BE759458A - IMPROVED DAWN STRUCTURE FOR TURBOMACHINES - Google Patents
IMPROVED DAWN STRUCTURE FOR TURBOMACHINESInfo
- Publication number
- BE759458A BE759458A BE759458DA BE759458A BE 759458 A BE759458 A BE 759458A BE 759458D A BE759458D A BE 759458DA BE 759458 A BE759458 A BE 759458A
- Authority
- BE
- Belgium
- Prior art keywords
- turbomachines
- dawn
- improved
- improved dawn
- dawn structure
- Prior art date
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
- F01D5/189—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US75273668A | 1968-08-13 | 1968-08-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
BE759458A true BE759458A (en) | 1971-01-01 |
Family
ID=25027599
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE759458D BE759458A (en) | 1968-08-13 | 1970-11-26 | IMPROVED DAWN STRUCTURE FOR TURBOMACHINES |
Country Status (2)
Country | Link |
---|---|
US (1) | US3700348A (en) |
BE (1) | BE759458A (en) |
Families Citing this family (39)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1304678A (en) * | 1971-06-30 | 1973-01-24 | ||
GB1355558A (en) * | 1971-07-02 | 1974-06-05 | Rolls Royce | Cooled vane or blade for a gas turbine engine |
US3982854A (en) * | 1971-12-20 | 1976-09-28 | General Electric Company | Friction welded metallic turbomachinery blade element |
GB1400285A (en) * | 1972-08-02 | 1975-07-16 | Rolls Royce | Hollow cooled vane or blade for a gas turbine engine |
US3934322A (en) * | 1972-09-21 | 1976-01-27 | General Electric Company | Method for forming cooling slot in airfoil blades |
US3819295A (en) * | 1972-09-21 | 1974-06-25 | Gen Electric | Cooling slot for airfoil blade |
US3846041A (en) * | 1972-10-31 | 1974-11-05 | Avco Corp | Impingement cooled turbine blades and method of making same |
US3866448A (en) * | 1973-01-02 | 1975-02-18 | Gen Electric | Apparatus for constructing air cooled turbomachinery blading |
US3921271A (en) * | 1973-01-02 | 1975-11-25 | Gen Electric | Air-cooled turbine blade and method of making same |
US3834831A (en) * | 1973-01-23 | 1974-09-10 | Westinghouse Electric Corp | Blade shank cooling arrangement |
US3867068A (en) * | 1973-03-30 | 1975-02-18 | Gen Electric | Turbomachinery blade cooling insert retainers |
US3902820A (en) * | 1973-07-02 | 1975-09-02 | Westinghouse Electric Corp | Fluid cooled turbine rotor blade |
US3864199A (en) * | 1973-07-26 | 1975-02-04 | Gen Motors Corp | Angular discharge porous sheet |
JPS5048309A (en) * | 1973-08-31 | 1975-04-30 | ||
US3966357A (en) * | 1974-09-25 | 1976-06-29 | General Electric Company | Blade baffle damper |
US3973874A (en) * | 1974-09-25 | 1976-08-10 | General Electric Company | Impingement baffle collars |
US3994622A (en) * | 1975-11-24 | 1976-11-30 | United Technologies Corporation | Coolable turbine blade |
GB1564608A (en) * | 1975-12-20 | 1980-04-10 | Rolls Royce | Means for cooling a surface by the impingement of a cooling fluid |
JPS5390509A (en) * | 1977-01-20 | 1978-08-09 | Koukuu Uchiyuu Gijiyutsu Kenki | Structure of air cooled turbine blade |
DE3003347A1 (en) * | 1979-12-20 | 1981-06-25 | BBC AG Brown, Boveri & Cie., Baden, Aargau | COOLED WALL |
GB2237846B (en) * | 1989-11-09 | 1993-12-15 | Rolls Royce Plc | Rim parasitic weight reduction |
FR2798422B1 (en) * | 1990-01-24 | 2002-07-26 | United Technologies Corp | COOLED BLADES FOR A GAS TURBINE ENGINE |
US6237344B1 (en) | 1998-07-20 | 2001-05-29 | General Electric Company | Dimpled impingement baffle |
US6193465B1 (en) * | 1998-09-28 | 2001-02-27 | General Electric Company | Trapped insert turbine airfoil |
US6238182B1 (en) | 1999-02-19 | 2001-05-29 | Meyer Tool, Inc. | Joint for a turbine component |
US6742984B1 (en) * | 2003-05-19 | 2004-06-01 | General Electric Company | Divided insert for steam cooled nozzles and method for supporting and separating divided insert |
EP1953342A1 (en) * | 2007-02-01 | 2008-08-06 | Siemens Aktiengesellschaft | Turbine blade |
US7695245B1 (en) * | 2007-03-06 | 2010-04-13 | Florida Turbine Technologies, Inc. | Turbine airfoil with a multi-impingement cooled spar and shell |
US8449249B2 (en) | 2010-04-09 | 2013-05-28 | Williams International Co., L.L.C. | Turbine nozzle apparatus and associated method of manufacture |
US8622702B1 (en) | 2010-04-21 | 2014-01-07 | Florida Turbine Technologies, Inc. | Turbine blade with cooling air inlet holes |
EP2383435A1 (en) * | 2010-04-29 | 2011-11-02 | Siemens Aktiengesellschaft | Turbine vane hollow inner rail |
US9567859B2 (en) * | 2013-03-14 | 2017-02-14 | General Electric Company | Cooling passages for turbine buckets of a gas turbine engine |
US20160222796A1 (en) * | 2013-09-18 | 2016-08-04 | United Technologies Corporation | Manufacturing method for a baffle-containing blade |
US20150198050A1 (en) * | 2014-01-15 | 2015-07-16 | Siemens Energy, Inc. | Internal cooling system with corrugated insert forming nearwall cooling channels for airfoil usable in a gas turbine engine |
JP6651378B2 (en) * | 2016-02-22 | 2020-02-19 | 三菱日立パワーシステムズ株式会社 | Insert assembly, blade, gas turbine, and method of manufacturing blade |
US10738622B2 (en) | 2016-08-09 | 2020-08-11 | General Electric Company | Components having outer wall recesses for impingement cooling |
CN107416184A (en) * | 2017-08-01 | 2017-12-01 | 西华酷农无人机产业园运营有限公司 | A kind of unmanned plane propeller of high efficiency and heat radiation |
JP7003265B2 (en) * | 2017-12-01 | 2022-01-20 | シーメンス エナジー インコーポレイテッド | Brazing heat transfer mechanism for cooling turbine parts |
US11149568B2 (en) * | 2018-12-20 | 2021-10-19 | Rolls-Royce Plc | Sliding ceramic matrix composite vane assembly for gas turbine engines |
Family Cites Families (5)
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 |
GB685769A (en) * | 1949-11-22 | 1953-01-14 | Rolls Royce | Improvements relating to compressor and turbine blading |
DE926397C (en) * | 1952-09-25 | 1955-04-18 | Ernst Heinkel Dr Dr | Hollow blade, preferably for axially flowed turbines |
DE1069153B (en) * | 1956-03-14 | 1959-11-19 | D. Naoier S. Son Limited, London | Hollow blades for turbines or compressors |
FR1177035A (en) * | 1957-05-28 | 1959-04-20 | Snecma | Method and device for cooling machine parts |
-
1968
- 1968-08-13 US US752736A patent/US3700348A/en not_active Expired - Lifetime
-
1970
- 1970-11-26 BE BE759458D patent/BE759458A/en unknown
Also Published As
Publication number | Publication date |
---|---|
US3700348A (en) | 1972-10-24 |
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