Patent Number: 
Section: claims

1. A method of manufacturing a laminated scintillator panel having a structure in which a scintillator layer and a non-scintillator layer are repeatedly laminated in a direction substantially parallel to the direction of radiation incidence, the method comprising: a step of forming a laminate by repeatedly laminating the scintillator layer and the non-scintillator layer; and a joining step of pressurizing the laminate to join the scintillator layer and the non-scintillator layer integrally,wherein:the step of forming the laminate comprises a step of forming a plurality of partial laminates in which the scintillator layer and the non-scintillator layer are joined, and a step of laminating the plurality of partial laminates to form the laminate, andeach of the partial laminates is formed by coating a composition containing scintillator particles and an adhesive resin on a polymer film. 2. The method of manufacturing a laminated scintillator panel according to claim 1 , wherein the scintillator layer contains at least one adhesiveness resin. 3. The method of manufacturing a laminated scintillator panel according to claim 1, wherein the non-scintillator layer is composed mainly of a polymer film. 4. The method of manufacturing a laminated scintillator panel according to claim 1, wherein, in the joining step, the laminate is pressurized in such a manner that the scintillator layer and the non-scintillator layer are substantially parallel to the direction of radiation incidence. 5. The method of manufacturing a laminated scintillator panel according to claim 1, wherein, in the joining step, the laminate is heated in a pressurized state. 6. The method of manufacturing a laminated scintillator panel according to claim 1, further comprising a step of flattening a joining end face of the laminate joined in the joining step. 7. The method of manufacturing a laminated scintillator panel according to claim 1, further comprising a step of bonding the laminate joined in the joining step to a support. 8. A method of manufacturing a lattice for Talbot selected from G0 lattice, G1 lattice and G2 lattice, comprising a step of forming a laminate by applying a composition containing high-X-ray-absorbing particles and an adhesive resin on a polymer film to form a partial laminate and laminating a plurality of the partial laminate to form the laminate, and a joining step of pressurizing the laminate in such a manner that the partial laminates are substantially parallel to the direction of radiation incidence to join the partial laminates integrally. 9. The method of manufacturing a lattice for Talbot according to claim 8, wherein, in the joining step, the laminate is heated in a pressurized state. 10. The method of manufacturing a lattice for Talbot according to claim 8, further comprising a step of flattening a joining end face of the laminate joined in the joining step. 11. The method of manufacturing a lattice for Talbot according to claim 8, further comprising a step of bonding the laminate joined in the joining step to a support. 12. The method of manufacturing a lattice for Talbot according to claim 9, further comprising a step of flattening a joining end face of the laminate joined in the joining step. 13. The method of manufacturing a lattice for Talbot according to claim 9, further comprising a step of bonding the laminate joined in the joining step to a support. 14. The method of manufacturing a lattice for Talbot according to claim 10, further comprising a step of bonding the laminate joined in the joining step to a support.