JPS5940481A - Ignitor plug - Google Patents

Ignitor plug

Info

Publication number
JPS5940481A
JPS5940481A JP15112482A JP15112482A JPS5940481A JP S5940481 A JPS5940481 A JP S5940481A JP 15112482 A JP15112482 A JP 15112482A JP 15112482 A JP15112482 A JP 15112482A JP S5940481 A JPS5940481 A JP S5940481A
Authority
JP
Japan
Prior art keywords
annular space
porcelain insulator
mounting bracket
center electrode
metal sleeve
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.)
Granted
Application number
JP15112482A
Other languages
Japanese (ja)
Other versions
JPS6123632B2 (en
Inventor
栗本 圭司
五十嵐 一博
松村 修造
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.)
Nippon Tokushu Togyo KK
Niterra Co Ltd
Original Assignee
NGK Spark Plug Co Ltd
Nippon Tokushu Togyo KK
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 NGK Spark Plug Co Ltd, Nippon Tokushu Togyo KK filed Critical NGK Spark Plug Co Ltd
Priority to JP15112482A priority Critical patent/JPS5940481A/en
Publication of JPS5940481A publication Critical patent/JPS5940481A/en
Publication of JPS6123632B2 publication Critical patent/JPS6123632B2/ja
Granted legal-status Critical Current

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  • Ignition Installations For Internal Combustion Engines (AREA)
  • Spark Plugs (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 本発明は航空機用等のガスタービンエンジンに用いるイ
グナイタプラグに関するもので、その目的とするところ
はプラグ内部に空気を導入して磁器絶縁体および消耗の
はげしい中心電極チップを冷却することにより、そのオ
ーバーヒートを防止して耐消耗性を向上しようとするも
のである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an igniter plug used in gas turbine engines for aircraft, etc., and its purpose is to introduce air into the plug to remove the porcelain insulator and the rapidly wearable center electrode tip. By cooling, overheating is prevented and wear resistance is improved.

従来この種の空気導入方式を採用するイグナイタプラグ
としては第1図に示すUSP 3,330,911号公
報に記載されたものが知られている。このイグナイタプ
ラグは、磁器絶縁体が別体の上部lと下部λの三部分に
分割されて取付金具tの内腔で軸方向に同君的に一部重
合して配設され、前記上部絶縁体lと取付金具弘の内壁
面との間には長手方向に沿って第一外側環状スペースj
を形成してここに上部導入口≠aを開口させる。
Conventionally, as an igniter plug employing this type of air introduction method, the one described in USP No. 3,330,911 shown in FIG. 1 is known. In this igniter plug, the porcelain insulator is divided into three parts, an upper part L and a lower part λ, which are disposed in the inner cavity of the mounting bracket T so as to be partially overlapped in the axial direction, and the above-mentioned upper insulator There is a first outer annular space j along the longitudinal direction between the body l and the inner wall surface of the mounting bracket.
is formed, and an upper inlet port ≠a is opened there.

下部絶縁体λは取付金具内腔の段部/−2に気密パツキ
ン/3を介して固定されるので、前記上部導入口<za
からの空気流はここで下向き流通が遮断され、そのため
上部磁器絶縁体/の下端l≠を経て上下両磁器絶縁体が
互いに重合して形成する中間の環状スペースを内を上昇
し、さらに空気流は下部磁器絶縁体コの頂部/J−から
反転して中心電極3と下部磁器絶縁体コの間の内側環状
スペース7を下方に向い、中心電極3の先端の点火チッ
プ3aの外周と下部磁器絶縁体コの内端面、2aが形成
する開ロアaから火花ギャップlの空間に向って流出す
る。一方、取付金具下部には別の下部導入口+bを設け
、取付金具≠内壁面と下部磁器絶縁体コの間の第二外側
環状スペースタに開口させ、該環状スペースタを経て取
付金具先端に形成した外側電極IOの周辺の開口部ll
に通ずる空気流通路を形成させる。第一環状スペースj
と第二外側環状スペースタとは前記のごとく気密パツキ
ン/3によって相互の空気流通は遮断されている。
Since the lower insulator λ is fixed to the step part /-2 of the mounting bracket inner cavity via the airtight packing /3, the upper inlet port < za
The downward flow of the airflow from the porcelain insulator is interrupted here, and therefore the airflow passes through the upper porcelain insulator/lower end l≠ and ascends through the intermediate annular space formed by the upper and lower porcelain insulators overlapping each other, and further airflow continues. is inverted from the top /J- of the lower porcelain insulator and faces downward into the inner annular space 7 between the center electrode 3 and the lower porcelain insulator, and connects the outer periphery of the ignition tip 3a at the tip of the center electrode 3 and the lower porcelain insulator. It flows out toward the space of the spark gap l from the open lower a formed by the inner end surface 2a of the insulator. On the other hand, another lower inlet +b is provided at the bottom of the mounting bracket, which opens into the second outer annular spacer between the mounting bracket ≠ inner wall surface and the lower porcelain insulator, and passes through the annular spacer to the tip of the mounting bracket. Opening ll around the formed outer electrode IO
form an air flow path leading to the first circular space j
As described above, air circulation between the spacer and the second outer annular spacer is blocked by the airtight packing /3.

