JPS62131261U - - Google Patents
Info
- Publication number
- JPS62131261U JPS62131261U JP1752386U JP1752386U JPS62131261U JP S62131261 U JPS62131261 U JP S62131261U JP 1752386 U JP1752386 U JP 1752386U JP 1752386 U JP1752386 U JP 1752386U JP S62131261 U JPS62131261 U JP S62131261U
- Authority
- JP
- Japan
- Prior art keywords
- liner
- turbine engine
- combustor
- gas turbine
- air
- 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
- 239000007789 gas Substances 0.000 claims 3
- 239000000567 combustion gas Substances 0.000 claims 2
Landscapes
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
第１図は本考案の第１実施例に係るガスタービ
ンエンジン用燃焼器のライナの縦断面図、第２図
は第１図の装置の部分縦断面図、第３図は第２図
の―線に沿う横断面図、第４図は本考案の第
２実施例に係るガスタービンエンジン用燃焼器の
ライナの部分横断面図、第５図は従来のライナの
縦断面図、第６図は別の従来のライナの部分縦断
面図、第７図はさらに別の従来のライナの部分半
断面図、である。
１１，２２……ライナ、１２……コンプレツサ
側、１３……空気孔、１４……点火プラグ、１５
……タービン側、１７……ライナの中心軸、１８
，２１……スリツト、１８ａ，２１ａ……スリツ
トの開口部、１９……空気孔。
FIG. 1 is a longitudinal sectional view of a liner of a gas turbine engine combustor according to a first embodiment of the present invention, FIG. 2 is a partial longitudinal sectional view of the device shown in FIG. 1, and FIG. FIG. 4 is a partial cross-sectional view of a liner of a gas turbine engine combustor according to a second embodiment of the present invention, FIG. 5 is a vertical cross-sectional view of a conventional liner, and FIG. 6 is a cross-sectional view taken along the line. FIG. 7 is a partial longitudinal sectional view of another conventional liner, and FIG. 7 is a partial half sectional view of yet another conventional liner. 11, 22... Liner, 12... Compressor side, 13... Air hole, 14... Spark plug, 15
... Turbine side, 17 ... Center axis of liner, 18
, 21...Slit, 18a, 21a...Slit opening, 19...Air hole.
Claims (1)
なり複数の空気孔を有するライサ内に導入し、導
入された空気を用いて燃焼ガスを生成し、該燃焼
ガスをタービン側へと送るガスタービンエンジン
用燃焼器において、前記ライナに、該ライナの中
心軸に沿う方向に延びかつライナの周方向に向つ
て開口するスリツトを設けたことを特徴とするガ
スタービンエンジン用燃焼器。 (2) 前記空気孔の一つが、ライナの周方向でか
つ前記スリツトの開口方向に沿う方向にみて、点
火プラグの横に設けられている実用新案登録請求
の範囲第１項記載のガスタービンエンジン用燃焼
器。[Claims for Utility Model Registration] (1) Air from the compressor side is introduced into a cylindrical ricer having multiple air holes, the introduced air is used to generate combustion gas, and the combustion gas is A gas turbine engine combustor for a gas turbine engine, wherein the liner is provided with a slit extending in a direction along a central axis of the liner and opening in a circumferential direction of the liner. combustor. (2) The gas turbine engine according to claim 1, wherein one of the air holes is provided next to the spark plug when viewed in the circumferential direction of the liner and in the direction along the opening direction of the slit. combustor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1986017523U JPH0729403Y2 (en) | 1986-02-12 | 1986-02-12 | Combustor for gas turbine engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1986017523U JPH0729403Y2 (en) | 1986-02-12 | 1986-02-12 | Combustor for gas turbine engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS62131261U true JPS62131261U (en) | 1987-08-19 |
| JPH0729403Y2 JPH0729403Y2 (en) | 1995-07-05 |
Family
ID=30810359
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1986017523U Expired - Lifetime JPH0729403Y2 (en) | 1986-02-12 | 1986-02-12 | Combustor for gas turbine engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0729403Y2 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2015229924A (en) * | 2014-06-03 | 2015-12-21 | 株式会社Ihi | Jet engine combustor |
| JP2019199999A (en) * | 2018-05-17 | 2019-11-21 | 東芝エネルギーシステムズ株式会社 | Gas turbine combustor |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2950415B1 (en) * | 2009-09-21 | 2011-10-14 | Snecma | COMBUSTION CHAMBER FOR AERONAUTICAL TURBOMACHINE WITH DECAL COMBUSTION HOLES OR DIFFERENT RATES |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5577072U (en) * | 1978-11-17 | 1980-05-27 |
-
1986
- 1986-02-12 JP JP1986017523U patent/JPH0729403Y2/en not_active Expired - Lifetime
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5577072U (en) * | 1978-11-17 | 1980-05-27 |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2015229924A (en) * | 2014-06-03 | 2015-12-21 | 株式会社Ihi | Jet engine combustor |
| JP2019199999A (en) * | 2018-05-17 | 2019-11-21 | 東芝エネルギーシステムズ株式会社 | Gas turbine combustor |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0729403Y2 (en) | 1995-07-05 |