JPS5783637A - Fuel heater for gas turbine - Google Patents
Fuel heater for gas turbineInfo
- Publication number
- JPS5783637A JPS5783637A JP15954280A JP15954280A JPS5783637A JP S5783637 A JPS5783637 A JP S5783637A JP 15954280 A JP15954280 A JP 15954280A JP 15954280 A JP15954280 A JP 15954280A JP S5783637 A JPS5783637 A JP S5783637A
- Authority
- JP
- Japan
- Prior art keywords
- valve
- pipe
- cut
- oil
- bypass
- 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 title abstract 2
- 239000003921 oil Substances 0.000 abstract 4
- 239000000295 fuel oil Substances 0.000 abstract 3
- 238000010438 heat treatment Methods 0.000 abstract 1
Landscapes
- Feeding And Controlling Fuel (AREA)
Abstract
PURPOSE: In a system wherein a low-quality oil is used and heated, to enable heating of the entire ignition fuel oil at start of the system by disposing a bypass valve in a pipe which extends from the inlet to the outlet of a fuel oil cut- off valve and providing a return pipe which runs from the suction side of a nozzle to that of an oil feed equipment.
CONSTITUTION: A fuel transferred from a tank is boosted by a pump 1, is heated by a heater 2, passes through the first filter 3 and a cut-off valve 4, is further boosted by a pump 5, passes through the second filter 6, and is equivalently distributed by distributors 7. Each of the distributed oil is sent through a check valve 8 and injected from a nozzle 9 into a combustor 10. A fuel oil between the heater 2 and the cut-off valve 4 is detected by a temperature detector 12 and if its result is not so high as a required level, the oil is bypassed by a return 11. The inlet-side pipe of the nozzle 9 is connected with a return pipe 20, with a return valve 21 disposed therein, running via a check valve 22 up to an inlet- side pipe of the pump 1. A check valve 23 is disposed in a bypass pipe extending from the inlet of the cut-off valve 4 and another bypass pipe 24 is connected with the cut-off valve 4. A bypass valve 25 is disposed in the bypass 24.
COPYRIGHT: (C)1982,JPO&Japio
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15954280A JPS5783637A (en) | 1980-11-14 | 1980-11-14 | Fuel heater for gas turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15954280A JPS5783637A (en) | 1980-11-14 | 1980-11-14 | Fuel heater for gas turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS5783637A true JPS5783637A (en) | 1982-05-25 |
Family
ID=15696028
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP15954280A Pending JPS5783637A (en) | 1980-11-14 | 1980-11-14 | Fuel heater for gas turbine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5783637A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5977278U (en) * | 1982-11-16 | 1984-05-25 | 昭和電線電纜株式会社 | Mounting bracket for iron wire armored cable |
| JPS6090928A (en) * | 1983-10-24 | 1985-05-22 | Kawasaki Heavy Ind Ltd | Apparatus for assisting starting of gas turbine |
| JPH0249932A (en) * | 1988-08-09 | 1990-02-20 | Toshiba Corp | Fuel supply facility of gas turbine |
| US6820427B2 (en) * | 2002-12-13 | 2004-11-23 | General Electric Company | Method and apparatus for operating a turbine engine |
-
1980
- 1980-11-14 JP JP15954280A patent/JPS5783637A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5977278U (en) * | 1982-11-16 | 1984-05-25 | 昭和電線電纜株式会社 | Mounting bracket for iron wire armored cable |
| JPS6090928A (en) * | 1983-10-24 | 1985-05-22 | Kawasaki Heavy Ind Ltd | Apparatus for assisting starting of gas turbine |
| JPH0249932A (en) * | 1988-08-09 | 1990-02-20 | Toshiba Corp | Fuel supply facility of gas turbine |
| US6820427B2 (en) * | 2002-12-13 | 2004-11-23 | General Electric Company | Method and apparatus for operating a turbine engine |
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