JPS63123701U - - Google Patents

Info

Publication number
JPS63123701U
JPS63123701U JP1593987U JP1593987U JPS63123701U JP S63123701 U JPS63123701 U JP S63123701U JP 1593987 U JP1593987 U JP 1593987U JP 1593987 U JP1593987 U JP 1593987U JP S63123701 U JPS63123701 U JP S63123701U
Authority
JP
Japan
Prior art keywords
sword
point shape
blade
stator blade
abradable material
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
JP1593987U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP1593987U priority Critical patent/JPS63123701U/ja
Publication of JPS63123701U publication Critical patent/JPS63123701U/ja
Pending legal-status Critical Current

Links

Description

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

第1図は、本考案に係わる一実施例を示すター
ビン段落の概略縦断面図である。第2図は、従来
の代表的なタービン段落を示す概略縦断面図であ
る。 10……静翼、11……静翼翼根、12……ア
ブレーダブル材(フエルトメタル等)、20……
動翼、30……次段静翼、31……次段の静翼翼
根、32……アブレーダブル材、40……チツプ
シユラウド、41……入口側の剣先、42……出
口側の剣先、50……ラジアルフイン、60……
翼環。
FIG. 1 is a schematic vertical sectional view of a turbine stage showing one embodiment of the present invention. FIG. 2 is a schematic longitudinal sectional view showing a typical conventional turbine stage. 10...Stator blade, 11...Stator blade root, 12...Abradable material (felt metal, etc.), 20...
Moving blade, 30...Next-stage stator blade, 31...Next-stage stator blade root, 32...Abradable material, 40...Chipushiroud, 41...Inlet side tip, 42...Exit side tip, 50...Radial Finn, 60...
wing ring.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 蒸気タービン又はガスタービンの動翼シユラウ
ドの入口側と出口側の少なくとも片側を剣先形状
とし、かつ該剣先形状部と対向する静翼翼根端面
にアブレーダブル材料を装着したことを特徴とす
る翼シール構造。
A blade seal structure characterized in that at least one side of the inlet side and the outlet side of a rotor blade shroud of a steam turbine or a gas turbine has a sword-point shape, and an abradable material is attached to the root end surface of a stator blade facing the sword-point shape.
JP1593987U 1987-02-05 1987-02-05 Pending JPS63123701U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1593987U JPS63123701U (en) 1987-02-05 1987-02-05

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1593987U JPS63123701U (en) 1987-02-05 1987-02-05

Publications (1)

Publication Number Publication Date
JPS63123701U true JPS63123701U (en) 1988-08-11

Family

ID=30807338

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1593987U Pending JPS63123701U (en) 1987-02-05 1987-02-05

Country Status (1)

Country Link
JP (1) JPS63123701U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD808680S1 (en) 2014-12-03 2018-01-30 Munchkin, Inc. Cassette

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD808680S1 (en) 2014-12-03 2018-01-30 Munchkin, Inc. Cassette

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