GB624285A - Improvements in or relating to combustion apparatus - Google Patents
Improvements in or relating to combustion apparatusInfo
- Publication number
- GB624285A GB624285A GB16899/47A GB1689947A GB624285A GB 624285 A GB624285 A GB 624285A GB 16899/47 A GB16899/47 A GB 16899/47A GB 1689947 A GB1689947 A GB 1689947A GB 624285 A GB624285 A GB 624285A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ribs
- wall
- walls
- relating
- combustion apparatus
- 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.)
- Expired
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
- F23R3/002—Wall structures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2260/00—Function
- F05B2260/20—Heat transfer, e.g. cooling
- F05B2260/221—Improvement of heat transfer
- F05B2260/224—Improvement of heat transfer by increasing the heat transfer surface
- F05B2260/2241—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
624,285. Generating combustion products under pressure. WESTINGHOUSE ELECTRIC INTERNATIONAL CO. June 26, 1947, No. 16899. Convention date, July 1, 1946. [Class 51 (i)] The frusto-conical walls 31, 32, Fig. 2, of the annular combustion chamber of a gas turbine plant are formed with diagonal fluted ribs 41 of U-shaped cross-section as shown in Fig. 3. The ribs in one wall may be inclined oppositely to those in the other wall. The ribs reinforce the walls and provide for expansion in both radial and longitudinal directions.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US624285XA | 1946-07-01 | 1946-07-01 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB624285A true GB624285A (en) | 1949-06-01 |
Family
ID=22042423
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB16899/47A Expired GB624285A (en) | 1946-07-01 | 1947-06-26 | Improvements in or relating to combustion apparatus |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB624285A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2716933A1 (en) * | 1994-03-03 | 1995-09-08 | Snecma | Thermal protection jacket element for a turbomachine and its manufacturing processes. |
WO1999006771A1 (en) * | 1997-07-31 | 1999-02-11 | Alliedsignal Inc. | Rib turbulators for combustor external cooling |
EP1391583A1 (en) * | 2002-08-23 | 2004-02-25 | MAN Turbomaschinen AG | Air cooled transition duct |
-
1947
- 1947-06-26 GB GB16899/47A patent/GB624285A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2716933A1 (en) * | 1994-03-03 | 1995-09-08 | Snecma | Thermal protection jacket element for a turbomachine and its manufacturing processes. |
WO1999006771A1 (en) * | 1997-07-31 | 1999-02-11 | Alliedsignal Inc. | Rib turbulators for combustor external cooling |
EP1391583A1 (en) * | 2002-08-23 | 2004-02-25 | MAN Turbomaschinen AG | Air cooled transition duct |
US6996992B2 (en) | 2002-08-23 | 2006-02-14 | Man Turbo Ag | Gas collection pipe carrying hot gas |
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