Abstract: An aircraft seat arrangement includes a first aircraft seat module delimiting an aircraft seat region, the aircraft seat module includes an aircraft seat to be mounted in the aircraft cabin at an angle of more than 30°, to be oriented away from a central aisle towards a window and to form a substantially planar lying-down surface. The aircraft seat module includes one or more enclosure units delimiting the aircraft seat region at least partially, and includes one or more further aircraft seat modules arranged directly neighboring the first aircraft seat module and delimiting a further aircraft seat region. The further aircraft seat module also includes an enclosure unit which delimits the aircraft seat region at least partially, is realized substantially identically to the enclosure unit of the first aircraft seat module, and separates the aircraft seat regions of the first and second aircraft seat modules.

Abstract: An aircraft seat arrangement includes a first aircraft seat device and a second aircraft seat device. The second aircraft seat device has an enclosure which forms a backrest wall in a subregion of the enclosure of the second aircraft seat device. The second aircraft seat device includes in an aircraft seat region a seat bottom which has a seat bottom front edge, a main extension axis of the seat bottom front edge being oriented at an angle of at least 5 degrees with respect to an aircraft seat device transversal axis of the second aircraft seat device. A lying-down direction of the aircraft seat region is oriented at an angle of at least 30 degrees with respect to an aircraft seat device longitudinal axis of the second aircraft seat device, the lying-down direction being directed away from an access region of the aircraft seat region.

Abstract: An aircraft seat module, which forms an aircraft seat region, includes an aircraft seat that is configured to be mounted in an aircraft cabin at an angle ? of 30 degrees to 80 degrees, preferably 45 degrees to 65 degrees, and that comprises at least a base frame and a cinematics unit, with an enclosure unit comprising a first enclosure element, which delimits the aircraft seat region at least partially in the region of the aircraft seat, and a second enclosure element, which delimits the aircraft seat region partially at least in a region in front of the aircraft seat, and includes an ottoman providing a footrest region, and with a console unit that forms at least one stowage and/or depositing region of the aircraft seat region, wherein the aircraft seat is combined in a separately realized 16G module and the second enclosure element, the ottoman and the console unit are combined in a separately realized 9G module, wherein the 16G module and the 9G module are configured to be fastened to a cabin floor separat

Abstract: An aircraft seat arrangement includes a first aircraft seat module delimiting an aircraft seat region, the aircraft seat module includes an aircraft seat configured to be mounted in the aircraft cabin at an angle of more than 30°, to be oriented away from a central aisle towards a window and to form an at least substantially planar lying-down surface, wherein the aircraft seat module includes at least one enclosure unit delimiting the aircraft seat region at least partially, and includes at least one further aircraft seat module arranged directly neighboring the first aircraft seat module and delimiting a further aircraft seat region, wherein the further aircraft seat module also includes an enclosure unit which delimits the aircraft seat region at least partially, is realized substantially identically to the enclosure unit of the first aircraft seat module, and separates the aircraft seat regions of the first and second aircraft seat modules.

Abstract: An aircraft seat arrangement includes a first aircraft seat device and a second aircraft seat device, wherein the second aircraft seat device has an enclosure which forms a backrest wall in a subregion of the enclosure of the second aircraft seat device, wherein the second aircraft seat device comprises in an aircraft seat region a seat bottom which has a seat bottom front edge, a main extension axis of the seat bottom front edge being oriented at an angle of at least 5 degrees with respect to an aircraft seat device transversal axis of the second aircraft seat device, wherein a lying-down direction of the aircraft seat region is oriented at an angle of at least 30 degrees with respect to an aircraft seat device longitudinal axis of the second aircraft seat device, the lying-down direction being directed away from an access region of the aircraft seat region.

