GAS TURBINE ENGINE CENTER BODY ARCHITECTURE

A center body support (64) for a gas turbine engine (20) includes an outer annular wall (68). An aft flange (72) extends radially outward from the outer annular wall (68). A brace (69) interconnects the aft flange (72) to a forward portion (74) of the outer annular wall (68). The aft flange (72), br...

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Bibliographische Detailangaben
Hauptverfasser:	DITOMASSO, John C, REINHARDT, Gregory E
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A center body support (64) for a gas turbine engine (20) includes an outer annular wall (68). An aft flange (72) extends radially outward from the outer annular wall (68). A brace (69) interconnects the aft flange (72) to a forward portion (74) of the outer annular wall (68). The aft flange (72), brace (69) and forward portion (74) of the outer annual wall (68) provide a unitary, one-piece structure.