JPS6323556U - - Google Patents
Info
- Publication number
- JPS6323556U JPS6323556U JP11199886U JP11199886U JPS6323556U JP S6323556 U JPS6323556 U JP S6323556U JP 11199886 U JP11199886 U JP 11199886U JP 11199886 U JP11199886 U JP 11199886U JP S6323556 U JPS6323556 U JP S6323556U
- Authority
- JP
- Japan
- Prior art keywords
- combustor
- fuel nozzle
- nozzle
- axial direction
- inlet opening
- 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
- 238000002485 combustion reaction Methods 0.000 claims description 8
- 238000009792 diffusion process Methods 0.000 claims description 3
- 239000000446 fuel Substances 0.000 claims 3
Landscapes
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
Description
第１図は本考案によるガスタービン用燃焼器の
一実施例を示す概略断面図、第２図は第１図の
部の拡大断面図、第３図は従来例を示す断面図で
ある。
１……燃焼器、２……燃焼ノズル本体、３……
燃焼用空気口、４……拡散燃焼ノズル、５……予
混合燃焼ノズル。
FIG. 1 is a schematic sectional view showing an embodiment of a gas turbine combustor according to the present invention, FIG. 2 is an enlarged sectional view of the portion shown in FIG. 1, and FIG. 3 is a sectional view showing a conventional example. 1... Combustor, 2... Combustion nozzle body, 3...
Combustion air port, 4...Diffusion combustion nozzle, 5...Premix combustion nozzle.
Claims (1)
燃料ノズル本体を同心円状に配置されているとと
もに、これらの各燃料ノズル本体と前記燃焼器の
入口開口端とで限定された空隙部で燃焼用空気を
形成し、かつ前記燃料ノズル本体の各前端面の平
面部には拡散燃焼ノズルを前記燃焼器の軸線方向
に対して平行に設けるとともに、各壁面円周上に
は予混合燃焼ノズルを前記燃焼器の軸線方向に対
して直角に設けてなるガスタービン用燃焼器。 A large number of hollow cylindrical fuel nozzle bodies are arranged concentrically at the inlet opening end of the combustor, and a gap defined by each of these fuel nozzle bodies and the inlet opening end of the combustor is used. A diffusion combustion nozzle is provided on the flat surface of each front end surface of the fuel nozzle body to form combustion air, and a diffusion combustion nozzle is provided parallel to the axial direction of the combustor, and a premix combustion nozzle is provided on the circumference of each wall surface. A combustor for a gas turbine, wherein the combustor is provided at right angles to the axial direction of the combustor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11199886U JPS6323556U (en) | 1986-07-23 | 1986-07-23 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11199886U JPS6323556U (en) | 1986-07-23 | 1986-07-23 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6323556U true JPS6323556U (en) | 1988-02-16 |
Family
ID=30992449
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP11199886U Pending JPS6323556U (en) | 1986-07-23 | 1986-07-23 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6323556U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH05264009A (en) * | 1992-03-17 | 1993-10-12 | Hitachi Ltd | Combustion device |
-
1986
- 1986-07-23 JP JP11199886U patent/JPS6323556U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH05264009A (en) * | 1992-03-17 | 1993-10-12 | Hitachi Ltd | Combustion device |