NL267395A - - Google Patents
Info
- Publication number
- NL267395A NL267395A NL267395DA NL267395A NL 267395 A NL267395 A NL 267395A NL 267395D A NL267395D A NL 267395DA NL 267395 A NL267395 A NL 267395A
- Authority
- NL
- Netherlands
Links
Classifications
-
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting means
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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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- 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
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
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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
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US44586A US3086363A (en) | 1960-07-22 | 1960-07-22 | Annular transition duct |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| NL267395A true NL267395A (xx) |
Family
ID=21933179
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NL267395D NL267395A (xx) | 1960-07-22 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US3086363A (xx) |
| BE (1) | BE606411A (xx) |
| CH (1) | CH402517A (xx) |
| GB (1) | GB924333A (xx) |
| NL (1) | NL267395A (xx) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4411134A (en) * | 1981-10-26 | 1983-10-25 | Moir David L | Apparatus for the repair and replacement of transition ducts on jet engines and bracket therefor |
| US4720236A (en) * | 1984-12-21 | 1988-01-19 | United Technologies Corporation | Coolable stator assembly for a gas turbine engine |
| US5274991A (en) * | 1992-03-30 | 1994-01-04 | General Electric Company | Dry low NOx multi-nozzle combustion liner cap assembly |
| DE69306025T2 (de) * | 1992-03-30 | 1997-05-28 | Gen Electric | Konstruktion eines Brennkammerdomes |
| EP1284391A1 (de) * | 2001-08-14 | 2003-02-19 | Siemens Aktiengesellschaft | Brennkammeranordnung für Gasturbinen |
| GB2402714A (en) * | 2003-06-12 | 2004-12-15 | Rolls Royce Plc | Cannular combustor with directly associated nozzle guide vanes |
| FR2887588B1 (fr) * | 2005-06-24 | 2011-06-03 | Snecma Moteurs | Interface ventilee entre une chambre de combustion et un distributeur haute pression de turboreacteur et turboreacteur comportant cette interface |
| US8091365B2 (en) * | 2008-08-12 | 2012-01-10 | Siemens Energy, Inc. | Canted outlet for transition in a gas turbine engine |
| EP2206885A1 (de) * | 2009-01-08 | 2010-07-14 | Siemens Aktiengesellschaft | Gasturbine |
| US8381526B2 (en) * | 2010-02-15 | 2013-02-26 | General Electric Company | Systems and methods of providing high pressure air to a head end of a combustor |
| FR3047544B1 (fr) * | 2016-02-10 | 2018-03-02 | Safran Aircraft Engines | Chambre de combustion de turbomachine |
| GB2571591B (en) * | 2018-03-03 | 2020-08-05 | Rolls Royce Plc | Rear outer discharge nozzle |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR963256A (xx) * | 1947-03-14 | 1950-07-05 | ||
| US2670600A (en) * | 1947-06-17 | 1954-03-02 | Bristol Aeroplane Co Ltd | Air distribution system for flame tubes of gas turbine engines |
| US2609663A (en) * | 1951-07-21 | 1952-09-09 | United Aircraft Corp | Rotatable combustion apparatus for aligning individual flame tubes with access partsor manholes |
| US2916874A (en) * | 1957-01-31 | 1959-12-15 | United Aircraft Corp | Engine construction |
-
0
- NL NL267395D patent/NL267395A/xx unknown
-
1960
- 1960-07-22 US US44586A patent/US3086363A/en not_active Expired - Lifetime
-
1961
- 1961-07-14 GB GB25564/61A patent/GB924333A/en not_active Expired
- 1961-07-20 BE BE606411A patent/BE606411A/fr unknown
- 1961-07-21 CH CH864461A patent/CH402517A/de unknown
Also Published As
| Publication number | Publication date |
|---|---|
| GB924333A (en) | 1963-04-24 |
| CH402517A (de) | 1965-11-15 |
| US3086363A (en) | 1963-04-23 |
| BE606411A (fr) | 1962-01-22 |