Gas turbine engine having an accessory gearbox
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United States of America Patent
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Jan 9, 2024
Grant Date -
Oct 5, 2023
app pub date -
Jul 19, 2021
filing date -
Jul 29, 2020
priority date (Note) -
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status (Latency Note)
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Abstract
A gas turbine engine has an accessory gearbox disposed outside of a bypass channel and connected to a housing part, which radially delimits the bypass channel, in a connection region near the housing part and in a connection region far from the housing part. A connecting element is provided between the housing part and the connection region far from the housing part. A longitudinal axis of the connecting element includes an angle in the range of 75° to 115° with a vertical axis of the accessory gearbox. The connecting element can vary a distance between the far connection region and a connection point of the connecting element on the housing part such that deformation of the housing part and a resulting position change of the connection point cause a lesser deflection of the accessory gearbox than a deflection with an unchanged length of the connecting element.
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