FR973649A - Dispositif pour le refroidissement de turbines à gaz, notamment de turbines à gaz d'échappement de moteurs à combustion interne
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Dispositif pour le refroidissement de turbines à gaz, notamment de turbines à gaz d'échappement de moteurs à combustion interne
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BMW Flugmotorenbau GmbH
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BMW Flugmotorenbau GmbH
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Publication of FR973649ApublicationCriticalpatent/FR973649A/fr
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
F02C7/125—Cooling of plants by partial arc admission of the working fluid or by intermittent admission of working and cooling fluid
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
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Engineering & Computer Science
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Chemical & Material Sciences
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Combustion & Propulsion
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Mechanical Engineering
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General Engineering & Computer Science
(AREA)
FR973649D1941-10-281941-10-28Dispositif pour le refroidissement de turbines à gaz, notamment de turbines à gaz d'échappement de moteurs à combustion interne
ExpiredFR973649A
(fr)
Dispositif pour le refroidissement des paliers de turbines à gaz chaud, notamment de turbines alimentées par l'échappement de moteurs à combustion interne
Dispositif de réglage de l'air de combustion pendant le démarrage des moteurs à combustion interne fonctionnant suivant le principe des moteurs à gaz diesel
Dispositif de refroidissement des moteurs à combustion interne, particulièrement des chambres d'explosion et, de préférence, pour l'actionnement des turbines à gaz