GB0305458D0 - Enhancement of heat transfer - Google Patents
Enhancement of heat transferInfo
- Publication number
- GB0305458D0 GB0305458D0 GBGB0305458.2A GB0305458A GB0305458D0 GB 0305458 D0 GB0305458 D0 GB 0305458D0 GB 0305458 A GB0305458 A GB 0305458A GB 0305458 D0 GB0305458 D0 GB 0305458D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- enhancement
- heat transfer
- transfer
- heat
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F13/00—Arrangements for modifying heat-transfer, e.g. increasing, decreasing
- F28F13/18—Arrangements for modifying heat-transfer, e.g. increasing, decreasing by applying coatings, e.g. radiation-absorbing, radiation-reflecting; by surface treatment, e.g. polishing
- F28F13/185—Heat-exchange surfaces provided with microstructures or with porous coatings
-
- 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
-
- 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
- F05D2260/221—Improvement of heat transfer
- F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
- F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/40—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only inside the tubular element
-
- 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)
- Crystallography & Structural Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0305458A GB2399405A (en) | 2003-03-10 | 2003-03-10 | Enhancement of heat transfer |
DE102004010747A DE102004010747A1 (en) | 2003-03-10 | 2004-03-05 | Reinforcement of heat transfer |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0305458A GB2399405A (en) | 2003-03-10 | 2003-03-10 | Enhancement of heat transfer |
Publications (2)
Publication Number | Publication Date |
---|---|
GB0305458D0 true GB0305458D0 (en) | 2003-04-16 |
GB2399405A GB2399405A (en) | 2004-09-15 |
Family
ID=9954478
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0305458A Withdrawn GB2399405A (en) | 2003-03-10 | 2003-03-10 | Enhancement of heat transfer |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE102004010747A1 (en) |
GB (1) | GB2399405A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112105800A (en) * | 2018-05-29 | 2020-12-18 | 赛峰飞机发动机公司 | Turbine blade comprising an internal fluid flow channel equipped with a plurality of optimally arranged disrupting elements |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7690893B2 (en) * | 2006-07-25 | 2010-04-06 | United Technologies Corporation | Leading edge cooling with microcircuit anti-coriolis device |
DE102011088709A1 (en) * | 2011-12-15 | 2013-06-13 | Continental Automotive Gmbh | Housing for electric machine, has coolant duct which is provided with turbulence bar for generating turbulence in the cooling liquid transverse to the flow direction of the cooling liquid |
DE102013102181B3 (en) | 2013-03-05 | 2014-05-15 | Phitea GmbH | Flow body with low-friction surface structure and method for modifying the surface of a flow body |
US20150152738A1 (en) * | 2013-12-02 | 2015-06-04 | George Liang | Turbine airfoil cooling passage with diamond turbulator |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4514144A (en) * | 1983-06-20 | 1985-04-30 | General Electric Company | Angled turbulence promoter |
FR2694080B1 (en) * | 1992-07-24 | 1996-06-21 | Furukawa Electric Co Ltd | FLAT AND POROUS CONDENSER TUBE. |
US5797726A (en) * | 1997-01-03 | 1998-08-25 | General Electric Company | Turbulator configuration for cooling passages or rotor blade in a gas turbine engine |
JP3586637B2 (en) * | 2000-10-27 | 2004-11-10 | 三菱重工業株式会社 | Gas turbine blade cooling structure |
-
2003
- 2003-03-10 GB GB0305458A patent/GB2399405A/en not_active Withdrawn
-
2004
- 2004-03-05 DE DE102004010747A patent/DE102004010747A1/en not_active Withdrawn
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112105800A (en) * | 2018-05-29 | 2020-12-18 | 赛峰飞机发动机公司 | Turbine blade comprising an internal fluid flow channel equipped with a plurality of optimally arranged disrupting elements |
CN112105800B (en) * | 2018-05-29 | 2023-04-07 | 赛峰飞机发动机公司 | Aircraft turbine blade, additive manufacturing method thereof and aircraft engine |
Also Published As
Publication number | Publication date |
---|---|
DE102004010747A1 (en) | 2004-10-07 |
GB2399405A (en) | 2004-09-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
COOA | Change in applicant's name or ownership of the application |
Owner name: ALSTOM TECHNOLOGY LTD Free format text: FORMER APPLICANT(S): ALSTOM (SWITZERLAND) LTD |
|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |