Cockpit pedestal and aircraft with a cockpit pedestal
A cockpit pedestal and an aircraft with a cockpit pedestal. The cockpit pedestal includes an integrally-formed frame including an instrument receiving portion defining a plurality of compartments for receiving instruments therein; and a plurality of legs supporting the instrument receiving portion, the plurality of legs being integrally formed with the instrument receiving portion, the plurality of legs being adapted for transferring a load of the plurality of instruments from the instrument receiving portion to a floor of the aircraft cockpit when the cockpit pedestal and the instruments are installed in the aircraft cockpit. In some versions the cockpit pedestal includes a conductive layer electrically grounding the instruments in the cockpit.
1. A cockpit pedestal for supporting a plurality of instruments in an aircraft cockpit, the cockpit pedestal comprising:
an integrally-formed frame including:
an instrument receiving portion defining a plurality of compartments for receiving the plurality of instruments therein;
a plurality of legs supporting the instrument receiving portion, the plurality of legs being integrally formed with the instrument receiving portion,
a first side portion integrally connected to and supporting the instrument receiving portion, the first side portion including at least a first pair of legs of the plurality of legs, the first side extending from the instrument receiving portion, and
a second side portion integrally connected to and supporting the instrument receiving portion, the second side portion including at least a second pair of legs of the plurality of legs, the second side extending from the instrument receiving portion, the first and second side portions being disposed on opposite sides of the instrument receiving portion, and
said first pair of legs and said second pair of legs each forming generally upside-down-U shaped openings on said first and second side portions;
the plurality of legs being adapted for transferring a load of the plurality of instruments from the instrument receiving portion to a floor of the aircraft cockpit when the cockpit pedestal and the plurality of instruments are installed in the aircraft cockpit, wherein the frame is formed by additive manufacturing.
2. The cockpit pedestal of claim 1 , further comprising at least one cover panel connected to at least one lateral side of the frame, the at least one cover panel being a non-load bearing cover panel.
3. The cockpit pedestal of claim 1 , further comprising at least one cover panel connected to the frame, the at least one cover panel being a non-load bearing cover panel, the at least one cover panel covering an entirety of at least one side of the frame.
4. The cockpit pedestal of claim 1 , further comprising a plurality of cover panels connected to and at least partially covering the frame.
5. The cockpit pedestal of claim 1 , wherein the plurality of legs define at least in part at least one access opening for accessing a space defined within the frame, the space being disposed below the instrument receiving portion.
6. The cockpit pedestal of claim 5 , further comprising at least one access cover selectively covering the at least one access opening.
7. The cockpit pedestal of claim 1 , wherein the plurality of compartments includes at least one opening defined in the instrument receiving portion.
8. The cockpit pedestal of claim 1 , wherein the plurality of compartments includes at least one recess defined in the instrument receiving portion.
9. The cockpit pedestal of claim 1 , further comprising at least one conductive layer applied to at least a portion of the frame, the at least one conductive layer being adapted for being electrically connected to the plurality of instruments.