Abstract: The invention relates to a valve assembly (10) for a charging device, in particular for a wastegate of an exhaust gas turbocharger, comprising a spindle (100), a lever arm (110) coupled to the spindle (100), and a valve unit (200). The lever arm (110) has a connecting element (112), designed as at least partially spherical, and the valve unit (200) has an accommodation region (212) with at least one first conical accommodation surface (214) in which the connecting element (112) is arranged.

Abstract: A method produces a fiber composite preform for a fiber composite component. The fiber composite preform has a plurality of layers of a fiber roving. The method includes: providing a support core for arranging the fiber roving s on a braiding device, the support core having a support core longitudinal axis, producing a first braided fabric layer from fiber rovings on the support core in a first braiding direction parallel to the support core longitudinal axis of the support core by the braiding device, and producing a second braided fabric layer from fiber rovings on the first braided fabric layer by the braiding device. The second braided fabric layer is produced in a second braiding direction parallel to the support core longitudinal axis, the second braiding direction being opposite the first braiding direction.

Abstract: The invention relates to a valve assembly (10) for a charging device, in particular for a wastegate of an exhaust gas turbocharger, comprising a spindle (100), a lever arm (110) coupled to the spindle (100), and a valve unit (200). The lever arm (110) has a connecting element (112), designed as at least partially spherical, and the valve unit (200) has an accommodation region (212) with at least one first conical accommodation surface (214) in which the connecting element (112) is arranged.

Abstract: A method produces a fiber composite preform for a fiber composite component. The fiber composite preform has a plurality of layers of a fiber roving. The method includes: providing a support core for arranging the fiber roving s on a braiding device, the support core having a support core longitudinal axis, producing a first braided fabric layer from fiber rovings on the support core in a first braiding direction parallel to the support core longitudinal axis of the support core by the braiding device, and producing a second braided fabric layer from fiber rovings on the first braided fabric layer by the braiding device. The second braided fabric layer is produced in a second braiding direction parallel to the support core longitudinal axis, the second braiding direction being opposite the first braiding direction.

Abstract: To ensure during the braiding of braiding cores, which have a complex braiding core geometry, for example a rectangular braiding core cross-section or one-sided cross-sectional changes, that the braiding threads are always correctly following the braiding core contour in terms of storage, a braiding ring is provided. The braiding ring is composed of a number of adjustable segments, each of which can be actuated individually and independently of the other segments by an actuator.

Abstract: To ensure during the braiding of braiding cores, which have a complex braiding core geometry or vastly different side lengths, that the braiding threads are always correctly following the braiding core contour in terms of storage, at least two braiding rings are provided, which have a constant opening cross-section and are arranged in series directly adjacent to one another. The opening cross-sections delimited by the braiding rings overlap at least partially. The braiding rings are adjustable independently of one another.

Abstract: A method is provided for producing a fiber preform for a composite fiber component. In the method, at least one first fiber structure is braided in a braiding process over the entire length of the fiber preform to be produced and at least one second fiber structure is wound in a winding process over part of the length of the fiber preform to be produced.

Abstract: To ensure during the braiding of braiding cores, which have a complex braiding core geometry or vastly different side lengths, that the braiding threads are always correctly following the braiding core contour in terms of storage, at least two braiding rings are provided, which have a constant opening cross-section and are arranged in series directly adjacent to one another. The opening cross-sections delimited by the braiding rings overlap at least partially. The braiding rings are adjustable independently of one another.

Abstract: To ensure during the braiding of braiding cores, which have a complex braiding core geometry, for example a rectangular braiding core cross-section or one-sided cross-sectional changes, that the braiding threads are always correctly following the braiding core contour in terms of storage, a braiding ring is provided. The braiding ring is composed of a number of adjustable segments, each of which can be actuated individually and independently of the other segments by an actuator.

Abstract: A method is provided for producing a fiber preform for a composite fiber component. In the method, at least one first fiber structure is braided in a braiding process over the entire length of the fiber preform to be produced and at least one second fiber structure is wound in a winding process over part of the length of the fiber preform to be produced.