IN2015DN00993A - - Google Patents
Info
- Publication number
- IN2015DN00993A IN2015DN00993A IN993DEN2015A IN2015DN00993A IN 2015DN00993 A IN2015DN00993 A IN 2015DN00993A IN 993DEN2015 A IN993DEN2015 A IN 993DEN2015A IN 2015DN00993 A IN2015DN00993 A IN 2015DN00993A
- Authority
- IN
- India
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
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- 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
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/602,480 US20140060001A1 (en) | 2012-09-04 | 2012-09-04 | Gas turbine engine with shortened mid section |
| PCT/US2013/055782 WO2014039246A1 (en) | 2012-09-04 | 2013-08-20 | Gas turbine engine with shortened mid section |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| IN2015DN00993A true IN2015DN00993A (en) | 2015-06-12 |
Family
ID=49081013
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IN993DEN2015 IN2015DN00993A (en) | 2012-09-04 | 2015-02-06 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US20140060001A1 (en) |
| EP (1) | EP2893151A1 (en) |
| JP (1) | JP2015526691A (en) |
| CN (1) | CN104812995A (en) |
| IN (1) | IN2015DN00993A (en) |
| RU (1) | RU2015106468A (en) |
| WO (1) | WO2014039246A1 (en) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20130081407A1 (en) * | 2011-10-04 | 2013-04-04 | David J. Wiebe | Aero-derivative gas turbine engine with an advanced transition duct combustion assembly |
| US9127554B2 (en) * | 2012-09-04 | 2015-09-08 | Siemens Energy, Inc. | Gas turbine engine with radial diffuser and shortened mid section |
| EP3023695A1 (en) * | 2014-11-20 | 2016-05-25 | Siemens Aktiengesellschaft | Thermal energy machine |
| US10145251B2 (en) | 2016-03-24 | 2018-12-04 | General Electric Company | Transition duct assembly |
| US10260752B2 (en) | 2016-03-24 | 2019-04-16 | General Electric Company | Transition duct assembly with late injection features |
| US10260360B2 (en) | 2016-03-24 | 2019-04-16 | General Electric Company | Transition duct assembly |
| US10260424B2 (en) | 2016-03-24 | 2019-04-16 | General Electric Company | Transition duct assembly with late injection features |
| US10227883B2 (en) | 2016-03-24 | 2019-03-12 | General Electric Company | Transition duct assembly |
Family Cites Families (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3546880A (en) * | 1969-08-04 | 1970-12-15 | Avco Corp | Compressors for gas turbine engines |
| US3631674A (en) * | 1970-01-19 | 1972-01-04 | Gen Electric | Folded flow combustion chamber for a gas turbine engine |
| US4896499A (en) * | 1978-10-26 | 1990-01-30 | Rice Ivan G | Compression intercooled gas turbine combined cycle |
| US5252860A (en) * | 1989-12-11 | 1993-10-12 | Westinghouse Electric Corp. | Gas turbine control system having maximum instantaneous load-pickup limiter |
| JP2904701B2 (en) * | 1993-12-15 | 1999-06-14 | 株式会社日立製作所 | Gas turbine and gas turbine combustion device |
| GB9415685D0 (en) * | 1994-08-03 | 1994-09-28 | Rolls Royce Plc | A gas turbine engine and a diffuser therefor |
| US5737915A (en) * | 1996-02-09 | 1998-04-14 | General Electric Co. | Tri-passage diffuser for a gas turbine |
| US6672072B1 (en) * | 1998-08-17 | 2004-01-06 | General Electric Company | Pressure boosted compressor cooling system |
| US6606864B2 (en) * | 2001-02-13 | 2003-08-19 | Robin Mackay | Advanced multi pressure mode gas turbine |
| JP2005042973A (en) * | 2003-07-22 | 2005-02-17 | Kawasaki Heavy Ind Ltd | Gas turbine with swirl type combustor |
| US7721547B2 (en) * | 2005-06-27 | 2010-05-25 | Siemens Energy, Inc. | Combustion transition duct providing stage 1 tangential turning for turbine engines |
| US20090266047A1 (en) * | 2007-11-15 | 2009-10-29 | General Electric Company | Multi-tube, can-annular pulse detonation combustor based engine with tangentially and longitudinally angled pulse detonation combustors |
| JP5010521B2 (en) * | 2008-03-28 | 2012-08-29 | 三菱重工業株式会社 | Combustor transition piece guide jig, gas turbine combustor removal method, and manufacturing method |
| JP5276345B2 (en) * | 2008-03-28 | 2013-08-28 | 三菱重工業株式会社 | Gas turbine and gas turbine combustor insertion hole forming method |
| CN101275750B (en) * | 2008-04-25 | 2010-12-08 | 北京航空航天大学 | Radial swirler turning zone direct injection premixing and prevapourising low pollution burning chamber |
| US8230688B2 (en) | 2008-09-29 | 2012-07-31 | Siemens Energy, Inc. | Modular transvane assembly |
| US8276389B2 (en) * | 2008-09-29 | 2012-10-02 | Siemens Energy, Inc. | Assembly for directing combustion gas |
| US9388738B2 (en) * | 2011-10-04 | 2016-07-12 | Siemens Energy, Inc. | Casing for a gas turbine engine |
| US9127554B2 (en) * | 2012-09-04 | 2015-09-08 | Siemens Energy, Inc. | Gas turbine engine with radial diffuser and shortened mid section |
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2012
- 2012-09-04 US US13/602,480 patent/US20140060001A1/en not_active Abandoned
-
2013
- 2013-08-20 JP JP2015529858A patent/JP2015526691A/en active Pending
- 2013-08-20 WO PCT/US2013/055782 patent/WO2014039246A1/en active Application Filing
- 2013-08-20 CN CN201380046098.8A patent/CN104812995A/en active Pending
- 2013-08-20 EP EP13753781.7A patent/EP2893151A1/en not_active Withdrawn
- 2013-08-20 RU RU2015106468A patent/RU2015106468A/en unknown
-
2015
- 2015-02-06 IN IN993DEN2015 patent/IN2015DN00993A/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| US20140060001A1 (en) | 2014-03-06 |
| JP2015526691A (en) | 2015-09-10 |
| EP2893151A1 (en) | 2015-07-15 |
| RU2015106468A (en) | 2016-10-27 |
| WO2014039246A1 (en) | 2014-03-13 |
| CN104812995A (en) | 2015-07-29 |