JPS6319003U - - Google Patents

Info

Publication number
JPS6319003U
JPS6319003U JP11206086U JP11206086U JPS6319003U JP S6319003 U JPS6319003 U JP S6319003U JP 11206086 U JP11206086 U JP 11206086U JP 11206086 U JP11206086 U JP 11206086U JP S6319003 U JPS6319003 U JP S6319003U
Authority
JP
Japan
Prior art keywords
seal
stator vane
groove
gas turbine
gas
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
JP11206086U
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 JP11206086U priority Critical patent/JPS6319003U/ja
Publication of JPS6319003U publication Critical patent/JPS6319003U/ja
Pending legal-status Critical Current

Links

Description

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

第1図は本考案の一実施例の静翼セグメントの
正面図、第2図は静翼セグメントの平面図、第3
図は第2図の矢視図、第4図はセグメント間に
シールプレートを装着した図、第5図はシールプ
レートの斜視図、第6図は従来構造のエンドウオ
ール端部とシール溝を示す図である。 1……静翼セグメント。
FIG. 1 is a front view of a stator vane segment according to an embodiment of the present invention, FIG. 2 is a plan view of a stator vane segment, and FIG.
The figure is a view taken in the direction of the arrow in Fig. 2, Fig. 4 is a view with the seal plate installed between the segments, Fig. 5 is a perspective view of the seal plate, and Fig. 6 shows the end wall end and seal groove of the conventional structure. It is a diagram. 1... Stationary wing segment.

Claims (1)

【実用新案登録請求の範囲】 セグメントに分割された静翼からなるガスター
ビンの静翼において、 隣接するエンドウオール端面のガス側の辺と並
行となるよう円弧状のシール溝を形成し、前記シ
ール溝に可撓性のシールプレートを挿入したこと
を特徴とするガスタービン静翼のセグメント間シ
ール。
[Claims for Utility Model Registration] In a stator vane of a gas turbine consisting of a stator vane divided into segments, an arcuate seal groove is formed parallel to the gas side side of the end face of an adjacent end wall, and the seal An intersegment seal for a gas turbine stationary blade, characterized by a flexible seal plate inserted into a groove.
JP11206086U 1986-07-23 1986-07-23 Pending JPS6319003U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11206086U JPS6319003U (en) 1986-07-23 1986-07-23

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11206086U JPS6319003U (en) 1986-07-23 1986-07-23

Publications (1)

Publication Number Publication Date
JPS6319003U true JPS6319003U (en) 1988-02-08

Family

ID=30992575

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11206086U Pending JPS6319003U (en) 1986-07-23 1986-07-23

Country Status (1)

Country Link
JP (1) JPS6319003U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH11148303A (en) * 1997-09-15 1999-06-02 Asea Brown Boveri Ag Segment unit for platform

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH11148303A (en) * 1997-09-15 1999-06-02 Asea Brown Boveri Ag Segment unit for platform

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