Abstract: An opening completely arranged in a skin panel of a structural portion of the aircraft is formed in the outer skin of the skin panel, and for each of the skin panels with one of the openings, an associated structural element of an electronic arrangement is separately provided. The structural element is designed and detachably fastened by a frame thereof to the outer skin in the corresponding skin panel on the side of the outer skin opposite the outer surface, such that it seals the corresponding opening such that the skin panel has at least the same pressure-tightness and at least the same strength relative to tension, pressure and shear forces which act in the skin panel in the extension direction of the outer skin as the same skin panel without the corresponding opening.

Abstract: An opening completely arranged in a skin panel of a structural portion of the aircraft is formed in the outer skin of the skin panel, and for each of the skin panels with one of the openings, an associated structural element of an electronic arrangement is separately provided. The structural element is designed and detachably fastened by a frame thereof to the outer skin in the corresponding skin panel on the side of the outer skin opposite the outer surface, such that it seals the corresponding opening such that the skin panel has at least the same pressure-tightness and at least the same strength relative to tension, pressure and shear forces which act in the skin panel in the extension direction of the outer skin as the same skin panel without the corresponding opening.

Abstract: An antenna arrangement for an aircraft for fastening to an outer side of an exterior skin of the aircraft has a body and side wall sections and a connecting section. The body is U-shaped or H-shaped if viewed from a predefined direction and can be flowed through with a low aerodynamic drag by a flow along the predefined direction. The antenna arrangement has one or more antennas in the form of a printed circuit board and of which each is fastened to the body and is fastenable directly to the outer side of the aircraft exterior skin at two first edges of the side wall sections which form two free ends of the U-shape or H-shape on a first side of the connecting section or, for the U-shape, on the connecting section and/or regions of the side wall sections, which regions adjoin the connecting section directly as the predefined direction is parallel to the flow direction during flight.

Abstract: An antenna arrangement for an aircraft for fastening to an outer side of an exterior skin of the aircraft has a body and side wall sections and a connecting section. The body is U-shaped or H-shaped if viewed from a predefined direction and can be flowed through with a low aerodynamic drag by a flow along the predefined direction. The antenna arrangement has one or more antennas in the form of a printed circuit board and of which each is fastened to the body and is fastenable directly to the outer side of the aircraft exterior skin at two first edges of the side wall sections which form two free ends of the U-shape or H-shape on a first side of the connecting section or, for the U-shape, on the connecting section and/or regions of the side wall sections, which regions adjoin the connecting section directly as the predefined direction is parallel to the flow direction during flight.

Abstract: An aircraft antenna assembly has a support element having a first and a second surface on opposite sides, an antenna element arranged on or in the support element, and a sealing device. The first surface and the sealing device are configured such that the antenna assembly is arranged on an outer skin section of an aircraft such that the first surface faces the outer skin section, the sealing device is situated between the support element and the outer skin section, and a cavity is defined by the sealing device, the outer skin section and the first surface. The support element or the sealing device y has a flow channel having a first and a second opening at opposite ends, the flow channel connecting the cavity and the environment and opening into the cavity at the first opening and opening into the environment at the second opening.

Abstract: A motor vehicle operating unit for a motor vehicle, having a haptic feedback device and an operating surface rotatable about an axis of rotation, the axis of rotation being substantially parallel to a plane spanned by the operating surface in the initial position of the motor vehicle operating unit, the haptic feedback device being arranged so as to control the operating surface such that the operating surface rotates about the axis of rotation. A method of confirming a switching command by means of a motor vehicle operating unit is furthermore described.

Abstract: A motor vehicle operating unit for a motor vehicle, having a haptic feedback device and an operating surface rotatable about an axis of rotation, the axis of rotation being substantially parallel to a plane spanned by the operating surface in the initial position of the motor vehicle operating unit, the haptic feedback device being arranged so as to control the operating surface such that the operating surface rotates about the axis of rotation. A method of confirming a switching command by means of a motor vehicle operating unit is furthermore described.

Abstract: An aircraft antenna assembly has a support element having a first and a second surface on opposite sides, an antenna element arranged on or in the support element, and a sealing device. The first surface and the sealing device are configured such that the antenna assembly is arranged on an outer skin section of an aircraft such that the first surface faces the outer skin section, the sealing device is situated between the support element and the outer skin section, and a cavity is defined by the sealing device, the outer skin section and the first surface. The support element or the sealing device y has a flow channel having a first and a second opening at opposite ends, the flow channel connecting the cavity and the environment and opening into the cavity at the first opening and opening into the environment at the second opening.

Abstract: An indexed rotary switch (10), in particular a rotary pushbutton switch in a vehicle, includes a base body (12) and a spring ring (26) which is locked to the base body (12) so as to prevent rotation.

Abstract: In an actuating assembly (16) for a control element in a vehicle, in particular for a steering column stalk (10), having an actuating element (18) that is adapted to be shifted in an actuating direction (B), and a seat (20) in which the actuating element (18) is supported for being shifted hi the actuating direction (B) between a basic position and at least one actuation position, at least one separate spring element (28) is provided between the seat (20) and the actuating element (18) and presses on the actuating element (18) by a spring force (F) acting substantially transversely to the actuating direction (B).

