Abstract: A cabin furnishing element for a cabin, such as a cabin of an aircraft, includes a panel having a panel body. The panel body includes an illumination surface having an illumination zone, and defines a lighting recess within the panel body relative to the illumination surface. The panel also includes a lighting system having a light source assembly and a light guide. The light source assembly and light guide are retained within the lighting recess defined by the panel body. The lighting system is adapted to selectively illuminate a portion of the illumination zone.

Abstract: A method detects a driving state of a vehicle. The vehicle has a drive train with at least one drive and an accelerator pedal. A rest state of the accelerator pedal is determined by evaluating an operating point position of the accelerator pedal by a first accelerator pedal gradient in a first time interval, and checking whether the first accelerator pedal gradient within the first time interval is less than a maximum value.

Abstract: A cabin furnishing element for a cabin, such as a cabin of an aircraft, includes a panel having a panel body. The panel body includes an illumination surface having an illumination zone, and defines a lighting recess within the panel body relative to the illumination surface. The panel also includes a lighting system having a light source assembly and a light guide. The light source assembly and light guide are retained within the lighting recess defined by the panel body. The lighting system is adapted to selectively illuminate a portion of the illumination zone.

Abstract: An aircraft lighting system includes a light unit configured to emit light, a portable measurement device, and a control unit. The portable measurement device is configured to measure at least one attribute of the light emitted from the light unit and output the measured attribute of the light in an output signal. The control unit is configured to receive the output signal and control the light unit based on the measured attribute. In some aspects, the light unit is positionable in an aircraft, in certain examples, a method of controlling a lighting system includes measuring at least one attribute of light of a light unit with a portable measurement device, transmitting the measured attribute to a control unit, and controlling the light unit based on the measured attribute. In some cases, the method includes measuring the at least one attribute of a light unit in an aircraft.

Abstract: A cabin furnishing element (100) for a cabin, such as a cabin of an aircraft, includes a panel (102) having a panel body. The panel body includes an illumination surface (106) having an illumination zone (110), and defines a lighting recess (112) within the panel body relative to the illumination surface (106). The panel (102) also includes a lighting system (104) having a light source assembly (120) and a light guide (122). The light source assembly (120) and light guide (122) are retained within the lighting recess (112) defined by the panel body. The lighting system (104) is adapted to selectively illuminate a portion of the illumination zone (110).

Abstract: An aircraft mirror assembly includes a light source, a front cover, and a light guide. The front cover is semi-transparent, the light source is arranged adjacent to an edge of the light guide, and the light guide is arranged adjacent to the front cover. In various aspects, the front cover includes an illumination zone, and, in an activated configuration, the light guide is configured to direct light from the light source to the illumination zone such that light is directed through the illumination zone. In certain aspects, the front cover includes an indicator, and, in an activated configuration, the light guide is configured to direct light from the light source to the indicator such that the indicator is activated. In various examples, the aircraft mirror assembly is provided with an aircraft cabin assembly positionable in a cabin of an aircraft.

Abstract: A cabin furnishing element (100) for a cabin, such as a cabin of an aircraft, includes a panel (102) having a panel body. The panel body includes an illumination surface (106) having an illumination zone (110), and defines a lighting recess (112) within the panel body relative to the illumination surface (106). The panel (102) also includes a lighting system (104) having a light source assembly (120) and a light guide (122). The light source assembly (120) and light guide (122) are retained within the lighting recess (112) defined by the panel body. The lighting system (104) is adapted to selectively illuminate a portion of the illumination zone (110).

Abstract: An aircraft lighting system includes a light unit configured to emit light, a portable measurement device, and a control unit. The portable measurement device is configured to measure at least one attribute of the light emitted from the light unit and output the measured attribute of the light in an output signal. The control unit is configured to receive the output signal and control the light unit based on the measured attribute. In some aspects, the light unit is positionable in an aircraft, in certain examples, a method of controlling a lighting system includes measuring at least one attribute of light of a light unit with a portable measurement device, transmitting the measured attribute to a control unit, and controlling the light unit based on the measured attribute. In some cases, the method includes measuring the at least one attribute of a light unit in an aircraft.

Abstract: An aircraft mirror assembly includes a light source, a front cover, and a light guide. The front cover is semi-transparent, the light source is arranged adjacent to an edge of the light guide, and the light guide is arranged adjacent to the front cover. In various aspects, the front cover includes an illumination zone, and, in an activated configuration, the light guide is configured to direct light from the light source to the illumination zone such that light is directed through the illumination zone. In certain aspects, the front cover includes an indicator, and, in an activated configuration, the light guide is configured to direct light from the light source to the indicator such that the indicator is activated. In various examples, the aircraft mirror assembly is provided with an aircraft cabin assembly positionable in a cabin of an aircraft.