従って空気導入口は互いに独立した上下のλ箇所に設け
ることが不可欠であった。このため取付金具の先端がガ
スタービンの燃焼室内に深く突出する場合には二次空気
室に配設される下部導入口の位置は上部側に設ける必要
からイグナイタプラグの全長が著しく長大となってさら
にエンジン側の二次空気室を拡げなければならず不経済
となる欠点があった。また下部磁器絶縁体−の径方向に
第二外側環状スペースタから内側環状スペース7に通ず
る貫孔を設けることも部応力の不均一によりクラックが
入シ易く且つ焼成歪が生じ実用的でないことがわかった
Therefore, it was essential to provide the air inlets at mutually independent upper and lower λ locations. For this reason, if the tip of the mounting bracket protrudes deeply into the combustion chamber of the gas turbine, the lower inlet installed in the secondary air chamber must be located on the upper side, making the overall length of the igniter plug significantly longer. Furthermore, the secondary air chamber on the engine side had to be expanded, which was uneconomical. Furthermore, providing a through hole in the radial direction of the lower porcelain insulator from the second outer annular spacer to the inner annular space 7 is not practical because cracks are likely to occur due to uneven stress and firing distortion occurs. Understood.

本発明はこのような不具合を解決するための提案であっ
て、取付金具の空気導入口をガスタービンエンジンの二
次空気室内に挿着される部分に一箇所設け、かつ取付金
具内腔の段部に下部絶縁体コを固定するにあたり、気密
パツキンの代シに外周壁の軸方向に複数の切割溝を並設
した中空の金属スリーブを用いて固定し、上下の環状ス
ペース!、り間の流通を遮断することなく、前記一箇所
の導入口よシ取り入れた空気を前記第二外側環状スペー
スと第一外側環状スペースj→中間環状スペースt→内
側環状スペース7の二つの系統に分配することにより達
成するものである。
The present invention is a proposal to solve such problems, and the present invention is to provide the air inlet of the mounting bracket at one place in the part inserted into the secondary air chamber of the gas turbine engine, and to install the air inlet of the mounting bracket at one place in the part inserted into the secondary air chamber of the gas turbine engine. To fix the lower insulator to the upper and lower annular spaces, a hollow metal sleeve with multiple cut grooves arranged in parallel in the axial direction of the outer peripheral wall is used instead of the airtight packing. , the air taken in through the one inlet is divided into two systems: the second outer annular space and the first outer annular space j→intermediate annular space t→inner annular space 7, without interrupting the flow between the two. This is achieved by distributing it to

以下本発明を図面の実施例について詳説する。The present invention will be explained in detail below with reference to embodiments shown in the drawings.

第2図は本発明のイグナイタプラグの要部縦断面図であ
って、同一構造部分に対しては従来例と同一符号を与え
て説明する。第V図は本発明のイグナイタプラグに使用
する金属スリーブを装着した状態の要部縦断正面図で、
第V図は金属スリーブの一部切截正面図、第5図は平面
図である。第を図は別の実施例を示す縦断面図である。
FIG. 2 is a longitudinal cross-sectional view of the main parts of the igniter plug of the present invention, and the same structural parts are given the same reference numerals as in the conventional example and will be explained. FIG.
FIG. V is a partially cutaway front view of the metal sleeve, and FIG. 5 is a plan view. Figure 5 is a longitudinal sectional view showing another embodiment.

