Abstract: Tetraisopentyl esters of butanetetracarboxylic acid are useful as plasticizers or as part of a plasticizer composition for polymers, A process for the production thereof, plasticizer compositions containing the tetraisopentyl esters of butanetetracarboxylic acid, and plastics compositions containing the tetraisopentyl esters of butanetetracarboxylic acid are also provided,

Abstract: Cylinder liner for an internal combustion engine, comprising: a cylindrical portion having an outer diameter and an inner diameter, the inner diameter at least partly realizing a cylinder wall, when the cylinder liner is mounted in the internal combustion engine, a circumferential recess at the inner diameter of the cylindrical portion having a larger diameter than the inner diameter of the cylinder wall, wherein the circumferential recess is located at one end of the cylindrical portion, and a removable scraper ring, wherein the recess comprises at least one groove, wherein a size of the scraper ring is adapted to fit into the recess and to cover the at least one groove.

Abstract: Various embodiments include a tool for fitting a stator into a housing comprising: a housing mounting; a tool holder; and a stator gripper. The housing mounting includes a positioning device for holding the housing. The tool holder defines a tool holder volume and has a receiving opening. The stator gripper is arranged in the tool holder and moves between a first position and a second position. The stator gripper comprises a gripper head for holding the stator, in the first position, the gripper head is arranged in the tool holder volume and, in the second position, the gripper head is guided, at least in one section, through the receiving opening. The housing mounting and/or the tool holder move toward one another or away from one another. The housing mounting or the tool holder or the stator gripper includes a pressure medium feed opening.

Abstract: A device for performing or enabling an electrical measurement on a measurement layer includes: at least one measurement layer having a layer thickness, and electrical connections connected to and/or adjacent to and serving to determine the electrical resistance of the at least one measuring layer. At least some electrical connections are connected to or adjacent to different length portions of the at least one measuring layer, whereby a measurement for determining the electrical resistance of the at least one measuring layer in the direction of its layer thickness is carried out or made possible. At least some of the electrical connections are connected to or adjacent to different, preferably mutually opposite, surfaces of the at least one measuring layer, whereby a measurement for determining the electrical resistance of the at least one measuring layer is carried out or made possible in the direction transverse to its layer thickness.

Abstract: An object has a first conductor structure, an electronic unit, a second conductor structure galvanically isolated from the first conductor structure and/or from the electronic unit but coupleable electrically thereto, and a carrier structure with a first pliable carrier layer having a first carrier layer region and with a second carrier layer region. The carrier structure is a layer stack in a base surface region including at least part of the carrier structure base surface and includes at least the first and second carrier layer regions. At least part of the conductor structures is in the base surface region. The first conductor structure and/or the electronic unit is joined with the first carrier layer region. The second conductor structure is joined with the second carrier layer region and coupleable electrically to the first conductor structure and/or the electronic unit by a layer stack surface region outside the electronic unit.

Abstract: An unmanned aerial vehicle (UAV) includes a body that supports breakaway components. One component is a battery pack which powers the vehicle. Two other components are pod assemblies, which each include at least one motor and one propeller. Each motor is supported within a support ring using spokes or filament. The spokes keep the motor firmly stable during operation and also effectively encage the otherwise dangerous spinning propeller. This allows the vehicle to operate with a higher level of safety than conventional UAVs. The breakaway feature can be established using magnets.

Abstract: An unmanned aerial vehicle (UAV) includes a fuselage that supports breakaway components that are attached using magnets. One component is a battery pack which powers the vehicle. Another component is a rotor set including two identical pod pairs that each support a motor and a propeller. Each motor is attached to a hub assembly that includes a plurality of spokes captured in a motor hub and sandwiched by a rigid motor printed circuit board on top and a rigid hub plate. The hub assembly construction is rigid in plane and functions to keep the motor firmly stable during operation. The hub assembly is compliant and resilient when impacted parallel to the plane. Other features of the pod pairs encage the otherwise dangerous spinning propeller. This allows the vehicle to operate with a higher level of safety than conventional UAVs.

Abstract: A modular unmanned aerial system (UAS) can be configured to detect an anomalous UAS configuration or operating condition, and to notify the user or inhibit further operation of the UAS in response to such a detection. An indication of the actual rotational speed of the motor or of the flight power needed to hold the UAS in a hover state may be compared to a predicted value based upon the expected UAS configuration. A variance between the actual values and the predicted values may indicate that the UAS is in an unauthorized configuration, which may be due to an unauthorized payload. The UAS may be a modular system, and may take into account authorized and attached modules in predicting the thrust required to hold the UAS in a hover state.

Abstract: A foil structure with generation of visible light via LED technology has a carrier foil and an LED chip for generation of UV light. The LED chip is disposed on a first portion of the carrier foil and is provided with a light output face for emission of the UV light. The foil structure further has a color reaction layer for conversion of the UV light into the visible light, wherein the color reaction layer is disposed on a second portion of the carrier foil. The carrier foil is folded over in such a way that the second portion of the carrier foil is disposed above the first portion of the carrier foil and the color reaction layer is disposed above the LED chip or in a manner laterally offset relative to the LED chip.

