BE673345A - - Google Patents
Info
- Publication number
- BE673345A BE673345A BE673345DA BE673345A BE 673345 A BE673345 A BE 673345A BE 673345D A BE673345D A BE 673345DA BE 673345 A BE673345 A BE 673345A
- Authority
- BE
- Belgium
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
- 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
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
-
- 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
-
- 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)
- Architecture (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US416387A US3269700A (en) | 1964-12-07 | 1964-12-07 | Heat shield for turbine strut |
Publications (1)
Publication Number | Publication Date |
---|---|
BE673345A true BE673345A (de) | 1966-04-01 |
Family
ID=23649762
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE673345D BE673345A (de) | 1964-12-07 | 1965-12-06 |
Country Status (5)
Country | Link |
---|---|
US (1) | US3269700A (de) |
BE (1) | BE673345A (de) |
DE (1) | DE1297938B (de) |
FR (1) | FR1457118A (de) |
GB (1) | GB1063240A (de) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009151701A2 (en) | 2008-03-18 | 2009-12-17 | United Technologies Corporation | Gas turbine engine systems involving fairings with locating data |
EP2218894A3 (de) * | 2009-02-16 | 2013-07-24 | Rolls-Royce plc | Anordnung zur Befestigung einer Leitschaufel |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3403889A (en) * | 1966-04-07 | 1968-10-01 | Gen Electric | Frame assembly having low thermal stresses |
US3529902A (en) * | 1968-05-22 | 1970-09-22 | Gen Motors Corp | Turbine vane |
GB2168111B (en) * | 1984-12-08 | 1988-05-18 | Rolls Royce | Rotor aerofoil blade containment |
US4820117A (en) * | 1987-07-09 | 1989-04-11 | United Technologies Corporation | Crossed I-beam structural strut |
US5085559A (en) * | 1990-04-16 | 1992-02-04 | The United States Of America As Represented By The Secretary Of The Air Force | Composite vane |
GB9202982D0 (en) * | 1992-02-13 | 1992-03-25 | Preci Spark Ltd | Reinforced vane |
US5509783A (en) * | 1993-02-09 | 1996-04-23 | Preci-Spark, Ltd. | Reinforced vane |
US6796765B2 (en) | 2001-12-27 | 2004-09-28 | General Electric Company | Methods and apparatus for assembling gas turbine engine struts |
US8366047B2 (en) * | 2005-05-31 | 2013-02-05 | United Technologies Corporation | Electrothermal inlet ice protection system |
US7950899B2 (en) * | 2005-05-31 | 2011-05-31 | United Technologies Corporation | Modular fan inlet case |
EP1930544A1 (de) * | 2006-10-30 | 2008-06-11 | Siemens Aktiengesellschaft | Turbinenschaufel |
GB2467791B (en) * | 2009-02-16 | 2011-06-01 | Rolls Royce Plc | Vane |
FR2981700B1 (fr) * | 2011-10-24 | 2016-08-26 | Snecma Propulsion Solide | Dispositif de fixation d'une piece creuse |
CN102400721B (zh) * | 2011-11-01 | 2014-04-02 | 沈阳黎明航空发动机(集团)有限责任公司 | 一种涡轮支承支点隔热屏的更换方法 |
CH705838A1 (de) * | 2011-12-05 | 2013-06-14 | Alstom Technology Ltd | Abgasgehäuse für eine Gasturbine sowie Gasturbine mit einem Abgasgehäuse. |
US9995160B2 (en) | 2014-12-22 | 2018-06-12 | General Electric Company | Airfoil profile-shaped seals and turbine components employing same |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2500745A (en) * | 1944-09-21 | 1950-03-14 | Gen Electric | Bucket structure for high-temperature turbomachines |
US2771622A (en) * | 1952-05-09 | 1956-11-27 | Westinghouse Electric Corp | Diaphragm apparatus |
BE529252A (de) * | 1953-06-01 |
-
1964
- 1964-12-07 US US416387A patent/US3269700A/en not_active Expired - Lifetime
-
1965
- 1965-12-02 GB GB51187/65A patent/GB1063240A/en not_active Expired
- 1965-12-06 FR FR4858A patent/FR1457118A/fr not_active Expired
- 1965-12-06 BE BE673345D patent/BE673345A/xx unknown
- 1965-12-07 DE DEU12250A patent/DE1297938B/de active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009151701A2 (en) | 2008-03-18 | 2009-12-17 | United Technologies Corporation | Gas turbine engine systems involving fairings with locating data |
WO2009151701A3 (en) * | 2008-03-18 | 2010-11-18 | United Technologies Corporation | Gas turbine engine systems with fairing |
EP2218894A3 (de) * | 2009-02-16 | 2013-07-24 | Rolls-Royce plc | Anordnung zur Befestigung einer Leitschaufel |
Also Published As
Publication number | Publication date |
---|---|
DE1297938B (de) | 1969-06-19 |
GB1063240A (en) | 1967-03-30 |
US3269700A (en) | 1966-08-30 |
FR1457118A (fr) | 1966-10-28 |