Patent SE-336852-B (SE)
Inventor: GATLEY J
IPC: G21C3/18
Filed: 1968-12-10
Abstract: 1,246,275. Fuel elements. UNITED KING- DOM ATOMIC ENERGY AUTHORITY. 22 Nov., 1968 [20 Dec., 1967], No. 57972/67. Heading G6C. A tubular fuel pin for use in a fuel assembly of a liquid metal cooled fast breeder reactor comprises inner and outer tubular sheaths 1, 5 of stainless steel secured by welding to an upper end fitting 3 with the lower end of the main length 28 of the outer sheath 5 welded to a flange 33 of an outer sheath part 29, a sleeve part 34 of which is a clearance fit on the lower end portion 24 of the inner sheath 1. The lower end portion of the outer sheath 5 is formed in three parts 29, 30, 31 butt-welded to one another, the part 31 also having a sleeve part 37 which is a clearance fit on the lower end portion 24 of the inner sheath 1. The part 31 which terminates the annular space between the sheaths 1, 5 has a single longitudinal bore 38 communicating with a capillary tube 39 helically wound around the exterior of the outer sheath 5 with its upper end 61 in a recess 62 in an inwardly sloping part 63 of the upper end fitting 3. A bellows seal 41 between the sheaths 1, 5 consists of spaced coaxial sleeve parts 42, 43 welded to the lower end portion 24 of the inner sheath 1 and trapping between them the upper cylindrical part 44 of a bellows 45, the lower cylindrical part 46 of which is trapped between the sleeve part 34 of the outer sheath part 29 and a sleeve part 47 welded to the sleeve part 34. A further bellows seal 49 is secured in a similar manner immediately below the bellows seal 41. The annular space between the sheaths 1, 5 contains in descending order an annular distance-piece 7 abutting the end fitting 3, a column of stacked annular pellets 8 of breeder fuel, an annular separator 9, fissile fuel 10 in the form of vibrocompacted particles of mixed UO 2  and PuO 2  within which five spacers 12 are disposed equidistantly, an apertured platform 11, a body 15 of molybdenum knitmesh, an apertured platform 14, a spacer ring 20, a column of annular breeder fuel pellets 21, and an apertured retaining ring 22. The spacers 12 are of stainless steel and have radial projections 13, the positions of which are staggered from one spacer to the next. These spacers provide a measure of prevention against fuel clumping after inadvertent overheating by acting as chills. The remainder of the fuel pin serves largely as a reservoir 27 for gaseous fission products and is sealed by the bellows seal 41. Should this seal fail, the gas will leak into the annular space 48 situated beneath the seal and containing the bellows seal 49, from which space the gas is discharged through the tube 39 into the coolant at the upper end of the fuel pin. The tube 39 provides a long capillary path for decay of short-lived fission products and serves, by engagement with the outer sheaths of adjoining fuel pins, to space the fuel pins in a fuel assembly. An orifice plate 59 is mounted in the bore of the lower end fitting 56, the orifice area being chosen to control the flow of coolant through the inner sheath 1. The fuel pins in the outer region of a fuel assembly may have a larger orifice area than do those in the central region.