Method and system for mounting radio avionics

Details Method and system for mounting radio avionics Method and system for mounting radio avionics

2006-04-25

2006-04-25

Eldred, J. Woodrow (Department: 3644)

Aeronautics and astronautics

Aircraft structure

Details

C211S103000, C211S126150, C211S187000, C211S207000, C211S125000, C248S125100

Reexamination Certificate

active

07032862

ABSTRACT:
A mounting bar system permitting infinite adjustability in mounting avionics-components trays and Dzus-mounted avionics in at least one aircraft cockpit instrument panel assembly. Each mounting bar is slotted along its longitudinal axis. The slot is made to include the shape of a T such that a wider channel exists below the opening of the slot. Spring-loaded nut assemblies set to receive mounting screws from the avionics-components trays are fit within the T slot. Friction provided by the spring holds the nut assembly at any desired location within the T slot. As the nut assembly can be positioned at any location within the T slot, the mounting bar can readily be adjusted to support any avionics-components tray intended for at least one aircraft cockpit instrument panel assembly.

REFERENCES:
patent: 5208735 (1993-05-01), Twachtmann et al.
patent: 5372265 (1994-12-01), Monch
patent: 5695078 (1997-12-01), Otema
patent: 6322040 (2001-11-01), Robertson et al.
patent: 6410995 (2002-06-01), Grouse et al.
patent: 6549424 (2003-04-01), Beseth et al.

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