Abstract: The present invention provides a cover for a seat in an aircraft or spacecraft, including a receiver which is configured to receive in an exchangeable manner an electronic device which is fitted with a screen, at least one recess being provided in the region of the receiver such that the screen of the electronic device is exposed for viewing.

Abstract: The present disclosure pertains to a seat device of an aircraft or spacecraft, having a seat which comprises a headrest, and a loudspeaker device which includes at least one pair of loudspeakers which are spaced apart from one another and located in the region of the headrest.

Abstract: The present disclosure pertains to a seat device for an aircraft or spacecraft with at least one photoelectric device, which is designed to provide electrical energy such that this energy can be used to charge or supply an electrical device, and/or amplify audio signals, and/or transmit data.

Abstract: A lighting system includes at least one illumination device having a luminaire and a luminaire controller configured to control the operational state of the luminaire according to lighting control data, and a lighting controller configured to transmit the lighting control data to at least one illumination device. The lighting controller is configured to pre-format the lighting control data for the at least one illumination device in one or more color space representation matrices having matrix entries corresponding to color space representation values for the luminaire. The lighting controller is further configured to encode the pre-formatted color space representation matrices using a data compression algorithm.

Abstract: A method for displaying information by means of a dual-view-display in a passenger-cabin of an air-/spacecraft, comprising the following steps: providing the dual-view-display on a predetermined portion of the passenger-cabin; providing first information by means of the dual-view-display, in such a way that said information can be perceived from a gangway between rows of seats of the passenger cabin; and simultaneously providing second information, different from the first information, by means of the dual-view-display, in such a way that said information can be perceived from one of the rows of seats. A display device for displaying information in a passenger-cabin of an air-/spacecraft, comprising a dual-view-display which is arranged on a predetermined portion of the passenger-cabin, the dual-view-display being configured to provide first and second information in the above described ways. A passenger-cabin for an air-/spacecraft comprising said display-device.

Abstract: A cabin management system (CMS) for an aircraft is provided. The CMS comprises a functional unit, a control unit for controlling the functional unit, and a display arrangement for displaying a three-dimensional virtual scenario. The display arrangement comprises a display element and a position detection unit for detecting the position of an input element for interacting with the three-dimensional virtual scenario. The display element is for displaying at least one three-dimensional virtual object. The position detection unit is interconnected with the control unit as to transmit the position of the input element to the control unit. The control unit compares the position of the input element in the three-dimensional virtual scenario with the virtual position of the three-dimensional virtual object. The control unit provides a control command to the CMS which control command is assigned to a status of a three-dimensional virtual object which is selected by the input element.

Abstract: A method for presenting information by means of an autostereoscopic 3D-display in a passenger cabin of an aircraft or spacecraft, comprising the following steps: provision of the autostereoscopic 3D-display in a predetermined portion of the passenger cabin; provision of a first item of information by means of the autostereoscopic 3D-display such that this information can be detected from a first seat in the passenger cabin; simultaneous provision of a second item of information, which is different from the first item of information, by the autostereoscopic 3D-display such that this second item of information can be detected from a second seat in the passenger cabin. A display device for implementing a method of this type. A passenger cabin for an aircraft or spacecraft comprises a display device of this type. An aircraft or spacecraft having a display device of this type or having a passenger cabin of this type.

Abstract: The present disclosure pertains to a seat device of an aircraft or spacecraft, having a seat which comprises a headrest, and a loudspeaker device which includes at least one pair of loudspeakers which are spaced apart from one another and located in the region of the headrest.

Abstract: The present invention provides a cover for a seat in an aircraft or spacecraft, including a receiver which is configured to receive in an exchangeable manner an electronic device which is fitted with a screen, at least one recess being provided in the region of the receiver such that the screen of the electronic device is exposed for viewing.

Abstract: The present disclosure pertains to a seat device for an aircraft or spacecraft with at least one photoelectric device, which is designed to provide electrical energy such that this energy can be used to charge or supply an electrical device, and/or amplify audio signals, and/or transmit data.

Abstract: An autostereoscopic projection screen including a projection area and a control, wherein the projection area includes micromirrors, wherein the control is adapted to adjust orientation of the micromirrors such that the micromirrors can reflect light emitted by an image source into directions creating an image in each direction at a viewing distance such that each image can only be seen by one eye of a viewer located in said direction at said viewing distance, and wherein two images are created at a first viewing distance and spaced apart such that a viewer in the first viewing distance can see one of the two images with a first eye only and the other of the two images with a second eye only, wherein the viewer has the impression of seeing the two images simultaneously. The invention further relates to a method and a system for autostereoscopic projection.

Abstract: A method for presenting information by means of an autostereoscopic 3D-display in a passenger cabin of an aircraft or spacecraft, comprising the following steps: provision of the autostereoscopic 3D-display in a predetermined portion of the passenger cabin; provision of a first item of information by means of the autostereoscopic 3D-display such that this information can be detected from a first seat in the passenger cabin; simultaneous provision of a second item of information, which is different from the first item of information, by the autostereoscopic 3D-display such that this second item of information can be detected from a second seat in the passenger cabin. A display device for implementing a method of this type. A passenger cabin for an aircraft or spacecraft comprises a display device of this type. An aircraft or spacecraft having a display device of this type or having a passenger cabin of this type.

Abstract: A display apparatus for a passenger cabin of an aircraft or spacecraft, said display apparatus comprising a display device, which is arranged at a predetermined display device inclination angle to a supply duct of the passenger cabin, wherein the display device is configured in such a way that a virtual image plane of the display device has a predetermined virtual image plane inclination angle to the supply duct, said virtual image plane inclination angle differing from the display device inclination angle. A passenger cabin for an aircraft or spacecraft comprising a display apparatus of this type, and an aircraft or spacecraft comprising a display apparatus of this type or comprising a passenger cabin of this type.

Abstract: A method for displaying information by means of a dual-view-display in a passenger-cabin of an air-/spacecraft, comprising the following steps: providing the dual-view-display on a predetermined portion of the passenger-cabin; providing first information by means of the dual-view-display, in such a way that said information can be perceived from a gangway between rows of seats of the passenger cabin; and simultaneously providing second information, different from the first information, by means of the dual-view-display, in such a way that said information can be perceived from one of the rows of seats. A display device for displaying information in a passenger-cabin of an air-/spacecraft, comprising a dual-view-display which is arranged on a predetermined portion of the passenger-cabin, the dual-view-display being configured to provide first and second information in the above described ways. A passenger-cabin for an air-/spacecraft comprising said display-device.