BE692211A - - Google Patents
Info
- Publication number
- BE692211A BE692211A BE692211DA BE692211A BE 692211 A BE692211 A BE 692211A BE 692211D A BE692211D A BE 692211DA BE 692211 A BE692211 A BE 692211A
- 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
- 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
- F01D5/187—Convection cooling
- F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
-
- 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)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US540967A US3369792A (en) | 1966-04-07 | 1966-04-07 | Airfoil vane |
Publications (1)
Publication Number | Publication Date |
---|---|
BE692211A true BE692211A (pl) | 1967-07-05 |
Family
ID=24157651
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE692211D BE692211A (pl) | 1966-04-07 | 1967-01-05 |
Country Status (8)
Country | Link |
---|---|
US (1) | US3369792A (pl) |
BE (1) | BE692211A (pl) |
CH (1) | CH470575A (pl) |
DE (1) | DE1476804A1 (pl) |
FR (1) | FR1504913A (pl) |
GB (1) | GB1115948A (pl) |
NL (1) | NL6700156A (pl) |
SE (1) | SE307263B (pl) |
Families Citing this family (40)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3630707A (en) * | 1969-06-11 | 1971-12-28 | Corning Glass Works | Temperature control system for glass-shaping molds |
US3628885A (en) * | 1969-10-01 | 1971-12-21 | Gen Electric | Fluid-cooled airfoil |
CH582305A5 (pl) * | 1974-09-05 | 1976-11-30 | Bbc Sulzer Turbomaschinen | |
US4153386A (en) * | 1974-12-11 | 1979-05-08 | United Technologies Corporation | Air cooled turbine vanes |
US4025226A (en) * | 1975-10-03 | 1977-05-24 | United Technologies Corporation | Air cooled turbine vane |
US4063851A (en) * | 1975-12-22 | 1977-12-20 | United Technologies Corporation | Coolable turbine airfoil |
US4073599A (en) * | 1976-08-26 | 1978-02-14 | Westinghouse Electric Corporation | Hollow turbine blade tip closure |
US4236870A (en) * | 1977-12-27 | 1980-12-02 | United Technologies Corporation | Turbine blade |
US4257734A (en) * | 1978-03-22 | 1981-03-24 | Rolls-Royce Limited | Guide vanes for gas turbine engines |
FR2468727A1 (fr) * | 1979-10-26 | 1981-05-08 | Snecma | Perfectionnement aux aubes de turbine refroidies |
US4930980A (en) * | 1989-02-15 | 1990-06-05 | Westinghouse Electric Corp. | Cooled turbine vane |
US5407321A (en) * | 1993-11-29 | 1995-04-18 | United Technologies Corporation | Damping means for hollow stator vane airfoils |
GB9402442D0 (en) * | 1994-02-09 | 1994-04-20 | Rolls Royce Plc | Cooling air cooled gas turbine aerofoil |
US5507621A (en) * | 1995-01-30 | 1996-04-16 | Rolls-Royce Plc | Cooling air cooled gas turbine aerofoil |
US6132169A (en) * | 1998-12-18 | 2000-10-17 | General Electric Company | Turbine airfoil and methods for airfoil cooling |
US6238182B1 (en) * | 1999-02-19 | 2001-05-29 | Meyer Tool, Inc. | Joint for a turbine component |
KR20010020925A (ko) | 1999-08-11 | 2001-03-15 | 제이 엘. 차스킨, 버나드 스나이더, 아더엠. 킹 | 가동성 노즐 리브를 갖는 노즐 날개 |
DE19963716A1 (de) | 1999-12-29 | 2001-07-05 | Alstom Power Schweiz Ag Baden | Gekühlte Strömungsumlenkvorrichtung für eine bei hohen Temperaturen arbeitende Strömungsmaschine |
DE10215375A1 (de) * | 2002-04-08 | 2003-10-16 | Siemens Ag | Turbinenlaufschaufel |
DE10217389A1 (de) * | 2002-04-18 | 2003-10-30 | Siemens Ag | Turbinenschaufel |
US6932570B2 (en) * | 2002-05-23 | 2005-08-23 | General Electric Company | Methods and apparatus for extending gas turbine engine airfoils useful life |
US6746209B2 (en) | 2002-05-31 | 2004-06-08 | General Electric Company | Methods and apparatus for cooling gas turbine engine nozzle assemblies |
US6884036B2 (en) * | 2003-04-15 | 2005-04-26 | General Electric Company | Complementary cooled turbine nozzle |
US6955523B2 (en) * | 2003-08-08 | 2005-10-18 | Siemens Westinghouse Power Corporation | Cooling system for a turbine vane |
US6923616B2 (en) * | 2003-09-02 | 2005-08-02 | General Electric Company | Methods and apparatus for cooling gas turbine engine rotor assemblies |
