CONFLUENCE STRUCTURE OF A PRIMARY STREAM AND A SECONDARY STREAM IN A BYPASS TURBINE ENGINE

The invention relates to a confluence structure of an aircraft bypass turbine engine which comprises a confluence plate (13) with a downstream end (16) supported by a portion (20) that is movable in the direction of the axis (X) by a control mechanism (26 to 32) which can optionally be adjusted in f...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	CABRE, Jean-François, LE PANNERER, Brice Marie Yves Emile, CURLIER, Nicolas Camille Claude, PFLIEGER, Lucas Arthur
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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