GB520045A - Improvements in or relating to elastic fluid turbines - Google Patents
Improvements in or relating to elastic fluid turbinesInfo
- Publication number
- GB520045A GB520045A GB29694/38A GB2969438A GB520045A GB 520045 A GB520045 A GB 520045A GB 29694/38 A GB29694/38 A GB 29694/38A GB 2969438 A GB2969438 A GB 2969438A GB 520045 A GB520045 A GB 520045A
- Authority
- GB
- United Kingdom
- Prior art keywords
- passages
- rotor
- turbine
- compressor
- nozzles
- 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
- 239000012530 fluid Substances 0.000 title abstract 4
- 238000001816 cooling Methods 0.000 abstract 4
- 239000007789 gas Substances 0.000 abstract 2
- 230000004048 modification Effects 0.000 abstract 2
- 238000012986 modification Methods 0.000 abstract 2
- 230000005540 biological transmission Effects 0.000 abstract 1
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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US176979A US2283176A (en) | 1937-11-29 | 1937-11-29 | Elastic fluid mechanism |
Publications (1)
Publication Number | Publication Date |
---|---|
GB520045A true GB520045A (en) | 1940-04-12 |
Family
ID=22646680
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB29694/38A Expired GB520045A (en) | 1937-11-29 | 1938-10-13 | Improvements in or relating to elastic fluid turbines |
Country Status (5)
Country | Link |
---|---|
US (1) | US2283176A (en:Method) |
BE (1) | BE431014A (en:Method) |
CH (1) | CH220012A (en:Method) |
FR (1) | FR845652A (en:Method) |
GB (1) | GB520045A (en:Method) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4453888A (en) * | 1981-04-01 | 1984-06-12 | United Technologies Corporation | Nozzle for a coolable rotor blade |
GB2263313A (en) * | 1991-11-14 | 1993-07-21 | Geoffrey Light Wilde | Turbocharger with exhaust gas cooling. |
Families Citing this family (35)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE952853C (de) * | 1942-05-23 | 1956-11-22 | Alfred Buechi Dr Ing | Gasturbine mit einer tangential von aussen beaufschlagten, das Treibgas von der radialen Eintritts- in die axiale Austrittsrichtung umlenkenden Laufradscheibe |
DE849038C (de) * | 1942-05-23 | 1952-09-11 | Alfred Dr-Ing Buechi | Gasturbine |
US2477683A (en) * | 1942-09-30 | 1949-08-02 | Turbo Engineering Corp | Compressed air and combustion gas flow in turbine power plant |
US2429936A (en) * | 1943-12-18 | 1947-10-28 | Allis Chalmers Mfg Co | Turbine mounting |
US2490064A (en) * | 1945-01-12 | 1949-12-06 | Kollsman Paul | Thermodynamic machine |
US2597249A (en) * | 1945-08-24 | 1952-05-20 | Kollsman Paul | Thermodynamic engine |
US2514874A (en) * | 1945-08-24 | 1950-07-11 | Kollsman Paul | Rotating combustion products generator with turbulent fuel injection zone |
US2514875A (en) * | 1945-08-29 | 1950-07-11 | Kollsman Paul | U-passage gas turbine with turbulent heat transfer zone |
US2694291A (en) * | 1948-02-07 | 1954-11-16 | Henning C Rosengart | Rotor and combustion chamber arrangement for gas turbines |
US2792197A (en) * | 1948-08-06 | 1957-05-14 | Garrett Corp | Gas turbine apparatus |
DE970089C (de) * | 1948-08-11 | 1958-08-21 | Geraetebau Eberspaecher O H G | Abgasturbolader fuer Kolbenmotoren mit Schutz gegen Waermeuebertragung |
US2709893A (en) * | 1949-08-06 | 1955-06-07 | Laval Steam Turbine Co | Gas turbine power plant with heat exchanger and cooling means |
GB705387A (en) * | 1951-02-15 | 1954-03-10 | Power Jets Res & Dev Ltd | Improvements relating to radial-flow turbine or centrifugal compressors |
