Patent Number: 062122509
Section: claims

1. A method for providing a leak-tight metal enclosure to a fuel matrix penetrated by coolant channels, wherein the mutually contacting surfaces of said metal enclosure and said fuel matrix are metallurgically bonded, said method comprising the steps of: (a) placing a metal cladding about the lateral surface of said fuel matrix;  (b) disposing metal coolant tubes which have been sealed at one end within said coolant channels;  (c) placing a first perforated header plate having tubular extensions at that end of the fuel matrix from which the open coolant tube ends protrude, said coolant tubes passing through said first perforated header plate and said tubular extensions and terminating even with the ends of said extensions;  (d) placing a second perforated header plate at the other end of said fuel matrix, said sealed coolant tube ends terminating within the perforations substantially even with the outer end thereof;  (e) welding, under vacuum, said cladding to said first and second header plates, the open ends of said coolant tubes to the ends of said tubular extensions, and a cover plate over said second header plate;  (f) exposing the assembly comprising the fuel matrix and enclosure to a gas at high temperature and pressure; and  (g) machining said first and second header plates to provide a finished fuel element.  (a) placing a thin continuous sheet of metal cladding about the lateral surface of said fuel matrix;  (b) disposing metal coolant tubes which have been sealed at one end within said coolant channels;  (c) placing a first perforated header plate at that end of said fuel matrix from which the open ends of said coolant tubes protrude, said header plate having tubular extensions on its face disposed away from said fuel matrix, said tubular extensions being coaxial with the perforations through said header plate and spaced to receive said coolant tubes which terminate substantially even with the ends of said tubular extensions, said metal cladding partially overlapping said first header plate;  (d) placing a second perforated header plate at that end of said fuel matrix from which the sealed ends of said coolant tubes protrude, said sealed coolant tube ends terminating within the perforations through said second header plate substantially even with the outer end thereof, said metal cladding partially overlapping said second header plate;  (e) welding the ends of said metal cladding to said first and second header plates while under vacuum;  (f) welding a metal cover plate over said second header plate while under vacuum so as to seal the end thereof;  (g) welding the open ends of said coolant tubes to the ends of said tubular extensions while under vacuum;  (h) exposing said fuel matrix and metal enclosure to a gas at high temperature and pressure to effect a diffusion bond between the mutually contacting surfaces of said cladding, coolant tubes, header plates, and fuel matrix; and  (i) machining said header plates so as to open said sealed coolant tube ends and achieve a finished fuel element.  (a) placing a thin continuous sheet of tantalum cladding about the lateral surface of said tungsten matrix;  (b) depositing tantalum coolant tubes which have been sealed at one end within said coolant channels;  (c) placing a first perforated tantalum header plate at that end of said tungsten matrix from which the open ends of said tantalum coolant tubes protrude, said header plate having integral tubular extensions on its face disposed away from said tungsten matrix, said tubular extensions being coaxial with the perforations through said header plate and spaced to receive said coolant tubes, said coolant tubes terminating substantially even with the ends of said tubular extensions, said tantalum cladding partially overlapping said first header plate;  (d) placing a second perforated tantalum header plate at that end of said tungsten matrix from which the sealed ends of said coolant tubes protrude, said sealed coolant tube ends terminating within the perforations through said second header plate substantially even with the outer end thereof, said tantalum cladding partially overlapping said second header plate;  (e) electron beam welding the ends of said tantalum cladding to said first and second header plates while under vacuum;  (f) electron beam welding a metal cover plate over said second header plate while under vacuum so as to seal the end thereof;  (g) electron beam welding the open ends of said coolant tubes to the ends of said tubular extensions while under vacuum;  (h) exposing said tantalum-enclosed tungsten matrix to helium at high temperature and pressure for a time sufficient for a diffusion bond to develop between the mutually contacting surfaces of said tantalum cladding, coolant tubes, header plates, and the uranium fueled tungsten matrix;  (i) machining away said tubular extensions together with the coolant tube portions contained therein; and  (j) removing said cover plate and machining away a sufficient portion of said second perforated header plate so as to open said coolant tube ends bonded therein.  (a) placing a metal cladding about the lateral surface of said fuel matrix;  (b) disposing metal coolant tubes within said coolant channels;  (c) placing a perforated header plate having tubular extensions at each end of the fuel matrix from which the coolant tube ends protrude, said coolant tubes passing through said perforated header plate and said tubular extensions and terminating even with the ends of said extensions;  (d) welding, under vacuum, said cladding to said header plates, and the ends of said coolant tubes to the ends of said tubular extensions;  (e) exposing the assembly comprising the fuel matrix and enclosure to a gas at high temperature and pressure; and  (f) machining said header plates to provide a finished fuel element. 2. A method for providing a leak-tight metal enclosure to a fuel matrix penetrated longitudinally by a multiplicity of coolant channels, wherein the mutually contacting surfaces of said metal enclosure and said fuel matrix are metallurgically bonded, said method comprising the steps of: 3. A method for providing a leak-tight tantalum enclosure to a uranium fueled tungsten matrix penetrated longitudinally by a multiplicity of coolant channels, wherein said tantalum enclosure is diffusion bonded to said tungsten matrix, said method comprising the steps of: 4. A method for providing a leak-tight metal enclosure to a fuel matrix penetrated by coolant channels, wherein the mutually contacting surfaces of said metal enclosure and said fuel matrix are metallurgically bonded, said method comprising the steps of: