GAS TURBINE ENGINE ACCESSORY ARCHITECTURE
First Claim
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1. A gas turbine engine comprising:
- a compressor, a combustor and a turbine; and
a housing for said gas turbine engine, with said housing including a mount member to define a vertically upper location, and sides of the engine being 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 said sides.
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Abstract
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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Citations
20 Claims
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1. A gas turbine engine comprising:
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a compressor, a combustor and a turbine; and a housing for said gas turbine engine, with said housing including a mount member to define a vertically upper location, and sides of the engine being 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 said sides. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20)
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Specification