ASYMMETRIC INLET PARTICLE SEPARATOR FOR GAS TURBINE ENGINE

ASYMMETRIC INLET PARTICLE SEPARATOR FOR GAS TURBINE ENGINE

An asymmetric inlet particle separator (200) for a gas turbine engine (100) includes an inlet (202) having a first cross-sectional shape, and a duct (204) downstream of the inlet. The duct includes a bend (238) upstream from a splitter (226), a scavenge branch (228) and an engine airflow branch (230...

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Hauptverfasser: JUDD, Zedic, SHEORAN, Yogendra, TUCKER, Bradley, HOLLINGSHEAD, Douglas, PEARSON, John
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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creator JUDD, Zedic
SHEORAN, Yogendra
TUCKER, Bradley
HOLLINGSHEAD, Douglas
PEARSON, John
description An asymmetric inlet particle separator (200) for a gas turbine engine (100) includes an inlet (202) having a first cross-sectional shape, and a duct (204) downstream of the inlet. The duct includes a bend (238) upstream from a splitter (226), a scavenge branch (228) and an engine airflow branch (230). The splitter is outside of a line of sight from the inlet and the splitter separates the scavenge branch from the engine airflow branch. The asymmetric inlet particle separator includes an annulus (206) downstream of the engine airflow branch configured to be coupled to the gas turbine engine. The annulus has a second cross-sectional shape, and the engine airflow branch transitions from the first cross-sectional shape to the second cross-sectional shape.
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subjects AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title ASYMMETRIC INLET PARTICLE SEPARATOR FOR GAS TURBINE ENGINE
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