GB1083175A - Blades for high-speed axial-flow compressors - Google Patents
Blades for high-speed axial-flow compressorsInfo
- Publication number
- GB1083175A GB1083175A GB34788/65A GB3478865A GB1083175A GB 1083175 A GB1083175 A GB 1083175A GB 34788/65 A GB34788/65 A GB 34788/65A GB 3478865 A GB3478865 A GB 3478865A GB 1083175 A GB1083175 A GB 1083175A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tube
- axial
- blade
- moulding
- aug
- 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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/324—Blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/34—Blade mountings
- F04D29/36—Blade mountings adjustable
-
- 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
Abstract
1,083,175. Axial-flow compressors. BRITISH AIRCRAFT CORPORATION (OPERATING) Ltd. Aug.11, 1966 [Aug.13, 1965], No.34788/65. Headings F1C and F1T. A blade 4 of an axial-flow compressor is constructed by moulding a glass-reinforced plastics material over a flattened end 6 of a steel tube forming the blade root. The end 6 has holes 14 to improve bonding. Moreover, bonding is improved by the process of first applying resin and powder ingredients to the cleaned tube, curing the ingredients by heating and then moulding the plastics material on to the tube. A thrust bearing may be secured to a plug 18 screwed, bronzed, or welded to the tube. The plug may carry a lever arm movable in a plane normal to the axis 19 for adjusting the blade pitch.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB34788/65A GB1083175A (en) | 1965-08-13 | 1965-08-13 | Blades for high-speed axial-flow compressors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB34788/65A GB1083175A (en) | 1965-08-13 | 1965-08-13 | Blades for high-speed axial-flow compressors |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1083175A true GB1083175A (en) | 1967-09-13 |
Family
ID=10369957
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB34788/65A Expired GB1083175A (en) | 1965-08-13 | 1965-08-13 | Blades for high-speed axial-flow compressors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1083175A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2197913A (en) * | 1986-11-19 | 1988-06-02 | Gen Electric | Propulsor blade |
US4971641A (en) * | 1988-11-14 | 1990-11-20 | General Electric Company | Method of making counterrotating aircraft propeller blades |
USRE34207E (en) * | 1986-11-19 | 1993-03-30 | General Electric Company | Counterrotating aircraft propulsor blades |
CN109026117A (en) * | 2018-08-29 | 2018-12-18 | 上海诺地乐通用设备制造有限公司 | A kind of jet blower |
-
1965
- 1965-08-13 GB GB34788/65A patent/GB1083175A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2197913A (en) * | 1986-11-19 | 1988-06-02 | Gen Electric | Propulsor blade |
GB2197913B (en) * | 1986-11-19 | 1991-07-31 | Gen Electric | Counterrotating aircraft propulsor blades |
USRE34207E (en) * | 1986-11-19 | 1993-03-30 | General Electric Company | Counterrotating aircraft propulsor blades |
US4971641A (en) * | 1988-11-14 | 1990-11-20 | General Electric Company | Method of making counterrotating aircraft propeller blades |
CN109026117A (en) * | 2018-08-29 | 2018-12-18 | 上海诺地乐通用设备制造有限公司 | A kind of jet blower |
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