METHOD OF VARYING AN ANNULAR FAN EXIT AREA OF A GAS TURBINE ENGINE

METHOD OF VARYING AN ANNULAR FAN EXIT AREA OF A GAS TURBINE ENGINE

A method of varying an annular fan exit area of a gas turbine engine (10) comprising the step of asymmetrically adjusting a first flap assembly segment (44A ... 44D) relative a second flap assembly segment to adjust an annular fan exit throat area.

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Hauptverfasser: WINTER, Michael, HANSON, Russell B
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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creator WINTER, Michael
HANSON, Russell B
description A method of varying an annular fan exit area of a gas turbine engine (10) comprising the step of asymmetrically adjusting a first flap assembly segment (44A ... 44D) relative a second flap assembly segment to adjust an annular fan exit throat area.
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subjects BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title METHOD OF VARYING AN ANNULAR FAN EXIT AREA OF A GAS TURBINE ENGINE
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