Ex Parte Ackerman et al - Page 4


                  Appeal 2007-0687                                                                                         
                  Application 10/797,422                                                                                   
             1           Further, according to the Appellants’ specification, the terms                                    
             2    “alumina” and “aluminum oxide” refer interchangeably to those compounds                                  
             3    and compositions comprising Al2O3.  Specification, p. 5, ll. 27-29.                                      
             4           The Appellants disclose that the term “alumina precursor” refers to                               
             5    those aluminum compounds that are capable of being converted to alumina.                                 
             6    Suitable alumina precursors include alumina sols and aluminum alkoxides.                                 
             7    Specification, p. 12, ll. 3-8.                                                                           
             8           Hasz discloses a method for protecting thermal barrier coatings from                              
             9    degradation caused by environmental contaminants.  Hasz, col. 1, ll. 9-11.                               
           10            Environmental contaminants include contaminants from fuel and air                                 
           11     sources.  Hasz, col. 2, ll. 64-67.                                                                       
           12            More specifically, the invention disclosed in Hasz relates to the use of                          
           13     an impermeable coating on a thermal barrier coating, where the impermeable                               
           14     coating reduces infiltration of liquid contaminant compositions into the                                 
           15     thermal barrier coating.  Hasz, col. 1, ll. 11-15.                                                       
           16            According to Hasz, thermal barrier coatings are deposited onto gas                                
           17     turbine and other heat engine parts to reduce heat flow and to limit the                                 
           18     operating temperature of metal parts.  These coatings are generally a ceramic                            
           19     material, such as yttria-stabilized zirconia ceramic coating.  Hasz, col. 1, ll.                         
           20     19-27.                                                                                                   
           21            Hasz discloses that the ideal system for a hot high temperature engine                            
           22     part consists of a thermal barrier ceramic layer deposited onto a bond coat                              
           23     which exhibits good corrosion resistance and closely matched thermal                                     
           24     expansion coefficients.  Hasz, col. 1, ll. 41-45.                                                        



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