【0005】
【発明が解決しようとする課題】
かかる構成要素からなるイグナイタプラグにおいて、イグナイタプラグの電極間に電気火花が生ぜず、エンジンが始動しないという不具合が生じる場合があった。電気火花が生じないのはイグナイタプラグ内部に異物が混入し、それが原因となっていること判った。即ち、かかる異物は成分分析の結果、イグナイタプラグを構成する各部品には含まれない金属成分を主体とするものであり、かかる異物によって、点火電源から送られてきた電気エネルギがリークしイグナイタプラグの放電間隙63に電気火花が発生するのを妨げている。かかる異物による着火不良は、特に非常用発電機の様に一瞬の停電も許されない諸設備にとって影響が大きく、この対策が急がれている。
【0006】
本発明の目的は、安価にかつ簡便に二次空気中に存在する異物がイグナイタプラグ内部に侵入することを防止することができるイグナイタプラグを提供することにある。
【0007】
先端部の内方への突き出し部を有し、側面に内外を連通する通気孔が設けられた筒状を呈する主体金具と、
前記主体金具にはめ込まれた軸孔の付けられた絶縁体と、
前記主体金具の先端部の内周の内方への突き出し部と対向するように前記絶縁体の軸孔の先端より突き出して嵌挿された中心電極とからなり、
前記先端部から間隙を空けて、前記通気孔を覆う円筒状のプロテクタを配設したことを要旨とする。
【0008】
請求項2に記載の発明は、さらに前記プロテクタの内径と前記主体金具の先端部の外径とで形成する面積が、前記通気孔の面積以上であることを要旨とする。
【0009】
請求項3に記載の発明は、請求項1の発明において、前記プロテクタの内径と前記主体金具の先端部の外径とで形成する間隙が、前記絶縁体と前記主体金具の先端部の内周の内方への突き出し部とで形成する最小の間隙以下であることを特徴とすることを要旨とする。
【0010】
請求項4に記載の発明は、先端部の内周の内方への突き出し部と、該先端部の側面に内外を連通する通気孔が設けられた筒状を呈する主体金具と、
前記主体金具にはめ込まれた軸孔の付けられた絶縁体と、
前記主体金具の先端部の内周の内方への突き出し部と対向するように前記絶縁体の軸孔の先端より突き出して嵌挿された中心電極とからなり、
前記通気孔に網状又はスリット状のネットを配設したことを要旨とする。
【0011】
請求項1に記載の発明によって、プロテクタを設けたことにより飛来してきた異物が直接通気孔内に侵入する機会が大幅に減少する。
【0012】
請求項2に記載の発明によって、プロテクタ内径と、主体金具の先端部の外径とで形成する面積が通気孔の面積よりも大きいことからイグナイタプラグ内部を通過する冷却空気用二次空気の流量の低下はわずかである。
【0013】
請求項3に記載の発明によって、プロテクタ内径と、主体金具の先端部の外径とで形成する間隙が、絶縁体と前記主体金具の内径とで形成する最小の間隙よりも狭いことから、飛来してきたイグナイタプラグ内部に留まるような異物が直接通気孔内に侵入することがなく、また、侵入してきた場合にも前記絶縁体と前記主体金具の先端部の内周の内方への突き出し部とで形成する最小の間隙を通過して外部に排泄される。
【0014】
請求項4に記載の発明によって、主体金具、絶縁体及び中心電極の冷却能力が落ちることもなく、イグナイタプラグの寿命に影響することがないとともに、飛来してきた異物が直接通気孔内に侵入することがない。
特に網目の大きさ、スリット間隔を前記絶縁体と前記主体金具の先端部の内周の内方への突き出し部とで形成する最小の間隙以下にすれば該間隙に引っかかるような異物はイグナイタプラグ内部に侵入しない。また、侵入してきた異物は微小なものであるため、前記絶縁体と前記主体金具の先端部の内周の内方への突き出し部とで形成する最小の間隙に引っかかることなく排泄される。
【0015】
【発明の実施の形態】
(第1実施例)図1は本発明の第1実施例におけるイグナイタプラグの要部断面図を示す。
本発明の第1実施例におけるイグナイタプラグ100は、筒状の主体金具300と、絶縁体600と、中心電極500等とからなりガスタービンエンジンの燃焼チャンバー(図示せず)に装着されている。
主体金具300は、ステンレス製の耐熱性金属で形成され、該主体金具300の先端に形成された先端部302はテーパ面を介して中段部301よりも径小とされ、後端には六角部303が形成されている。また、中段部301と六角部303の間にはねじ部304が設けられ、このねじ部304によって前記燃焼チャンバーの外壁取付部に螺着される。
【0016】
主体金具300の先端部302の先端の先端内周は略直角に曲げられ、内方への突き出し面3021として突き出されている。この突き出し面3021と前記中心電極500の先端501との間には、絶縁体600の先端部601に沿って放電する沿面放電間隙602と、絶縁体600の先端部601の周側と主体金具300の突き出し面3021との間の気中放電間隙502を備えたセミ沿面放電間隙604を形成している。
【0017】
主体金具300の先端部302の後端側の側面には冷却用の通気孔305が4カ所等間隔に形成されている。さらに僅かな間隙を空けて通気孔を覆うように中段部301と同一寸法の外周の径を有する円筒状のプロテクタ700が溶接接合されている。該間隙は後述する主体金具の内方への突き出し面と絶縁体脚長部の先端面との最小の間隙以下となるように設定されている。即ち図2に示すように2B>(φ −φ の関係が成立するようにプロテクタ700の内径φdが決められている。
【0018】
