FR1151368A - Couronne d'aubes directrices de turbine, avec aubes réglables - Google Patents
Couronne d'aubes directrices de turbine, avec aubes réglablesInfo
- Publication number
- FR1151368A FR1151368A FR1151368DA FR1151368A FR 1151368 A FR1151368 A FR 1151368A FR 1151368D A FR1151368D A FR 1151368DA FR 1151368 A FR1151368 A FR 1151368A
- Authority
- FR
- France
- Prior art keywords
- guide vane
- turbine guide
- adjustable vanes
- vane crown
- crown
- 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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
- F01D17/167—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes of vanes moving in translation
-
- 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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
- F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
-
- 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
- F01D5/186—Film cooling
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL333663X | 1955-06-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1151368A true FR1151368A (fr) | 1958-01-29 |
Family
ID=19784465
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1151368D Expired FR1151368A (fr) | 1955-06-17 | 1956-06-12 | Couronne d'aubes directrices de turbine, avec aubes réglables |
Country Status (5)
Country | Link |
---|---|
AT (1) | AT195186B (fr) |
CH (1) | CH333663A (fr) |
FR (1) | FR1151368A (fr) |
GB (1) | GB805015A (fr) |
NL (2) | NL198161A (fr) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3224194A (en) * | 1963-06-26 | 1965-12-21 | Curtiss Wright Corp | Gas turbine engine |
US3423069A (en) * | 1967-09-29 | 1969-01-21 | Trw Inc | Airfoil |
US4026659A (en) * | 1975-10-16 | 1977-05-31 | Avco Corporation | Cooled composite vanes for turbine nozzles |
US4221114A (en) * | 1967-01-18 | 1980-09-09 | Rolls-Royce Limited | Gas turbine jet propulsion engine |
US4384823A (en) * | 1980-10-27 | 1983-05-24 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Curved film cooling admission tube |
FR2586268A1 (fr) * | 1985-08-14 | 1987-02-20 | Snecma | Dispositif de variation de la section de passage d'un distributeur de turbine |
ES2063636A2 (es) * | 1992-04-23 | 1995-01-01 | Turbo Propulsores Ind | Conjunto de alabes de estator para motores de turbina de gas. |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1113787B (de) * | 1958-09-12 | 1961-09-14 | Bbc Brown Boveri & Cie | Axialverdichter mit verdrehbaren Leitschaufeln fuer staubhaltiges Gas |
DE1204021B (de) * | 1959-04-27 | 1965-10-28 | Rolls Royce | Schaufel fuer Axialstroemungsmaschinen, insbesondere Gasturbinen |
US3089679A (en) * | 1960-06-06 | 1963-05-14 | Chrysler Corp | Gas turbine nozzle suspension and adjustment |
DE1173292B (de) * | 1960-08-02 | 1964-07-02 | M A N I Turbomotoren G M B H | Hubstrahltriebwerk fuer Senkrechtstart-Flugzeuge |
DE1245218B (de) * | 1963-05-15 | 1967-07-20 | Hitachi Ltd | Gasturbinenrotor |
US3316714A (en) * | 1963-06-20 | 1967-05-02 | Rolls Royce | Gas turbine engine combustion equipment |
GB1048968A (en) * | 1964-05-08 | 1966-11-23 | Rolls Royce | Combustion chamber for a gas turbine engine |
US4169692A (en) * | 1974-12-13 | 1979-10-02 | General Electric Company | Variable area turbine nozzle and means for sealing same |
CA1038298A (fr) * | 1975-10-14 | 1978-09-12 | John Korta | Rotor a pales orientables pour turbine a gaz |
US3990810A (en) * | 1975-12-23 | 1976-11-09 | Westinghouse Electric Corporation | Vane assembly for close coupling the compressor turbine and a single stage power turbine of a two-shaped gas turbine |
EP0196450B1 (fr) * | 1985-03-15 | 1989-05-03 | Siemens Aktiengesellschaft | Régulateur de la résistance d'un courant d'air |
GB2210935B (en) * | 1987-10-10 | 1992-05-27 | Rolls Royce Plc | Variable stator vane assembly |
US4856962A (en) * | 1988-02-24 | 1989-08-15 | United Technologies Corporation | Variable inlet guide vane |
GB2218746B (en) * | 1988-05-17 | 1992-06-17 | Rolls Royce Plc | A nozzle guide vane for a gas turbine engine |
