GB586554A - Improvements in or relating to turbines - Google Patents
Improvements in or relating to turbinesInfo
- Publication number
- GB586554A GB586554A GB15077/41A GB1507741A GB586554A GB 586554 A GB586554 A GB 586554A GB 15077/41 A GB15077/41 A GB 15077/41A GB 1507741 A GB1507741 A GB 1507741A GB 586554 A GB586554 A GB 586554A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- compressor
- pressure
- blading
- low
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
- F02C3/073—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages the compressor and turbine stages being concentric
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/072—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with counter-rotating, e.g. fan rotors
-
- 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
Abstract
586,554. Gas turbines. BAUMANN, K., and METROPOLITAN-VICKERS ELECTRICAL CO., Ltd. Nov. 22, 1941, No. 15077. [Class 110 (iii)] In a combustion product jet-propulsion plant, high-pressure contra-rotational turbine blades 3a drive a high-pressure air-compressor 3 and low-pressure contra-rotational turbine blades I drive a lesser number of outer air blading rings 1a and inner low-pressure air-compressor bladings 1b. Air from the bladings 1 a passes in part to mix with the turbine exhaust going to the propulsion jet and in part through cross-over ducts 11 to the low-pressure air-compressor. Or the whole of the air from blading 1a may pass to the jet and the air-compressor may receive air from an outermost duct 13. Or, air for the compressor may pass through bladings situated between the low-pressure turbine blading and the outer air blading. Specifications 586,551, 586,552 and 586,553 are referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB15077/41A GB586554A (en) | 1941-11-22 | 1941-11-22 | Improvements in or relating to turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB15077/41A GB586554A (en) | 1941-11-22 | 1941-11-22 | Improvements in or relating to turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB586554A true GB586554A (en) | 1947-03-24 |
Family
ID=10052603
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB15077/41A Expired GB586554A (en) | 1941-11-22 | 1941-11-22 | Improvements in or relating to turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB586554A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2835332A (en) * | 1955-10-20 | 1958-05-20 | Vern K Fry | Power drive suitable for airplanes and helicopters |
EP0395497A1 (en) * | 1989-04-26 | 1990-10-31 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Counter rotating prop-fan engine |
GB2309745A (en) * | 1996-02-02 | 1997-08-06 | John Peter Miller | Multi-stage compressor |
EP3056712A1 (en) * | 2015-02-13 | 2016-08-17 | United Technologies Corporation | Turbine engine with a turbo-compressor |
US10041408B2 (en) | 2015-02-13 | 2018-08-07 | United Technologies Corporation | Turbine engine with a turbo-compressor |
US10125722B2 (en) | 2015-02-13 | 2018-11-13 | United Technologies Corporation | Turbine engine with a turbo-compressor |
US10337401B2 (en) | 2015-02-13 | 2019-07-02 | United Technologies Corporation | Turbine engine with a turbo-compressor |
CN111828177A (en) * | 2019-04-17 | 2020-10-27 | 通用电气公司 | Fluid exchange device and method for exchanging fluid between streams |
-
1941
- 1941-11-22 GB GB15077/41A patent/GB586554A/en not_active Expired
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2835332A (en) * | 1955-10-20 | 1958-05-20 | Vern K Fry | Power drive suitable for airplanes and helicopters |
EP0395497A1 (en) * | 1989-04-26 | 1990-10-31 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Counter rotating prop-fan engine |
FR2646473A1 (en) * | 1989-04-26 | 1990-11-02 | Snecma | ENGINE WITH TRACTRIC CONTROTOTATIVE BLOWERS |
US5105618A (en) * | 1989-04-26 | 1992-04-21 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." | Counterrotating fan engine |
GB2309745A (en) * | 1996-02-02 | 1997-08-06 | John Peter Miller | Multi-stage compressor |
EP3056712A1 (en) * | 2015-02-13 | 2016-08-17 | United Technologies Corporation | Turbine engine with a turbo-compressor |
US10041408B2 (en) | 2015-02-13 | 2018-08-07 | United Technologies Corporation | Turbine engine with a turbo-compressor |
US10100731B2 (en) | 2015-02-13 | 2018-10-16 | United Technologies Corporation | Turbine engine with a turbo-compressor |
US10125722B2 (en) | 2015-02-13 | 2018-11-13 | United Technologies Corporation | Turbine engine with a turbo-compressor |
US10337401B2 (en) | 2015-02-13 | 2019-07-02 | United Technologies Corporation | Turbine engine with a turbo-compressor |
CN111828177A (en) * | 2019-04-17 | 2020-10-27 | 通用电气公司 | Fluid exchange device and method for exchanging fluid between streams |
US11898492B2 (en) | 2019-04-17 | 2024-02-13 | General Electric Company | Fluid exchange apparatuses and methods of exchanging fluids between streams |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1113087A (en) | Gas turbine power plant | |
GB1113542A (en) | Gas turbine engine | |
GB1229007A (en) | ||
GB586554A (en) | Improvements in or relating to turbines | |
GB1125251A (en) | Improved gas turbine engine | |
GB585331A (en) | Improvements in or relating to internal-combustion turbines | |
GB577017A (en) | Improvements in turbines | |
GB586551A (en) | Improvements in or relating to internal combustion power turbine plant for propulsion in air | |
GB586556A (en) | Improvements in internal combustion turbine plant for propulsion | |
GB780240A (en) | Improvements in or relating to the construction of axial flow turbines or compressors | |
GB695891A (en) | Improvements in or relating to gas-turbine engines | |
GB881816A (en) | Improved gas turbine engine | |
GB586553A (en) | Improvements in or relating to turbines | |
GB712633A (en) | Improvements relating to gas-turbine engines | |
GB654411A (en) | Improvements in or relating to jet propulsion units | |
GB710300A (en) | Axial flow compressor | |
GB992931A (en) | Gas turbine jet propulsion engine | |
GB118650A (en) | Improvements in Air or Gas Turbines. | |
GB694414A (en) | Improvements in or relating to internal combustion gas turbine engines | |
GB594522A (en) | Improvements in or relating to internal combustion turbine power plants | |
GB932000A (en) | Improvements relating to gas turbine engines | |
GB586555A (en) | Improvements in internal combustion gas turbine plant, supercharger plant, air conditioning plant and the like | |
GB578005A (en) | Improvements in and relating to jet propulsion plant | |
GB1077583A (en) | Improvements relating to gas turbines with pulsating gas flows | |
GB727869A (en) | Improvements in axial flow compressors, for example for jet propulsion units |