GAS TURBINE ENGINE CONVERGENT/DIVERGENT NOZZLE WITH UNITARY SYNCHRONIZATION RING FOR ROLLER TRACK NOZZLE

GAS TURBINE ENGINE CONVERGENT/DIVERGENT NOZZLE WITH UNITARY SYNCHRONIZATION RING FOR ROLLER TRACK NOZZLE

A nozzle system includes a static structure (52) including a multiple of convergent flap rails (114) and a synchronization ring (80) including an inner ring (90) radially spaced from an outer ring (94) via a multiple of struts (130). The multiple of convergent flap rails (114) extend at least partia...

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Bibliographische Detailangaben
1. Verfasser: PETERS, DONALD W
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Beschreibung
Zusammenfassung:A nozzle system includes a static structure (52) including a multiple of convergent flap rails (114) and a synchronization ring (80) including an inner ring (90) radially spaced from an outer ring (94) via a multiple of struts (130). The multiple of convergent flap rails (114) extend at least partially between the inner ring (90) and the outer ring (94).