PL397899A1 - Turbine exhaust diffuser system - Google Patents
Turbine exhaust diffuser systemInfo
- Publication number
- PL397899A1 PL397899A1 PL397899A PL39789912A PL397899A1 PL 397899 A1 PL397899 A1 PL 397899A1 PL 397899 A PL397899 A PL 397899A PL 39789912 A PL39789912 A PL 39789912A PL 397899 A1 PL397899 A1 PL 397899A1
- Authority
- PL
- Poland
- Prior art keywords
- turbine exhaust
- exhaust diffuser
- diffuser system
- wall
- access tunnel
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/30—Exhaust heads, chambers, or the like
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/06—Fluid supply conduits to nozzles or the like
- F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Supercharger (AREA)
- Exhaust Silencers (AREA)
Abstract
Uklad dyfuzora wydechowego turbiny zawiera wiele sluz osobowych (202). Kazda sposród tych sluz osobowych rozciaga sie pomiedzy scianka zewnetrzna (198) ukladu dyfuzora wydechowego turbiny oraz wewnetrznym tunelem dostepu ukladu dyfuzora wydechowego turbiny. Wiele sluz osobowych rozciaga sie pomiedzy scianka zewnetrzna oraz tunelem dostepu (206) pod katem, który nie jest prostopadly do osi srodkowej (105) ukladu dyfuzora wydechowego turbiny (188).The turbine exhaust diffuser system includes a plurality of passenger locks (202). Each of these passenger locks extends between the outer wall (198) of the turbine exhaust diffuser system and the inner access tunnel of the turbine exhaust diffuser system. Many passenger locks extend between the outer wall and the access tunnel (206) at an angle that is not perpendicular to the central axis (105) of the turbine exhaust diffuser (188) system.
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL397899A PL221113B1 (en) | 2012-01-25 | 2012-01-25 | Turbine exhaust diffuser system |
US13/430,603 US20130189088A1 (en) | 2012-01-25 | 2012-03-26 | Turbine exhaust diffuser system manways |
JP2013007964A JP2013151934A (en) | 2012-01-25 | 2013-01-21 | Turbine exhaust diffuser system |
RU2013102779/06A RU2013102779A (en) | 2012-01-25 | 2013-01-23 | EXHAUST TURBINE DIFFUSER (OPTIONS) |
EP13152397.9A EP2620596A2 (en) | 2012-01-25 | 2013-01-23 | Turbine exhaust diffuser system |
CN2013100287242A CN103225520A (en) | 2012-01-25 | 2013-01-25 | Turbine exhaust diffuser system manways |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL397899A PL221113B1 (en) | 2012-01-25 | 2012-01-25 | Turbine exhaust diffuser system |
Publications (2)
Publication Number | Publication Date |
---|---|
PL397899A1 true PL397899A1 (en) | 2013-08-05 |
PL221113B1 PL221113B1 (en) | 2016-02-29 |
Family
ID=47631305
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL397899A PL221113B1 (en) | 2012-01-25 | 2012-01-25 | Turbine exhaust diffuser system |
Country Status (6)
Country | Link |
---|---|
US (1) | US20130189088A1 (en) |
EP (1) | EP2620596A2 (en) |
JP (1) | JP2013151934A (en) |
CN (1) | CN103225520A (en) |
PL (1) | PL221113B1 (en) |
RU (1) | RU2013102779A (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2997997B1 (en) * | 2012-11-12 | 2014-12-26 | Snecma | AIR TUBE SUPPORT SUPPORT IN A TURBOMACHINE |
FR2997996B1 (en) * | 2012-11-12 | 2015-01-09 | Snecma | AIR TUBE SUPPORT SUPPORT IN A TURBOMACHINE |
US10255406B2 (en) * | 2015-02-24 | 2019-04-09 | Siemens Corporation | Designing the geometry of a gas turbine exhaust diffuser on the basis of fluid dynamics information |
US10563543B2 (en) | 2016-05-31 | 2020-02-18 | General Electric Company | Exhaust diffuser |
US10612420B2 (en) * | 2016-11-17 | 2020-04-07 | General Electric Company | Support structures for rotors |
CN109630219B (en) * | 2018-12-16 | 2022-03-04 | 中国航发沈阳发动机研究所 | Gas turbine exhaust apparatus |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2655307A (en) * | 1947-06-11 | 1953-10-13 | Gen Electric | Gas turbine rotor arrangement |
GB695482A (en) * | 1950-11-28 | 1953-08-12 | Rolls Royce | Improvements in or relating to gas-turbine engines |
GB846329A (en) * | 1957-12-12 | 1960-08-31 | Napier & Son Ltd | Combustion turbine power units |
CH672004A5 (en) * | 1986-09-26 | 1989-10-13 | Bbc Brown Boveri & Cie | |
US5404713A (en) * | 1993-10-04 | 1995-04-11 | General Electric Company | Spillage drag and infrared reducing flade engine |
US20040109756A1 (en) * | 2002-12-09 | 2004-06-10 | Mitsubishi Heavy Industries Ltd. | Gas turbine |
US6866479B2 (en) * | 2003-05-16 | 2005-03-15 | Mitsubishi Heavy Industries, Ltd. | Exhaust diffuser for axial-flow turbine |
US20080159856A1 (en) * | 2006-12-29 | 2008-07-03 | Thomas Ory Moniz | Guide vane and method of fabricating the same |
US8438859B2 (en) * | 2008-01-08 | 2013-05-14 | Rolls-Royce North American Technologies, Inc. | Integrated bypass engine structure |
US8408011B2 (en) * | 2009-04-30 | 2013-04-02 | Pratt & Whitney Canada Corp. | Structural reinforcement strut for gas turbine case |
US20130091865A1 (en) * | 2011-10-17 | 2013-04-18 | General Electric Company | Exhaust gas diffuser |
US9032721B2 (en) * | 2011-12-14 | 2015-05-19 | Siemens Energy, Inc. | Gas turbine engine exhaust diffuser including circumferential vane |
US9316108B2 (en) * | 2012-03-05 | 2016-04-19 | General Electric Company | Gas turbine frame stiffening rails |
-
2012
- 2012-01-25 PL PL397899A patent/PL221113B1/en unknown
- 2012-03-26 US US13/430,603 patent/US20130189088A1/en not_active Abandoned
-
2013
- 2013-01-21 JP JP2013007964A patent/JP2013151934A/en active Pending
- 2013-01-23 RU RU2013102779/06A patent/RU2013102779A/en not_active Application Discontinuation
- 2013-01-23 EP EP13152397.9A patent/EP2620596A2/en not_active Withdrawn
- 2013-01-25 CN CN2013100287242A patent/CN103225520A/en active Pending
Also Published As
Publication number | Publication date |
---|---|
CN103225520A (en) | 2013-07-31 |
PL221113B1 (en) | 2016-02-29 |
EP2620596A2 (en) | 2013-07-31 |
US20130189088A1 (en) | 2013-07-25 |
JP2013151934A (en) | 2013-08-08 |
RU2013102779A (en) | 2014-07-27 |
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