Abstract: A conveyor bowl for a vibratory conveyor device includes a main body made of stainless steel and manufactured by primary shaping. The main body has an interface section for coupling to a vibration unit, and a conveyor section for conveying conveyed parts. The main body may be designed as a cast part. The main body may be a precision cast part or an investment cast part. The main body may be made of austenite. The interface section and the conveyor section may be formed in one piece or formed integrally with the main body.

Abstract: A conveyor bowl for a vibratory conveyor device includes a main body made of stainless steel and manufactured by primary shaping. The main body has an interface section for coupling to a vibration unit, and a conveyor section for conveying conveyed parts. The main body may be designed as a cast part. The main body may be a precision cast part or an investment cast part. The main body may be made of austenite. The interface section and the conveyor section may be formed in one piece or formed integrally with the main body.

Abstract: The present invention relates to anaerobically curable compositions demonstrating resistance to elevated temperature conditions.

Abstract: The present invention relates to anaerobically curable compositions demonstrating resistance to elevated temperature conditions.

Abstract: A high lift system for an aircraft with at least one high lift flap arranged on each of the main wings of the aircraft. The high lift system includes an input device for the generation of flight phase-related requirements for the high lift flap. The high lift system further includes a control device, with a conversion function with which the flight phase-related requirements are converted into setting commands for the actuation of a lift device for the adjustment of the high lift flap. The conversion function is configured such that from a take-off requirement, a setting command to the drive device is generated with which the leading edge flap of the high lift flap is arranged in a set state in which a gap exists between the leading edge flap and the main wing with a gap width of between 0.1% and 0.4% relative to the local wing chord.

Abstract: A high lift system for an aircraft with at least one high lift flap arranged on each of the main wings of the aircraft. The high lift system includes an input device for the generation of flight phase-related requirements for the high lift flap. The high lift system further includes a control device, with a conversion function with which the flight phase-related requirements are converted into setting commands for the actuation of a lift device for the adjustment of the high lift flap. The conversion function is configured such that from a take-off requirement, a setting command to the drive device is generated with which the leading edge flap of the high lift flap is arranged in a set state in which a gap exists between the leading edge flap and the main wing with a gap width of between 0.1% and 0.4% relative to the local wing chord.

Abstract: In the case of a method for working a tube made from a metallic material, wherein at least one punching is made in a tube wall of the tube at at least one first circumferential location of the tube wall, the tube wall is provided, at at least one second circumferential location, which faces away from the first circumferential location in the circumferential direction, with at least one forming selected from the group that consists of at least one depression of the tube wall, at least one throughhole in the tube wall.

Abstract: An arrangement for connecting a tubular first component to a second component, in particular for connecting a tensioning tube to an A-pillar of a vehicle body, has a first structural element which forms a receptacle for a screw element and is arranged at an end of the first component that faces the second component, and a second structural element which is secured in such a manner at that end of the first component which faces the second component that the first structural element is held between the first component and the second structural element, and the screw element is held by the second structural element in the first structural element in loss-proof fashion, the screw element being movable in the first structural element, at least in a direction transversely with respect to a longitudinal axis of the first component, for compensation of tolerances in the connection of the first component to the second component. Furthermore, a method for producing an arrangement of this type is described.

Abstract: An arrangement for connecting a tubular first component to a second component, in particular for connecting a tensioning tube to an A-pillar of a vehicle body, has a first structural element which forms a receptacle for a screw element and is arranged at an end of the first component that faces the second component, and a second structural element which is secured in such a manner at that end of the first component which faces the second component that the first structural element is held between the first component and the second structural element, and the screw element is held by the second structural element in the first structural element in loss-proof fashion, the screw element being movable in the first structural element, at least in a direction transversely with respect to a longitudinal axis of the first component, for compensation of tolerances in the connection of the first component to the second component. Furthermore, a method for producing an arrangement of this type is described.

Abstract: The present invention generally relates to an interlocking device and in more particular to an interlocking device with a rotary latch that receives a latching bolt. In operation, the rotary latch can swing out of a release position into a locked position, by means of the bolt engaging a coupling jaw of the rotary latch. When the rotary latch is in a locked position, a safety element in an arresting position prevents rotary latch from swinging into its release position.

Abstract: The invention relates to an apparatus for external modulation of high-efficiency CO.sub.2 laser beams of defined wavelength, particularly for use in CO.sub.2 laser material working apparatuses. According to the invention two plates made of transparent material are arranged parallel to each other, the inner surfaces of the plates are reflective and the outer surfaces are non-reflective.