Abstract: An aircraft seat module, which forms an aircraft seat region, includes an aircraft seat that is configured to be mounted in an aircraft cabin at an angle ? of 30 degrees to 80 degrees, preferably 45 degrees to 65 degrees, and that comprises at least a base frame and a cinematics unit, with an enclosure unit comprising a first enclosure element, which delimits the aircraft seat region at least partially in the region of the aircraft seat, and a second enclosure element, which delimits the aircraft seat region partially at least in a region in front of the aircraft seat, and includes an ottoman providing a footrest region, and with a console unit that forms at least one stowage and/or depositing region of the aircraft seat region, wherein the aircraft seat is combined in a separately realized 16G module and the second enclosure element, the ottoman and the console unit are combined in a separately realized 9G module, wherein the 16G module and the 9G module are configured to be fastened to a cabin floor separat

Abstract: A parking lock for a transmission of an electric or hybrid vehicle is disclosed. The parking lock includes a lock device including an actuatable actuating element and a setting element adjustable between a deployed position and a retracted position. The locking device is configured such that, in response to repeated actuation of the actuating element, the setting element is, via a coupling mechanism, adjusted alternately between the retracted position and the deployed position. A camshaft is provided with a cam arranged on the camshaft that is connected in terms of drive to the lock device. A ratchet wheel is provided with a pawl that is adjustable between an engagement position, where the pawl blocks a rotation of the ratchet wheel, and a release position, where the blocking of the ratchet wheel is released. The setting element adjusts the pawl between the engagement position and the release position.

Abstract: In a passenger seating arrangement in an aircraft cabin, the passenger seating arrangement has exactly two rows of seat units and exactly one aisle. A first row of seat units and a second row of seat units are separated by the aisle. The rows of seat units and the aisle all extend in a longitudinal direction parallel to a longitudinal axis of the aircraft cabin. Each seat unit includes a seat, an upper shell and a lower shell, the lower shell forming a footwell. The seats are arranged in parallel to each other in a seating direction. An upper shell of a first seat unit and a lower shell of a second seat unit, which, viewed in the longitudinal direction, is arranged behind the first seat unit, partially overlap in a vertical direction.

Abstract: A parking lock for a transmission of a motor vehicle may include a park gear rotatable about an axis of rotation, and an actuation device adjustable into a locking position and an unlocking position radially relative to the axis of rotation. In the unlocking position, rotating of the park gear may be possible, and in the locking position, rotating of the park gear may be prevented by way of positive locking. The actuation device may include a shifting drum and a locking lever, wherein the shifting drum may be rotatable about a guiding axis that is radial relative to the axis of rotation. The locking lever, by way of a guide track formed in the shifting drum, may interact with the guide track so that when the shifting drum is rotated, the locking lever may be guidable by the guide track radially relative to the axis of rotation and parallel to the guiding axis, and thereby the actuation device may be adjustable into the locking position and into the unlocking position.

Abstract: A parking lock for a transmission of an electric or hybrid vehicle is disclosed. The parking lock includes a lock device including an actuatable actuating element and a setting element adjustable between a deployed position and a retracted position. The locking device is configured such that, in response to repeated actuation of the actuating element, the setting element is, via a coupling mechanism, adjusted alternately between the retracted position and the deployed position. A camshaft is provided with a cam arranged on the camshaft that is connected in terms of drive to the lock device. A ratchet wheel is provided with a pawl that is adjustable between an engagement position, where the pawl blocks a rotation of the ratchet wheel, and a release position, where the blocking of the ratchet wheel is released. The setting element adjusts the pawl between the engagement position and the release position.

Abstract: A parking lock for a transmission of a motor vehicle may include a park gear rotatable about an axis of rotation, and an actuation device adjustable into a locking position and an unlocking position radially relative to the axis of rotation. In the unlocking position, rotating of the park gear may be possible, and in the locking position, rotating of the park gear may be prevented by way of positive locking. The actuation device may include a shifting drum and a locking lever, wherein the shifting drum may be rotatable about a guiding axis that is radial relative to the axis of rotation. The locking lever, by way of a guide track formed in the shifting drum, may interact with the guide track so that when the shifting drum is rotated, the locking lever may be guidable by the guide track radially relative to the axis of rotation and parallel to the guiding axis, and thereby the actuation device may be adjustable into the locking position and into the unlocking position.

Abstract: An internal combustion engine may include at least one cylinder, a first outlet valve and a second outlet valve for directing exhaust gas out from a combustion chamber of the at least one cylinder. The first outlet valve may include a first valve opening and a first valve body where the first valve opening is adjustable between a closed position and an open position. The second outlet valve may include a second valve opening and a second valve body where the second valve body is adjustable between a closed position and an open position. An adjusting lever may adjust one or both of the first valve body and the second valve body between the open position and the closed position.