US4950129A (en) * | 1989-02-21 | 1990-08-21 | General Electric Company | Variable inlet guide vanes for an axial flow compressor |
GB9203168D0 (en) * | 1992-02-13 | 1992-04-01 | Rolls Royce Plc | Guide vanes for gas turbine engines |
US5931636A (en) * | 1997-08-28 | 1999-08-03 | General Electric Company | Variable area turbine nozzle |
ITTO20010444A1 (it) * | 2001-05-11 | 2002-11-11 | Fiatavio Spa | Turbina assiale per applicazioni aeronautiche. |
JP4096706B2 (ja) * | 2002-11-13 | 2008-06-04 | 株式会社Ihi | 薄肉軽量冷却タービン翼 |
EP2623717A1 (fr) * | 2012-02-02 | 2013-08-07 | Siemens Aktiengesellschaft | Couronne d'aube pour une turbomachine axiale et procédé d'ajustement de la capacité de débit massique de la couronne d'aube |
GB201419951D0 (en) | 2014-11-10 | 2014-12-24 | Rolls Royce Plc | A guide vane |
BE1026411B1 (fr) | 2018-06-21 | 2020-01-30 | Safran Aero Boosters Sa | Virole extérieure de turbomachine |
CN112727955B (zh) * | 2021-01-18 | 2023-04-18 | 一汽解放汽车有限公司 | 一种液力缓速器转子 |
-
0
- NL NL86599D patent/NL86599C/xx active
- NL NL198161D patent/NL198161A/xx unknown
-
1955
- 1955-09-15 CH CH333663D patent/CH333663A/de unknown
-
1956
- 1956-05-24 AT AT195186D patent/AT195186B/de active
- 1956-06-12 FR FR1151368D patent/FR1151368A/fr not_active Expired
- 1956-06-12 GB GB18082/56A patent/GB805015A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3224194A (en) * | 1963-06-26 | 1965-12-21 | Curtiss Wright Corp | Gas turbine engine |
US4221114A (en) * | 1967-01-18 | 1980-09-09 | Rolls-Royce Limited | Gas turbine jet propulsion engine |
US3423069A (en) * | 1967-09-29 | 1969-01-21 | Trw Inc | Airfoil |
US4026659A (en) * | 1975-10-16 | 1977-05-31 | Avco Corporation | Cooled composite vanes for turbine nozzles |
US4384823A (en) * | 1980-10-27 | 1983-05-24 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Curved film cooling admission tube |
FR2586268A1 (fr) * | 1985-08-14 | 1987-02-20 | Snecma | Dispositif de variation de la section de passage d'un distributeur de turbine |
EP0214038A1 (fr) * | 1985-08-14 | 1987-03-11 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Dispositif de variation de la section de passage d'un distributeur de turbine |
ES2063636A2 (es) * | 1992-04-23 | 1995-01-01 | Turbo Propulsores Ind | Conjunto de alabes de estator para motores de turbina de gas. |
Also Published As
Publication number | Publication date |
---|---|
NL198161A (fr) | |
NL86599C (fr) | |
CH333663A (de) | 1958-10-31 |
AT195186B (de) | 1958-01-25 |
GB805015A (en) | 1958-11-26 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR1151368A (fr) | Couronne d'aubes directrices de turbine, avec aubes réglables | |
FR1097531A (fr) | Perfectionnements aux aubages de turbines ou de compresseurs | |
CH297551A (de) | Gasturbinenanlage. | |
CH294130A (de) | Gasturbinenanlage. | |
FR1028630A (fr) | Perfectionnements aux aubes de turbines | |
FR1163559A (fr) | Perfectionnement aux turbines | |
CH337214A (fr) | Couronne d'aubes pour turbo-machine | |
FR1173534A (fr) | Turbine | |
FR1084493A (fr) | Turbo-machine possédant des ailettes-guides réglables | |
FR1055261A (fr) | Perfectionnements apportés aux réacteurs avec aubes de stator réglables | |
FR1068395A (fr) | Perfectionnements apportés aux aubes de turbines | |
CH343180A (de) | Gasturbinenanlage | |
CH284895A (de) | Gasturbinenanlage. | |
FR1121079A (fr) | Turbine volumétrique | |
FR1164465A (fr) | Perfectionnements apportés aux aubes de turbines | |
FR1074886A (fr) | Perfectionnements aux turbines | |
FR1129087A (fr) | Perfectionnements aux régulateurs de turbines | |
FR1214681A (fr) | Perfectionnements aux aubages de turbines | |
FR1120816A (fr) | Perfectionnements aux éoliennes | |
FR1162664A (fr) | Perfectionnements aux aubes creuses de turbine | |
CH336228A (de) | Gasturbinenrotor | |
FR1155252A (fr) | Perfectionnements aux turbines | |
FR1137267A (fr) | Perfectionnements aux turbines | |
CA527374A (fr) | Turbine a vent | |
FR1197189A (fr) | Moyeu d'éolienne |