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
2022-04-19
Patent
Electronic Resource
English
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
European Patent Office | 2022
|THERMAL PROTECTION SYSTEM FOR LIGHTWEIGHT HYPERSONIC MISSILE FIN
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|Thermal protection system for lightweight hypersonic missile fin
European Patent Office | 2023
|THERMAL PROTECTION SYSTEM FOR LIGHTWEIGHT HYPERSONIC MISSILE FIN
European Patent Office | 2021
|Hypersonic Missile Propulsion System
NTIS | 1998
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