Abstract: An embodiment method for automatized selection and documentation of personal highlights during journeys with a vehicle includes capturing journey data during a journey of the vehicle, the journey data including audio, image, or video data taken of an interior or an exterior of the vehicle, storing selected aspects of the journey data to a non-transient data storage in response to a trigger criteria being met during the journey in an associated driving situation, and generating a selection of personal journey highlights based on the selected aspects stored during the journey for presentation during or after the journey.

Abstract: A driverless transportation vehicle for piece goods has a chassis, a traction drive, a load-transfer device with a load-transfer drive, and a control system. The chassis has at least two wheels arranged on an axle and the traction drive is configured to drive the wheels. The load-transfer device picks up an item of piece goods and transfer its center of mass on the vehicle. The control system controls the traction drive to prevent the transportation vehicle from tilting about the axle of the chassis, while the driverless transportation vehicle balances on only the at least two wheels. The control system additionally actuates the load-transfer drive in such a way that the position of the center of mass of the cargo is adapted for a driving maneuver that is to be carried out.

Abstract: A driverless transportation vehicle for piece goods has a chassis, a traction drive, a load-transfer device with a load-transfer drive, and a control system. The chassis has at least two wheels arranged on an axle and the traction drive is configured to drive the wheels. The load-transfer device picks up an item of piece goods and transfer its center of mass on the vehicle. The control system controls the traction drive to prevent the transportation vehicle from tilting about the axle of the chassis, while the driverless transportation vehicle balances on only the at least two wheels. The control system additionally actuates the load-transfer drive in such a way that the position of the center of mass of the cargo is adapted for a driving maneuver that is to be carried out.

Abstract: A method is provided comprising, receiving, by a computer system comprising a processor and a tangible, non-transitory memory, particle parameters, creating, by the computer system, particle elements in accordance with the particle parameters, and building, by the computer system, a pattern using the particle elements.

Abstract: The present disclosure generally relates to various composite slurries for use in seamless surface coverings and various methods for making the same. In particular, the present disclosure teaches various composite slurry compositions comprising, for example, a clear hardening material, a plurality of particles, a stabilizing filler, and an aggregate. Additionally, the present disclosure teaches various methods of forming composite slurry compositions for use in seamless surface coverings.

Abstract: A method is provided comprising, receiving, by a computer system comprising a processor and a tangible, non-transitory memory, particle parameters, creating, by the computer system, particle elements in accordance with the particle parameters, and building, by the computer system, a pattern using the particle elements.

Abstract: A method is provided comprising, receiving, by a computer system comprising a processor and a tangible, non-transitory memory, particle parameters, creating, by the computer system, particle elements in accordance with the particle parameters, and building, by the computer system, a pattern using the particle elements.

Abstract: An apparatus is provided comprising a shaft having an axis and mounted to a boom structure, a support structure configured to be coupled to the shaft, wherein the support structure is configured to rotate about the axis. In addition, a method is provided comprising translating a cradle along a vertical axis, and rotating, in response to the translating, a support structure about a shaft, wherein the cradle is supported by the support structure, wherein the cradle remains stationary with regard to pitch rotation during the translating.

Abstract: An aircraft comprising a rear opening and a rear door to close such rear opening, wherein the rear door is attached to the fuselage of the aircraft by means of an arrangement having two links due to which the rear door can be displaced longitudinally and in elevation up to a position at the interior of the fuselage.

Abstract: An apparatus is provided comprising a shaft having an axis and mounted to a boom structure, a support structure configured to be coupled to the shaft, wherein the support structure is configured to rotate about the axis. In addition, a method is provided comprising translating a cradle along a vertical axis, and rotating, in response to the translating, a support structure about a shaft, wherein the cradle is supported by the support structure, wherein the cradle remains stationary with regard to pitch rotation during the translating.

Abstract: An apparatus is provided comprising a shaft having an axis and mounted to a boom structure, a support structure configured to be coupled to the shaft, wherein the support structure is configured to rotate about the axis. In addition, a method is provided comprising translating a cradle along a vertical axis, and rotating, in response to the translating, a support structure about a shaft, wherein the cradle is supported by the support structure, wherein the cradle remains stationary with regard to pitch rotation during the translating.

Abstract: An aircraft with a fuselage that accommodates at least one air breathing propulsion engine, the fuselage having a maximum fuselage width determined in the region of the at least one air breathing propulsion engine and comprising at least one front fuselage cowling and at least one rear fuselage cowling that are each covering the at least one air breathing propulsion engine at least partly, the at least one front and rear fuselage cowlings being spaced apart from each other in a direction transverse to a longitudinal axis of the at least one air breathing propulsion engine by a predetermined cowling offset to define a dynamic air intake through which an intake air stream is supplied to the at least one air breathing propulsion engine in operation.

Abstract: The present disclosure generally relates to various composite slurries for use in seamless surface coverings and various methods for making the same. In particular, the present disclosure teaches various composite slurry compositions comprising, for example, a clear hardening material, a plurality of particles, a stabilizing filler, and an aggregate. Additionally, the present disclosure teaches various methods of forming composite slurry compositions for use in seamless surface coverings.

Abstract: The present disclosure generally relates to various composite slurries for use in seamless surface coverings and various methods for making the same. In particular, the present disclosure teaches various composite slurry compositions comprising, for example, a clear hardening material, a plurality of particles, a stabilizing filler, and an aggregate. Additionally, the present disclosure teaches various methods of forming composite slurry compositions for use in seamless surface coverings.

Abstract: An aircraft comprising a rear opening and a rear door to close such rear opening, wherein the rear door is attached to the fuselage of the aircraft by means of an arrangement having two links due to which the rear door can be displaced longitudinally and in elevation up to a position at the interior of the fuselage.

Abstract: An apparatus is provided comprising a shaft having an axis and mounted to a boom structure, a support structure configured to be coupled to the shaft, wherein the support structure is configured to rotate about the axis. In addition, a method is provided comprising translating a cradle along a vertical axis, and rotating, in response to the translating, a support structure about a shaft, wherein the cradle is supported by the support structure, wherein the cradle remains stationary with regard to pitch rotation during the translating.

Abstract: An aircraft with a fuselage that accommodates at least one air breathing propulsion engine, the fuselage having a maximum fuselage width determined in the region of the at least one air breathing propulsion engine and comprising at least one front fuselage cowling and at least one rear fuselage cowling that are each covering the at least one air breathing propulsion engine at least partly, the at least one front and rear fuselage cowlings being spaced apart from each other in a direction transverse to a longitudinal axis of the at least one air breathing propulsion engine by a predetermined cowling offset to define a dynamic air intake through which an intake air stream is supplied to the at least one air breathing propulsion engine in operation.