JPS61166141U - - Google Patents
Info
- Publication number
- JPS61166141U JPS61166141U JP4981285U JP4981285U JPS61166141U JP S61166141 U JPS61166141 U JP S61166141U JP 4981285 U JP4981285 U JP 4981285U JP 4981285 U JP4981285 U JP 4981285U JP S61166141 U JPS61166141 U JP S61166141U
- Authority
- JP
- Japan
- Prior art keywords
- compressor
- gas
- combustor
- auxiliary
- turbine
- 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
- 239000000446 fuel Substances 0.000 claims description 3
- 239000007789 gas Substances 0.000 claims 8
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims 1
- 239000010687 lubricating oil Substances 0.000 claims 1
- 239000001301 oxygen Substances 0.000 claims 1
- 229910052760 oxygen Inorganic materials 0.000 claims 1
- 238000011144 upstream manufacturing Methods 0.000 claims 1
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
第１図は、本考案の実施例を示すフローシート
、第２図は従来例のフローシートである。
１……コンプレツサー、２……ガスタービン、
３……給気路、４……ガス燃料供給用流路、５…
…燃焼器、８……補助コンプレツサー、９……補
助タービン、１１……還元流路、１２……ガスモ
ータ、１４……ポンプ、Ａ……給油装置。
FIG. 1 is a flow sheet showing an embodiment of the present invention, and FIG. 2 is a flow sheet of a conventional example. 1...Compressor, 2...Gas turbine,
3... Air supply path, 4... Gas fuel supply flow path, 5...
...Combustor, 8...Auxiliary compressor, 9...Auxiliary turbine, 11...Reduction flow path, 12...Gas motor, 14...Pump, A...Oil supply device.
Claims (1)
をガスタービン２に連動連結し、前記コンプレツ
サー１から前記ガスタービン２への給気路３に燃
焼器５を介装し、その燃焼器５にガス燃料を加圧
供給する補助コンプレツサー８を補助タービン９
に連動連結し、前記燃焼器５の排気側に前記補助
タービン９を接続し、前記補助コンプレツサー８
と燃焼器５の間からその補助コンプレツサー８の
上流側に余剰ガス燃料を戻す還元流路１１を設け
、前記コンプレツサー１，８とガスタービン２，
９の軸受部１７ａ，１７ｂに潤滑油を循環供給す
る給油装置Ａを設けた熱風発生装置であつて、前
記還元流路１１にガスモータ１２を設け、前記給
油装置Ａのポンプ１４に前記ガスモータ１２を連
動連結してある熱風発生装置。 Compressor 1 that supplies oxygen-containing gas under pressure
A combustor 5 is interposed in the air supply path 3 from the compressor 1 to the gas turbine 2, and an auxiliary compressor 8 that supplies gas fuel under pressure to the combustor 5 is connected to the gas turbine 2. 9
The auxiliary turbine 9 is connected to the exhaust side of the combustor 5, and the auxiliary compressor 8
A return passage 11 for returning excess gas fuel is provided between the combustor 5 and the auxiliary compressor 8 on the upstream side of the auxiliary compressor 8, and the compressor 1, 8 and the gas turbine 2,
A hot air generator is provided with a refueling device A that circulates lubricating oil to bearing portions 17a and 17b of 9, a gas motor 12 is provided in the return flow path 11, and a pump 14 of the refueling device A is connected to the gas motor 12. A hot air generator that is linked together.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4981285U JPS61166141U (en) | 1985-04-03 | 1985-04-03 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4981285U JPS61166141U (en) | 1985-04-03 | 1985-04-03 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS61166141U true JPS61166141U (en) | 1986-10-15 |
Family
ID=30567350
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4981285U Pending JPS61166141U (en) | 1985-04-03 | 1985-04-03 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS61166141U (en) |
-
1985
- 1985-04-03 JP JP4981285U patent/JPS61166141U/ja active Pending
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