TRANSPIRATIONALLY COOLED EXHAUST CENTER BODY FOR AN AIRCRAFT PROPULSION SYSTEM

An assembly is provided for an aircraft propulsion system. This assembly includes an exhaust center body (52) and a duct system (70). The exhaust center body includes an exterior skin (72). The duct system is fluidly coupled with a plurality of exterior skin perforations (82) in the exterior skin. T...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	SAUNDERS, Adam, ALLOWAY, Richard S, HASLIM, Richard, KELFORD, Bryce T, FRAZIER, Travis M
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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	An assembly is provided for an aircraft propulsion system. This assembly includes an exhaust center body (52) and a duct system (70). The exhaust center body includes an exterior skin (72). The duct system is fluidly coupled with a plurality of exterior skin perforations (82) in the exterior skin. The duct system is configured to direct bypass air received from a bypass flow path (44) within the aircraft propulsion system to the exterior skin perforations.