Propelling gas exhaust assembly in an aircraft with two elbow-shaped channels

The assembly (20) has a transition element (21) divided into two duct elements (22, 23) which communicate with semi exhaust nozzles (24, 26), where the divided nozzle part is visible from sides due to a bevel exhaust plane. The duct elements form bends in downstream of the transition element that is...

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Bibliographische Detailangaben
Hauptverfasser:	DARIS, THOMAS, BRUNET, EDGAR, SCHENHER, FREDERIC HENRI PAUL, PROUTEAU, JACKIE RAYMOND JULIEN
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	The assembly (20) has a transition element (21) divided into two duct elements (22, 23) which communicate with semi exhaust nozzles (24, 26), where the divided nozzle part is visible from sides due to a bevel exhaust plane. The duct elements form bends in downstream of the transition element that is defined by two parts for guiding gaseous flow in radial directions, where the bends are symmetrical with respect to each other. An independent claim is also included for a method for operating a propelling gas exhaust assembly.