FR1083235A - Aubes creuses pour turbo-machines - Google Patents
Aubes creuses pour turbo-machinesInfo
- Publication number
- FR1083235A FR1083235A FR1083235DA FR1083235A FR 1083235 A FR1083235 A FR 1083235A FR 1083235D A FR1083235D A FR 1083235DA FR 1083235 A FR1083235 A FR 1083235A
- Authority
- FR
- France
- Prior art keywords
- turbo
- machines
- hollow blades
- blades
- hollow
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Butt Welding And Welding Of Specific Article (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB323715X | 1952-09-12 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1083235A true FR1083235A (fr) | 1955-01-06 |
Family
ID=10337581
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1083235D Expired FR1083235A (fr) | 1952-09-12 | 1953-09-10 | Aubes creuses pour turbo-machines |
Country Status (4)
Country | Link |
---|---|
US (1) | US2853272A (fr) |
CH (1) | CH323715A (fr) |
DE (1) | DE968525C (fr) |
FR (1) | FR1083235A (fr) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1041971B (de) * | 1955-11-08 | 1958-10-30 | Napier & Son Ltd | Hohlschaufel fuer Axialturbinen oder Verdichter |
DE1074594B (de) * | 1961-02-23 | 1960-02-04 | D Napier &. Son Limited, London | Befestigung hohler tragflugelprofilierter Axialturbmen oder Axialverdichter Schaufeln |
US4019832A (en) * | 1976-02-27 | 1977-04-26 | General Electric Company | Platform for a turbomachinery blade |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1069153B (de) * | 1956-03-14 | 1959-11-19 | D. Naoier S. Son Limited, London | Hohlschaufeln für Turbinen ader Verdichter |
US3066910A (en) * | 1958-07-09 | 1962-12-04 | Thompson Ramo Wooldridge Inc | Cooled turbine blade |
US3196526A (en) * | 1961-06-13 | 1965-07-27 | Bristol Siddeley Engines Ltd | Method of making turbine blades |
US3294364A (en) * | 1962-01-02 | 1966-12-27 | Gen Electric | Rotor assembly |
DE1221497B (de) * | 1962-05-09 | 1966-07-21 | Rolls Royce | Verdichter- oder Turbinenbaugruppe in einem Gasturbinenaggregat, insbesondere Gasturbinenstrahltriebwerk |
US3950114A (en) * | 1968-02-23 | 1976-04-13 | General Motors Corporation | Turbine blade |
US3635587A (en) * | 1970-06-02 | 1972-01-18 | Gen Motors Corp | Blade cooling liner |
US6735956B2 (en) | 2001-10-26 | 2004-05-18 | Pratt & Whitney Canada Corp. | High pressure turbine blade cooling scoop |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE550328C (de) * | 1932-05-11 | Siemens Schuckertwerke Akt Ges | Verfahren zur Befestigung von Hohlschaufeln im Radkranz einer Dampf- oder Gasturbine | |
DE580898C (de) * | 1933-11-13 | Christian Lorenzen | Hohlschaufel fuer Turbinen | |
DE391880C (de) * | 1921-05-14 | 1924-07-29 | Christian Lorenzen | Schaufelbefestigung fuer Gasturbinen mit durch die Turbinenschaufeln hindurchgefuehrter Verbrennungsluft |
US1516607A (en) * | 1923-07-30 | 1924-11-25 | Gen Electric | Hollow turbine bucket and method of manufacturing same |
DE433122C (de) * | 1925-04-01 | 1926-08-23 | Actiengesellschaft Der Maschin | Herstellung einer Turbinenleitschaufel |
DE566638C (de) * | 1931-01-20 | 1932-12-23 | Bbc Brown Boveri & Cie | Mehrteilige Turbinenschaufel, insbesondere fuer Gasturbinen |
DE673166C (de) * | 1933-09-30 | 1939-03-16 | Aeg | Schaufel fuer Kreiselmaschinen, insbesondere fuer Dampfturbinen |
BE444269A (fr) * | 1938-09-12 | |||
CH225232A (de) * | 1941-02-06 | 1943-01-15 | Bmw Flugmotorenbau Gmbh | Innengekühlte Turbinenschaufel. |
DE872695C (de) * | 1941-03-28 | 1953-04-27 | Versuchsanstalt Fuer Luftfahrt | Hohlschaufel, insbesondere fuer Gas- oder Abgasturbinen |
DE860438C (de) * | 1941-03-28 | 1952-12-22 | Versuchsanstalt Fuer Luftfahrt | Hohlschaufel fuer Gas- oder Abgasturbinen |
DE829969C (de) * | 1943-02-27 | 1952-01-31 | Maschf Augsburg Nuernberg Ag | Hohlschaufel fuer Laufraeder von axial durchstroemten Kreiselradmaschinen |
US2563269A (en) * | 1943-05-22 | 1951-08-07 | Lockheed Aircraft Corp | Gas turbine |
DE848883C (de) * | 1943-07-02 | 1952-09-08 | Brown | Mehrteilige innengekuehlte Turbinenschaufel, insbesondere fuer Gas- und Dampfturbinen |
US2618120A (en) * | 1946-06-07 | 1952-11-18 | Papini Anthony | Coaxial combustion products generator and turbine with cooling means |
US2656146A (en) * | 1948-04-08 | 1953-10-20 | Curtiss Wright Corp | Turbine blade construction |
FR965814A (fr) * | 1948-04-22 | 1950-09-22 | ||
GB724074A (en) * | 1948-08-05 | 1955-02-16 | Edward Archibald Stalker | Improvements in blade structures as may be employed in axial flow compressors |
FR981133A (fr) * | 1949-02-21 | 1951-05-22 | Parsons C A & Co Ltd | Procédé pour la fabrication d'aubes creuses pour turbines à combustion interne |
US2647368A (en) * | 1949-05-09 | 1953-08-04 | Hermann Oestrich | Method and apparatus for internally cooling gas turbine blades with air, fuel, and water |
GB679931A (en) * | 1949-12-02 | 1952-09-24 | Bristol Aeroplane Co Ltd | Improvements in or relating to blades for turbines or the like |
FR1262552A (fr) * | 1950-03-02 | 1961-06-05 | Structure et fixation de chemises pour le guidage du fluide assurant le refroidissement interne d'aubes creuses pour machines à écoulement de fluide |
-
1953
- 1953-09-08 US US378935A patent/US2853272A/en not_active Expired - Lifetime
- 1953-09-10 FR FR1083235D patent/FR1083235A/fr not_active Expired
- 1953-09-11 DE DEN7720A patent/DE968525C/de not_active Expired
- 1953-09-12 CH CH323715D patent/CH323715A/fr unknown
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1041971B (de) * | 1955-11-08 | 1958-10-30 | Napier & Son Ltd | Hohlschaufel fuer Axialturbinen oder Verdichter |
DE1074594B (de) * | 1961-02-23 | 1960-02-04 | D Napier &. Son Limited, London | Befestigung hohler tragflugelprofilierter Axialturbmen oder Axialverdichter Schaufeln |
US4019832A (en) * | 1976-02-27 | 1977-04-26 | General Electric Company | Platform for a turbomachinery blade |
Also Published As
Publication number | Publication date |
---|---|
CH323715A (fr) | 1957-08-15 |
DE968525C (de) | 1958-02-27 |
US2853272A (en) | 1958-09-23 |
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