Abstract: A method detects a driving state of a vehicle. The vehicle has a drive train with at least one drive and an accelerator pedal. A rest state of the accelerator pedal is determined by evaluating an operating point position of the accelerator pedal by a first accelerator pedal gradient in a first time interval, and checking whether the first accelerator pedal gradient within the first time interval is less than a maximum value.

Abstract: A sealing system for sealing a sealing gap between an outer housing and a rotor shaft of a rotor of a steam turbine, having a blocking medium wall for producing a blocking medium area between the rotor shaft and the outer housing in the region in front of and/or in the sealing gap, wherein the blocking medium wall is secured to the outer housing. The sealing system also has a blocking medium opening in the blocking medium wall in order to feed a blocking medium from the outside into the blocking medium area. The sealing system also has a shaft seal for sealing the blocking medium area from a second area, which has a second pressure that is lower than the first pressure, and a sliding ring seal for sealing the blocking medium area from a third area, which has a third pressure that is lower than the second pressure.

Abstract: A sealing system for sealing a sealing gap between an outer housing and a rotor shaft of a rotor of a steam turbine, having a blocking medium wall for producing a blocking medium area between the rotor shaft and the outer housing in the region in front of and/or in the sealing gap, wherein the blocking medium wall is secured to the outer housing. The sealing system also has a blocking medium opening in the blocking medium wall in order to feed a blocking medium from the outside into the blocking medium area. The sealing system also has a shaft seal for sealing the blocking medium area from a second area, which has a second pressure that is lower than the first pressure, and a sliding ring seal for sealing the blocking medium area from a third area, which has a third pressure that is lower than the second pressure.

Abstract: A method (600) for exiting a sailing mode of a vehicle (100) is described. The vehicle (100) comprises a clutch unit (103) which is disengaged in order to decouple a driving shaft (102) of the vehicle (100) from a driven shaft (105) of the vehicle (100), when the vehicle (100) is operated in the sailing mode. The method (600) comprises predicting (601) that a trigger for an exit of the sailing mode will occur, and initiating (602) the preparation of the clutch unit (103) for engagement, subject to predicting that a trigger for the exit of the sailing mode will occur. Furthermore, the method (600) comprises detecting (603) a trigger for the exit of the sailing mode, and adapting (604) a shaft speed (230) of the driving shaft (102), subject to detecting a trigger for the exit of the sailing mode. In addition, the method (600) comprises engaging (605) the clutch unit (103), subject to preparing the clutch unit (103) for engagement and subject to adapting the shaft speed (130), in order to exit the sailing mode.

Abstract: A method (600) for exiting a sailing mode of a vehicle (100) is described. The vehicle (100) comprises a clutch unit (103) which is disengaged in order to decouple a driving shaft (102) of the vehicle (100) from a driven shaft (105) of the vehicle (100), when the vehicle (100) is operated in the sailing mode. The method (600) comprises predicting (601) that a trigger for an exit of the sailing mode will occur, and initiating (602) the preparation of the clutch unit (103) for engagement, subject to predicting that a trigger for the exit of the sailing mode will occur. Furthermore, the method (600) comprises detecting (603) a trigger for the exit of the sailing mode, and adapting (604) a shaft speed (230) of the driving shaft (102), subject to detecting a trigger for the exit of the sailing mode. In addition, the method (600) comprises engaging (605) the clutch unit (103), subject to preparing the clutch unit (103) for engagement and subject to adapting the shaft speed (130), in order to exit the sailing mode.

Abstract: The invention relates to a hybrid drive, comprising an internal combustion engine, an electric machine and a torque superposition device, by means of which a torque supplied by the internal combustion engine can be superposed on a torque supplied by the electric machine, wherein the torque superposition device has a first and a second torque input and a torque output. The electric machine is coupled to the first torque input via a first transmission device, and the internal combustion engine is coupled to the second torque input via a second transmission device.

Abstract: The invention relates to a hybrid drive, comprising an internal combustion engine, an electric machine and a torque superposition device, by means of which a torque supplied by the internal combustion engine can be superposed on a torque supplied by the electric machine, wherein the torque superposition device has a first and a second torque input and a torque output. The electric machine is coupled to the first torque input via a first transmission device, and the internal combustion engine is coupled to the second torque input via a second transmission device.

Abstract: Aromatic diamines having the formula ##STR1## wherein R is alkyl or alkoxy having up to 6 carbon atoms are prepared by treating dinitro compounds having the formula ##STR2## wherein R is as previously defined, with hydrogen in the presence of one or more noble metals from the platinum or palladium groups as catalysts, optionally on catalyst supports, and in the presence of optionally substituted aniline as the solvent.The catalyst is generally used in amounts of 0.0005 to 0.1% by weight based on the amount of dinitro compound employed.