Aircraft engine mount comprising at least one transverse nut and aircraft comprising the said engine mount
AssigneeAirbus Operations GmbH
InventorsFrederic JOURNADE, Eric BOUCHET, Nicolas GROSSEAU, Antoine MUTIN
Life of this patent
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Abstract
An aircraft engine mount which comprises first and second parts connected by connecting elements and wherein one of the two connected parts comprises at least one transverse hole opening onto an access face of the part and into which there open at least two passage holes each intended to house a threaded shank of one of the connecting elements. The engine mount comprises a transverse nut which comprises at least two bodies joined together each having a tapped hole configured to engage with one of the threaded shanks.
Claims9
An aircraft engine assembly connecting an engine to a pylon and comprising:
- a first part secured to or forming part of a first of the elements that are the engine and the pylon,
- a second part secured to or forming part of a second of the elements that are the engine and the pylon,
- connecting elements each of which comprises a screw which comprises a head configured to bear against the first part in operation and a threaded shank,
- the first and second parts each comprising a passage orifice for each connecting element,
- the second part comprising at least one transverse hole opening onto an access face of the second part and into which there open at least two passage orifices, and
- a nut configured to engage with one of the threaded shanks, the nut comprising a transverse nut which comprises at least two bodies joined together and which each comprise a tapped hole, the tapped holes of the nut having axes that substantially coincide with axes of the passage orifices in operation.
Dependencies are inferred from the claim text.