Abstract: Various embodiments include a tool for fitting a stator into a housing comprising: a housing mounting; a tool holder; and a stator gripper. The housing mounting includes a positioning device for holding the housing. The tool holder defines a tool holder volume and has a receiving opening. The stator gripper is arranged in the tool holder and moves between a first position and a second position. The stator gripper comprises a gripper head for holding the stator, in the first position, the gripper head is arranged in the tool holder volume and, in the second position, the gripper head is guided, at least in one section, through the receiving opening. The housing mounting and/or the tool holder move toward one another and away from one another. The housing mounting and/or the tool holder and/or the stator gripper includes a pressure medium feed opening.

Abstract: A method is provided for allowing UAV pilots to create a flight path profile and upload the same to a central server, allowing access to other UAV pilots. The method includes the steps of having creating a first flight path profile, uploading the flight path profile to a central server, allowing access of the flight path profile to others, and downloading the first flight path profile to a UAV so that the UAV follows the downloaded first flight profile. The flight path profile includes control of three dimensional motion and orientation of a UAV, control of the view orientation of a camera, as well as other camera settings such as video and still image modes, frame rate, and exposure, altitude and speed and dwell times.

Abstract: A quadcopter has a fuselage and four rotors, each defining a thrust vector. An onboard camera system includes a gimbal with a roll axis and a pitch axis. Right side motors are mounted with a dihedral angle so that their respective thrust vectors intersect at a common focal point located above the fuselage. Left side motors are mounted with a dihedral angle so that their respective thrust vectors intersect at a common focal point located above the fuselage. The tilted thrust vectors provide yaw stability which allows flight yaw control to be used as yaw control of the onboard camera.

Abstract: A foil structure with generation of visible light using LED technology includes a carrier foil and an LED chip for generation of UV light. The LED chip is disposed on the carrier foil and is provided with a light output face for emission of the UV light. Furthermore, the foil structure includes a color reaction layer for conversion of the UV light into the visible light. The color reaction layer is disposed above the LED chip or in a manner laterally offset relative to the LED chip. The color reaction layer is provided with a structuring, so that the UV light emitted from the light output face of the LED chip is not emitted into the surroundings of the foil structure.

Abstract: A unmanned aerial vehicle (UAV) includes a body with plurality of motors, a motor controlling circuit, a microprocessor for controlling the flight state of the UAV, a plurality of motion sensors, and a capacitive touch sensor incorporated into a battery. When the user grasps the UAV by the battery, the touch sensor is activated and the microprocessor alters the flight state of the UAV.

Abstract: A propeller drive assembly includes an electric motor having a stator and a rotor. During operation the motor generates heat. A propeller made from a thermally conductive plastic includes a hub that is secured to the rotor portion of the motor so that the heat generated within the motor is transferred by conductance through the thermally conductive hub and propeller and then, by convection, is absorbed by the surrounding air, as the propeller rotates through the air. A thermally conductive interface material can be positioned between the rotor portion of the motor and the hub of the propeller to increase the thermal efficiency of the heat transfer between the motor and the propeller. A thermally conductive grease can be used as the interface material and an O-ring seal can be provided about the rotor to prevent the grease from escaping during motor operation.

Abstract: A method for synchronizing an audio track that is being recorded at a first location with a video track that is being recorded at a second location, such as on a flying UAV, is disclosed. First, the audio and video recorders being to record sound and video. Then, a GPS receive is used to pick up the very accurate GPS clock signal. A real-time clock is also used locally to generate a real-time value. At a predetermined time, the GPS time data is interrogated and a time-stamp is generated. A video encoder is then used to embed the time-stamp, either during recording, or shortly thereafter. A networked audio recording device records audio with a time stamp acquired from the network. These respective time-stamps are then used in post-processing to accurately synchronize the audio and video tracks.

Abstract: A modular unmanned aerial system (UAS) can be configured to detect an anomalous UAS configuration or operating condition, and to notify the user or inhibit further operation of the UAS in response to such a detection. An indication of the actual rotational speed of the motor or of the flight power needed to hold the UAS in a hover state may be compared to a predicted value based upon the expected UAS configuration. A variance between the actual values and the predicted values may indicate that the UAS is in an unauthorized configuration, which may be due to an unauthorized payload. The UAS may be a modular system, and may take into account authorized and attached modules in predicting the thrust required to hold the UAS in a hover state.

Abstract: A foil structure with generation of visible light using LED technology includes a carrier foil and an LED chip for generation of UV light. The LED chip is disposed on the carrier foil and is provided with a light output face for emission of the UV light. Furthermore, the foil structure includes a color reaction layer for conversion of the UV light into the visible light. The color reaction layer is disposed above the LED chip or in a manner laterally offset relative to the LED chip. The color reaction layer is provided with a structuring, so that the UV light emitted from the light output face of the LED chip is not emitted into the surroundings of the foil structure.

Abstract: A foil structure with generation of visible light via LED technology has a carrier foil and an LED chip for generation of UV light. The LED chip is disposed on a first portion of the carrier foil and is provided with a light output face for emission of the UV light. The foil structure further has a color reaction layer for conversion of the UV light into the visible light, wherein the color reaction layer is disposed on a second portion of the carrier foil. The carrier foil is folded over in such a way that the second portion of the carrier foil is disposed above the first portion of the carrier foil and the color reaction layer is disposed above the LED chip or in a manner laterally offset relative to the LED chip.

Abstract: A modular unmanned aerial vehicle (UAV) can include a main body and one or more peripherals configured to be removably attached to the main body. The main body can be configured to identify the peripheral, such as through the provision of an identifying signal on the provisional. The processor can cause the UAV to execute a function based at least in part on the identification of the attached peripheral, or by user interaction with the peripheral or another component of the UAV.