Abstract: A method for determining an altered measurement strategy for measurement of a measurement object using a coordinate measuring machine includes measuring the measurement object according to an initial measurement strategy. The method includes determining a measurement quality of the measurement. The method includes, in response to the measurement quality being greater than a predetermined target minimum measurement quality, altering the initial measurement strategy to produce the altered measurement strategy. The altering is performed such that at least one of time required to measure the measurement object in accordance with the altered measurement strategy is reduced, computational outlay required to measure the measurement object in accordance with the altered measurement strategy is reduced, and data storage capacity required to measure the measurement object in accordance with the altered measurement strategy is reduced.

Abstract: A fastening device is disclosed for releasably fastening a mechanism in the region of a floor of an aircraft or spacecraft and includes a base component and a latch component. The latch component includes at least one holding portion including a latch-component-side holding face and is movably coupled to the base component between an unlocked and a locked position. When positioned in a predefined mounting position on the floor component and/or on the base component, the holding portion of the latch component engages a fastening portion, and the latch-component-side holding face faces the mechanism-side holding face. During passage of the latch component from locked position into unlocked position a gap between the latch-component-side holding face and the mechanism-side holding face continuously widens. The invention further relates to an arrangement for a cargo loading system.

Abstract: A fastening device is disclosed for releasably fastening a mechanism in the region of a floor of an aircraft or spacecraft and includes a base component and a latch component. The latch component includes at least one holding portion including a latch-component-side holding face and is movably coupled to the base component between an unlocked and a locked position. When positioned in a predefined mounting position on the floor component and/or on the base component, the holding portion of the latch component engages a fastening portion, and the latch-component-side holding face faces the mechanism-side holding face. During passage of the latch component from locked position into unlocked position a gap between the latch-component-side holding face and the mechanism-side holding face continuously widens. The invention further relates to an arrangement for a cargo loading system.

Abstract: A fastening device is disclosed for releasably fastening a mechanism in the region of a floor of an aircraft or spacecraft and includes a base component and a latch component. The latch component includes at least one holding portion including a latch-component-side holding face and is movably coupled to the base component between an unlocked and a locked position. When positioned in a predefined mounting position on the floor component and/or on the base component, the holding portion of the latch component engages a fastening portion, and the latch-component-side holding face faces the mechanism-side holding face. During passage of the latch component from locked position into unlocked position a gap between the latch-component-side holding face and the mechanism-side holding face continuously widens. The invention further relates to an arrangement for a cargo loading system.

Abstract: The present invention relates to a process for preparing hydromagnesite in an aqueous environment. The invention further relates to such hydromagnesite having a specific platy-like morphology in combination with a specific average particle size and to their use as minerals, fillers and pigments in the paper, paint, rubber and plastics industries and to the use as flame-retardant.

Abstract: An end stop device for restraining an ULD from movement across a cargo deck surface of an aircraft includes a main body; and a mounting interface connected to the main body which is configured and arranged to attach the end stop device to the cargo deck by means of a corresponding tie down ring. Each mounting interface includes a tongue-like support plate which is partially protruding below a bottom side of the main body, at least one recess arranged in an area above the support plate, wherein side walls of the recess form a frame-like structure. and a bolt portion extending from the support plate into the recess and partially surrounded by the frame-like structure. The bolt portion is configured to engage the tie down ring in an operation mode where the end stop device is fixed to a tie down ring.

Abstract: An end stop device for restraining an ULD from movement across a cargo deck surface of an aircraft includes a main body; and a mounting interface connected to the main body which is configured and arranged to attach the end stop device to the cargo deck by means of a corresponding tie down ring. Each mounting interface includes a tongue-like support plate which is partially protruding below a bottom side of the main body, at least one recess arranged in an area above the support plate, wherein side walls of the recess form a frame-like structure. and a bolt portion extending from the support plate into the recess and partially surrounded by the frame-like structure. The bolt portion is configured to engage the tie down ring in an operation mode where the end stop device is fixed to a tie down ring.

Abstract: A fastening device is disclosed for releasably fastening a mechanism in the region of a floor of an aircraft or spacecraft and includes a base component and a latch component. The latch component includes at least one holding portion including a latch-component-side holding face and is movably coupled to the base component between an unlocked and a locked position. When positioned in a predefined mounting position on the floor component and/or on the base component, the holding portion of the latch component engages a fastening portion, and the latch-component-side holding face faces the mechanism-side holding face. During passage of the latch component from locked position into unlocked position a gap between the latch-component-side holding face and the mechanism-side holding face continuously widens. The invention further relates to an arrangement for a cargo loading system.

Abstract: The present invention relates to a process for preparing hydromagnesite in an aqueous environment. The invention further relates to such hydromagnesite having a specific platy-like morphology in combination with a specific average particle size and to their use as minerals, fillers and pigments in the paper, paint, rubber and plastics industries and to the use as flame-retardant.

Abstract: The present invention relates to a process for preparing hydromagnesite in an aqueous environment. The invention further relates to such hydromagnesite having a specific platy-like morphology in combination with a specific average particle size and to their use as minerals, fillers and pigments in the paper, paint, rubber and plastics industries and to the use as flame-retardant.

Abstract: The present invention relates to a process for preparing hydromagnesite in an aqueous environment. The invention further relates to such hydromagnesite having a specific platy-like morphology in combination with a specific average particle size and to their use as minerals, fillers and pigments in the paper, paint, rubber and plastics industries and to the use as flame-retardant.