絶縁体600は、アルミナの焼結体からなり、中心に軸孔400が形成され、前記中心電極500が嵌込まれている。先端は径小の脚長部603となり後端はコルゲーション604となっている。絶縁体600の脚長部603の先端面601は、前記主体金具300の先端面3022から若干引込んで配設され、沿面放電面となっている。脚長部603の後端はテーパ面となり板パッキンを挟んで前記主体金具300と当接している。絶縁体600の脚長部603の外周と主体金具300の内周との間隙は先端にいくほど広く形成されており、前記の主体金具300の先端部302の先端の先端内周に内方への突き出し面3021として突き出された面と絶縁体600の該脚長部603の先端面近傍が最も間隙が小さくなっている。
【0019】
中心電極500は、ニッケル合金で形成され、先端部501が前記主体金具300の先端面3022より突き出して嵌着されている。また後端は高圧電源と接続される端子部800となっている。
【0020】
(第2実施例)次に第二実施例に基づいて以下に説明をする。
前記プロテクタ内径と前記主体金具の先端部の外径とで形成される間隙の面積は、主体金具300の先端部302に配設されている通気孔305の面積の合計よりも小さくなるように設定されている。即ち、通気孔が4個設けられている場合には、通気孔305の直径をφDとすると(φd −φd )>4×φDの関係が成立するようにプロテクタ700の内径φdが決められている。その他の点については第一実施例と同一である。これによってイグナイタプラグ内部に残存するような異物が侵入することが少なくなり、冷却能力も十分に確保できる。
【0021】
即ち、該異物が飛散する燃焼チャンバー内部は始動時であってもかなりの流速で二次空気が流れており、プロテクタがない場合には、イグナイタプラグの主体金具の先端部に設けられた通気孔32に直接異物が侵入することがあるが、本プロテクタにより異物ははじき飛ばされてしまい、流れの速い二次空気によってはじき飛ばされた異物は燃焼チャンバー内の内壁に開けられた他の通気孔から燃焼室内部に入り排泄されてしまう。
また、図3の如く、前記プロテクタの代わりに前記絶縁体と前記主体金具の先端部の内周の内方への突き出し部とで形成する最小の間隙よりも網目幅又はスリット巾の小さい網目状又はスリット状のネットCであってもよい。これによって冷却能力が低下することなくイグナイタプラグ内部に残留するような異物が混入することもない。
【0022】
【発明の効果】
請求項1に記載の発明は、異物が通気孔内に侵入する機会が大幅に減少するため、イグナイタプラグの発火不良を大幅に減らすことができる。
【0023】
請求項2に記載の発明は、イグナイタプラグ内部を通過する冷却空気用二次空気の流量が低下することはないため、主体金具、絶縁体及び中心電極の冷却能力が落ちることもなく、イグナイタプラグの寿命に影響することがない。
【0024】
請求項3に記載の発明は、飛来してきたイグナイタプラグ内部に留まるような異物が直接通気孔内に侵入することがなく、また、侵入してきた場合にも外部に排泄されることから、異物の侵入によるイグナイタプラグの発火不良を起こすことがない。
【0025】
但し、冷却能力が若干低下することもあるが、本イグナイタプラグの使用状態を考慮すれば本質的な問題とはならない。即ち、本イグナイタプラグはガスタービンエンジンの始動時にのみ発火させるのみで足りる。従って、ガスタービンエンジンが定常運転状態においては通常発火させないため、自動車エンジン用スパークプラグのように高温時での発火による電極消耗が多大となることがなくイグナイタプラグの寿命が低下するような状態にはなりにくい。またエンジンの定常運転状態において燃焼ガスが主体金具、絶縁体等を溶融するほどの高温にはならないためイグナイタプラグ自体が溶融し、発火不良とはなり難い。
【0026】
請求項4に記載の発明は、イグナイタプラグの寿命に影響せずに、イグナイタプラグの発火不良を防止できる。
【図面の簡単な説明】
【図1】本発明に係るガスタービン用イグナイタプラグの一実施例の要部断面図を示す。
【図2】本発明に係るガスタービン用イグナイタプラグの要部断面拡大図を示す。
【図3】本発明に係るガスタービン用イグナイタプラグの他の実施例を示す。
【図4】従来のガスタービン用イグナイタプラグを示す。
【図5】従来のガスタービン用イグナイタプラグを燃焼チャンバーに装着した状態を示す断面図である。
【符号の説明】
100 イグナイタプラグ
300 主体金具
305 通気孔
500 中心電極
600 絶縁体
700 プロテクタ
B 最小の間隙
[0001]
TECHNICAL FIELD OF THE INVENTION
The present invention relates to an igniter plug mainly used for a gas turbine of a ground generator.
[0002]
[Prior art]
