Abstract: A rotor blade for a driven horizontal rotor of a rotary-wing aircraft comprises an elongated main body which includes a leading edge, a trailing edge, and an upper surface extending between the leading edge and the trailing edge. The rotor blade further comprises at least one flap having a front end and a rear end and mounted to the main body at its front end swiveling about a swiveling axis running in parallel to the radial or spanwise axis of the rotor blade. The flap has a basic position in which it lies flat against the upper surface of the main body. Further, the flap is passively swiveled by aerodynamic forces and inertial forces about its swivel axis to raise above the upper surface of the main body, and a reset force acts upon the flap to reset it into its basic position on the surface of the main body.

Abstract: The invention relates to a method for determining a potential conflict situation (2) between objects within a multidimensional traffic area (1), with the objects each moving on predetermined trajectories (T1 to T11), having the following steps: a) subdivision of the traffic area (1), with respect to at least one dimension (x, y, z, t) of the traffic area (1), into at least two partial traffic areas (11, 12, 13, 14, 41, 42, 51, 52, 53, 61), and b) repetition of steps a) and b) corresponding to those partial traffic areas (11, 12, 13, 14, 41, 42, 51, 52, 53, 61) which were subdivided in step a) and are influenced by at least two trajectories (T2, T3), with a potential conflict situation (2) between at least two trajectories (T2, T3) which jointly influence a partial traffic area (113) being determined as a function of an extent with respect to at least one dimension (x, y, z, t) of the partial traffic area (113).

Abstract: The invention relates to a reflection device that can track the location of sun, focusing solar radiation on a radiation receiver. The tracking is controlled by means of an auxiliary mirror guiding an auxiliary beam to a target. The position of the point of incidence of the auxiliary beam on the target is detected by a video camera and an image capture system, and said actual position is adjusted to a prescribed target position. It is thus achieved that the main beam is always precisely aimed at the radiation receiver.

Abstract: A handling device, which is in particular a robot, has a receiving device for receiving different instruments. To this end, the receiving device and the different instruments have mutually compatible connecting elements. In order to ensure error-free connection of the correctly selected instrument to the receiving device, the instruments have changeable indicator devices. The indicator devices are changed with the aid of a control device, for example on the basis of a schedule.

Abstract: A method for the calculation of flight paths taking into consideration events of relevance for the radiation dose comprises the following steps: a) collection of radiation data for atmospheric radiation (10); b) examination of the radiation data and conclusion about an event of relevance for radiation dose generating a temporary increase in exposure; c) creation of a model using the radiation data, wherein the model contains at least one estimate of the geographical location of a region with a radiation intensity increased by the event of relevance for radiation dose; d) determination of flight-relevant parameters; e) calculation of a possible flight path in the light of the flight-relevant parameters taking into consideration the model created in step c), wherein the flight path is adjusted in respect of a reduction of exposure to radiation.

Abstract: The device for receiving signals which have carrier frequencies and codes, said signals being navigation or communication signals, has multiple individual antennas (114) for receiving a signal, each individual antenna (114) having an antenna output (116) at which the received signal is present. Furthermore, the device is provided with an analog preprocessing unit (122) for preprocessing the signals received by the individual antennas (114), said preprocessing unit (122) having signal transmitting and signal preprocessing channels (124) which are assigned to the individual antennas (114), and the device is provided with a digital signal processor (134). The device additionally has a calibration signal generating unit (148) for generating a calibration signal which, like the signals received by the individual antennas (114), has a carrier frequency and a code and which is used for calibrating the propagation time and the phase of the signal transmission paths.

Abstract: Minimally invasive instrument for robotic surgery including a functional element, a force, torque and/or pressure transmission device for transmitting force, torque and/or pressure from a drive to the functional element, a coupling device for coupling the instrument to a medical robot such that the functional element can be actuated by the drive, wherein an operating element for manually operating the functional element in a state in which the instrument is uncoupled from the medical robot.

Abstract: A method for early detection of the vortex ring state in a helicopter includes steps of establishing flight control signals for flight control with regard to the vertical movement axis of the helicopter, detecting resultant movements in the vertical movement axis of the helicopter, and detecting an impending vortex ring state of the helicopter in accordance with a correlation between the flight control signals and the vertical movements in the vertical movement axis.

Abstract: The invention relates to a method for operating a robot, including detecting the spatial position and/or location of at least one delimiting structure which causes a kinematic delimitation of the work space that can be reached by an instrument connected to a robotic arm of the telemanipulation robot; and continuously representing the reachable work space on an object to be manipulated by the instrument in such a way that a change in the position and/or location of the delimiting structure results, in real time, in a change of the represented reachable work space.

Abstract: A method for recovery of lost data and for correction of corrupted data transmitted from a sending device to a receiver device, the method comprising the steps: encoding the data by an encoder connected to the sending device, transmitting the data from the sending device to the receiver device via a transmitting device, and decoding the data by a decoder connected to the receiver device, whereby lost and/or corrupted data is recovered during decoding is conducted by solving the system of equations of a parity check matrix H.

