GB515716A - Improvements in and relating to gas or steam turbines - Google Patents
Improvements in and relating to gas or steam turbinesInfo
- Publication number
- GB515716A GB515716A GB17292/38A GB1729238A GB515716A GB 515716 A GB515716 A GB 515716A GB 17292/38 A GB17292/38 A GB 17292/38A GB 1729238 A GB1729238 A GB 1729238A GB 515716 A GB515716 A GB 515716A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- decrease
- profile
- centre
- towards
- 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
- F01D5/141—Shape, i.e. outer, aerodynamic form
-
- 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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
515,716. Elastic-fluid turbines. KOHLER, G., and BRAGARD, T. June 10, 1938, No. 17292. [Class 110 (iii)] A reaction rotor blade for radial-flow gas or steam turbines is so shaped that the angle a, Fig, 2, between the lines R, yy of radial centrifugal force and minimum moment of inertia respectively decreases with increase in bending moment. With blades held at one end Fig. 6, this decrease is towards the hub, while with the blades held at both ends, Fig. 7, this decrease is towards the centre of the blade. In Fig. 1, the sections 4... 1 correspond to the lines A ... D of Figs. 6 and 7. This decrease may be effected by increasing the inlet angle of the blade, or by increasing the ratio of the inlet and outlimb lengths, reckoned from the centre of sharpest concave curvature, as by a tangential extension. The under profile of the blade may be moved out, keeping the rear profile constant, and the blade thickness may be increased. The profile form generating the under and rear faces may move in a curved path such as a circular arc.
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DEK135570D DE679925C (en) | 1934-10-11 | 1934-10-11 | Overpressure blade for radially pressurized steam or gas turbines |
| GB17292/38A GB515716A (en) | 1934-10-11 | 1938-06-10 | Improvements in and relating to gas or steam turbines |
| FR839279D FR839279A (en) | 1934-10-11 | 1938-06-14 | Reaction-driven blades for radial injection steam or gas turbines and turbines fitted with such blades |
| CH224726D CH224726A (en) | 1934-10-11 | 1939-06-01 | Overpressure rotor blade for gas or steam turbines with radial pressure. |
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DEK135570D DE679925C (en) | 1934-10-11 | 1934-10-11 | Overpressure blade for radially pressurized steam or gas turbines |
| GB17292/38A GB515716A (en) | 1934-10-11 | 1938-06-10 | Improvements in and relating to gas or steam turbines |
| FR839279T | 1938-06-14 | ||
| CH224726T | 1939-06-01 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB515716A true GB515716A (en) | 1939-12-12 |
Family
ID=10092630
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB17292/38A Expired GB515716A (en) | 1934-10-11 | 1938-06-10 | Improvements in and relating to gas or steam turbines |
Country Status (4)
| Country | Link |
|---|---|
| CH (1) | CH224726A (en) |
| DE (1) | DE679925C (en) |
| FR (1) | FR839279A (en) |
| GB (1) | GB515716A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109083798A (en) * | 2017-06-13 | 2018-12-25 | 国网江苏省电力公司常州供电公司 | Fluid power generation device |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB675494A (en) * | 1949-05-20 | 1952-07-09 | Ado Vecchiotti | Improvements in or relating to cartridges for shotguns |
| US3215075A (en) * | 1962-12-06 | 1965-11-02 | Remington Arms Co Inc | Shotshell |
| WO1994012390A2 (en) * | 1992-11-24 | 1994-06-09 | United Technologies Corporation | Coolable rotor blade structure |
-
1934
- 1934-10-11 DE DEK135570D patent/DE679925C/en not_active Expired
-
1938
- 1938-06-10 GB GB17292/38A patent/GB515716A/en not_active Expired
- 1938-06-14 FR FR839279D patent/FR839279A/en not_active Expired
-
1939
- 1939-06-01 CH CH224726D patent/CH224726A/en unknown
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109083798A (en) * | 2017-06-13 | 2018-12-25 | 国网江苏省电力公司常州供电公司 | Fluid power generation device |
| CN109083798B (en) * | 2017-06-13 | 2024-02-06 | 国网江苏省电力公司常州供电公司 | Fluid power generation device |
Also Published As
| Publication number | Publication date |
|---|---|
| CH224726A (en) | 1942-12-15 |
| FR839279A (en) | 1939-03-30 |
| DE679925C (en) | 1939-08-18 |
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