Conventionally, an igniter plug 1 used for a gas turbine engine is provided with a metal shell 3 having a distal end portion 2 having a small diameter in order to reduce a projecting area into the engine as shown in FIG. An insulator 6 having a central electrode 5 protruding and fitted into the shaft hole 4 is fitted into the metal shell 3, and the front end surface of the insulator 6 is slightly retracted from the front end surface 31 of the metal shell 3, and semi-creeping discharge The surface 61 is formed. At substantially the center of the metal shell 3, a mounting screw portion 34 for mounting on the gas turbine engine is formed. A hexagonal bolt-shaped hexagonal portion 35 is provided on the rear end side of the mounting screw portion 34, and a large diameter portion 33 having a larger diameter than the distal end portion 2 is provided between the mounting screw portion 34 and the distal end portion 2. I have. A cooling vent 32 is formed on the rear end side of the distal end portion 2 of the metal shell 3.
[0003]
Then, as shown in FIGS. 4 and 5, the igniter plug 1 is mounted in the combustion chamber 91 of the gas turbine engine 9.
The combustion chamber 91 is provided with an outer wall 912 and an inner wall 911, and secondary air 93 is supplied between the outer wall 912 and the inner wall 911 to supply air necessary for cooling and combustion.
In addition, a plurality of ventilation holes 9111 are formed at various places in the inner wall 911 to promote combustion and cool the inner wall material. The igniter plug 1 is located near the top of the side surface of the inner wall 911. The metal shell 3, the insulator 6, and the center electrode 5 of the igniter plug 1 are cooled by the secondary air 93, thereby increasing electrode consumption and oxidizing corrosion. It has the function of suppressing the increase.
On the other hand, since the secondary air 93 passes through the discharge gap 63 through the ventilation hole 32 provided in the igniter plug, the electric spark generated between the electrodes moves toward the inside of the combustion chamber 91 due to the inflow of the secondary air 93. It also contributes to improving the ignitability of the fuel.
[0004]
A fuel injection nozzle 95 is provided at the top of the inner wall 911, and the fuel injection nozzle 95 injects atomized fuel 951. The ignition of the fuel is performed by igniting a high-energy electric spark 2 to 5 times per second from an ignition power supply having a maximum energy of 20 kV and 1-2 joules in the igniter plug 1 when the gas turbine engine is started. I have. At the time of this ignition, secondary air 93 having a wind speed of 2 to 3 m / s is sent into the vent 32 of the plug. Then, a turbine (not shown) is driven by the high compression combustion gas generated by the ignition.
