Turbine Engine having First and Second Accessory Gearboxes
Number of patents in Portfolio can not be more than 2000
United States of America
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Issued Date -
Mar 6, 2025
app pub date -
Sep 5, 2023
filing date -
Sep 5, 2023
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Abstract
A turbine engine having an inner cowl that circumscribes at least a portion of an engine core, where the inner cowl is radially spaced from the engine core to define an inner cowl space. An outer cowl circumscribes at least a portion of the inner cowl where the outer cowl includes a radially outer surface spaced from a radially inner surface to define an outer cowl space. A fairing extends radially between the inner cowl and the outer cowl. A first accessory gearbox is located in the inner cowl space and the fairing. A second accessory gearbox is located in the outer cowl space and operably couples to the first accessory gearbox.
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