GB152689A - Improvements in and relating to turbo-compressors and turbo-blowers - Google Patents
Improvements in and relating to turbo-compressors and turbo-blowersInfo
- Publication number
- GB152689A GB152689A GB29817/20A GB2981720A GB152689A GB 152689 A GB152689 A GB 152689A GB 29817/20 A GB29817/20 A GB 29817/20A GB 2981720 A GB2981720 A GB 2981720A GB 152689 A GB152689 A GB 152689A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- space
- air
- width
- turbo
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
- F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
- F04D29/444—Bladed diffusers
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Non-Positive Displacement Air Blowers (AREA)
Abstract
152,689. Plohl, M. July 11, 1919, [Convention date]. Void [Published under Sect. 91 of the Act] Addition to 152,673. Casings; introducing air at high pressure at rotor discharge apertures. - In a method of increasing efficiency in a pump as described in the parent Specification, air at high pressure is led back from the pressure space b to a portion t of the width of the rotor h against the flow of air through the pump. Two annular discs a, a<1>, inclined to each other as shown, connect the pressure space b of the guide-chamber with the space t which immediately surrounds the rotor and has a width of at least one-third of the width of the rotor blades. The space between the discs is divided into a number of ducts, with cross sections of equal areas throughout, by partitions s placed approximately in the direction of air flow from the rotor. In a modification, a number of annular discs may be employed to form annular spaces without the partitions s.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT152689X | 1919-07-11 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB152689A true GB152689A (en) | 1921-03-17 |
Family
ID=3647241
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB29817/20A Expired GB152689A (en) | 1919-07-11 | 1920-10-21 | Improvements in and relating to turbo-compressors and turbo-blowers |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB152689A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3150823A (en) * | 1962-02-12 | 1964-09-29 | Ass Elect Ind | Diffusers |
| US3644055A (en) * | 1969-10-02 | 1972-02-22 | Ingersoll Rand Co | Fluid-motion apparatus |
| USRE32462E (en) * | 1979-08-01 | 1987-07-21 | Hitachi, Ltd. | Centrifugal fluid machine |
| EP2806170A4 (en) * | 2012-01-17 | 2015-11-18 | Mitsubishi Heavy Ind Ltd | Centrifugal compressor |
-
1920
- 1920-10-21 GB GB29817/20A patent/GB152689A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3150823A (en) * | 1962-02-12 | 1964-09-29 | Ass Elect Ind | Diffusers |
| US3644055A (en) * | 1969-10-02 | 1972-02-22 | Ingersoll Rand Co | Fluid-motion apparatus |
| USRE32462E (en) * | 1979-08-01 | 1987-07-21 | Hitachi, Ltd. | Centrifugal fluid machine |
| EP2806170A4 (en) * | 2012-01-17 | 2015-11-18 | Mitsubishi Heavy Ind Ltd | Centrifugal compressor |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB1240568A (en) | Outlet housing of an axial-flow turbomachine | |
| GB1349170A (en) | Rotor for a gas turbine engine | |
| GB141698A (en) | Improvements in rotors for multistage high-speed turbines, pumps and compressors and particularly for rotors of the disc-type for steam turbines | |
| GB152689A (en) | Improvements in and relating to turbo-compressors and turbo-blowers | |
| GB213256A (en) | Wheel for internal combustion turbines | |
| GB1148339A (en) | Compressors or turbines for gas turbine engines | |
| GB499357A (en) | Improvements relating to centrifugal blowers | |
| GB800098A (en) | Improvements in or relating to multi-stage axial-flow compressors | |
| GB1282142A (en) | Improvements in or relating to gas turbine engines | |
| GB577017A (en) | Improvements in turbines | |
| GB1605282A (en) | Bladed rotor for gas turbine engine | |
| GB1302661A (en) | ||
| GB512301A (en) | An arrangements for cooling solid blades for exhaust gas turbines | |
| GB515926A (en) | Rotor for turbines, rotary compressors and the like rotary machines | |
| GB1137630A (en) | Improvements in axial flow gas turbines | |
| GB506479A (en) | Improvements in or relating to turbines | |
| GB1066678A (en) | A rotor for use in a gas turbine engine | |
| GB167131A (en) | Improvements in and relating to turbo-compressors and turboblowers | |
| GB322570A (en) | Superchargers for internal combustion engines | |
| GB504263A (en) | Improvements in and to gas turbines | |
| GB412006A (en) | Improvements in rotary engines | |
| GB740944A (en) | Improvements in and relating to thermal turbines | |
| GB368318A (en) | Improvements in or relating to turbines | |
| GB368317A (en) | Improvements in or relating to turbines | |
| SU89083A1 (en) | The sewage system cooling air in the rotor of a multi-stage gas turbine with closed hollow blades |