JPH0364354U - - Google Patents
Info
- Publication number
- JPH0364354U JPH0364354U JP12440389U JP12440389U JPH0364354U JP H0364354 U JPH0364354 U JP H0364354U JP 12440389 U JP12440389 U JP 12440389U JP 12440389 U JP12440389 U JP 12440389U JP H0364354 U JPH0364354 U JP H0364354U
- Authority
- JP
- Japan
- Prior art keywords
- fuel
- fuel injection
- engine case
- inlet
- passage
- 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 15
- 238000002347 injection Methods 0.000 claims description 6
- 239000007924 injection Substances 0.000 claims description 6
Landscapes
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
- Fuel-Injection Apparatus (AREA)
Description
第１図及び第２図は本考案によるガスタービン
の燃料供給装置の一例を示し、第１図は第２図の
−線断面図、第２図は第１図の−線端面
図である。第３図〜第５図は従来のガスタービン
の燃料供給装置を示し、第３図は第４図の−
線断面図、第４図は第３図の−線端面図、第
５図は第４図の一部分の分解図である。
１……燃料噴射弁、２……燃料噴射通路、２ａ
……入口、２ｂ……出口、３……エンジンケース
、６……燃焼器、７……燃料、１１……燃料通路
部材、１２……燃料入口部。
1 and 2 show an example of a fuel supply system for a gas turbine according to the present invention, in which FIG. 1 is a cross-sectional view taken along the line -- in FIG. 2, and FIG. 2 is an end view taken along the line -- in FIG. 1. 3 to 5 show a conventional gas turbine fuel supply system, and FIG. 3 shows the -
FIG. 4 is a line sectional view, FIG. 4 is a - line end view of FIG. 3, and FIG. 5 is an exploded view of a portion of FIG. 4. 1...Fuel injection valve, 2...Fuel injection passage, 2a
...Inlet, 2b...Outlet, 3...Engine case, 6...Combustor, 7...Fuel, 11...Fuel passage member, 12...Fuel inlet section.
Claims (1)
をその燃料噴射通路の入口及び出口が共にエンジ
ンケースの中に位置するように該エンジンケース
の一端に取付け、このエンジンケースの一端の内
壁には前記燃料噴射弁の燃料噴射通路の各入口が
開口する環状の燃料通路部材を設けるとともに、
前記エンジンケースの一端には前記燃料通路部材
の内部に連通する燃料入口部を設けたことを特徴
とするガスタービンの燃料供給装置。 A plurality of fuel injection valves arranged along the circumferential direction are attached to one end of the engine case so that the inlet and outlet of the fuel injection passage are both located inside the engine case, and is provided with an annular fuel passage member in which each inlet of the fuel injection passage of the fuel injection valve opens;
A fuel supply device for a gas turbine, wherein one end of the engine case is provided with a fuel inlet portion that communicates with the inside of the fuel passage member.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12440389U JPH0364354U (en) | 1989-10-24 | 1989-10-24 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12440389U JPH0364354U (en) | 1989-10-24 | 1989-10-24 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0364354U true JPH0364354U (en) | 1991-06-24 |
Family
ID=31672323
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP12440389U Pending JPH0364354U (en) | 1989-10-24 | 1989-10-24 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0364354U (en) |
-
1989
- 1989-10-24 JP JP12440389U patent/JPH0364354U/ja active Pending