JPH0267042U - - Google Patents
Info
- Publication number
- JPH0267042U JPH0267042U JP14656588U JP14656588U JPH0267042U JP H0267042 U JPH0267042 U JP H0267042U JP 14656588 U JP14656588 U JP 14656588U JP 14656588 U JP14656588 U JP 14656588U JP H0267042 U JPH0267042 U JP H0267042U
- Authority
- JP
- Japan
- Prior art keywords
- combustion gas
- intake air
- passage
- heat exchanger
- exhaust system
- 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
- 239000000567 combustion gas Substances 0.000 claims description 5
- 238000001816 cooling Methods 0.000 claims description 3
- 239000007789 gas Substances 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 1
Landscapes
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Description
第１図は本考案によるガスタービンエンジンの
熱交換器の端面図、第２図はガスタービンエンジ
ンの概略構成図、第３図は第１図の線―に沿
つた断面図、第４図は細パイプに取りつけた放熱
板の拡大斜視図、第５図は熱交換器に冷却装置を
取りつける分解斜視図である。
２０……熱交換器、３０……燃焼ガス通路、３
２……冷却装置、３４……放熱板、３６，３８…
…パイプ、４０……ラジエータ。
Figure 1 is an end view of a heat exchanger for a gas turbine engine according to the present invention, Figure 2 is a schematic configuration diagram of the gas turbine engine, Figure 3 is a sectional view taken along the line - in Figure 1, and Figure 4 is FIG. 5 is an enlarged perspective view of a heat sink attached to a thin pipe, and FIG. 5 is an exploded perspective view of a cooling device attached to a heat exchanger. 20... Heat exchanger, 30... Combustion gas passage, 3
2... Cooling device, 34... Heat sink, 36, 38...
...pipe, 40...radiator.
Claims (1)
ービンを通つた燃焼ガスとの間で熱交換を行うた
めに吸入空気通路と燃焼ガス通路とを有する熱交
換器を備え、該熱交換器の該燃焼ガス通路の出口
部に冷却手段を設けたことを特徴とするガスター
ビンエンジンの排気装置。 A heat exchanger having an intake air passage and a combustion gas passage for exchanging heat between intake air traveling from the compressor to the combustor and combustion gas passing through the turbine, the combustion gas passage of the heat exchanger having an intake air passage and a combustion gas passage. An exhaust system for a gas turbine engine, characterized in that a cooling means is provided at an outlet portion of the exhaust system.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14656588U JPH0267042U (en) | 1988-11-11 | 1988-11-11 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14656588U JPH0267042U (en) | 1988-11-11 | 1988-11-11 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0267042U true JPH0267042U (en) | 1990-05-21 |
Family
ID=31416176
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP14656588U Pending JPH0267042U (en) | 1988-11-11 | 1988-11-11 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0267042U (en) |
-
1988
- 1988-11-11 JP JP14656588U patent/JPH0267042U/ja active Pending
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