GB507264A - Improvements in and relating to turbines - Google Patents
Improvements in and relating to turbinesInfo
- Publication number
- GB507264A GB507264A GB1497738A GB1497738A GB507264A GB 507264 A GB507264 A GB 507264A GB 1497738 A GB1497738 A GB 1497738A GB 1497738 A GB1497738 A GB 1497738A GB 507264 A GB507264 A GB 507264A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- discs
- casing
- guide
- balancing device
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
507,264. Elastic - fluid turbines. KOHLER, G., and BRAGARD, T. May 19, 1938, No. 14977. [Class 110 (iii)] The rotor 4 of a radial-flow turbine may be moved axially until the fixed and moving blades are unmeshed so as to facilitate the removal of the upper half of the casing 1. Spaces 8 are left between the rotor discs 5 and the unbladed sides of 'the guide discs. The space behind the last disc may be sealed by a labyrinth packing 7 and used as an end thrust balancing device. In a modification, Fig. 4, the front of the first rotor disc is fitted with a labyrinth packing and used as an end thrust balancing device; this arrangement lessens the leakage across the gland 9. The guide and rotor discs may be made integral with the casing and rotor shaft, the guide discs having radial expansion joints and being bolted together in a plane at right-angles to the turbine axis, to prevent casing distortion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1497738A GB507264A (en) | 1938-05-19 | 1938-05-19 | Improvements in and relating to turbines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1497738A GB507264A (en) | 1938-05-19 | 1938-05-19 | Improvements in and relating to turbines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB507264A true GB507264A (en) | 1939-06-13 |
Family
ID=10050895
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1497738A Expired GB507264A (en) | 1938-05-19 | 1938-05-19 | Improvements in and relating to turbines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB507264A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11022125B2 (en) * | 2017-02-28 | 2021-06-01 | Mitsubishi Heavy Industries Compressor Corporation | Centrifugal compressor |
-
1938
- 1938-05-19 GB GB1497738A patent/GB507264A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11022125B2 (en) * | 2017-02-28 | 2021-06-01 | Mitsubishi Heavy Industries Compressor Corporation | Centrifugal compressor |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB1125920A (en) | Turbomachine rotors | |
| GB723813A (en) | Improvements in or relating to bladed rotors for compressors, turbines and like fluid flow machines | |
| GB1335145A (en) | Turbine casing for a gas turbine engine | |
| GB1148339A (en) | Compressors or turbines for gas turbine engines | |
| GB586560A (en) | Improvements in axial flow compressors and like machines | |
| GB507264A (en) | Improvements in and relating to turbines | |
| GB586562A (en) | Improvements in high speed axial flow elastic fluid turbines, compressors, superchargers and like apparatus | |
| GB786689A (en) | Improvements relating to elastic-fluid turbines | |
| GB929103A (en) | Improvements in turbines | |
| GB815032A (en) | Improvements in or relating to multi-stage axial-flow turbines and compressors | |
| GB844020A (en) | Stator vane assemblies for axial-flow compressors and turbines | |
| GB700859A (en) | Improvements in axial flow turbines | |
| GB814809A (en) | Improvements in or relating to axial-flow turbines employing hot propellant media, especially gas turbines | |
| GB800524A (en) | Improvements in and relating to rotary compressors of the axial flow type | |
| GB466259A (en) | Improvements in and relating to turbo-blowers | |
| GB822172A (en) | Improvements in or relating to the blade rotors for gas turbine engines | |
| GB1491479A (en) | Bladed rotor for fluid flow machine | |
| GB927915A (en) | Turbo blowers | |
| GB585086A (en) | Improvements in internal combustion and other high speed, high temperature turbines | |
| GB532992A (en) | Improvements in or relating to turbine glands | |
| GB574752A (en) | Improvements in or relating to rotors for rotary machines, particularly steam or gasturbines | |
| GB592939A (en) | Fluid sealing means for a row of double blades of a turbine or other rotor | |
| GB994886A (en) | Gas turbine installation | |
| GB882480A (en) | Improvements in or relating to rotors for axial-flow turbines | |
| GB594203A (en) | Improved tightening device for radial flow elastic fluid turbines or compressors |