第3図で示すように、取付金具≠の内径の大きい部分と
外側電極をふくむ小さい部分とは段部/、2によって区
切られ、第V図に示すような中空の金属スリーブ/6は
該段部/、2で取付金具≠の内腔に固定される。
As shown in FIG. 3, the larger inner diameter portion of the mounting bracket ≠ and the smaller portion containing the outer electrode are separated by a step 2, and the hollow metal sleeve 6 as shown in FIG. It is fixed to the inner cavity of the mounting bracket≠ by the part/, 2.

金属スリーブ/6は中心電極3、下部磁器絶縁体コと同
君的にその外側に位置し、外周壁、23には軸芯に平行
に複数の切割溝/gが並設され、該切割溝/lと取付金
具内周面との間には軸芯方向の空気流路が形成され、第
一外側環状スペースよと第二外側環状スペースタとは相
互に連通ずる。金属スリーブ/&は管状本体/7と下部
磁器絶縁体2の外周面との間に滑石粉のようなシール材
lりを充填し、その上下端にパツキン、20..2/を
設けた後、前記管状本体17の先端、2.2を内方に加
締める。第二外側環状スペースタに開口する導入0.2
グを穿設する。
The metal sleeve /6 is located on the outer side of the center electrode 3 and the lower porcelain insulator, and the outer peripheral wall 23 has a plurality of cut grooves /g arranged in parallel with the axis. An axial air flow path is formed between /l and the inner circumferential surface of the mounting bracket, and the first outer annular space and the second outer annular spacer communicate with each other. The metal sleeve /& is filled with a sealing material such as talc powder between the tubular body /7 and the outer circumferential surface of the lower porcelain insulator 2, and has gaskets 20. .. 2/, the tip of the tubular body 17, 2.2, is crimped inward. Introduction 0.2 opening into the second outer annular spacer
drill a hole.

第6図に示す別の実施例では空気導入0.2jは金属ス
リーブよシ上方の第一外側環状スペースに開口する構成
であって、金属スリーブより下部には設けない。
In another embodiment shown in FIG. 6, the air inlet 0.2j opens into the first outer annular space above the metal sleeve, but is not provided below the metal sleeve.

本発明のイグナイタプラグは叙上の構成であって、第7
図に示すようなガスタービンエンジンに装着されたとき
イグナイタプラグの先端の  。
The igniter plug of the present invention has the above configuration, and has the seventh
of the tip of the igniter plug when installed in a gas turbine engine as shown in the figure.

点火部Aはコンプレサー、26と燃料ノズル、27を備
えた燃焼室2rに挿入され、導入0.24tまたは、2
tを有する取付金具グの部分は二次空気室λり内に位置
するので、第2図および第3図実施例の場合は導入口か
ら流入した二次空気は冷却空気として一部は第二外側環
状スペースタ内を下降して外側電極IOの周辺の開口部
/lから噴出して外側電極10および下部磁器絶縁体の
先端に対し冷却作用を及はし、他の一部は第二外側環状
スペースタ内を上昇して金属スリーブ/6の切割溝ll
rを通9、中間環状スペースtから下部磁器絶縁体20
頂部l!を経て内側環状スペース7に入り、中心電極3
に沿って下降して先端の点火チップ3aの外周と下部磁
器絶縁体コの内端面λaとが形成する開ロアaから火花
ギャップ♂に向って噴出し、同時に中心電極の先端点火
チップ3aと磁器絶縁体の先端部分を冷却する。また第
を図の実施例では空気導入口2jは金属スリーブの上方
の第一外側環状スペースjに開口するので、流入空気は
一部が金属スリーブ/&の切割溝/Iを経て第二外側環
状スペースタ内を下降し、外側電極IQの開口部iiか
ら噴出する。他の一部は中間環状スペースtを上昇し、
頂部l!で反転して内側環状スペース7内を下降し、点
火チップ3aの周υの開ロアaから火花ギャップtに向
って噴出する。噴出の際、冷却作用を呈することは同様
である。
The ignition part A is inserted into a combustion chamber 2r equipped with a compressor 26 and a fuel nozzle 27, and the ignition part A is inserted into a combustion chamber 2r equipped with a compressor 26 and a fuel nozzle 27.
Since the part of the mounting bracket having t is located within the secondary air chamber λ, in the embodiments shown in FIGS. It descends inside the outer annular spacer and ejects from the opening /l around the outer electrode IO, exerting a cooling effect on the outer electrode 10 and the tip of the lower ceramic insulator, and the other part is emitted from the second outer spacer. Rising inside the annular spacer and cutting groove ll of metal sleeve/6
r through 9 and from the intermediate annular space t to the lower porcelain insulator 20
Top l! enters the inner annular space 7 through the center electrode 3
, and ejects from the open lower a formed by the outer periphery of the tip ignition tip 3a and the inner end surface λa of the lower porcelain insulator toward the spark gap ♂, and at the same time the tip ignition tip 3a of the center electrode and the porcelain Cool the tip of the insulator. Further, in the embodiment shown in Fig. 1, the air inlet 2j opens into the first outer annular space j above the metal sleeve, so that a part of the incoming air passes through the cut groove /I of the metal sleeve /& and enters the second outer annular space. It descends inside the spacer and is ejected from the opening ii of the outer electrode IQ. The other part ascends the intermediate annular space t,
Top l! The spark ignition tip 3a reverses itself and moves downward in the inner annular space 7, and is ejected from the open lower a of the periphery υ of the ignition tip 3a toward the spark gap t. Similarly, it exhibits a cooling effect when ejected.

