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ventilated interface between a combustion chamber and a high pressure distributor of turbojet and turbojet comprising this interface
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Assembly of an annular combustion chamber of turbomachine
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Fastener system for fastening together parts using pins having collars
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Piece for protecting the edge of a blade
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METHOD OF ASSEMBLING TWO PARTS OF WHICH AT LEAST ONE IS OF COMPOSITE MATERIAL, INSERT FOR THE REALIZATION OF THE ASSEMBLY
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VENTILATION OF THE HIGH PRESSURE TURBINE WHEEL OF AERONAUTICAL GAS TURBINE ENGINE
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CONNECTION DEVICE BETWEEN A COOLING AIR PASSING ENCLOSURE AND A DISTRIBUTOR'S TANK IN A TURBOMACHINE
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DEVIATION SYSTEM FOR A GAS FLOW IN A TUYERE
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DUAL-BODY TURBOMOTEUR WITH MOTION-TENSIONING MEANS ON LOW-PRESSURE, HIGH-PRESSURE ROTORS, TURBOMOTING MOTION-TENSIONING MODULE, AND TURBOMOTING MOUNTING METHOD
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TURBOMACHINE COMBUSTION CHAMBER FAIRING
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Device for positioning a dashboard and aubage disk comprising such a device
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Twin-spool turbojet with means for driving ancillary machines
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Cooling system for hot parts of an aircraft engine, and aircraft engine equipped with such a cooling system
