GB910400A - Improvements in or relating to blades for axial flow rotary machines and the like - Google Patents
Improvements in or relating to blades for axial flow rotary machines and the likeInfo
- Publication number
- GB910400A GB910400A GB4021860A GB4021860A GB910400A GB 910400 A GB910400 A GB 910400A GB 4021860 A GB4021860 A GB 4021860A GB 4021860 A GB4021860 A GB 4021860A GB 910400 A GB910400 A GB 910400A
- Authority
- GB
- United Kingdom
- Prior art keywords
- bosses
- blade
- rotary machines
- flow rotary
- blades
- 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
- F01D5/18—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
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
-
- 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
Abstract
910,400. Turbine blades. ENTWICK. LUNGSBAU PIRNA VEB. Nov. 23, 1960, No. 40218/60. Class 110 (3). A hollow blade for axial-flow rotary machines, particularly turbines, comprises two cambered parts 1, 8, connected together at their leading and trailing edges, having bosses 3, 5 respectively, projecting from the inside of each part, the bosses on one half being staggered with respect to those on the opposite half, said bosses having different heights so that they interpenetrate and their free ends terminate short of the inside surface of the opposite part of the blade. A duet for the entry of cooling air, is located in the root of the blade. The bosses 3, 5 are tapered and their tips are rounded and their cross-section is square with rounded edges or alternatively circular except in the vicinity of the leading and trailing edges.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4021860A GB910400A (en) | 1960-11-23 | 1960-11-23 | Improvements in or relating to blades for axial flow rotary machines and the like |
FR849670A FR1277685A (en) | 1960-11-23 | 1961-01-13 | Hollow fin, especially for turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4021860A GB910400A (en) | 1960-11-23 | 1960-11-23 | Improvements in or relating to blades for axial flow rotary machines and the like |
Publications (1)
Publication Number | Publication Date |
---|---|
GB910400A true GB910400A (en) | 1962-11-14 |
Family
ID=10413800
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4021860A Expired GB910400A (en) | 1960-11-23 | 1960-11-23 | Improvements in or relating to blades for axial flow rotary machines and the like |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB910400A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1265495B (en) * | 1963-08-30 | 1968-04-04 | Gen Electric | Hollow stator or rotor blade |
US3836283A (en) * | 1972-05-08 | 1974-09-17 | Nat Aerospace Lab | Construction of axial-flow turbine blades |
GB2163219A (en) * | 1981-10-31 | 1986-02-19 | Rolls Royce | Cooled turbine blade |
EP0416542A1 (en) * | 1989-09-04 | 1991-03-13 | Hitachi, Ltd. | Turbine blade |
GB2272731A (en) * | 1992-11-18 | 1994-05-25 | Snecma | Hollow blade for the fan or compressor of a turbomachine |
-
1960
- 1960-11-23 GB GB4021860A patent/GB910400A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1265495B (en) * | 1963-08-30 | 1968-04-04 | Gen Electric | Hollow stator or rotor blade |
US3836283A (en) * | 1972-05-08 | 1974-09-17 | Nat Aerospace Lab | Construction of axial-flow turbine blades |
GB2163219A (en) * | 1981-10-31 | 1986-02-19 | Rolls Royce | Cooled turbine blade |
US4684322A (en) * | 1981-10-31 | 1987-08-04 | Rolls-Royce Plc | Cooled turbine blade |
EP0416542A1 (en) * | 1989-09-04 | 1991-03-13 | Hitachi, Ltd. | Turbine blade |
GB2272731A (en) * | 1992-11-18 | 1994-05-25 | Snecma | Hollow blade for the fan or compressor of a turbomachine |
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