[0005]
[Problems to be solved by the invention]
In the igniter plug composed of such components, there is a case where electric spark does not occur between the electrodes of the igniter plug and the engine does not start. It was found that the reason why the electric spark did not occur was that foreign matter was mixed in the igniter plug, which was the cause. That is, as a result of the component analysis, such foreign matter is mainly composed of a metal component that is not included in each component constituting the igniter plug, and the foreign matter leaks electric energy sent from the ignition power supply and causes the igniter plug to leak. Of the discharge gap 63 is prevented from being generated. The ignition failure due to such foreign matter has a great effect on various facilities, such as an emergency generator, in which a momentary power outage is not allowed.
[0006]
An object of the present invention is to provide an igniter plug that can easily and inexpensively prevent foreign substances existing in secondary air from entering the inside of the igniter plug.
[0007]
A metallic shell having a cylindrical shape having a protruding portion inward of the distal end portion and provided with a ventilation hole communicating the inside and outside on the side surface,
An insulator with a shaft hole fitted in the metal shell,
A central electrode protruding from the distal end of the shaft hole of the insulator so as to face the inwardly protruding portion of the inner periphery of the distal end of the metallic shell, and
The gist is that a cylindrical protector that covers the ventilation hole is provided with a gap from the tip .
[0008]
The gist of the invention described in claim 2 is that the area formed by the inner diameter of the protector and the outer diameter of the distal end of the metal shell is greater than or equal to the area of the ventilation hole.
[0009]
According to a third aspect of the present invention, in the first aspect of the present invention, a gap formed by the inner diameter of the protector and the outer diameter of the distal end of the metal shell is formed by the inner circumference of the insulator and the distal end of the metal shell. It is characterized in that it is smaller than the minimum gap formed by the inwardly protruding portion.
[0010]
The invention according to claim 4 is a metal shell having a cylindrical shape provided with an inwardly projecting portion on the inner periphery of the distal end portion, and a vent hole communicating with the inside and outside on a side surface of the distal end portion,
An insulator with a shaft hole fitted in the metal shell,
A central electrode protruding from the distal end of the shaft hole of the insulator so as to face the inwardly protruding portion of the inner periphery of the distal end of the metallic shell, and
The gist is that a net in the form of a net or a slit is provided in the vent hole.
[0011]
According to the first aspect of the present invention, the chance that foreign matter that has flown due to the provision of the protector directly enters the ventilation hole is greatly reduced.
[0012]
According to the second aspect of the present invention, since the area formed by the inner diameter of the protector and the outer diameter of the distal end of the metallic shell is larger than the area of the ventilation hole, the flow rate of the secondary air for cooling air passing through the inside of the igniter plug The decrease is slight.
[0013]
According to the third aspect of the present invention, the gap formed by the inner diameter of the protector and the outer diameter of the distal end of the metal shell is smaller than the minimum gap formed by the insulator and the internal diameter of the metal shell. The foreign matter that remains inside the igniter plug does not directly enter the vent hole, and even when it enters, the protrusion protrudes inward from the inner circumference of the distal end of the insulator and the metal shell. Excreted through the minimum gap formed by
[0014]
According to the fourth aspect of the present invention, the cooling performance of the metal shell, the insulator, and the center electrode does not decrease, the life of the igniter plug is not affected, and the foreign matter that has entered directly enters the ventilation hole. Nothing.
In particular, if the mesh size and the slit interval are set to be equal to or less than the minimum gap formed by the insulator and the inwardly protruding portion of the inner periphery of the tip of the metal shell, foreign matter that is caught in the gap will be igniter plug. Do not enter inside. Further, since the foreign matter that has entered is minute, it is excreted without being caught in the minimum gap formed by the insulator and the inwardly projecting portion of the inner periphery of the distal end of the metal shell.
[0015]
BEST MODE FOR CARRYING OUT THE INVENTION
(First Embodiment) FIG. 1 is a sectional view showing a main part of an igniter plug according to a first embodiment of the present invention.
The igniter plug 100 according to the first embodiment of the present invention includes a cylindrical metal shell 300, an insulator 600, a center electrode 500, and the like, and is mounted on a combustion chamber (not shown) of a gas turbine engine.
The metal shell 300 is formed of a heat-resistant metal made of stainless steel, and a front end 302 formed at the front end of the metal shell 300 has a smaller diameter than the middle section 301 via a tapered surface, and a hexagonal section at the rear end. 303 are formed. A screw portion 304 is provided between the middle portion 301 and the hexagonal portion 303, and the screw portion 304 is screwed to the outer wall mounting portion of the combustion chamber.
