Method for controlling aluminum titanate ceramic filter properties
Abstract
A method for improving the thermo-mechanical properties of an aluminum-titanate composite, the composite including at least one of strontium-feldspar, mullite, cordierite, or a combination thereof, including: combining a glass source and an aluminum-titanate source into a batch composition; and firing the combined batch composite composition to produce the aluminum-titanate composite. Another method for improving the thermo-mechanical properties of the composite dips a fired composite article into phosphoric acid, and then anneal the dipped composite article. The resulting composites have a thin glass film situated between the ceramic granules of the composite, which can arrest microcrack propagation.
Claims
exact text as granted — not AI-modified1 .- 11 . (canceled)
12 . A method for improving the thermo-mechanical properties of an aluminum titanate-based composite, comprising:
dipping a fully fired aluminum titanate composite into an aqueous phosphoric acid solution of 0.5 to 10 wt %; and annealing the dipped composite, to provide phosphorous incorporation into the resulting composite of 0.5 to 2 wt %, the weight % being based on a superaddition relative to the weight of the un-dipped composite.
13 . A method for toughening a microcracked aluminum titanate ceramic, comprising:
creating an intergranular glass film within the ceramic, the film having a thickness of from about 20 nm to 500 nm, and the film interacts with the microcracks and limits uncontrolled growth of the microcracks.
14 . The method of claim 13 wherein the ceramic is toughened from about 5 to about 25%, as demonstrated by an increase in the modulus of rupture measured by 4-point bending relative to a ceramic prepared without the intergranular glass film.
15 . The method of claim 12 wherein the dipped and annealed aluminum titanate-based composite has an average CTE that is substantially unchanged by the dipping procedure, the microcrack density of the dipped and annealed aluminum titanate-based composite is increased, and the dipped and annealed aluminum titanate-based composite has a significantly larger hysteresis in a heating-cooling cycle compared to an undipped and annealed composite.
16 . The method of claim 12 wherein the dipping is accomplished in aqueous 10 wt % phosphoric acid.
17 . The method of claim 12 wherein the annealing is accomplished at 1400° C.
18 . The method of claim 12 wherein the aluminum titanate-based composite comprises grains of an aluminum-titanate crystalline phase and grains of a strontium-feldspar crystalline phase, and an intergranular glass phase between the grains of the aluminum-titanate crystalline phase and the strontium-feldspar crystalline phase.
19 . The method of claim 12 wherein the thermo-mechanical property of the dipped and annealed composite is material strength and the material strength is improved from 310 psi to 467 psi compared to an un-dipped composite.
20 . The method of claim 12 wherein the thermo-mechanical property of the dipped composite is the CTE which is decreased from 8.4 10 −7 K −1 to 7.6 10 −7 K −1 over 25 to 1000° C. for a dipped and annealed composite having a pore size increased by 3 micrometers compared to an un-dipped and annealed composite.
21 . The method of claim 12 wherein the resulting annealed aluminum titanate-based composite has a porosity greater than 42%, a median pore size greater than 16 micrometers, and a CTE of less than 9×10 −7 K −1 from 25 to 1000° C.
22 . The method of claim 12 wherein the resulting annealed aluminum titanate-based composite is a honeycomb filter.
23 . The method of claim 12 further comprising selectively plugging the ends of the honeycomb filter in an alternating checkerboard pattern to form a through wall filter for exhaust gas particle filtration.
24 . The method of claim 22 further comprising washcoating the honeycomb filter with a catalyst suitable for catalytic conversion applications.
25 . The method of claim 12 wherein the feldspar phase, prior to annealing, has a monoclinic structure.
26 . The method of claim 12 wherein the annealing produces a strengthened product having a feldspar phase with a triclinic symmetry.Join the waitlist — get patent alerts
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