GB381442A - Thin walled disc with high resistance to thrust - Google Patents
Thin walled disc with high resistance to thrustInfo
- Publication number
- GB381442A GB381442A GB399932A GB399932A GB381442A GB 381442 A GB381442 A GB 381442A GB 399932 A GB399932 A GB 399932A GB 399932 A GB399932 A GB 399932A GB 381442 A GB381442 A GB 381442A
- Authority
- GB
- United Kingdom
- Prior art keywords
- discs
- thrust
- radial
- angle
- high resistance
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
- F01D5/041—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the Ljungström type
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
381,442. Turbine rotors. MEINING- HAUS, U., 4, Margarethenplatz, Mulheim, Ruhr, Germany. Feb. 10, 1932, No. 3999. [Class 110 (iii).] A turbine motor is constructed of several concentrically arranged discs whose axial dimensions are greater than their radial dimensions. In the form shown in Fig. 1 separate discs 1 .. 8 have claw - shaped ends to secure cohesion between the discs. Fig. 2 shows another arrangement. The inner element 20 is of a radial thickness and axial length to secure an angle of distortion under load at the root 25 the same as the angle of distortion of the adjacent annular disc 21. The invention is stated to be suitable for radial flow turbines.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB399932A GB381442A (en) | 1932-02-10 | 1932-02-10 | Thin walled disc with high resistance to thrust |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB399932A GB381442A (en) | 1932-02-10 | 1932-02-10 | Thin walled disc with high resistance to thrust |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB381442A true GB381442A (en) | 1932-10-06 |
Family
ID=9768842
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB399932A Expired GB381442A (en) | 1932-02-10 | 1932-02-10 | Thin walled disc with high resistance to thrust |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB381442A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3032318A (en) * | 1956-08-11 | 1962-05-01 | Lindblom Erik David | Radial flow elastic fluid compressors or turbines |
| CN109684757A (en) * | 2018-12-29 | 2019-04-26 | 南京安维士传动技术股份有限公司 | Wind turbine gearbox shrink disk calculation method |
-
1932
- 1932-02-10 GB GB399932A patent/GB381442A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3032318A (en) * | 1956-08-11 | 1962-05-01 | Lindblom Erik David | Radial flow elastic fluid compressors or turbines |
| CN109684757A (en) * | 2018-12-29 | 2019-04-26 | 南京安维士传动技术股份有限公司 | Wind turbine gearbox shrink disk calculation method |
| CN109684757B (en) * | 2018-12-29 | 2023-10-20 | 南京安维士传动技术股份有限公司 | Wind power gear box shrink disk calculation method |
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