Abstract: The invention proposes a periodically actuable tappet (1) for a valve train, said tappet (1) comprising a hollow cylindrical skirt (2) that can be arranged through an outer peripheral surface (3) in a guide bore (4) of a surrounding structure (5), said skirt (2) comprising a window-type aperture (6) in which a separate anti-rotation device (8) is arranged through a radially inner portion (7), a radially outer portion (9) of the anti-rotation device (8) extending beyond the skirt (2) for guidance in a longitudinal groove (10) that intersects the guide bore (4), wherein the anti-rotation device (8), as viewed in cross-section, is substantially mushroom-shaped, the inner portion (7) has a rectangular cross-section corresponding to a geometry of the aperture (6) of the skirt (2), into which cross-section, the outer portion (9) merges in the manner of a roof through a fractional cylindrical outer peripheral surface (11), inner legs (12) of the outer portion (9) extend beyond the aperture (6) in peripheral directio

Abstract: A switch element (1) is proposed for valve shut-off, fabricated as cam follower for a plunger rod valve drive of an internal combustion engine, having an outer part (2) and an inner element (4) axially movable in its bore (3) and with rotational security (15) relative to the guided inner element (4). The outer part (2), inside the bore (3), has an annular groove (6), and the inner element (4) has a radial bore (7) with two diametrically opposed pistons (8), which to couple the elements (2, 4) in their axially remote relative position achieved by a lost-motion spring (5) are displaceable towards the annular groove (6). On their cam-side under side, emanating from their radially outward, bulbous face, the pistons (8) segmentwise comprise a plane transverse surface as contact area for a facing under side (27) of the annular groove (6). The latter is intersected by two diametrically opposed oil ports (11) running offset 90° from the pistons (8) in circumferential direction.

Abstract: The invention proposes a switching element (1) for a valve train of an internal combustion engine, particularly for valve deactivation, with a simple-to-implement measure for adjusting the coupling lash of its coupling means (8) in a receptacle (6) using two retaining rings (19, 20), one of which is stocked in a variety of thicknesses.

Abstract: In a guide rail for the valve train of an internal combustion engine, having receiving spaces disposed in an elongate body in spaced-apart relationship behind one another and accommodating valve lifters, flats are formed upon the outer surface area of each valve lifter to prevent the lifter from rotating about its central longitudinal axis. These flats are supported by flats of the guide rail which are located within the pertaining receiving space. An inlet bore is assigned to each receiving space of the elongate body for insertion of the valve lifter with an attached trumpet-like end in direction of its longitudinal axis. Subsequently the valve lifter is shifted in axis-parallel relationship to the flats of the guide rail, which act as rotation-inhibiting surfaces, and then is slightly displaced again in axial direction.

Abstract: The invention proposes a periodically actuable tappet (1) for a valve train, said tappet (1) comprising a hollow cylindrical skirt (2) that can be arranged through an outer peripheral surface (3) in a guide bore (4) of a surrounding structure (5), said skirt (2) comprising a window-type aperture (6) in which a separate anti-rotation device (8) is arranged through a radially inner portion (7), a radially outer portion (9) of the anti-rotation device (8) extending beyond the skirt (2) for guidance in a longitudinal groove (10) that intersects the guide bore (4), wherein the anti-rotation device (8), as viewed in cross-section, is substantially mushroom-shaped, the inner portion (7) has a rectangular cross-section corresponding to a geometry of the aperture (6) of the skirt (2), into which cross-section, the outer portion (9) merges in the manner of a roof through a fractional cylindrical outer peripheral surface (11), inner legs (12) of the outer portion (9) extend beyond the aperture (6) in peripheral directio

Abstract: The invention proposes a switching element (1) for a valve train of an internal combustion engine, particularly for valve deactivation, with a simple-to-implement measure for adjusting the coupling lash of its coupling means (8) in a receptacle (6) using two retaining rings (19, 20), one of which is stocked in a variety of thicknesses.

Abstract: In a guide rail for the valve train of an internal combustion engine, having receiving spaces disposed in an elongate body in spaced-apart relationship behind one another and accommodating valve lifters, flats are formed upon the outer surface area of each valve lifter to prevent the lifter from rotating about its central longitudinal axis. These flats are supported by flats of the guide rail which are located within the pertaining receiving space. An inlet bore is assigned to each receiving space of the elongate body for insertion of the valve lifter with an attached trumpet-like end in direction of its longitudinal axis. Subsequently the valve lifter is shifted in axis-parallel relationship to the flats of the guide rail, which act as rotation-inhibiting surfaces, and then is slightly displaced again in axial direction.

Abstract: A switching element (1) for a valve drive of an internal combustion engine, preferably for shutting off valves, is provided, and includes an external part (2) in whose bore (3) an inner element (5) is axially movable. The external part (2) and the inner element (5) have at least a respective mutually aligned recess (7, 8) due to an axially spaced relative position obtained through a lost motion spring (6), and in one of the recesses, in the direction of the other recess, displaceable coupling means (9) are mutually applied in the relative position for coupling the inner element (5) with the external part (2). Two pistons (10) are provided as coupling means (9), which travel in the recess (8) formed as a radial bore of the inner element (5), and which diametrically oppose one another.

Abstract: A wing gap closure flap is positioned in an aircraft wing so that a gap between the wing structure and the leading edge of a landing flap can be closed during normal cruising positions of the landing flap and opened when the landing flap is in a starting position or in a landing position. The gap is formed on the underside of the aircraft wing and the gap closure flap is operated by a positioning shaft which itself is driven through a drive lever linkage by the drive shaft for the landing flap. The wing gap closure flap is connected through a lever mechanism to the positioning shaft which is preferably divided into shaft sections where a plurality of wing gap closure flaps are used. Each shaft section is driven by the landing flap drive shaft. A defined motion of the wing gap closure flap or flaps is achieved in that the positioning of the wing gap closure flaps is synchronized in a limited angular range with the positioning of the landing flap by the cooperation of the respective drive mechanisms.