Abstract: The invention relates to a strut for the landing gear, preferably the nose landing gear, of an aircraft, which strut comprises a structure branched in a Y shape, wherein the Y-shaped structure is produced as a multi-piece structure and comprises at least two bars, wherein a first bar forms the first branch of the structure and a second bar forms the second branch of the structure and wherein both bars are composed partially or completely of a fiber composite material.

Abstract: The invention relates to a strut for the landing gear, preferably the nose landing gear, of an aircraft, which strut comprises a structure branched in a Y shape, wherein the Y-shaped structure is produced as a multi-piece structure and comprises at least two bars, wherein a first bar forms the first branch of the structure and a second bar forms the second branch of the structure and wherein both bars are composed partially or completely of a fiber composite material.

Abstract: The invention provides a method of manufacturing a hollow fiber reinforced structural member, in particular for air vehicles, comprising the steps of providing a first circular braiding layer, positioning a flat strengthening body comprising at least one fabric layer having warp fibers and a woof fiber against a part of the surface of the first braiding layer, providing a second braiding layer around the first braiding layer and the strengthening body, positioning the combination of the first braiding layer, the strengthening body and the second braiding layer in a mold, impregnating the combination with resin, removing the combination as impregnated with a resin from the mold.

Abstract: The invention provides a device for injecting a resin into at least one fiber layer of a fiber-reinforced product (5) to be manufactured, comprising a mold (2, 3) having a mold cavity (4) that is surrounded by a mold wall for abutment of the product thereagainst in the closed condition of the mold. A rigid part (3a, 3b, 3c, 3d) of the mold wall is movable with respect to another part of the mold wall in the closed condition of the mold so as to ensure a continued abutment of the movable part of the mold wall with the products when shrinkage of the resin caused by curing thereof takes place subsequent to the injection process.

Abstract: The invention provides a device for injecting a resin into at least one fibre layer of a fibre-reinforced product (5) to be manufactured, comprising a mould (2, 3) having a mould cavity (4) that is surrounded by a mould wall for abutment of the product thereagainst in the closed condition of the mould. A rigid part (3a, 3b, 3c, 3d) of the mould wall is movable with respect to another part of the mould wall in the closed condition of the mould so as to ensure a continued abutment of the movable part of the mould wall with the products when shrinkage of the resin caused by curing thereof takes place subsequent to the injection process.

Abstract: The invention provides a method of manufacturing a hollow fiber reinforced structural member, in particular for air vehicles, comprising the steps of providing a first circular braiding layer, positioning a flat strengthening body comprising at least one fabric layer having warp fibers and a woof fiber against a part of the surface of the first braiding layer, providing a second braiding layer around the first braiding layer and the strengthening body, positioning the combination of the first braiding layer, the strengthening body and the second braiding layer in a mould, impregnating the combination with resin, removing the combination as impregnated with a resin from the mould.