US7600972B2 (en) * | 2003-10-31 | 2009-10-13 | General Electric Company | Methods and apparatus for cooling gas turbine engine rotor assemblies |
US6984112B2 (en) * | 2003-10-31 | 2006-01-10 | General Electric Company | Methods and apparatus for cooling gas turbine rotor blades |
US7150601B2 (en) * | 2004-12-23 | 2006-12-19 | United Technologies Corporation | Turbine airfoil cooling passageway |
US7762784B2 (en) * | 2007-01-11 | 2010-07-27 | United Technologies Corporation | Insertable impingement rib |
GB2467791B (en) * | 2009-02-16 | 2011-06-01 | Rolls Royce Plc | Vane |
US7824150B1 (en) * | 2009-05-15 | 2010-11-02 | Florida Turbine Technologies, Inc. | Multiple piece turbine airfoil |
CN102741675B (zh) | 2010-01-15 | 2015-11-25 | 斯凯旺蒂尔国际(英国)有限责任公司 | 风洞导流叶片热交换器 |
US8702375B1 (en) * | 2011-05-19 | 2014-04-22 | Florida Turbine Technologies, Inc. | Turbine stator vane |
WO2015012918A2 (en) * | 2013-06-04 | 2015-01-29 | United Technologies Corporation | Gas turbine engine airfoil trailing edge suction side cooling |
US10138735B2 (en) * | 2015-11-04 | 2018-11-27 | General Electric Company | Turbine airfoil internal core profile |
US10408090B2 (en) * | 2016-11-17 | 2019-09-10 | United Technologies Corporation | Gas turbine engine article with panel retained by preloaded compliant member |
US10544682B2 (en) * | 2017-08-14 | 2020-01-28 | United Technologies Corporation | Expansion seals for airfoils |
US11242760B2 (en) * | 2020-01-22 | 2022-02-08 | General Electric Company | Turbine rotor blade with integral impingement sleeve by additive manufacture |
US11365636B2 (en) * | 2020-05-25 | 2022-06-21 | General Electric Company | Fan blade with intrinsic damping characteristics |
US11898463B2 (en) * | 2021-03-29 | 2024-02-13 | Rtx Corporation | Airfoil assembly with fiber-reinforced composite rings |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2647368A (en) * | 1949-05-09 | 1953-08-04 | Hermann Oestrich | Method and apparatus for internally cooling gas turbine blades with air, fuel, and water |
US2866616A (en) * | 1951-03-02 | 1958-12-30 | Stalker Dev Company | Fabricated bladed structures for axial flow machines |
US2817490A (en) * | 1951-10-10 | 1957-12-24 | Gen Motors Corp | Turbine bucket with internal fins |
US2801071A (en) * | 1952-01-31 | 1957-07-30 | Westinghouse Electric Corp | Bladed rotor construction |
US2801073A (en) * | 1952-06-30 | 1957-07-30 | United Aircraft Corp | Hollow sheet metal blade or vane construction |
US2873944A (en) * | 1952-09-10 | 1959-02-17 | Gen Motors Corp | Turbine blade cooling |
US2859011A (en) * | 1953-07-27 | 1958-11-04 | Gen Motors Corp | Turbine bucket and liner |
US2840298A (en) * | 1954-08-09 | 1958-06-24 | Gen Motors Corp | Heated compressor vane |
US2906495A (en) * | 1955-04-29 | 1959-09-29 | Eugene F Schum | Turbine blade with corrugated strut |
US2923525A (en) * | 1958-04-04 | 1960-02-02 | Orenda Engines Ltd | Hollow gas turbine blade |
US3095180A (en) * | 1959-03-05 | 1963-06-25 | Stalker Corp | Blades for compressors, turbines and the like |
-
1966
- 1966-04-07 US US540967A patent/US3369792A/en not_active Expired - Lifetime
- 1966-11-22 DE DE19661476804 patent/DE1476804A1/de active Pending
- 1966-11-23 GB GB51495/66A patent/GB1115948A/en not_active Expired
- 1966-12-06 FR FR86382A patent/FR1504913A/fr not_active Expired
- 1966-12-14 SE SE17143/66A patent/SE307263B/xx unknown
-
1967
- 1967-01-04 CH CH5567A patent/CH470575A/de not_active IP Right Cessation
- 1967-01-05 NL NL6700156A patent/NL6700156A/xx unknown
- 1967-01-05 BE BE692211D patent/BE692211A/xx unknown
Also Published As
Publication number | Publication date |
---|---|
SE307263B (pl) | 1968-12-23 |
DE1476804A1 (de) | 1970-03-26 |
NL6700156A (pl) | 1967-10-09 |
FR1504913A (fr) | 1967-12-08 |
CH470575A (de) | 1969-03-31 |
US3369792A (en) | 1968-02-20 |
GB1115948A (en) | 1968-06-06 |