GB844068A - Improvements relating to turbine and compressor blades - Google Patents
Improvements relating to turbine and compressor bladesInfo
- Publication number
- GB844068A GB844068A GB18195/57A GB1819557A GB844068A GB 844068 A GB844068 A GB 844068A GB 18195/57 A GB18195/57 A GB 18195/57A GB 1819557 A GB1819557 A GB 1819557A GB 844068 A GB844068 A GB 844068A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- holes
- turbine
- tip
- passages
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/02—Making uncoated products
- B21C23/04—Making uncoated products by direct extrusion
- B21C23/14—Making other products
- B21C23/16—Making turbo blades or propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/22—Making metal-coated products; Making products from two or more metals
- B21C23/24—Covering indefinite lengths of metal or non-metal material with a metal coating
- B21C23/26—Applying metal coats to cables, e.g. to insulated electric cables
-
- 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
- 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
- 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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
-
- 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
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/24—Manufacture essentially without removing material by extrusion
-
- 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)
- Materials Engineering (AREA)
- Architecture (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
Abstract
844,068. Making turbine and like blades. WIGGIN & CO. Ltd., H. May 23, 1958 [June 7, 1957], No. 18195/57. Class 83 (2). [Also in Group XXVI] A turbine or compressor blade comprises longitudinal cooling passages arranged in pairs, the two passages of each pair merging into one another close to the tip of the blade. The blade may be made by partial extrusion of a billet 1, Fig. 1, in which the holes have been drilled and filled with a filler which flows with the metal of the billet during the extrusion, and is then subsequently leached out by acid. In Fig. 6, the cooling passages consist of holes 4, 5 merging into each other close to the tip and holes 6, 7 meeting each other in the root of the blade thus forming a diamond pattern. At one or both edges of the blade are one or more single holes 2, Fig. 1. A modification, Fig. 11, has a slot 11 which is formed by machining (e.g. spark erosion) the single row of passages at the blade tip.
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BE568389D BE568389A (en) | 1957-06-07 | ||
NL228237D NL228237A (en) | 1957-06-07 | ||
NL104493D NL104493C (en) | 1957-06-07 | ||
GB18195/57A GB844068A (en) | 1957-06-07 | 1957-06-07 | Improvements relating to turbine and compressor blades |
US736637A US3014693A (en) | 1957-06-07 | 1958-05-20 | Turbine and compressor blades |
DEW23414A DE1081276B (en) | 1957-06-07 | 1958-05-30 | Blade for turbines or compressors |
FR1196738D FR1196738A (en) | 1957-06-07 | 1958-06-06 | Improvements to turbine and compressor fins |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB18195/57A GB844068A (en) | 1957-06-07 | 1957-06-07 | Improvements relating to turbine and compressor blades |
Publications (1)
Publication Number | Publication Date |
---|---|
GB844068A true GB844068A (en) | 1960-08-10 |
Family
ID=10108284
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB18195/57A Expired GB844068A (en) | 1957-06-07 | 1957-06-07 | Improvements relating to turbine and compressor blades |
Country Status (6)
Country | Link |
---|---|
US (1) | US3014693A (en) |
BE (1) | BE568389A (en) |
DE (1) | DE1081276B (en) |
FR (1) | FR1196738A (en) |
GB (1) | GB844068A (en) |
NL (2) | NL104493C (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10330112B2 (en) * | 2013-12-30 | 2019-06-25 | United Technologies Corporation | Fan blade with root through holes |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3420502A (en) * | 1962-09-04 | 1969-01-07 | Gen Electric | Fluid-cooled airfoil |
CH580750A5 (en) * | 1974-07-17 | 1976-10-15 | Bbc Sulzer Turbomaschinen | |
US5980209A (en) * | 1997-06-27 | 1999-11-09 | General Electric Co. | Turbine blade with enhanced cooling and profile optimization |
US7357623B2 (en) * | 2005-05-23 | 2008-04-15 | Pratt & Whitney Canada Corp. | Angled cooling divider wall in blade attachment |
US7901182B2 (en) * | 2007-05-18 | 2011-03-08 | Siemens Energy, Inc. | Near wall cooling for a highly tapered turbine blade |
US8740567B2 (en) | 2010-07-26 | 2014-06-03 | United Technologies Corporation | Reverse cavity blade for a gas turbine engine |
EP2853689A1 (en) * | 2013-09-25 | 2015-04-01 | Siemens Aktiengesellschaft | Arrangement of cooling channels in a turbine blade |
US11542820B2 (en) | 2017-12-06 | 2023-01-03 | General Electric Company | Turbomachinery blade and method of fabricating |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1657192A (en) * | 1923-03-22 | 1928-01-24 | Belluzzo Giuseppe | Wheel for internal-combustion turbines |
DE597556C (en) * | 1931-12-29 | |||
CH195736A (en) * | 1936-11-24 | 1938-02-15 | Alfred Buechi | Turbine rotor with at least one impeller. |
US2514525A (en) * | 1944-03-09 | 1950-07-11 | Curtiss Wright Corp | Method of producing blade constructions and propeller blades |
US2440127A (en) * | 1944-07-31 | 1948-04-20 | Curtiss Wright Corp | Art of producing propeller blades |
FR949459A (en) * | 1947-07-09 | 1949-08-31 | Blades for rotors | |
US2648520A (en) * | 1949-08-02 | 1953-08-11 | Heinz E Schmitt | Air-cooled turbine blade |
GB694241A (en) * | 1950-04-18 | 1953-07-15 | Rolls Royce | Improvements relating to turbine blades |
US2778601A (en) * | 1951-05-28 | 1957-01-22 | Ernst R G Eckert | Fluid cooled turbine blade construction |
US2787441A (en) * | 1952-03-05 | 1957-04-02 | Thompson Prod Inc | Hollow turbine bucket |
US2780435A (en) * | 1953-01-12 | 1957-02-05 | Jackson Thomas Woodrow | Turbine blade cooling structure |
US2848193A (en) * | 1953-04-08 | 1958-08-19 | Gen Electric | Air cooled turbomachine blading |
DE1066387B (en) * | 1955-03-01 | 1959-10-01 | ||
BE555897A (en) * | 1956-05-07 | |||
US2972182A (en) * | 1957-02-22 | 1961-02-21 | Rolls Royce | Turbine and compressor blades |
-
0
- NL NL228237D patent/NL228237A/xx unknown
- NL NL104493D patent/NL104493C/xx active
- BE BE568389D patent/BE568389A/xx unknown
-
1957
- 1957-06-07 GB GB18195/57A patent/GB844068A/en not_active Expired
-
1958
- 1958-05-20 US US736637A patent/US3014693A/en not_active Expired - Lifetime
- 1958-05-30 DE DEW23414A patent/DE1081276B/en active Pending
- 1958-06-06 FR FR1196738D patent/FR1196738A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10330112B2 (en) * | 2013-12-30 | 2019-06-25 | United Technologies Corporation | Fan blade with root through holes |
Also Published As
Publication number | Publication date |
---|---|
NL228237A (en) | |
US3014693A (en) | 1961-12-26 |
BE568389A (en) | |
DE1081276B (en) | 1960-05-05 |
NL104493C (en) | |
FR1196738A (en) | 1959-11-25 |
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