EXHAUST STUB FOR AN AIRCRAFT ENGINE ASSEMBLY

An aircraft engine assembly (15) can include an engine (16) having an exhaust turbine with drive shaft (21) and exhaust collector (25), a propeller (17) rotationally coupled to the drive shaft (21) and defining a rotational axis (20), and an exhaust stub (30) to direct exhaust gases away from the ai...

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Bibliographische Detailangaben
1. Verfasser:	IGLEWSKI, Tomasz
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINE PLANTS IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PARACHUTES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	An aircraft engine assembly (15) can include an engine (16) having an exhaust turbine with drive shaft (21) and exhaust collector (25), a propeller (17) rotationally coupled to the drive shaft (21) and defining a rotational axis (20), and an exhaust stub (30) to direct exhaust gases away from the aircraft (1).