従来、高エネルギー用イグナイタプラグの中心電極には
火花耐久性をあげるため火花に対して強く耐消耗性のあ
るタングステンまたはタングステン合金を使用していた
が、耐熱性が乏しいためその受熱温度がSOO℃位から
表面に酸化スケールが形成され、さらにその高温での受
熱状態が続くとタングステンの表面に形成された酸化ス
ケールが層状に肥大し、剥離してしまう欠点があり、こ
のような現象を防ぐためには極。
Conventionally, tungsten or tungsten alloys, which are strong against sparks and wear-resistant, have been used for the center electrode of high-energy igniter plugs in order to increase spark durability, but because of their poor heat resistance, the heat receiving temperature is SOO℃. Oxide scale is formed on the surface of tungsten, and if the heat-receiving condition at high temperatures continues, the oxide scale formed on the surface of tungsten will enlarge into a layer and peel off.To prevent this phenomenon, is extreme.

力中心電極の受熱温度をいかにして下げるかにかかつて
いた。
The problem was how to lower the heat receiving temperature of the force center electrode.

本発明のイグナイタプラグでは、取付金具内腔の段部に
金属スリーブを固定してその上下の環状スペースを連通
させたので、空気導入口はその上部或いは下部のいずれ
か一箇所に開設すれば中心電極のまわりの内側環状スペ
ースは勿論外側環状スペースの両スペースを通して冷却
空気を流通させることができるもので、取付金具の長さ
を長大化させる不利がない。空気導入口の位1t’iの
接定を極めて容易にするものである。
In the igniter plug of the present invention, the metal sleeve is fixed to the stepped part of the inner cavity of the mounting bracket, and the upper and lower annular spaces are communicated with each other. Cooling air can be circulated through both the inner annular space around the electrode as well as the outer annular space, without the disadvantage of increasing the length of the mounting bracket. This makes it extremely easy to connect the air inlet.

中心電極の受熱温度を低下させることにより点火部のタ
ングステンの使用を安定し、耐熱性不足を掩睦する。従
って中心電極の酸化スケール形成の防止、中心電極の消
耗の緩和に役立ち並びに−冷却空気が発火部側に噴出す
ることにより火花の光芒を長くして燃焼ガスの着火性に
好影響を与える効果もある。
By lowering the heat receiving temperature of the center electrode, the use of tungsten in the ignition part is stabilized and the lack of heat resistance is alleviated. Therefore, it helps prevent the formation of oxide scale on the center electrode and alleviates the wear and tear of the center electrode, and also has the effect of elongating the beam of the spark by ejecting cooling air toward the ignition part, which has a positive effect on the ignitability of the combustion gas. be.

