Thermal barrier coatings for substrates comprising titanium. The thermal barrier coating may include a bond layer, an insulating layer, and a sealant layer. The bond layer may include titanium, a titanium alloy, an intermetallic compound of titanium, and/or a titanium metal matrix composite. The bond layer may have a superlattice structure having a periodically repeating group of layers. Methods for producing the thermal barrier coatings and articles of manufacture employing the thermal barrier coatings.
Thermal protection system for lightweight hypersonic missile fin
19.04.2022
Patent
Elektronische Ressource
Englisch
IPC: | B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64G Raumfahrt , COSMONAUTICS / C23C Beschichten metallischer Werkstoffe , COATING METALLIC MATERIAL |
THERMAL PROTECTION SYSTEM FOR LIGHTWEIGHT HYPERSONIC MISSILE FIN
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|Thermal protection system for lightweight hypersonic missile fin
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|Hypersonic Missile Propulsion System
NTIS | 1998
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