INLOPP TILL GASTURBINKRAFTANLEGGNING

An inlet for a gas turbine power plant with a translating annular ring which cooperates with the nose cone to reduce the effective inlet area, serving to reduce compressor noise.

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Bibliographic Details
Main Authors R A STREIB, D J STEWART
Format Patent
LanguageSwedish
Published 04.12.1978
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
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Summary:An inlet for a gas turbine power plant with a translating annular ring which cooperates with the nose cone to reduce the effective inlet area, serving to reduce compressor noise.
Bibliography:Application Number: SE19750012630