Abstract:
The present inventions incorporate self-healing mechanisms into current and future EBC systems. Such approaches have the potential to form environmental protection materials (i.e. thermally grown silicate compositions) in-situ to enable the ability to provide environmental protection to SiC based ceramics even in the event that cracks or voids form from within the EBC layer. In this disclosure, novel, self-healing EBC systems are disclosed along with coating synthesis techniques required to deposit the materials, microstructures and architectures. This research is anticipated to result in a thermal/environmental barrier coating system (T/EBC) that provides improved durability over current coatings. These advancements will aid the use of Si-based ceramics in a range of high temperature applications such a gas turbine engines and heat exchangers. These advances will not only benefit military engines, but also commercial and industrial engines requiring greater performance.
Abstract:
The present inventions incorporate self-healing mechanisms into current and future EBC systems. Such approaches have the potential to form environmental protection materials (i.e. thermally grown silicate compositions) in-situ to enable the ability to provide environmental protection to SiC based ceramics even in the event that cracks or voids form from within the EBC layer. In this disclosure, novel, self-healing EBC systems are disclosed along with coating synthesis techniques required to deposit the materials, microstructures and architectures. This research is anticipated to result in a thermal/environmental barrier coating system (T/EBC) that provides improved durability over current coatings. These advancements will aid the use of Si-based ceramics in a range of high temperature applications such a gas turbine engines and heat exchangers. These advances will not only benefit military engines, but also commercial and industrial engines requiring greater performance.
Abstract:
A method is disclosed, which can comprise via a transonic gas jet, depositing a thin film of LiPON on a substrate via a directed vapor deposition process. The transonic gas jet transports a thermally evaporated vapor cloud comprising the LiPON, wherein, the transonic gas jet comprises one of (a) substantially entirely nitrogen (N2) gas; or (b) nitrogen (N2) gas as a dopant in a concentration greater than 10% by volume in an inert carrier gas.
Abstract:
Certain exemplary embodiments can provide a method, which can comprise via a transonic gas jet, depositing a thin film of LiPON on a substrate via a directed vapor deposition process. The transonic gas jet transports a thermally evaporated vapor cloud comprising the LiPON, wherein, the transonic gas jet comprises one of (a) substantially entirely nitrogen (N2) gas; or (b) nitrogen (N2) gas as a dopant in a concentration greater than 10% by volume in an inert carrier gas.
Abstract:
Certain exemplary embodiments can provide a system, which can comprise an ultra-thin polymer ceramic composite separator. The ultra-thin polymer ceramic composite separator can comprise Li-ion conducting ceramic material. The ceramic composite separator has a columnar grained microstructure. The ultra-thin polymer ceramic composite separator can comprise a single or bi-layer combination of LiPON, LATP, garnets, lithium sulfides, or Li1+2xZr2−zCa(PO4)3.
Abstract:
Certain exemplary embodiments can provide a method, which can comprise depositing a substantially uniform coating on a substrate. The coating is deposited via a coating material stream that emanates from one or more vapor sources. The coating material stream is directed toward the substrate via a carrier gas in a chamber under vacuum.
Abstract:
Certain exemplary embodiments can provide a method, which can comprise stabilizing adherence of a ceramic layer to a bond coat of a thermal barrier coating system, via incorporation of iron and cobalt into the bond coat at a given level. The bond coat can comprise MCrAlY, wherein M is selected from the group consisting of nickel, cobalt, iron and mixtures thereof.
Abstract:
A deposition method that improves the direct vapor deposition process by enabling the vapor deposition from multiple evaporate sources to form new compositions of deposition layers over larger and broader substrate surface areas than heretofore could be covered by a DVD process, including providing layers with varying vapor pressures onto the substrate, as well as columnar thermal barrier over an environmental barrier and the gradual modification of the composition of the environment barrier coating and/or columnar thermal barrier coating.
Abstract:
The present invention provides for a method and apparatus for the directed vapor deposition (DVD) on non-line of sight (NLOS) portions of a substrate. The method and apparatus includes evaporating a first material for deposition on to the substrate, the evaporating generating a plurality of vapor molecules. The method and apparatus therein provides for the insertion of a carrier gas and the direction of the vapor molecules to be deposited in NLOS regions of the substrate. One embodiment utilizes plasma activation to ionize the vapor particles and bias the substrate to attract the charged vapor molecules onto the NLOS portion. Another embodiment uses an inert gas as the carrier gas. Another embodiment includes pre-heating the carrier gas prior to its insertion into the deposition chamber. Whereby the varying embodiments and combinations herein improve NLOS DVD.