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Application filed by Rover Co LtdfiledCriticalRover Co Ltd
Publication of CH354988ApublicationCriticalpatent/CH354988A/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
F02C7/26—Starting; Ignition
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Engineering & Computer Science
(AREA)
Chemical & Material Sciences
(AREA)
Combustion & Propulsion
(AREA)
Mechanical Engineering
(AREA)
General Engineering & Computer Science
(AREA)
Feeding And Controlling Fuel
(AREA)
CH354988D1956-10-111957-10-04Dispositif d'alimentation en combustible d'un groupe à turbine à gaz
CH354988A
(fr)