IT8124871A0 - Condotto di passaggio raffreddato efficacemente per una grande turbina a combustione per impianti. - Google Patents
Condotto di passaggio raffreddato efficacemente per una grande turbina a combustione per impianti.Info
- Publication number
- IT8124871A0 IT8124871A0 IT8124871A IT2487181A IT8124871A0 IT 8124871 A0 IT8124871 A0 IT 8124871A0 IT 8124871 A IT8124871 A IT 8124871A IT 2487181 A IT2487181 A IT 2487181A IT 8124871 A0 IT8124871 A0 IT 8124871A0
- Authority
- IT
- Italy
- Prior art keywords
- plants
- combustion turbine
- effectively cooled
- large combustion
- cooled connector
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title 1
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
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
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/002—Wall structures
-
- 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)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US20444180A | 1980-11-06 | 1980-11-06 |
Publications (2)
Publication Number | Publication Date |
---|---|
IT8124871A0 true IT8124871A0 (it) | 1981-11-05 |
IT1142046B IT1142046B (it) | 1986-10-08 |
Family
ID=22757890
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT24871/81A IT1142046B (it) | 1980-11-06 | 1981-11-05 | Condotto di passaggio raffreddato efficacemente per una grande turbina a combustione per impianti |
Country Status (8)
Country | Link |
---|---|
JP (1) | JPS6027816B2 (it) |
AR (1) | AR225977A1 (it) |
BE (1) | BE891023A (it) |
BR (1) | BR8106793A (it) |
CA (1) | CA1183695A (it) |
GB (1) | GB2087066B (it) |
IT (1) | IT1142046B (it) |
MX (1) | MX154157A (it) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0752014B2 (ja) * | 1986-03-20 | 1995-06-05 | 株式会社日立製作所 | ガスタ−ビン燃焼器 |
US6018950A (en) * | 1997-06-13 | 2000-02-01 | Siemens Westinghouse Power Corporation | Combustion turbine modular cooling panel |
CA2288557C (en) * | 1998-11-12 | 2007-02-06 | Mitsubishi Heavy Industries, Ltd. | Gas turbine combustor cooling structure |
US6412268B1 (en) * | 2000-04-06 | 2002-07-02 | General Electric Company | Cooling air recycling for gas turbine transition duct end frame and related method |
US7310938B2 (en) * | 2004-12-16 | 2007-12-25 | Siemens Power Generation, Inc. | Cooled gas turbine transition duct |
US8015818B2 (en) | 2005-02-22 | 2011-09-13 | Siemens Energy, Inc. | Cooled transition duct for a gas turbine engine |
JP2010085052A (ja) * | 2008-10-01 | 2010-04-15 | Mitsubishi Heavy Ind Ltd | 燃焼器尾筒およびその設計方法ならびにガスタービン |
-
1981
- 1981-10-08 GB GB8130376A patent/GB2087066B/en not_active Expired
- 1981-10-13 MX MX189619A patent/MX154157A/es unknown
- 1981-10-19 CA CA000388209A patent/CA1183695A/en not_active Expired
- 1981-10-22 BR BR8106793A patent/BR8106793A/pt unknown
- 1981-10-30 AR AR287296A patent/AR225977A1/es active
- 1981-11-05 IT IT24871/81A patent/IT1142046B/it active
- 1981-11-06 JP JP56177265A patent/JPS6027816B2/ja not_active Expired
- 1981-11-06 BE BE0/206466A patent/BE891023A/fr not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
IT1142046B (it) | 1986-10-08 |
GB2087066A (en) | 1982-05-19 |
BR8106793A (pt) | 1982-07-06 |
JPS57113923A (en) | 1982-07-15 |
CA1183695A (en) | 1985-03-12 |
AR225977A1 (es) | 1982-05-14 |
JPS6027816B2 (ja) | 1985-07-01 |
GB2087066B (en) | 1984-09-19 |
BE891023A (fr) | 1982-05-06 |
MX154157A (es) | 1987-05-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19931119 |