JPH0236767U - - Google Patents
Info
- Publication number
- JPH0236767U JPH0236767U JP11127688U JP11127688U JPH0236767U JP H0236767 U JPH0236767 U JP H0236767U JP 11127688 U JP11127688 U JP 11127688U JP 11127688 U JP11127688 U JP 11127688U JP H0236767 U JPH0236767 U JP H0236767U
- Authority
- JP
- Japan
- Prior art keywords
- ring
- shell
- gas turbine
- fins
- combustor
- 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.)
- Granted
Links
- 238000001816 cooling Methods 0.000 claims description 4
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
- Gas Burners (AREA)
Description
第１図及び第２図は本考案によるガスタービン
燃焼器の異なる２つの例を示す要部の断面図、第
３ａ図は従来のガスタービン燃焼器の一例を示す
要部の断面図、第３ｂ図は第３ａ図の３ｂ―３ｂ
線断面図、第３ｃ図は第３ａ図の３ｃ―３ｃ線断
面図、第４図は従来のガスタービン燃焼器の他の
例を示す要部の断面図である。
１……燃焼器シエル、２，２ａ，２ｂ，２ｃ…
…対流冷却用空気通路、３……リング、４……板
状フイン、５……冷却空気、６……冷却空気孔、
７……次段のリング、８……デポジツト、９……
フインの不連続部。
1 and 2 are sectional views of essential parts showing two different examples of a gas turbine combustor according to the present invention; FIG. 3a is a sectional view of essential parts showing an example of a conventional gas turbine combustor; and 3b The figure is 3b-3b in Figure 3a.
3c is a sectional view taken along line 3c-3c of FIG. 3a, and FIG. 4 is a sectional view of essential parts showing another example of a conventional gas turbine combustor. 1... Combustor shell, 2, 2a, 2b, 2c...
...Convection cooling air passage, 3...Ring, 4...Plate fin, 5...Cooling air, 6...Cooling air hole,
7...Next ring, 8...Deposit, 9...
Fin discontinuity.
Claims (1)
内壁面との間に対流冷却用空気通路を形成するリ
ングを配置し、このリングの外表面にはリングの
長手方向に沿つて細長くてリング出口端まで延び
る多数の板状フインを取付けるとともに、その途
中にフインの不連続部を設けたことを特徴とする
ガスタービン燃焼器。 A ring is arranged inside the combustor shell of a gas turbine to form a convection cooling air passage between the shell and the inner wall surface of the shell, and the outer surface of the ring has an elongated ring extending along the longitudinal direction of the ring to the ring outlet end. A gas turbine combustor characterized in that a large number of extending plate-like fins are attached and a discontinuous part of the fins is provided in the middle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11127688U JPH0645148Y2 (en) | 1988-08-26 | 1988-08-26 | Gas turbine combustor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11127688U JPH0645148Y2 (en) | 1988-08-26 | 1988-08-26 | Gas turbine combustor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH0236767U true JPH0236767U (en) | 1990-03-09 |
| JPH0645148Y2 JPH0645148Y2 (en) | 1994-11-16 |
Family
ID=31349179
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP11127688U Expired - Lifetime JPH0645148Y2 (en) | 1988-08-26 | 1988-08-26 | Gas turbine combustor |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0645148Y2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5844503B1 (en) * | 2014-10-21 | 2016-01-20 | 住友精密工業株式会社 | Heat exchanger for aircraft engine |
-
1988
- 1988-08-26 JP JP11127688U patent/JPH0645148Y2/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5844503B1 (en) * | 2014-10-21 | 2016-01-20 | 住友精密工業株式会社 | Heat exchanger for aircraft engine |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0645148Y2 (en) | 1994-11-16 |