Method of varying a fan duct nozzle throat area of a gas turbine engine

A method of varying a fan duct nozzle throat area of a gas turbine engine includes pivoting a fan nozzle outwardly relative to a longitudinal axis of the gas turbine engine. The fan nozzle is configured to move axially non-contemporaneously with the pivoting of the fan nozzle.

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Bibliographische Detailangaben
1. Verfasser:	HOWE MARK E
Format:	Patent
Sprache:	eng
Schlagworte:	AMUSEMENTS BLASTING CARD, BOARD, OR ROULETTE GAMES CHECKING-DEVICES COIN-FREED OR LIKE APPARATUS COMBUSTION ENGINES ELECTRIC COMMUNICATION TECHNIQUE ELECTRICITY GAMES GAMES NOT OTHERWISE PROVIDED FOR HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS HUMAN NECESSITIES INDOOR GAMES USING SMALL MOVING PLAYING BODIES JET-PROPULSION PLANTS LIGHTING MARINE PROPULSION OR STEERING MECHANICAL ENGINEERING PERFORMING OPERATIONS PHYSICS RELATED EQUIPMENT SHIPS OR OTHER WATERBORNE VESSELS SPORTS TELEPHONIC COMMUNICATION TRANSPORTING VIDEO GAMES WEAPONS
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Beschreibung
Zusammenfassung:	A method of varying a fan duct nozzle throat area of a gas turbine engine includes pivoting a fan nozzle outwardly relative to a longitudinal axis of the gas turbine engine. The fan nozzle is configured to move axially non-contemporaneously with the pivoting of the fan nozzle.