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

A confluence structure of an aircraft bypass turbine engine which includes a confluence plate with a downstream end supported by a portion that is movable in the direction of the axis by a control mechanism which can optionally be adjusted in flight. A mobile portion of a sleeve delimiting the secon...

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
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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