US2780174A (en) * | 1951-03-19 | 1957-02-05 | Solar Aircraft Co | Pump and power plant assembly |
US2646210A (en) * | 1951-05-05 | 1953-07-21 | Eberspaecher J | Turbocompressor |
DE966394C (de) * | 1951-11-18 | 1957-08-01 | Bayerische Motoren Werke Ag | Abgasturbolader fuer Brennkraftmaschinen |
US2697986A (en) * | 1952-04-05 | 1954-12-28 | Jr James M Meagher | Axial flow glandless impeller pump |
GB757591A (en) * | 1953-04-07 | 1956-09-19 | British Leyland Motor Corp | Turbine-driven supercharger |
US2701682A (en) * | 1953-06-01 | 1955-02-08 | Garrett Corp | Rotojet impeller |
DE1291943B (de) * | 1961-09-15 | 1969-04-03 | Birmann Rudolph | Abgasturbolader fuer eine Brennkraftmaschine |
DE1296875B (de) * | 1962-02-09 | 1969-06-04 | Laval Turbine | Laeufer fuer eine Zentripetalgasturbine |
DE1301634B (de) * | 1965-09-29 | 1969-08-21 | Curtiss Wright Corp | Gasturbinentriebwerk |
US3493169A (en) * | 1968-06-03 | 1970-02-03 | United Aircraft Corp | Bleed for compressor |
DE2757236C3 (de) * | 1977-12-22 | 1982-02-25 | Dr.Ing.H.C. F. Porsche Ag, 7000 Stuttgart | Antriebsaggregat, insbesondere für Kraftfahrzeuge |
DE3023219A1 (de) * | 1980-06-21 | 1982-01-07 | Klein, Schanzlin & Becker Ag, 6710 Frankenthal | Turbopumpe |
DE3326992C1 (de) * | 1983-07-27 | 1984-12-13 | Dr.Ing.H.C. F. Porsche Ag, 7000 Stuttgart | Antriebsaggregat,insbesondere fuer Kraftfahrzeuge |
DE3339505A1 (de) * | 1983-10-31 | 1985-05-09 | Bernd 6352 Ober-Mörlen Jung | Gasturbine mit einem vorgeschalteten turbokompressor |
EP0162340A1 (en) * | 1984-05-15 | 1985-11-27 | A. S. Kongsberg Väpenfabrikk | Apparatus for controlling the axial component of running clearance in radial gas turbine engines |
DE3629494C1 (de) * | 1986-08-29 | 1988-02-11 | Porsche Ag | Abwaermeturbineneinheit |
US5224842A (en) * | 1992-01-10 | 1993-07-06 | Dziorny Paul J | Air cycle machine with interstage venting |
US6485640B2 (en) * | 2001-04-18 | 2002-11-26 | Gary Fout | Flow diverter and exhaust blower for vibrating screen separator assembly |
US7107972B1 (en) | 2004-08-03 | 2006-09-19 | Accessible Technologies, Inc. | Multi-phase centrifugal supercharging air induction system |
FR2944060B1 (fr) | 2009-04-06 | 2013-07-19 | Turbomeca | Systeme d'air secondaire pour compresseur centrifuge ou mixte |
US8991176B2 (en) * | 2012-03-28 | 2015-03-31 | GM Global Technology Operations LLC | Fluid drive mechanism for turbocharger |
WO2015061344A1 (en) | 2013-10-21 | 2015-04-30 | Williams International Co., L.L.C. | Centrifugal turbomachine diffuser with large vaneless portion upstream of a small vaned portion |
-
1937
- 1937-11-29 US US176979A patent/US2283176A/en not_active Expired - Lifetime
-
1938
- 1938-10-13 GB GB29694/38A patent/GB520045A/en not_active Expired
- 1938-11-05 FR FR845652D patent/FR845652A/fr not_active Expired
- 1938-11-07 CH CH220012D patent/CH220012A/de unknown
- 1938-11-08 BE BE431014D patent/BE431014A/xx unknown
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4453888A (en) * | 1981-04-01 | 1984-06-12 | United Technologies Corporation | Nozzle for a coolable rotor blade |
GB2263313A (en) * | 1991-11-14 | 1993-07-21 | Geoffrey Light Wilde | Turbocharger with exhaust gas cooling. |
GB2263313B (en) * | 1991-11-14 | 1994-11-09 | Geoffrey Light Wilde | Turbo charger |
Also Published As
Publication number | Publication date |
---|---|
FR845652A (fr) | 1939-08-30 |
CH220012A (de) | 1942-03-15 |
US2283176A (en) | 1942-05-19 |
BE431014A (en:Method) | 1938-12-31 |
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