JPS6193258A - 航空機用ガスタ−ビンエンジン及びその運転方法 - Google Patents
航空機用ガスタ−ビンエンジン及びその運転方法Info
- Publication number
- JPS6193258A JPS6193258A JP21239284A JP21239284A JPS6193258A JP S6193258 A JPS6193258 A JP S6193258A JP 21239284 A JP21239284 A JP 21239284A JP 21239284 A JP21239284 A JP 21239284A JP S6193258 A JPS6193258 A JP S6193258A
- Authority
- JP
- Japan
- Prior art keywords
- compartment
- nacelle
- engine
- air
- aircraft
- 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 28
- 238000000034 method Methods 0.000 claims description 3
- 239000000446 fuel Substances 0.000 description 15
- 239000007789 gas Substances 0.000 description 10
- 230000007423 decrease Effects 0.000 description 6
- 230000000694 effects Effects 0.000 description 6
- 230000008901 benefit Effects 0.000 description 4
- 238000011144 upstream manufacturing Methods 0.000 description 3
- 230000002411 adverse Effects 0.000 description 2
- 238000013459 approach Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 230000008602 contraction Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000007654 immersion Methods 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 230000011514 reflex Effects 0.000 description 1
- 238000013022 venting Methods 0.000 description 1
Landscapes
- Engine Equipment That Uses Special Cycles (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP21239284A JPS6193258A (ja) | 1984-10-09 | 1984-10-09 | 航空機用ガスタ−ビンエンジン及びその運転方法 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP21239284A JPS6193258A (ja) | 1984-10-09 | 1984-10-09 | 航空機用ガスタ−ビンエンジン及びその運転方法 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6193258A true JPS6193258A (ja) | 1986-05-12 |
| JPH0526944B2 JPH0526944B2 (enExample) | 1993-04-19 |
Family
ID=16621821
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP21239284A Granted JPS6193258A (ja) | 1984-10-09 | 1984-10-09 | 航空機用ガスタ−ビンエンジン及びその運転方法 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6193258A (enExample) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7395026B2 (en) | 2004-05-03 | 2008-07-01 | Samsung Electronics Co., Ltd. | Image forming apparatus having auxiliary tray |
| JP2013093574A (ja) * | 2011-10-26 | 2013-05-16 | General Electric Co <Ge> | 過渡電圧抑制器のための方法およびシステム |
| JP2017223212A (ja) * | 2016-06-16 | 2017-12-21 | 早川 秀樹 | エンジンと多目的ファンモーターターボ |
-
1984
- 1984-10-09 JP JP21239284A patent/JPS6193258A/ja active Granted
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7395026B2 (en) | 2004-05-03 | 2008-07-01 | Samsung Electronics Co., Ltd. | Image forming apparatus having auxiliary tray |
| JP2013093574A (ja) * | 2011-10-26 | 2013-05-16 | General Electric Co <Ge> | 過渡電圧抑制器のための方法およびシステム |
| JP2017223212A (ja) * | 2016-06-16 | 2017-12-21 | 早川 秀樹 | エンジンと多目的ファンモーターターボ |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0526944B2 (enExample) | 1993-04-19 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4493184A (en) | Pressurized nacelle compartment for active clearance controlled gas turbine engines | |
| JP5080076B2 (ja) | アクティブクリアランス制御のためのガスタービンエンジンリングの熱制御 | |
| US4826397A (en) | Stator assembly for a gas turbine engine | |
| EP2236772B1 (en) | Gas turbine engine with active tip clearance control device and corresponding operating method | |
| US4474001A (en) | Cooling system for the electrical generator of a turbofan gas turbine engine | |
| US8721257B2 (en) | Rotor blade tip clearance control | |
| JP5383973B2 (ja) | ガスタービンエンジンアクティブクリアランス制御の使用済み冷却空気を排気するシステム及び方法 | |
| CA2266449C (en) | Gas turbine airfoil cooling | |
| US5203162A (en) | Compressor bleed manifold for a gas turbine engine | |
| US6269628B1 (en) | Apparatus for reducing combustor exit duct cooling | |
| US9605593B2 (en) | Gas turbine engine with soft mounted pre-swirl nozzle | |
| US20090053041A1 (en) | Gas turbine engine case for clearance control | |
| EP2375005B1 (en) | Method for controlling turbine blade tip seal clearance | |
| EP2236750B1 (en) | An impingement cooling arrangement for a gas turbine engine | |
| US2599879A (en) | Exhaust induced cooling system for gas turbines | |
| US20140341711A1 (en) | Shroud arrangement for a gas turbine engine | |
| US3437313A (en) | Gas turbine blade cooling | |
| US9920647B2 (en) | Dual source cooling air shroud arrangement for a gas turbine engine | |
| US8137075B2 (en) | Compressor impellers, compressor sections including the compressor impellers, and methods of manufacturing | |
| US8206079B2 (en) | Temperature controlling apparatus | |
| JPH06507000A (ja) | 航空機ナセルの防氷装置用排気口 | |
| EP2497908B1 (en) | A conduit for bleed air in a gas turbine engine | |
| EP3095958B1 (en) | System for thermally shielding a portion of a gas turbine shroud assembly | |
| EP1783350B1 (en) | Non axi-symmetric shaped cooling liner within a gas turbine engine exhaust duct | |
| JP2006200530A (ja) | ロータアセンブリ先端隙間を維持する方法および装置 |