GB586573A - Improvements in or relating to internal combustion turbine plant - Google Patents
Improvements in or relating to internal combustion turbine plantInfo
- Publication number
- GB586573A GB586573A GB1665643A GB1665643A GB586573A GB 586573 A GB586573 A GB 586573A GB 1665643 A GB1665643 A GB 1665643A GB 1665643 A GB1665643 A GB 1665643A GB 586573 A GB586573 A GB 586573A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- compressor
- nozzle
- blown
- relating
- 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
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
- F04D27/0215—Arrangements therefor, e.g. bleed or by-pass valves
Landscapes
- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
586,573. Air compressors. SMITH. D. M., and METROPOLITAN-VICKERS ELECTRICAL CO., Ltd. Oct. 11, 1943, No. 16656. [Class 110 (i)] Air which is blown off from an axial-flow compressor, to avoid stalling at low speeds, is discharged through convergent-divergent nozzles whereby the fraction of the total air which is blown off decreases rapidly with increase in the pressure ratio of the compressor. Two nozzles 1a, 2a, discharging from spaced points in a compressor may be arranged in series, as shown in Fig. 3. In this arrangement, discharge from the lower pressure point ceases when the pressure ratio rises sufficiently. In Fig. 4, the nozzle 1b is situated axially and air vented out of the compressor at 7 passes through a bladed rotor 8 on its way to the nozzle. Air from the nozzle, as well as from the rotor 8, may be used for cooling purposes. Specification 586,565 is referred to.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1665643A GB586573A (en) | 1943-10-11 | 1943-10-11 | Improvements in or relating to internal combustion turbine plant |
ES175321A ES175321A1 (en) | 1943-10-11 | 1946-10-17 | A MULTIPLE COMPRESSOR OF AIR OR GAS, OF AXIAL PASS |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1665643A GB586573A (en) | 1943-10-11 | 1943-10-11 | Improvements in or relating to internal combustion turbine plant |
Publications (1)
Publication Number | Publication Date |
---|---|
GB586573A true GB586573A (en) | 1947-03-24 |
Family
ID=10081243
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1665643A Expired GB586573A (en) | 1943-10-11 | 1943-10-11 | Improvements in or relating to internal combustion turbine plant |
Country Status (2)
Country | Link |
---|---|
ES (1) | ES175321A1 (en) |
GB (1) | GB586573A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1028389B (en) * | 1956-02-06 | 1958-04-17 | Bristol Aero Engines Ltd | Gas turbine with compressor |
GB2242930A (en) * | 1990-04-09 | 1991-10-16 | Gen Electric | Method and apparatus for compressor air extraction |
US5231825A (en) * | 1990-04-09 | 1993-08-03 | General Electric Company | Method for compressor air extraction |
US5680754A (en) * | 1990-02-12 | 1997-10-28 | General Electric Company | Compressor splitter for use with a forward variable area bypass injector |
CN114776403A (en) * | 2021-12-29 | 2022-07-22 | 东方电气集团东方汽轮机有限公司 | Air inlet structure and method suitable for large enthalpy drop small-flow turbine |
-
1943
- 1943-10-11 GB GB1665643A patent/GB586573A/en not_active Expired
-
1946
- 1946-10-17 ES ES175321A patent/ES175321A1/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1028389B (en) * | 1956-02-06 | 1958-04-17 | Bristol Aero Engines Ltd | Gas turbine with compressor |
US5680754A (en) * | 1990-02-12 | 1997-10-28 | General Electric Company | Compressor splitter for use with a forward variable area bypass injector |
GB2242930A (en) * | 1990-04-09 | 1991-10-16 | Gen Electric | Method and apparatus for compressor air extraction |
US5155993A (en) * | 1990-04-09 | 1992-10-20 | General Electric Company | Apparatus for compressor air extraction |
US5231825A (en) * | 1990-04-09 | 1993-08-03 | General Electric Company | Method for compressor air extraction |
CN114776403A (en) * | 2021-12-29 | 2022-07-22 | 东方电气集团东方汽轮机有限公司 | Air inlet structure and method suitable for large enthalpy drop small-flow turbine |
CN114776403B (en) * | 2021-12-29 | 2023-12-26 | 东方电气集团东方汽轮机有限公司 | Air inlet structure and method suitable for large enthalpy drop small flow turbine |
Also Published As
Publication number | Publication date |
---|---|
ES175321A1 (en) | 1946-11-16 |
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