JPH01111148U - - Google Patents
Info
- Publication number
- JPH01111148U JPH01111148U JP469088U JP469088U JPH01111148U JP H01111148 U JPH01111148 U JP H01111148U JP 469088 U JP469088 U JP 469088U JP 469088 U JP469088 U JP 469088U JP H01111148 U JPH01111148 U JP H01111148U
- Authority
- JP
- Japan
- Prior art keywords
- gas turbine
- turbine engine
- burner head
- spring
- fuel injection
- 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
- 239000000919 ceramic Substances 0.000 claims description 4
- 238000002485 combustion reaction Methods 0.000 claims description 4
- 239000000446 fuel Substances 0.000 claims description 3
- 238000002347 injection Methods 0.000 claims description 3
- 239000007924 injection Substances 0.000 claims description 3
Description
第1図は本考案の第1実施例に係るガスタービ
ンエンジンの燃焼器構造の断面図、第2図は本考
案の第2実施例に係るガスタービンエンジンの燃
焼器構造の断面図、第3図は、実願昭62―10
7070号におけるセラミツク製燃焼筒近傍の断
面図、である。
11……バーナヘツド、12……セラミツク製
燃焼筒、14……燃料噴射ノズル、21……スプ
リング、29……メインハウジング、30,40
……空気通路。
FIG. 1 is a sectional view of a combustor structure of a gas turbine engine according to a first embodiment of the present invention, FIG. 2 is a sectional view of a combustor structure of a gas turbine engine according to a second embodiment of the present invention, and FIG. The figure shows Jitsugan 1986-10.
7070 is a sectional view of the vicinity of the ceramic combustion tube. 11... Burner head, 12... Ceramic combustion tube, 14... Fuel injection nozzle, 21... Spring, 29... Main housing, 30, 40
...Air passage.
Claims (1)
セラミツク製燃焼筒内に臨ませ、該セラミツク製
燃焼筒の一方を、スプリングを介してメインハウ
ジング側に固定される前記バーナヘツドに保持さ
せたガスタービンエンジンの燃焼器であつて、前
記バーナヘツドに、該ガスタービンエンジンのコ
ンプレツサからの吐出空気を前記燃料噴射ノズル
と前記スプリングとに導く空気通路を設けたこと
を特徴とするガススタービンエンジンの燃焼器構
造。 A combustor for a gas turbine engine in which a fuel injection nozzle attached to a burner head faces into a ceramic combustion tube, and one side of the ceramic combustion tube is held by the burner head, which is fixed to the main housing side via a spring. A combustor structure for a gas turbine engine, characterized in that the burner head is provided with an air passage for guiding discharge air from a compressor of the gas turbine engine to the fuel injection nozzle and the spring.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP469088U JPH01111148U (en) | 1988-01-20 | 1988-01-20 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP469088U JPH01111148U (en) | 1988-01-20 | 1988-01-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH01111148U true JPH01111148U (en) | 1989-07-26 |
Family
ID=31207425
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP469088U Pending JPH01111148U (en) | 1988-01-20 | 1988-01-20 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH01111148U (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH05118549A (en) * | 1991-10-25 | 1993-05-14 | Nissan Motor Co Ltd | Burner for gas turbine |
WO2016096388A1 (en) * | 2014-12-15 | 2016-06-23 | Nuovo Pignone Srl | Combustor liner flexible support and method |
WO2017103232A1 (en) * | 2015-12-18 | 2017-06-22 | Dürr Systems Ag | Combustion chamber device and gas turbine device |
-
1988
- 1988-01-20 JP JP469088U patent/JPH01111148U/ja active Pending
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH05118549A (en) * | 1991-10-25 | 1993-05-14 | Nissan Motor Co Ltd | Burner for gas turbine |
WO2016096388A1 (en) * | 2014-12-15 | 2016-06-23 | Nuovo Pignone Srl | Combustor liner flexible support and method |
JP2018504572A (en) * | 2014-12-15 | 2018-02-15 | ヌオーヴォ ピニォーネ ソチエタ レスポンサビリタ リミタータNuovo Pignone S.R.L. | Combustor liner elastic support apparatus and method |
US11333361B2 (en) | 2014-12-15 | 2022-05-17 | Nuovo Pignone Srl | Combustor liner flexible support and method |
WO2017103232A1 (en) * | 2015-12-18 | 2017-06-22 | Dürr Systems Ag | Combustion chamber device and gas turbine device |