Abstract: An aqueous liquid formulation which comprises a compound of formula I: wherein Y is a hydroxy group, a carboxyl group, an acyloxy group or an alkoxycarbonyl group; R is a lower alkyl group or a lower alkyl group with one or more halogen atoms; or a pharmaceutically acceptable salt thereof or a pharmaceutically acceptable solvate of them as an active ingredient, together with one or more substances selected from the group consisting of boric acid, borax, phosphate salts and carbonate salts.

Abstract: A method of fabricating a panel of composite material. The panel includes two outside skins and stringers attached inside of the two outside skins for reinforcing the two outside skins. A plurality of stringers for reinforcing outside skins is formed from dry preformed fibers and are disposed at a predetermined interval.

Abstract: A water-based liquid preparation which contains as the active ingredient a compound represented by the formula (I)(wherein Y represents hydroxy, carboxyl, acyloxy, or alkoxycarbonyl; and R represents lower alkyl optionally having one or more halogen atoms), a pharmacologically acceptable salt of the compound, or a pharmacologically acceptable solvate of either and which further contains one or more substances selected from the group consisting of boric acid, borax, a phosphoric acid salt, and a carbonic acid salt.

Abstract: A wing of composite material has an upper skin, a lower skin and a plurality of intermediate spars arranged between the upper and the lower skin. The intermediate spars extend from roots to tips of the upper and the lower skins. The intermediate spars are integrally formed with the upper and the lower skins or are adhesively bonded to the upper and the lower skins. The wing has a small number of parts, needs greatly reduced time for fabrication and can be fabricated at a low cost.

Abstract: This invention is a method of fabricating a panel of composite material. The panel includes two outside skins and stringers attached inside of the two outside skins for reinforcing the two outside skins. A plurality of stringers for reinforcing outside skins is formed from dry preformed fibers. The plurality of stringers are disposed at a predetermined interval. Adjacent two stringers is connected with each other via a connecting member made from dry preformed fibers. The connected stringers and the connecting members are set into a forming mold. Resin is introduced into the forming mold to impregnate the dry preformed fibers of the stringers and the connecting members. The resin-impregnated stringers and the resin-impregnated connecting members are cured to unite the resin-impregnated stringers and the resin-impregnated connecting member into one body of “Rudder Shape” stringer. A prepreg is laminated onto an outside-skin shaping mold.

Abstract: A wing of composite material has an upper skin, a lower skin and a plurality of intermediate spars arranged between the upper and the lower skin. The intermediate spars extend from roots to tips of the upper and the lower skins. The intermediate spars are integrally formed with the upper and the lower skins or are adhesively bonded to the upper and the lower skins. The wing has a small number of parts, needs greatly reduced time for fabrication and can be fabricated at a low cost.

Abstract: A panel of composite material including two outside skin parts, a plurality of stringers, connecting members for connecting the plurality of stringers, and a reinforcing member connecting the two outside skin parts with each other. Each of the two outside skin parts is formed into one body. A portion protruding upward from the plurality of stringers is provided on the connecting members, and is connected to the reinforcing member by a fastener.

Abstract: A wing of composite material has an upper skin, a lower skin and a plurality of intermediate spars arranged between the upper and the lower skin. The intermediate spars extend from roots to tips of the upper and the lower skins. The intermediate spars are integrally formed with the upper and the lower skins or are adhesively bonded to the upper and the lower skins. The wing has a small number of parts, needs greatly reduced time for fabrication and can be fabricated at a low cost.

Abstract: This invention is a method of fabricating a panel of composite material. The panel includes two outside skins and stringers attached inside of the two outside skins for reinforcing the two outside skins. A plurality of stringers for reinforcing outside skins is formed from dry preformed fibers. The plurality of stringers are disposed at a predetermined interval. Adjacent two stringers is connected with each other via a connecting member made from dry preformed fibers The connected stringers and the connecting members are set into a forming mold. Resin is introduced into the forming mold to impregnate the dry preformed fibers of the stringers and the connecting members. The resin-impregnated stringers and the resin-impregnated connecting members are cured to unite the resin-impregnated stringers and the resin-impregnated connecting member into one body of “Rudder Shape” stringer. A prepreg is laminated onto an outside-skin shaping mold.