GAS TURBINE ENGINE ACCESSORY ARCHITECTURE
A gas turbine engine comprises a compressor, a combustor and a turbine. A housing for the gas turbine engine includes a mount member to define a vertically upper location. Sides of the engine are defined on opposed sides of the mount, with a fuel filter, a fuel pump and a fuel flow meter being posit...
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Main Authors | , , |
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Format | Patent |
Language | English French German |
Published |
18.01.2017
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Subjects | |
Online Access | Get full text |
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Summary: | A gas turbine engine comprises a compressor, a combustor and a turbine. A housing for the gas turbine engine includes a mount member to define a vertically upper location. Sides of the engine are defined on opposed sides of the mount, with a fuel filter, a fuel pump and a fuel flow meter being positioned on a first side and an oil pump, an oil filter and an oil tank positioned on a second of the sides. |
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Bibliography: | Application Number: EP20150783136 |