Abstract: A power assisted flying device is powered via a vector thrust control apparatus supporting the motor where the vector thrust control apparatus includes a gyratory group that allows the motor to pivot up and down and from side to side. At least two servo motors are attached to the vector thrust control apparatus to move said motor up and down and from side to side. Alternatively, the flying device may incorporate a non-rotating outer ring and a rotating inner ring disposed around a shaft. At least two servo motors are connected to the non-rotating outer ring and the rotating inner ring in relation to the rotational axis. At least two linkage rods connect between the rotating inner ring and the propeller. Tilting of the non-rotating outer ring is transmitted to the propeller to effectuate at least one of cyclic pitch modulation or teetering hub modulation of the propeller.

Abstract: An electric tool includes a vibratory means which is configured to impart a counteracting vibration which counteracts a housing vibration of the electric tool. A vibration-relevant characteristic of the vibratory means can be adapted during the operation of the electric tool in such a way that the amplitude, the phase position and/or the frequency of the counteracting vibration varies with a change in the vibration-relevant characteristic. The vibratory means of the electric tool has a natural frequency which can be varied by variation means of the electric tool. A method for compensating housing vibrations, in particular of the electric tool, includes imparting a counteracting vibration by a vibratory means which counteracts a housing vibration of the electric tool. The amplitude, the phase position and/or the frequency of the counteracting vibration is varied during the operation of the electric tool.

Abstract: An electric tool includes a striking mechanism assembly, which can be driven in and against a striking direction in a cyclic manner, and a counter-oscillator for compensating for vibrations of the electric tool, in particular of housing oscillations, comprising a balancing mass. The balancing mass can be driven in a movement direction by driving the striking mechanism assembly, wherein the movement direction extends at an angle to the striking direction.

Abstract: A power assisted flying device is powered via a vector thrust control apparatus supporting the motor where the vector thrust control apparatus includes a gyratory group that allows the motor to pivot up and down and from side to side. At least two servo motors are attached to the vector thrust control apparatus to move said motor up and down and from side to side. Alternatively, the flying device may incorporate a non-rotating outer ring and a rotating inner ring disposed around a shaft. At least two servo motors are connected to the non-rotating outer ring and the rotating inner ring in relation to the rotational axis. At least two linkage rods connect between the rotating inner ring and the propeller. Tilting of the non-rotating outer ring is transmitted to the propeller to effectuate at least one of cyclic pitch modulation or teetering hub modulation of the propeller.

Abstract: A power assisted flying device is disclosed, wherein a vector control apparatus is used to help lift and fly a kite or kite-like object. Two servo motors may be used to move a gimbal mechanism to which the control motor is attached. Another kite-like object is disclosed wherein there are brackets to directly connect servos and propulsion motors to a kite. An added structure is shown to quickly connect and disconnect a vector control apparatus from a kite frame. In addition, new kite frame fittings are disclosed and a vector control apparatus to lift and fly a rotating kite.

Abstract: The invention relates to a tool receptacle (1), in particular for a hammer drill and/or rotary hammer, comprising a receptacle body (2) which has an insertion opening (3) for accommodating a tool shank (4), an axially displaceable locking control element (41) for axially locking the tool shank (4) in the insertion opening (3), and a rotatably mounted locking control body (41) for rotationally locking the receptacle body (2). Provision is made for the locking control element and the locking control body to be designed as a common component (41).