GB574770A - Improvements relating to the blades of turbines and other machines - Google Patents
Improvements relating to the blades of turbines and other machinesInfo
- Publication number
- GB574770A GB574770A GB10832/42A GB1083242A GB574770A GB 574770 A GB574770 A GB 574770A GB 10832/42 A GB10832/42 A GB 10832/42A GB 1083242 A GB1083242 A GB 1083242A GB 574770 A GB574770 A GB 574770A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- materials
- turbines
- tensile strength
- machines
- 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
- 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
-
- 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)
- Architecture (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
574,770. Turbine and like blades. JULIEN, J. D. Aug. 3, 1942, No. 10832. [Class 110 (iii)] [Also in Groups XXII and XXXIII] The blades of water, steam or gas turbines, aircompressors, propellers and the like are formed of a core and a shell respectively of different materials and produced by forging or working a composite blank of the two materials. One part may be composed of a material having a lower tensile strength and adapted to resist heat, corrosion or vibration and the other part may be made of a material having a higher tensile strength and designed to reinforce the other part. The surfaces of the two materials are not integrally joined but the parts are interlocked, for example, by the bulbous end portions 3a of the core imbedded in the root portion 4a.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB10832/42A GB574770A (en) | 1942-08-03 | 1942-08-03 | Improvements relating to the blades of turbines and other machines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB10832/42A GB574770A (en) | 1942-08-03 | 1942-08-03 | Improvements relating to the blades of turbines and other machines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB574770A true GB574770A (en) | 1946-01-21 |
Family
ID=9975130
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB10832/42A Expired GB574770A (en) | 1942-08-03 | 1942-08-03 | Improvements relating to the blades of turbines and other machines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB574770A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2775426A (en) * | 1951-12-20 | 1956-12-25 | Westinghouse Electric Corp | Blade structure |
US2783966A (en) * | 1948-10-22 | 1957-03-05 | Maschf Augsburg Nuernberg Ag | Parts for machinery |
US3248082A (en) * | 1965-08-19 | 1966-04-26 | Whitfield Lab Inc | Reinforced gas-turbine blade or vane |
US3271004A (en) * | 1965-06-22 | 1966-09-06 | Smuland Robert John | Turbine vane adapted for high temperature operation |
GB2235733A (en) * | 1989-09-07 | 1991-03-13 | Gen Electric | Damper assembly for a jet engine strut |
-
1942
- 1942-08-03 GB GB10832/42A patent/GB574770A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2783966A (en) * | 1948-10-22 | 1957-03-05 | Maschf Augsburg Nuernberg Ag | Parts for machinery |
US2775426A (en) * | 1951-12-20 | 1956-12-25 | Westinghouse Electric Corp | Blade structure |
US3271004A (en) * | 1965-06-22 | 1966-09-06 | Smuland Robert John | Turbine vane adapted for high temperature operation |
US3248082A (en) * | 1965-08-19 | 1966-04-26 | Whitfield Lab Inc | Reinforced gas-turbine blade or vane |
GB2235733A (en) * | 1989-09-07 | 1991-03-13 | Gen Electric | Damper assembly for a jet engine strut |
US5056738A (en) * | 1989-09-07 | 1991-10-15 | General Electric Company | Damper assembly for a strut in a jet propulsion engine |
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