Abstract: Regardless of the type of specimen, such as a serum or heparinized plasma containing different anticoagulants, which are widely used in general, when a substance to be measured (for example, sIL-2R) in a biological sample is immunologically detected, a measuring method and a kit capable of stably obtaining with high accuracy, unaffected by interfering substances in the specimen, are provided. An immunocomplex between the substance to be measured and an antibody that specifically binds to the substance to be measured is formed in the presence of a sulfated polysaccharide. The kit comprises an antibody that specifically binds to the substance to be measured, and a buffer containing a sulfated polysaccharide.

Abstract: Regardless of the type of specimen, such as a serum or heparinized plasma containing different anticoagulants, which are widely used in general, when a substance to be measured (for example, sIL-2R) in a biological sample is immunologically detected, a measuring method and a kit capable of stably obtaining with high accuracy, unaffected by interfering substances in the specimen, are provided. An immunocomplex between the substance to be measured and an antibody that specifically binds to the substance to be measured is formed in the presence of a sulfated polysaccharide. The kit comprises an antibody that specifically binds to the substance to be measured, and a buffer containing a sulfated polysaccharide.

Abstract: A box-structure airfoil is constructed of a composite material uppers skin, a composite material lower a skin 12 and a spar. Ribs and an elongate projection are formed integrally on the inner surface of each of the two skins. The upper and lower skins and the spar are simultaneously bonded by an adhesive to form a single structure. Since the ribs and the elongate projection are one-piece formed with each skin, it is possible to reduce the number of principal constituent components. Furthermore, since assembly operation is made by using the adhesive, there is no need for fasteners or the like for assembling. Moreover, the flanges on both sides of the spar can also be bonded to the respective skins. According to the invention, it is possible to reduce the number of principal constituent components and that of assembling components of an airfoil, thereby achieving its cost reduction.

Abstract: A box-structure airfoil is constructed of a composite material upper skin, a composite material lower skin 12 and a spar. Ribs and an elongate projection are formed integrally on the inner surface of each of the two skins. The upper and lower skins and the spar are simultaneously bonded by an adhesive to form a single structure. Since the ribs and the elongate projection are one-piece formed with each skin, it is possible to reduce the number of principal constituent components. Furthermore, since assembly operation is made by using the adhesive, there is no need for fasteners or the like for assembling. Moreover, the spar is bonded not only to Moreover, because not only a web but also flanges on both sides of the spar are bonded to the respective skins, it is possible to obtain a large strength. According to the invention, it is possible to reduce the number of principal constituent components and that of assembling components of an airfoil, thereby achieving its cost reduction.

Abstract: A box-structure airfoil is constructed of a composite material upper skin, a composite material lower skin 12 and a spar. Ribs and an elongate projection are formed integrally on the inner surface of each of the two skins. The upper and lower skins and the spar are simultaneously bonded by an adhesive to form a single structure. Since the ribs and the elongate projection are one-piece formed with each skin, it is possible to reduce the number of principal constituent components. Furthermore, since assembly operation is made by using the adhesive, there is no need for fasteners or the like for assembling. Moreover, the spar is bonded not only to Moreover, because not only a web but also flanges on both sides of the spar are bonded to the respective skins, it is possible to obtain a large strength. According to the invention, it is possible to reduce the number of principal constituent components and that of assembling components of an airfoil, thereby achieving its cost reduction.