JPH0459301U - - Google Patents

Info

Publication number
JPH0459301U
JPH0459301U JP10107290U JP10107290U JPH0459301U JP H0459301 U JPH0459301 U JP H0459301U JP 10107290 U JP10107290 U JP 10107290U JP 10107290 U JP10107290 U JP 10107290U JP H0459301 U JPH0459301 U JP H0459301U
Authority
JP
Japan
Prior art keywords
view
gas turbine
side plate
gap
close
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
JP10107290U
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 JP10107290U priority Critical patent/JPH0459301U/ja
Publication of JPH0459301U publication Critical patent/JPH0459301U/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によるガスタービン
を示す断面図、第２図は第１図に示す動翼を拡大
して示す断面図、第３図は第１図の−線に沿
う拡大矢視図、第４図はデイスクの斜視図、第５
図はガスタービンの一般的構成例を示す系統図、
第６図は従来例を示す断面図、第７図は第５図に
示す動翼を拡大して示す断面図である。 ２……燃焼器、３……タービン、５……静翼、
６……動翼、６ａ……翼根、７……シヤンク部、
８……デイスク、８ａ……翼溝、９……燃焼ガス
、１０……冷却空気、１４……サイド板、１５…
…スリツト、１６……Ｌ形板、１７……立上り部
。 Fig. 1 is a sectional view showing a gas turbine according to an embodiment of the present invention, Fig. 2 is an enlarged sectional view of the rotor blade shown in Fig. 1, and Fig. 3 is an enlarged view taken along the - line in Fig. 1. Fig. 4 is a perspective view of the disk, Fig. 5 is a perspective view of the disk.
The figure is a system diagram showing a general configuration example of a gas turbine.
FIG. 6 is a sectional view showing a conventional example, and FIG. 7 is an enlarged sectional view showing the rotor blade shown in FIG. 5. 2...Combustor, 3...Turbine, 5...Stator blade,
6... Moving blade, 6a... Blade root, 7... Shank part,
8...Disc, 8a...Blade groove, 9...Combustion gas, 10...Cooling air, 14...Side plate, 15...
...Slit, 16...L-shaped plate, 17...Rising portion.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 隣接する動翼のシヤンク部間の隙間に、該隙間
を塞ぐ形状のサイド板を、デイスク部に一体的に
設けたことを特徴とするガスタービン。 A gas turbine characterized in that a side plate shaped to close a gap between shank portions of adjacent rotor blades is integrally provided on a disk portion.
JP10107290U 1990-09-28 1990-09-28 Pending JPH0459301U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10107290U JPH0459301U (en) 1990-09-28 1990-09-28

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10107290U JPH0459301U (en) 1990-09-28 1990-09-28

Publications (1)

Publication Number Publication Date
JPH0459301U true JPH0459301U (en) 1992-05-21

Family

ID=31844220

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10107290U Pending JPH0459301U (en) 1990-09-28 1990-09-28

Country Status (1)

Country Link
JP (1) JPH0459301U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013234588A (en) * 2012-05-08 2013-11-21 Mitsubishi Heavy Ind Ltd Turbine rotor, gas turbine, and method for assembling seal assembly in the turbine rotor
JP2013545926A (en) * 2010-12-09 2013-12-26 アルストム テクノロジー リミテッド Fluid flow devices, in particular gas turbines penetrated axially by hot gas flow

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013545926A (en) * 2010-12-09 2013-12-26 アルストム テクノロジー リミテッド Fluid flow devices, in particular gas turbines penetrated axially by hot gas flow
JP2013234588A (en) * 2012-05-08 2013-11-21 Mitsubishi Heavy Ind Ltd Turbine rotor, gas turbine, and method for assembling seal assembly in the turbine rotor

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