[0016]
The inner periphery of the distal end of the distal end portion 302 of the metal shell 300 is bent at substantially a right angle and protrudes as an inward protruding surface 3021. Between the protruding surface 3021 and the tip 501 of the center electrode 500, a creeping discharge gap 602 for discharging along the tip 601 of the insulator 600, a circumferential side of the tip 601 of the insulator 600, and the metal shell 300 A semi-creeping discharge gap 604 having an aerial discharge gap 502 between the protruding surface 3021 and the protrusion surface 3021 is formed.
[0017]
Cooling vents 305 are formed at four equally spaced locations on the rear end side surface of the distal end portion 302 of the metallic shell 300. Further, a cylindrical protector 700 having the same outer diameter as the middle section 301 is welded and joined so as to cover the ventilation hole with a slight gap. The gap is set to be equal to or smaller than the minimum gap between the inwardly protruding surface of the metal shell to be described later and the distal end surface of the insulator leg long portion. That inner diameter .phi.d 2 of the protector 700 so that the relation is established in 2B> 2 1) as shown in FIG. 2 are determined.
[0018]
The insulator 600 is made of a sintered body of alumina, has a shaft hole 400 formed at the center, and the center electrode 500 is fitted therein. The front end is a small leg portion 603 and the rear end is a corrugation 604. The distal end surface 601 of the leg portion 603 of the insulator 600 is slightly retracted from the distal end surface 3022 of the metal shell 300 and is provided as a creeping discharge surface. The rear end of the leg portion 603 has a tapered surface and is in contact with the metal shell 300 with a plate packing interposed therebetween. The gap between the outer periphery of the leg portion 603 of the insulator 600 and the inner periphery of the metal shell 300 is formed so as to be wider toward the tip, and the gap between the outer periphery of the tip of the tip 302 of the metal shell 300 and the inner periphery is formed inward. The gap is smallest between the surface protruding as the protruding surface 3021 and the vicinity of the distal end surface of the leg portion 603 of the insulator 600.
[0019]
The center electrode 500 is formed of a nickel alloy, and has a front end portion 501 protruding from the front end surface 3022 of the metal shell 300 and fitted. The rear end is a terminal section 800 connected to a high-voltage power supply.
[0020]
(Second Embodiment) Next, a description will be given below based on a second embodiment.
The area of the gap formed by the inner diameter of the protector and the outer diameter of the distal end of the metallic shell is set to be smaller than the total area of the ventilation holes 305 provided at the distal end 302 of the metallic shell 300. Have been. That is, when the vent hole is provided four, the inside diameter of the protector 700 such When [phi] D the diameter of the vent holes 305 (φd 2 2 -φd 1 2 )> 4 × φD 2 relationship is established .phi.d Two have been determined. The other points are the same as in the first embodiment. This reduces the intrusion of foreign matter remaining inside the igniter plug, and ensures a sufficient cooling capacity.
[0021]
That is, secondary air is flowing at a considerable flow rate even in the combustion chamber where the foreign matter is scattered even at the time of start-up. If there is no protector, a ventilation hole provided at the tip of the metal shell of the igniter plug Although foreign matter may directly enter the protector 32, the foreign matter is repelled by the protector, and the foreign matter repelled by the fast-flowing secondary air passes through another vent hole opened in the inner wall of the combustion chamber. It goes inside and is excreted.
Further, as shown in FIG. 3, a mesh having a mesh width or a slit width smaller than a minimum gap formed by the insulator and the inwardly projecting portion of the inner periphery of the tip of the metal shell in place of the protector. Alternatively, a slit-shaped net C may be used. As a result, there is no foreign substance remaining inside the igniter plug without lowering the cooling capacity.
[0022]
【The invention's effect】
According to the first aspect of the present invention, the chance of foreign matter entering the ventilation hole is greatly reduced, and thus the ignition failure of the igniter plug can be significantly reduced.
[0023]
According to the second aspect of the invention, since the flow rate of the secondary air for cooling air passing through the inside of the igniter plug does not decrease, the cooling capacity of the metal shell, the insulator, and the center electrode does not decrease, and the igniter plug does not fall. Does not affect the life of the device.
[0024]
According to the third aspect of the present invention, the foreign matter which stays inside the igniter plug does not directly enter the ventilation hole, and is excreted even when it enters, so that the foreign matter is prevented. It does not cause ignition failure of the igniter plug due to intrusion.