Abstract: An internal combustion engine may include at least one cylinder, a first outlet valve and a second outlet valve for directing exhaust gas out from a combustion chamber of the at least one cylinder. The first outlet valve may include a first valve opening and a first valve body where the first valve opening is adjustable between a closed position and an open position. The second outlet valve may include a second valve opening and a second valve body where the second valve body is adjustable between a closed position and an open position. An adjusting lever may adjust one or both of the first valve body and the second valve body between the open position and the closed position.

Abstract: The invention relates to an aircraft seat device comprising at least one table device which comprises at least one table surface and at least one adjustment device, which is provided for the purpose of adjusting the table surface between a stowed position and a use position. The adjustment device is provided for the purpose of moving the table surface in a linear displacement movement and a rotational movement at least substantially in one plane during an adjustment between the stowed position and the use position.

Abstract: The invention relates to an aircraft seat device comprising at least one table device which comprises at least one table surface and at least one adjustment device, which is provided for the purpose of adjusting the table surface between a stowed position and a use position. The adjustment device is provided for the purpose of moving the table surface in a linear displacement movement and a rotational movement at least substantially in one plane during an adjustment between the stowed position and the use position.

Abstract: A piston engine, having at least one cylinder that includes at least a first and a second discharge valve and a double overhead camshaft for controlling the first and a second discharge valves. The double overhead camshaft includes both an inner shaft, which has at least one first cam for controlling the first discharge valve, and an outer shaft that is coaxial to the first inner shaft and has at least one second cam for controlling the second discharge valve. The inner shaft and the outer shaft are rotationally adjustable relative to one another changing the discharge time frame of the discharge valves.

Abstract: The present invention relates to a cam drive (1) having a camshaft and having cams (18, 18?)arranged thereon and having at least one rocker arm (3) which has a cam follower (2) and which is operatively connected by means of its first arm (4) to a plunger-like bearing (5) and by means of its second arm (6) to at least one gas exchange valve (7) of an associated cylinder. The cam drive (1) also has a device (10) for varying the lift of the at least one gas exchange valve (7). Here, it is essential to the invention that the device (10) is embodied as a clutch device which acts between the plunger-like abutment (5) and the rocker arm (3, 3?, 3?)and which has an actuating element (12) which is mounted so as to be rotatable about an axis (13) of the plunger-like abutment (5) at least between two positions, wherein a valve lift in a first, coupled position of the actuating element (12) is varied in comparison with a second, decoupled position.

Abstract: The present invention relates to an adjustable camshaft (1), which is connected to a crankshaft via a sprocket/belt pulley (3) and has a phase adjusting device (4) for adjusting the phase between the camshaft (1) and the crankshaft. The essential idea of the invention is that the phase adjusting device (4) comprises a planetary gear (5) having at least two sun wheels (6 and 7) disposed coaxially to each other and planet wheels (8) surrounding said sun wheels, wherein said planet wheels are rotatably supported on a planet wheel carrier (10) via a planet wheel axis (9). Said planet wheel carrier (10) can be rotated in relation to the camshaft axis (11), wherein a rotation of the planet wheel carrier (10) brings about a phase adjustment between the camshaft (1) and the drive.

Abstract: A camshaft has at least two completely machined individual cams fixedly mounted on a shaft in predetermined angular positions. The shaft includes an outside shaft and an inside shaft arranged concentrically in the former, and is to be manufactured in such a way that remachining of the joined camshaft is not necessary. This is by combining the individual cams even before they are mounted on a shaft and joining them to this shaft to form a machining module, such that the individual cams are combined in their mutual arrangement in relation to one another in which the cams are to be mounted on the finished camshaft. The final machining of the cams is performed within this machining nodule. When the cams are completely machined in this way, the cams are joined to the shaft of the camshaft within the machining module. This ensures that the desired mutual arrangement is maintained, i.e., that remachining is not necessary.

Abstract: A piston engine, having at least one cylinder that includes at least a first and a second discharge valve and a double overhead camshaft for controlling the first and a second discharge valves. The double overhead camshaft includes both an inner shaft, which has at least one first cam for controlling the first discharge valve, and an outer shaft that is coaxial to the first inner shaft and has at least one second cam for controlling the second discharge valve. The inner shaft and the outer shaft are rotationally adjustable relative to one another changing the discharge time frame of the discharge valves.