Thermal barrier composition

Abstract
The thermal barrier composition of the present invention provides polymethylsilsesquioxane dissolved in a crosslinking agent, and a filler and/or hollow glass microspheres.
Description
FIELD AND BACKGROUND OF THE INVENTION

The present invention relates to a thermal barrier composition for use on a variety of substrates that are exposed to high temperatures. Exemplary substrates include pipelines, engine parts including jet engine components, water conduits including tubes in power plants, reactor vessels and exhaust manifolds.


Substrates, particularly metal substrates, can be subjected to high temperatures causing fatigue, cracking, distortion and the like of the substrate. For example, components of a jet engine or the surrounding parts of the jet can be exposed to temperatures in excess of 1800° F. In such a situation, it is readily apparent that fatiguing or cracking can lead to catastrophic failure. Similarly, piping used in various manufacturing facilities can be subjected to temperatures in excess of 400° F. caused by the liquid or gas passing through the pipe. In such an application, it is preferred that the coating not only provide a thermal barrier but also provide anti-corrosion properties and be abrasion resistant.


SUMMARY OF THE INVENTION

The thermal barrier composition of the present invention comprises polymethylsilsequioxane dissolved in a crosslinking agent, preferably titanium isopropoxide, hollow glass microspheres, and optionally a filler.


In another embodiment, the present invention provides a composition that is corrosion resistant and is able to be a pin hole free coating. The composition comprises polymethylsilsequioxane dissolved in a crosslinking agent, preferably titanium isopropoxide, and a mica filler.







DETAILED DESCRIPTION OF THE INVENTION

As briefly discussed above, the present invention provides a thermal barrier composition comprising polymethylsilsequioxane dissolved in a crosslinking agent and hollow glass microspheres and optionally a filler. Suitable crosslinking agents include titanium isopropoxide, titanium ethyl hexoxide, titanium methoxide, titanium ethoxide, titanium butoxide, titanium diisopropoxide (bis, 2,4 pentadionate), titanium diisopropoxide bis (ethyl acetoacetate), and titanium diisopropoxide (bis tetremethyl heptandionate). Preferably thin walled glass microspheres are used.


In another embodiment, the present invention provides a corrosion resistant composition comprising polymethylsilsequioxane dissolved in a crosslinking agent, (e.g., titanium isopropoxide), and a mica filler.


The thermal barrier composition of the present invention can be coated onto a wide variety of substrates including steel, stainless steel, titanium, aluminum, magnesium and zinc. The coating can withstand continuous use temperatures of 1800° F. or higher. Moreover, the composition is resistant to corrosive agents such as nitrogen and sulfur compounds.


The polymethylsilsesquioxane (“POSS”) is dissolved in a crosslinking agent preferably titanium isopropoxide. By dissolving in titanium propoxide, up to about 50 percent of the POSS can be dissolved as compared to about 10 percent or less solubility in solvents.


The thermal barrier composition may include a solvent such as isopropanol, ethanol, methanol and butanol. The thermal barrier composition may also optionally include fillers such as, without limitation, glass fibers, fumed silica, mica, kaolin, bentonite, talc, zinc oxides, iron oxides and pigments or other fillers, as will be readily apparent to those skilled in the art. Typically the volume percent of glass microspheres is from about 30 percent to about 80 percent. Anti-corrosion agents such as zinc phosphates and zinc salts can also be added.


In operation, the compositions of the present invention can be applied to a substrate by roll-coating, brush, spray coating dipping and the like.


The following specific examples are provided to afford a better understanding of the present invention to those skilled in the art. It is to be understood that these examples are intended to be illustrative only and is not intended to limit the invention in any way.


EXAMPLES
Example 1



  • 1. Prepare polymethylsilsequioxane (POSS)/Titanium isopropoxide (TIPO) solution by mixing 42 weight percent POSS with 58 weight percent TIPO. Heat for six (6) hours under pressure at 140° C.

  • 2. Mix the following ingredients at room temperature and pressure:



















POSS/TIPO (42/58) solution
29.76 wt %



Hollow Glass Microspheres 5–100 micron
16.67



Isopropanol
52.08



Fumed silica
 1.49











Application: Apply the coating in one continuous film build to the desired thickness. Insulation value is 100° C./millimeter.


