JPS60118306U - Sealing device for stationary blades in fluid machinery - Google Patents

Sealing device for stationary blades in fluid machinery

Info

Publication number
JPS60118306U
JPS60118306U JP520284U JP520284U JPS60118306U JP S60118306 U JPS60118306 U JP S60118306U JP 520284 U JP520284 U JP 520284U JP 520284 U JP520284 U JP 520284U JP S60118306 U JPS60118306 U JP S60118306U
Authority
JP
Japan
Prior art keywords
sealing device
stator vane
end wall
circumferential direction
seal plate
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
Application number
JP520284U
Other languages
Japanese (ja)
Inventor
雅美 野田
隆 池田
川池 和彦
Original Assignee
株式会社日立製作所
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 株式会社日立製作所 filed Critical 株式会社日立製作所
Priority to JP520284U priority Critical patent/JPS60118306U/en
Publication of JPS60118306U publication Critical patent/JPS60118306U/en
Pending legal-status Critical Current

Links

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

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

第1図は従来のシール装置を備えたガスタービンの静翼
部を示す断面図、第、2図は第1図における静翼セグメ
ントの斜視図、第3図は従来のシール装置を拡大して示
す断面図、第4図は本考案のシール装置における静翼セ
グメレトの内側エンドウオール部分のシール部を示す断
面図、第5図は第4図におけるシールプレートが弾性変
形した状態を示す断面図である。 1・・・外側エンドウオール、2・・・内側エンドウオ
ール、3・・・静翼、4・・・ケーシング、6・・・溝
、7・・・シールプレート
Fig. 1 is a sectional view showing a stator vane section of a gas turbine equipped with a conventional sealing device, Figs. 2 and 2 are perspective views of the stator vane segment in Fig. 1, and Fig. 3 is an enlarged view of the conventional sealing device. FIG. 4 is a cross-sectional view showing the sealing portion of the inner end wall portion of the stator vane segment in the sealing device of the present invention, and FIG. 5 is a cross-sectional view showing the seal plate in FIG. 4 in an elastically deformed state. be. 1...Outer end wall, 2...Inner end wall, 3...Stator blade, 4...Casing, 6...Groove, 7...Seal plate

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 円弧状の外側エンドウオール及び内側エンドウオールと
、両エンドウオール間に固設される複数の静翼とからな
る静翼セグメントを、ケーシング内の周方向に複数配設
して環状の静翼部を形成し、互に隣接する静翼セグメン
ト間には、冷却空気が作動流体側へ洩れるのを防止する
シール装置を備え、前記シール装置柱、互に隣合う外側
エンドウオールの周方向隣接面及び内側エンドウオール
の周方向隣接面にそれぞれ設けた溝と、その各溝内に挿
入したシールプレートとで構成している流体機械におい
て、前記溝を周方向にテーパ状に成形するとともに、前
記シールプレートとして、工の字状のシールプレートを
使用し、温度上昇に伴う前記静翼セグメントの周方向熱
膨張を拘束することなく前記シールプレートの弾性変形
により該シールプレートと溝内面とに接触部を形成させ
るようにしたことを特徴とする流体機械における静翼部
のシール装置。
A plurality of stator vane segments consisting of an arc-shaped outer end wall, an inner end wall, and a plurality of stator vanes fixedly installed between both end walls are arranged in the circumferential direction inside the casing to form an annular stator vane section. A sealing device for preventing cooling air from leaking to the working fluid side is provided between the stator vane segments adjacent to each other, and the sealing device column, the circumferentially adjacent surfaces of the mutually adjacent outer end walls, and the inner side thereof are provided. In a fluid machine comprising grooves provided on adjacent surfaces in the circumferential direction of an end wall, and seal plates inserted into each groove, the grooves are formed into a tapered shape in the circumferential direction, and the seal plates are , a square-shaped seal plate is used, and a contact portion is formed between the seal plate and the inner surface of the groove by elastic deformation of the seal plate without restricting the circumferential thermal expansion of the stationary vane segment due to temperature rise. A sealing device for a stator vane in a fluid machine, characterized in that:
JP520284U 1984-01-20 1984-01-20 Sealing device for stationary blades in fluid machinery Pending JPS60118306U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP520284U JPS60118306U (en) 1984-01-20 1984-01-20 Sealing device for stationary blades in fluid machinery

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP520284U JPS60118306U (en) 1984-01-20 1984-01-20 Sealing device for stationary blades in fluid machinery

Publications (1)

Publication Number Publication Date
JPS60118306U true JPS60118306U (en) 1985-08-10

Family

ID=30481487

Family Applications (1)

Application Number Title Priority Date Filing Date
JP520284U Pending JPS60118306U (en) 1984-01-20 1984-01-20 Sealing device for stationary blades in fluid machinery

Country Status (1)

Country Link
JP (1) JPS60118306U (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH08506640A (en) * 1993-02-05 1996-07-16 ユナイテッド テクノロジーズ コーポレイション Coolable outer air seal device for gas turbine engine
JPH10510022A (en) * 1994-12-07 1998-09-29 プラット アンド ホイットニー カナダ インコーポレイテッド Gas turbine engine feather seal
JP2001207998A (en) * 1999-12-07 2001-08-03 General Electric Co <Ge> Stator blade frame for gas turbine or jet engine
JP2004060657A (en) * 2002-07-29 2004-02-26 General Electric Co <Ge> End surface gap seal for interstage packing seal of steam turbine diaphragm and its assembling method
JP2004353675A (en) * 2003-05-29 2004-12-16 General Electric Co <Ge> Horizontal joint seal system for steam turbine diaphragm assembly
JP2005146896A (en) * 2003-11-11 2005-06-09 Toshiba Corp Nozzle diaphragm of steam turbine and steam turbine plant
JP2008002460A (en) * 2006-06-23 2008-01-10 Snecma Sector of compressor guide vanes assembly or sector of turbomachine nozzle assembly

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH08506640A (en) * 1993-02-05 1996-07-16 ユナイテッド テクノロジーズ コーポレイション Coolable outer air seal device for gas turbine engine
JPH10510022A (en) * 1994-12-07 1998-09-29 プラット アンド ホイットニー カナダ インコーポレイテッド Gas turbine engine feather seal
JP2001207998A (en) * 1999-12-07 2001-08-03 General Electric Co <Ge> Stator blade frame for gas turbine or jet engine
JP2004060657A (en) * 2002-07-29 2004-02-26 General Electric Co <Ge> End surface gap seal for interstage packing seal of steam turbine diaphragm and its assembling method
JP2004353675A (en) * 2003-05-29 2004-12-16 General Electric Co <Ge> Horizontal joint seal system for steam turbine diaphragm assembly
JP2005146896A (en) * 2003-11-11 2005-06-09 Toshiba Corp Nozzle diaphragm of steam turbine and steam turbine plant
JP2008002460A (en) * 2006-06-23 2008-01-10 Snecma Sector of compressor guide vanes assembly or sector of turbomachine nozzle assembly

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