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

第1図は従来のイグナイタプラグの縦断面図、第2図は
本発明のイグナイタプラグの一部切截要部縦断面図、第
3図は同じく要部の縦断面図、第φ図は本発明イグナイ
タプラグに使用する金属スリーブの一部切截正面図、第
5図は一半の平面図、第6図は別の実施例の要部縦断面
図、第7図はガスタービンエンジンに取付けられたイグ
ナイタプラグの状態図である。
Fig. 1 is a longitudinal cross-sectional view of a conventional igniter plug, Fig. 2 is a partially cutaway longitudinal cross-sectional view of the main part of the igniter plug of the present invention, Fig. 3 is a longitudinal cross-sectional view of the main part, and Fig. A partially cutaway front view of a metal sleeve used in the igniter plug of the invention, FIG. 5 is a plan view of one half, FIG. 6 is a vertical cross-sectional view of a main part of another embodiment, and FIG. 7 is a metal sleeve installed in a gas turbine engine. FIG. 3 is a state diagram of the igniter plug.

Claims (1)

【特許請求の範囲】[Claims] 径大部と径小部を段部で接続連成した取付金具内腔に中
心電極と同君的に中空の磁器絶縁体を少なくとも上下に
分割装着してその内外両側面に沿って環状のスペースを
形成し、且つ中心電極の点火チップとの間に前記内側環
状スペースに通ずる環状の狭小な空気流路を形成して外
側電極で支持して成るイグナイタプラグにおいて、前記
径大部内に外側面の軸芯方向に沿って複数の切割溝を並
設した中空の金属スリーブを中心電極と同君的に装着し
て前記段部に固定しその内側に下部磁器絶縁体を結合す
るとともに前記金属スリーブの上方或いは下方の取付金
具周壁に前記外側環状スペースに通ずる空気導入口を開
設して成るイグナイタプラグ。
A hollow porcelain insulator is installed in the inner cavity of the mounting bracket, in which the large-diameter part and the small-diameter part are interconnected by a stepped part, and the hollow porcelain insulator is divided into at least the upper and lower parts in the same manner as the center electrode, and an annular space is formed along both the inner and outer sides of the hollow porcelain insulator. and a narrow annular air flow path communicating with the inner annular space between the ignition tip of the center electrode and the inner annular space and supported by the outer electrode. A hollow metal sleeve having a plurality of cut grooves arranged in parallel along the axial direction is attached to the center electrode and fixed to the stepped portion, and a lower porcelain insulator is bonded to the inside of the sleeve. An igniter plug comprising an air inlet that communicates with the outer annular space in the upper or lower peripheral wall of the mounting bracket.
JP15112482A 1982-08-30 1982-08-30 Ignitor plug Granted JPS5940481A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15112482A JPS5940481A (en) 1982-08-30 1982-08-30 Ignitor plug

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15112482A JPS5940481A (en) 1982-08-30 1982-08-30 Ignitor plug

Publications (2)

Publication Number Publication Date
JPS5940481A true JPS5940481A (en) 1984-03-06
JPS6123632B2 JPS6123632B2 (en) 1986-06-06

Family

ID=15511885

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15112482A Granted JPS5940481A (en) 1982-08-30 1982-08-30 Ignitor plug

Country Status (1)

Country Link
JP (1) JPS5940481A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61240964A (en) * 1985-04-18 1986-10-27 帝人株式会社 Body fluid treating device and its production
JPH0212189U (en) * 1988-07-06 1990-01-25
JP2006029324A (en) * 2004-07-20 2006-02-02 General Electric Co <Ge> Method and device for cooling ignitor in turbine engine combustor
JP2010541178A (en) * 2007-10-02 2010-12-24 フェデラル−モーグル コーポレイション Spark plug
US8796909B2 (en) 2011-07-06 2014-08-05 Ngk Spark Plug Co., Ltd. Igniter plug with cooling fluid and method of manufacturing igniter plug

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61240964A (en) * 1985-04-18 1986-10-27 帝人株式会社 Body fluid treating device and its production
JPH0212189U (en) * 1988-07-06 1990-01-25
JPH0633672Y2 (en) * 1988-07-06 1994-08-31 日本特殊陶業株式会社 Cryogenic liquid hydrogen / liquid oxygen fuel igniter plug
JP2006029324A (en) * 2004-07-20 2006-02-02 General Electric Co <Ge> Method and device for cooling ignitor in turbine engine combustor
JP2010541178A (en) * 2007-10-02 2010-12-24 フェデラル−モーグル コーポレイション Spark plug
US8796909B2 (en) 2011-07-06 2014-08-05 Ngk Spark Plug Co., Ltd. Igniter plug with cooling fluid and method of manufacturing igniter plug

Also Published As

Publication number Publication date
JPS6123632B2 (en) 1986-06-06

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