Metal plated plastic ACM part with internal thermally adaptive structure
A component, having: a base having beads formed of with first and second thermoplastic polymers, respectively having first and second coefficients of thermal expansion (CTE), where each of the beads has an outer surface and an inner surface that abut each other; a lower support section formed on the base, having a mixture of a third thermoplastic polymer and a catalyst formed with metal; an upper support section on the component, formed on the lower support section via electrolysis deposition, a metallic coating, to thereby control thermal expansion and contraction of the component; and reinforcement fibers embedded the base, the lower support section and the upper support section.
1. A component, comprising:
a base having beads formed of with first and second thermoplastic polymers, respectively having first and second coefficients of thermal expansion (CTE), where each of the beads has an outer surface and an inner surface that abut each other;
a lower support section formed on the base, having a mixture of a third thermoplastic polymer and a catalyst formed with metal;
an upper support section on the component, formed on the lower support section via electrolysis deposition, a metallic coating, to thereby control thermal expansion and contraction of the component; and
reinforcement fibers embedded the base, the lower support section and the upper support section.
2. The component of claim 1 , wherein the first and second CTEs differ from each other.
3. The component of claim 1 , wherein:
the beads are formed as an interconnected lattice, and wherein a void is formed in a center of each of the beads.
4. The component of claim 1 , wherein:
the fibers extend at least partially through ones of the beads, from a location adjacent to the lower support section, extending through the lower support section, and the fibers extend at least partially thorough the upper support section.
5. The component of claim 3 , wherein:
the outer surface is formed to provide a first CTE gradient; and
printing the inner surface is formed to provide a second CTE gradient.
6. The component of claim 5 , wherein:
the first and second CTE gradients are opposite of each other to form a radial CTE gradient.
7. The component of claim 1 , wherein the first and second thermoplastic polymers are the same as each other.
8. The component of claim 1 , wherein the first thermoplastic polymer is Acrylonitrile butadiene styrene (ABS).
9. The component of claim 1 , wherein the catalyst is palladium(II) chloride (PdCl 2 ).
10. The component of claim 1 , wherein the component is formed via stereolithography (SLA) or fused deposition modeling (FDM).
11. An air cycle machine of an aircraft, comprising the component of claim 1 .