[0025]
However, although the cooling capacity may be slightly reduced, it does not become an essential problem in consideration of the usage state of the present igniter plug. That is, the igniter plug need only ignite only when the gas turbine engine is started. Accordingly, since the gas turbine engine is not normally ignited in a steady operation state, the exhaustion of the electrodes due to ignition at high temperature does not become large and the life of the igniter plug is shortened like a spark plug for an automobile engine. It is hard to become. Further, in a steady operation state of the engine, the igniter plug itself melts because the combustion gas does not reach a temperature high enough to melt the metal shell, the insulator, and the like, and ignition failure is unlikely to occur.
[0026]
The invention described in claim 4 can prevent ignition failure of the igniter plug without affecting the life of the igniter plug.
[Brief description of the drawings]
FIG. 1 is a sectional view showing a main part of an embodiment of an igniter plug for a gas turbine according to the present invention.
FIG. 2 is an enlarged cross-sectional view of a main part of an igniter plug for a gas turbine according to the present invention.
FIG. 3 shows another embodiment of the igniter plug for a gas turbine according to the present invention.
FIG. 4 shows a conventional igniter plug for a gas turbine.
FIG. 5 is a sectional view showing a state in which a conventional igniter plug for a gas turbine is mounted on a combustion chamber.
[Explanation of symbols]
Reference Signs List 100 igniter plug 300 metal shell 305 vent hole 500 center electrode 600 insulator 700 protector B Minimum gap

Claims (3)

先端部の内方への突き出し部を有し、側面に内外を連通する通気孔が設けられた筒状を呈する主体金具と、
前記主体金具にはめ込まれた軸孔の付けられた絶縁体と、
前記主体金具の先端部の内周の内方への突き出し部と対向するように前記絶縁体の軸孔の先端より突き出して嵌挿された中心電極とからなり、
前記先端部から間隙を空けて、前記通気孔を覆う円筒状のプロテクタを配設したことを特徴とする請求項1のイグナイタプラグ。
A metallic shell having a cylindrical shape having a protruding portion inward of the distal end portion and provided with a ventilation hole communicating the inside and outside on the side surface,
An insulator with a shaft hole fitted in the metal shell,
A central electrode protruding from the distal end of the shaft hole of the insulator so as to face the inwardly protruding portion of the inner periphery of the distal end of the metallic shell, and
2. The igniter plug according to claim 1, wherein a cylindrical protector that covers the air hole is provided with a gap from the tip .
前記プロテクタの内径と前記主体金具の先端部の外径とで形成する面積が、前記通気孔の面積以上であることを特徴とする請求項1のイグナイタプラグ。2. The igniter plug according to claim 1, wherein an area formed by an inner diameter of the protector and an outer diameter of a distal end portion of the metal shell is equal to or larger than an area of the vent hole. 3. 前記プロテクタの内径と前記主体金具の先端部の外径とで形成する間隙が、前記絶縁体と前記主体金具の先端部の内周の内方への突き出し部とで形成する最小の間隙以下であることを特徴とする請求項1のイグナイタプラグ。The gap formed by the inner diameter of the protector and the outer diameter of the tip of the metal shell is less than or equal to the minimum gap formed by the insulator and the inwardly projecting portion of the inner circumference of the metal shell tip. The igniter plug according to claim 1, wherein:
JP24838095A 1995-09-01 1995-09-01 Igniter plug Expired - Fee Related JP3569769B2 (en)

Priority Applications (1)

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JP24838095A JP3569769B2 (en) 1995-09-01 1995-09-01 Igniter plug

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Application Number Priority Date Filing Date Title
JP24838095A JP3569769B2 (en) 1995-09-01 1995-09-01 Igniter plug

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JP3569769B2 true JP3569769B2 (en) 2004-09-29

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009097267A3 (en) * 2008-01-28 2009-10-15 Honeywell International Inc. High thread ground shield

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009097267A3 (en) * 2008-01-28 2009-10-15 Honeywell International Inc. High thread ground shield
US7977857B2 (en) 2008-01-28 2011-07-12 Honeywell International Inc. High thread ground shield
US8216015B2 (en) 2008-01-28 2012-07-10 Fram Group Ip Llc High thread ground shield

Also Published As

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