Mechanical connection between a primary nut and secondary nut

Aeronautics and astronautics – Aircraft control – Specific control connection or actuator

Reexamination Certificate

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C244S099200, C244S099400

Reexamination Certificate

active

08052084

ABSTRACT:
The assembly comprises a first and a second nut intended to cooperate with a screw in particular provided in an adjustable tailplane actuator for an aircraft, and a mechanical connection between the first and the second nut comprising means for fusible driving of the second nut by the first nut, in which the mechanical connection also comprises adjustable spacing means forming a wedge between the first and second nuts.

REFERENCES:
patent: 6672540 (2004-01-01), Shaheen et al.
patent: 6685382 (2004-02-01), Capewell et al.
patent: 6851648 (2005-02-01), Perni et al.
patent: 7866602 (2011-01-01), Port-Robach et al.
patent: 2003/0029258 (2003-02-01), Davies et al.
patent: 2004/0200929 (2004-10-01), Perni et al.
patent: 2005/0132831 (2005-06-01), Scholz
patent: 12 94 132 (1969-04-01), None
patent: 103 48 320 (2005-05-01), None
patent: 1 398 542 (2004-03-01), None
patent: 2 885 396 (2006-11-01), None
patent: 2885396 (2006-11-01), None

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