Example 2



  • 1. Prepare polymethylsilsequioxane/Titanium isopropoxide solution by mixing 42 weight percent POSS with 58 weight percent TIPO. Heat for six (6) hours under pressure at 140° C.

  • 2. Mix the following ingredients at room temperature and pressure:



















POSS/TIPO (42/58) solution
10.53 wt %



Custer Mica A-325
52.00



Isopropanol
37.47











Application: Spray one layer of the coating to a thickness of 5–10 mils. Allow to tack over and spray a second layer of 5–10 mils. Two layers must be used to achieve a pin hole free coating.


The invention has been described with respect to the preferred embodiments set forth above. It should be appreciated however that these embodiments are for the purposes of illustrating the invention, and are not intended to limit the scope of the invention as defined by the claims.

Claims
  • 1. A thermal barrier coating composition (a) polymethylsilsesquioxane dissolved in a crosslinking agent; and(b) hollow glass microspheres.
  • 2. The thermal barrier coating composition according to claim 1, wherein the crosslinking agent is titanium isopropoxide.
  • 3. The thermal barrier coating compositiong according to claim 1, further comprising a filler selected from the group consisting of fumed silica, mica, kaolin, bentonite, talc, zinc oxides, iron oxides and pigments.
  • 4. A substrate coated with a thermal barrier composition comprising polymethylsilsesquioxane dissolved in a crosslinking agent and hollow glass microspheres.
  • 5. The substrate according to claim 4, wherein the substrate is selected from the group consisting of steel, stainless steel, titanium, aluminum, magnesium and zinc.
  • 6. The substrate according to claim 4, wherein the crosslinking agent is titanium isopropoxide.
  • 7. The substrate according to claim 4, wherein the composition includes a filler selected from the group consisting of fumed silica, mica, kaolin, bentonite, talc, zinc oxides, iron oxides, and pigments.
RELATED APPLICATION

This application claims priority to Provisional Application No. 60/461,800 filed Apr. 10, 2003 and is a continuation-in-part of patent application Ser. No. 10/814,213 filed Mar. 31, 2004, now abandoned the disclosures of which are hereby incorporated by reference in their entirety.

US Referenced Citations (30)
Number Name Date Kind
3933712 Vanaglash, Jr. Jan 1976 A
4000108 Yokokawa et al. Dec 1976 A
4405679 Fujioka et al. Sep 1983 A
4602959 Kurita et al. Jul 1986 A
4725501 Rukavina et al. Feb 1988 A
4753827 Yoldas et al. Jun 1988 A
4814017 Yoldas et al. Mar 1989 A
4816288 Rukavina et al. Mar 1989 A
4990547 Stovicek Feb 1991 A
5068277 Vukov et al. Nov 1991 A
5096488 Stovicek Mar 1992 A
5173110 Stovicek Dec 1992 A
5218059 Kishihara et al. Jun 1993 A
5232996 Shah et al. Aug 1993 A
5298060 Harakal et al. Mar 1994 A
5331074 Slater et al. Jul 1994 A
5433941 Patel Jul 1995 A
5593732 Griffith Jan 1997 A
5663215 Milligan Sep 1997 A
5688851 Kress Nov 1997 A
5939478 Beck et al. Aug 1999 A
5942583 Azechi Aug 1999 A
5958116 Kishihara et al. Sep 1999 A
6013724 Mizutani et al. Jan 2000 A
6045869 Gesser et al. Apr 2000 A
6313193 Simendinger, III Nov 2001 B1
6476095 Simendinger, III Nov 2002 B1
6559201 Simendinger, III May 2003 B1
6933334 Cosby et al. Aug 2005 B1
20040262739 Sethumadhavan et al. Dec 2004 A1
Foreign Referenced Citations (6)
Number Date Country
0563939 Oct 1993 EP
0664322 Jul 1995 EP
0851009 Jul 1998 EP
62-277475 Dec 1987 JP
2000319582 Nov 2000 JP
WO 0102506 Jan 2001 WO
Related Publications (1)
Number Date Country
20050106381 A1 May 2005 US
Provisional Applications (1)
Number Date Country
60461800 Apr 2003 US
Continuation in Parts (1)
Number Date Country
Parent 10814213 Mar 2004 US
Child 10960666 US