JPS58120834U - Internal cooling structure of gas turbine engine - Google Patents
Internal cooling structure of gas turbine engineInfo
- Publication number
- JPS58120834U JPS58120834U JP1631282U JP1631282U JPS58120834U JP S58120834 U JPS58120834 U JP S58120834U JP 1631282 U JP1631282 U JP 1631282U JP 1631282 U JP1631282 U JP 1631282U JP S58120834 U JPS58120834 U JP S58120834U
- Authority
- JP
- Japan
- Prior art keywords
- turbine
- turbine engine
- compressor
- gas turbine
- cooling structure
- 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
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
第1図は、従来のガスタービシエンジンの内部構造を示
す断面図、第2図は、この考案の一実施例を示す第1図
と同様な断面図である。
1・・・圧縮機インペラ、2・・・圧縮機、3・・・ガ
ス発生機主軸、4・・・センタボルト(コンプレッサタ
ービン側)、5・・・コンプレッサタービン、6・・・
ガス発生機、7・・・出力タービン、9・・・隔壁、1
1・・・センタボルト(出力タービン側)、12. 1
4・・・環状間隙。FIG. 1 is a sectional view showing the internal structure of a conventional gas turbine engine, and FIG. 2 is a sectional view similar to FIG. 1 showing an embodiment of this invention. DESCRIPTION OF SYMBOLS 1... Compressor impeller, 2... Compressor, 3... Gas generator main shaft, 4... Center bolt (compressor turbine side), 5... Compressor turbine, 6...
Gas generator, 7... Output turbine, 9... Partition wall, 1
1... Center bolt (output turbine side), 12. 1
4...Annular gap.
Claims (1)
通路のインナ側に隔壁を有する2軸式ガスタービンエン
ジンにおいて、ガス発生機主軸及びコンプレッサタービ
ン側センタボルトに相連通する中心孔を設けてガス発生
機主軸の中心孔を圧縮機インペラ背後の圧力室間に連通
させると共に、前記隔壁に、複数個の透孔を設け、これ
ら透孔の合計面積をコンプレッサタービンディスク及び
出力タービンディスクの軸方向の環状間隙の合計面積よ
り大きくしたことを特徴とするガスタービンエンジンの
内部冷却構造。In a two-shaft gas turbine engine that has a partition wall on the inner side of the gas passage that communicates the compressor turbine and the output turbine, a center hole is provided that communicates with the gas generator main shaft and the center bolt on the compressor turbine side. The central hole communicates with the pressure chamber behind the compressor impeller, and the partition wall is provided with a plurality of through holes, and the total area of these through holes is the sum of the annular gaps in the axial direction of the compressor turbine disk and the output turbine disk. An internal cooling structure for a gas turbine engine characterized by having a larger area.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1631282U JPS58120834U (en) | 1982-02-10 | 1982-02-10 | Internal cooling structure of gas turbine engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1631282U JPS58120834U (en) | 1982-02-10 | 1982-02-10 | Internal cooling structure of gas turbine engine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS58120834U true JPS58120834U (en) | 1983-08-17 |
Family
ID=30028688
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1631282U Pending JPS58120834U (en) | 1982-02-10 | 1982-02-10 | Internal cooling structure of gas turbine engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS58120834U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04358727A (en) * | 1991-06-06 | 1992-12-11 | Daihatsu Diesel Mfg Co Ltd | Turbine nozzle installing structure of gas turbine |
-
1982
- 1982-02-10 JP JP1631282U patent/JPS58120834U/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04358727A (en) * | 1991-06-06 | 1992-12-11 | Daihatsu Diesel Mfg Co Ltd | Turbine nozzle installing structure of gas turbine |
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