Abstract: The invention relates to novel bispecific antigen binding molecules, comprising at least two antigen binding domains capable of specific binding to OX40 and a particular antigen binding domain capable of specific binding to Fibroblast Activation Protein (FAP), and to methods of producing these molecules and to methods of using the same.

Abstract: The invention relates to an electronic component (1) having a corrosion-protected bonding connection and a method for producing said component. For this purpose the electronic component (1) has at least one semiconductor chip (3) on a substrate (4). Moreover, a bonding connection at risk of corrosion is provided on the semiconductor chip (3). For encapsulation of the at least one semiconductor chip (3) and the at least one bonding connection at risk of corrosion, said semiconductor chip and bonding connection are surrounded by a hermetically sealing housing (5). The hermetically sealed bonding connection is a bonding wire connection (2) which is fully enclosed in the housing (5), in which the substrate (4) is at least partially enclosed. The substrate (4) has at least one surface-mounted hydrolysis-sensitive component (6) in the housing (5).

Abstract: The invention relates to an electronic component (1) having a corrosion-protected bonding connection and a method for producing said component. For this purpose the electronic component (1) has at least one semiconductor chip (3) on a substrate (4). Moreover, a bonding connection at risk of corrosion is provided on the semiconductor chip (3). For encapsulation of the at least one semiconductor chip (3) and the at least one bonding connection at risk of corrosion, said semiconductor chip and bonding connection are surrounded by a hermetically sealing housing (5). The hermetically sealed bonding connection is a bonding wire connection (2) which is fully enclosed in the housing (5), in which the substrate (4) is at least partially enclosed. The substrate (4) has at least one surface-mounted hydrolysis-sensitive component (6) in the housing (5).

Abstract: A method and a device are for predicting a life expectancy of a product, which includes at least two components. The life expectancy is ascertained as a function of an assumed field loading of the product. The components of the product are acted upon by different loadings and are operated, in each instance, at the different loadings until they fail. An end-of-life curve of the component is recorded on the basis of the load-dependent failure times of a component. An EOL curve of the product is ascertained such that at the different loadings, it includes the EOL curve of the components which has, in each instance, the shortest failure time at the corresponding loading. The anticipated service life of the product is determined as a functional value of the EOL curve of the product as a function of the predefined loading of the product.

Abstract: A field-effect transistor, having a source electrode, a drain electrode and a gate electrode, which has a connection between the gate electrode and the source electrode or between the gate electrode and the drain electrode or between the gate electrode and the substrate which carries a leakage current.

Abstract: A method and a device are for predicting a life expectancy of a product, which includes at least two components. The life expectancy is ascertained as a function of an assumed field loading of the product. The components of the product are acted upon by different loadings and are operated, in each instance, at the different loadings until they fail. An end-of-life curve of the component is recorded on the basis of the load-dependent failure times of a component. An EOL curve of the product is ascertained such that at the different loadings, it includes the EOL curve of the components which has, in each instance, the shortest failure time at the corresponding loading. The anticipated service life of the product is determined as a functional value of the EOL curve of the product as a function of the predefined loading of the product.

Abstract: A method for damping vibrations in a tail boom of a rotary-wing aircraft includes the steps of detecting tail boom vibrations induced by external vibration excitation, and generating and introducing strains into the tail boom based on the detected tail boom vibrations. The strains are applied over a surface area and are out-of-phase with respect to the detected tail boom vibrations so as to damp the externally excited induced tail boom vibrations. In addition, a rotary-wing aircraft, includes a fuselage, a cockpit area integrated into the fuselage, a tail boom arranged on the fuselage and a tail boom vibration-damping device.