JPH02133556U - - Google Patents
Info
- Publication number
- JPH02133556U JPH02133556U JP4346089U JP4346089U JPH02133556U JP H02133556 U JPH02133556 U JP H02133556U JP 4346089 U JP4346089 U JP 4346089U JP 4346089 U JP4346089 U JP 4346089U JP H02133556 U JPH02133556 U JP H02133556U
- Authority
- JP
- Japan
- Prior art keywords
- combustor
- gas turbine
- main body
- substantially cylindrical
- control sleeve
- 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
- 239000000314 lubricant Substances 0.000 claims description 2
- 239000000919 ceramic Substances 0.000 claims 1
- 238000010790 dilution Methods 0.000 claims 1
- 239000012895 dilution Substances 0.000 claims 1
- 239000011343 solid material Substances 0.000 claims 1
- 239000007787 solid Substances 0.000 description 1
Description
第１図はこの考案に係るガスタービン用燃焼器
の一実施例を示す半断面図、第２図はその要部の
斜視図、第３図はライナ部の外観斜視図、第４図
はこの考案の異なる実施例を示す要部断面図、第
５図はその斜視図、第６図はこの考案の更に異な
る実施例を示す要部斜視図である。
２……燃焼器本体、５……空気制御用スリーブ
、７……ライナ部、９……ドーム部、１０……ス
クロール部、２１，２３，２４……固体潤滑材チ
ツプ。
Fig. 1 is a half-sectional view showing one embodiment of a gas turbine combustor according to this invention, Fig. 2 is a perspective view of its main parts, Fig. 3 is an external perspective view of the liner section, and Fig. 4 is a perspective view of the main part thereof. FIG. 5 is a sectional view of a main part showing a different embodiment of the invention, FIG. 5 is a perspective view thereof, and FIG. 6 is a perspective view of a main part showing a further different embodiment of this invention. 2... Combustor main body, 5... Air control sleeve, 7... Liner section, 9... Dome section, 10... Scroll section, 21, 23, 24... Solid lubricant chip.
Claims (1)
筒状のライナ部および該ライナ部の両端にそれぞ
れ接続されたドーム部ならびにスクロール部から
なる燃焼器本体と、上記ライナ部の外周に回転可
能に嵌合した略円筒状の空気制御用スリーブとを
備え、かつこれら各部がセラミツクにて形成され
てなるガスタービン用燃焼器において、上記燃焼
器本体と上記空気制御用スリーブとの摺接部に固
体潤滑材ピースを配設したことを特徴とするガス
タービン用燃焼器。 A combustor main body consisting of a substantially cylindrical liner portion with dilution air introduction holes formed around the periphery, a dome portion and a scroll portion connected to both ends of the liner portion, and a combustor body rotatable around the outer periphery of the liner portion. In a gas turbine combustor comprising a fitted substantially cylindrical air control sleeve, each of which is made of ceramic, a solid material is provided at the sliding contact portion between the combustor main body and the air control sleeve. A combustor for a gas turbine, characterized in that a lubricant piece is provided.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4346089U JPH02133556U (en) | 1989-04-13 | 1989-04-13 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4346089U JPH02133556U (en) | 1989-04-13 | 1989-04-13 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH02133556U true JPH02133556U (en) | 1990-11-06 |
Family
ID=31555887
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4346089U Pending JPH02133556U (en) | 1989-04-13 | 1989-04-13 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH02133556U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009047409A (en) * | 2007-08-14 | 2009-03-05 | General Electric Co <Ge> | Combustion liner stopper in gas turbine |
-
1989
- 1989-04-13 JP JP4346089U patent/JPH02133556U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009047409A (en) * | 2007-08-14 | 2009-03-05 | General Electric Co <Ge> | Combustion liner stopper in gas turbine |