Nut system and aircraft engine mounting structure comprising...

Aeronautics and astronautics – Aircraft power plants – Mounting

Reexamination Certificate

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Reexamination Certificate

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08042764

ABSTRACT:
A nut system including a nut including a main thread with pitch p1and arranged along a screwing axis of the nut. A threaded device is coupled in rotation with the nut, the threaded device including a secondary non-screwed thread on the main thread from which it is separated, the secondary thread being arranged along the screwing axis and having a pitch p2different from p1. Such a nut system may find application with a device for resistance of thrusts generated by an aircraft engine.

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patent: 2008/0023584 (2008-01-01), Beaufort
patent: 2008/0042007 (2008-02-01), Machado
patent: 0 879 759 (1998-11-01), None
patent: 2 010 969 (1979-07-01), None
patent: 2 191 299 (2002-10-01), None

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