Abstract: In an actuating assembly (16) for a control element in a vehicle, in particular for a steering column stalk (10), having an actuating element (18) that is adapted to be shifted in an actuating direction (B), and a seat (20) in which the actuating element (18) is supported for being shifted it the actuating direction (B) between a basic position and at least one actuation position, at least one separate spring element (28) is provided between the seat (20) and the actuating element (18) and presses on the actuating dement (18) by a spring force (F) acting substantially transversely to the actuating direction (B).

Abstract: A redundant switch includes a housing, an actuator, and a slide movable in the housing in two opposing directions. The slide is coupled to the actuator by two antagonistic springs. The switch includes a latching track with latching notches. At least two switch units are arranged one beside the other for simultaneous actuation by the slide. A latching cam is movably guided on the slide and is urged towards the latching track by a compression spring. The antagonistic springs force the slide to move into respective positions when the latching cam slides over an apex between the latching notches.

Abstract: In a switch, particularly a window lifter switch, with a housing, a switching rocker which is mounted in the housing and is associated with electrical contacts, and with a button which is likewise mounted in the housing, the button is acted upon elastically so that it is mounted free from play in the housing.

Abstract: A switch module includes a switch housing on which at least one operating button or operating rocker is movably guided. The switch module further includes a printed circuit board which is arranged in the switch housing and on which conductor paths with switching contacts are formed, a switching mat which rests on the conductor paths, and an actuating element which transfers the stroke of the operating button or operating rocker to the switching mat. The switching mat engages around the outer edge of the printed circuit board with a form fit.

Abstract: A redundant switch includes a housing and an actuator movable in the housing in two opposing translational directions. A slide is movable in the housing in the same two opposing directions as the actuator and is coupled to the actuator by two antagonistic springs with clearance in both directions of movement. The switch also includes a latching track with at least two latching notches, which are spaced from each other along the directions of movement. At least two switch units are arranged one beside the other for simultaneous actuation by the slide. A latching cam is movably guided on the slide perpendicular to its directions of translational movement and is urged towards the latching track by a compression spring. One of the latching notches in cooperation with the latching cam defines a rest position of the slide, in which the slide does not actuate the switch units.

Abstract: A device (10) for fastening a component to a steering column jacket (20, 20?), comprises a fastening sleeve (12) and an equalizer (14) associated with the fastening sleeve (12). The fastening sleeve (12) has at least one mounting section (18) and convexities (22) adjoining the mounting section (18). The mounting section (18) has a first mounting cross-section to receive the steering column jacket (20; 20?), and the equalizer (14) comprises equalizing jaws (16) laterally movable in the fastening sleeve (12), which are movable between a first position in which they are received in the convexities (22), and a second position in which they lie at least partially in the mounting section (18) and define a second mounting cross-section for the steering column jacket (20; 20?), which is smaller than the first mounting cross-section.

Abstract: In a switch, particularly a window lifter switch, with a housing, a switching rocker which is mounted in the housing and is associated with electrical contacts, and with a button which is likewise mounted in the housing, the button is acted upon elastically so that it is mounted free from play in the housing.

Abstract: A modular switch and control system for use in a motor vehicle is provided, that is easily and flexibly adapted to the particular needs and requires no additional wiring for added modules. The modular switch and control system comprises a main switch module and optional satellite modules of different types. The main and satellite modules have separate housings with matching engagement structures permitting each satellite module to be fitted to one side of the main module. Each satellite module is electrically connected with the main module through matching male and female connectors. Each satellite module is provided with electrical coding device accessible through the connectors and permitting each satellite to be provided with a code indicative of the module type.

Abstract: A rotary light switch for motor vehicles is presented that ensures a feel that is not susceptible to mechanical influences. The rotary light switch has an actuator that can be rotated around an axis and that can be moved in the axial direction, and that is non-rotatably coupled to a rotational position indicator and axially coupled to an axial position indicator. Moreover, it has an electronic evaluation circuit to which the signals from the rotational position indicator and from the axial position indicator are fed and, according to a permanently stored decision matrix, said evaluation circuit uses the signals to derive discrete switching states that are converted into switching signals that serve to actuate the lighting system of the vehicle. The rotational position indicator comprises a potentiometer that generates a negligible resistance to the rotational movement, so that no mechanical influences are caused by the rotational position indicator.

Abstract: A rotary switch for installation in the dashboard of a vehicle has a switch housing, an actuation shaft that is arranged rotatably in the switch housing, a knob that is mounted on one end of the actuation shaft, and a ring-shaped faceplate that surrounds the knob and that is detachably fastened to the switch housing. The faceplate is connected to the switch housing by a locking mechanism. This locking mechanism can be released by a relative rotation between the faceplate and the switch housing. The knob can be moved axially in a predetermined rotational position and is coupled non-rotatably to the faceplate by means of this axial movement. In order to detach the faceplate from the switch housing, the knob is moved into the predetermined rotational position and then moved axially and turned at the same time, whereby the faceplate also turns and the latched connection between the faceplate and the switch housing is released.