Abstract: A laser scanner device having a laser beam emission apparatus which is designed to emit at least one laser beam in an emission area, and a mirror arranged at least partially in the emission area, and having a receiving apparatus which is designed to receive reflections of the laser beam, includes a first drive device which can move a first kinematic chain, and a second drive device which can move a second kinematic chain. The is connected to the first and to the second kinematic chain and can be scanned in mutually independent coordinate directions (X, Y) via the first and the second kinematic chain.

Abstract: A surgical manipulation instrument which is particularly suitable for minimal invasive surgery, comprising an extra-corporeal drive device and a partial intra-corporeal manipulator part. The drive device comprises several axially displaceable first actuation elements. The first actuation elements are detachably connected to axially displaceable second actuation elements, by a coupling device, the second actuation elements being used to actuate an end effector. The coupling device comprises two coupling elements, one of the coupling elements having undercut recesses in which the second coupling element engages.

Abstract: An engine apparatus is provided for a flying object, the engine apparatus including a combustion chamber having a throat region and a nozzle region, the nozzle region having a nozzle wall, wherein the nozzle region expands from the throat region towards an exit end relative to a combustion chamber axis, wherein the nozzle region has associated therewith a skirt having a skirt wall, the skirt being positioned downstream relative to the exit end and surrounding the exit end of the nozzle region, and wherein the skirt wall is at an acute angle away from the combustion chamber axis with respect to the nozzle wall, at least at the exit end of the nozzle region.

Abstract: The invention relates to a device (10) for stabilizing the guidance of a vehicle (1), the vehicle (1) having at least one or two which is arranged in such a way that it can be turned relative to the longitudinal axis of the vehicle (1), and steering means that interact with the at least one wheel (2) and are designed to guide the vehicle (1) by turning the at least one wheel (2). The device (10) has a detecting unit (12), which is designed to detect an at least partial transition from static friction to dynamic friction between the at least one wheel (2) and a ground covering (3), and furthermore has a control unit (11), which, when the detecting unit (12) detects the transition from static friction to dynamic friction, is designed to turn the at least one wheel (2) by means of the steering means in such a way that the dynamic friction between the wheel (2) and the ground covering (3) changes back to static friction.

Abstract: A measuring device, in particular a measuring device for remote sensing, has a measuring instrument and an apparatus for movably mounting the measuring instrument. The apparatus has two non-parallel rotation axes. The rotation axes are different from a longitudinal axis of the measuring instrument. The measuring instrument is connected to a rotatable drive element via a power transmission element.

Abstract: In the method for geo-referencing of optical remote sensing images of an area of the earth's surface, the geo-referencing is corrected based on an SAR image which is geo-referenced.

Abstract: A nozzle, in particular an outlet nozzle of an aircraft jet engine, is formed with at least one nozzle wall. A turbulence-generating and/or vortex-generating structure is arranged on an inner face of the nozzle wall and projects radially inwardly from the nozzle wall. Alternatively, or in addition, a turbulence-generating and/or vortex-generating structure is arranged on an outer face of the nozzle wall and projects radially outwardly from the outer face. There is also described a structural element and a method of producing a nozzle.

Abstract: A device for determining the actual center of gravity of a vehicle, having a control command input interface, a movement modeling unit, a sensor interface, and a computation unit. The control command input interface determines control command inputs for controlling the movement of the vehicle. The movement modeling unit calculates reference acceleration data at a model reference point of the vehicle on the basis of movements of the vehicle, which are derived from a vehicle movement model, with respect to the control command inputs. The sensor interface determines sensor acceleration data which are measured at a sensor reference point of the vehicle and relate to the vehicle's actual movements resulting from the command inputs. The computation unit determines the actual center of gravity of the vehicle on the basis of an assumed center of gravity and the difference between the reference acceleration data and the sensor acceleration data.

Abstract: A wing for of aircraft has a wing tip shape that has a profile that extends in the direction of the span of the wing, and across the direction of the span of the wing extends from the wing leading edge to the wing trailing edge. The profile is delimited by a first skin and a second skin, with a winglet, arranged on the wing end. The winglet is substantially planar, and has a transition region arranged between the wing and the winglet, that extends from a connection on the wing to a connection on the winglet. The curvature of the local dihedral can increase in the transition region from a low level or a level of zero at or near the wing intersection in the outboard direction.

Abstract: The invention relates to an assistance system (1, 25) for providing support in situation-dependent planning and/or guidance tasks of a controlled system (2), comprising a state detection unit (3) for detecting at least one state (5, 5a) of the controlled system (2), an acoustic receiving unit (9, 27), which is designed to receive acoustic voice signals of voice communication (24) between at least two persons (21, 22), and a voice processing unit (7), which is designed to detect voice information (10) regarding the controlled system (2) from the received acoustic voice signals, wherein the state detection unit (3) is designed to adapt the detected state (5) and/or a predicted state (5a) of the controlled system (2) that can be derived from the current state, according to the detected voice information (10).