Abstract: Board game (1) with a board (2) having at least one playing surface (3) comprising multiple playing fields (4) and with playing pieces (5) and at least one holding device (6) for holding a playing piece (5) releasably attached to the playing field (4), with the board (2) being arranged such that the orientation of the playing surface (3) deviates from a horizontal orientation, wherein a rotating device (7) is provided for holding the playing piece (5) in a same vertical orientation for any rotation of the board (2) about an imaginary axis (A) substantially orthogonally to the playing surface (3).

Abstract: Board game (1) with a board (2) having at least one playing surface (3) comprising multiple playing fields (4) and with playing pieces (5) and at least one holding device (6) for holding a playing piece (5) releasably attached to the playing field (4), with the board (2) being arranged such that the orientation of the playing surface (3) deviates from a horizontal orientation, wherein a rotating device (7) is provided for holding the playing piece (5) in a same vertical orientation for any rotation of the board (2) about an imaginary axis (A) substantially orthogonally to the playing surface (3).

Abstract: A method of producing a composite panel member, especially a composite panel member having a foam core sandwich structure for an airframe of an aircraft or spacecraft, including: providing at least one fiber reinforcement layer in a panel molding tool; moving or transferring the molding tool to an infusion station that is pre-heated to an infusion temperature and infusing the fiber reinforcement layer in the molding tool with a polymer resin; moving or transferring the molding tool to a curing station that is pre-heated to a curing temperature and curing the at least one resin-infused fiber reinforcement layer in the molding tool to form a composite panel member; and moving or transferring the molding tool to a cooling station that is provided at a cooling temperature and cooling the composite panel member in the molding tool.

Abstract: A method of producing a composite panel member, especially a composite panel member having a foam core sandwich structure for an airframe of an aircraft or spacecraft, including: providing at least one fiber reinforcement layer in a panel molding tool; moving or transferring the molding tool to an infusion station that is pre-heated to an infusion temperature and infusing the fiber reinforcement layer in the molding tool with a polymer resin; moving or transferring the molding tool to a curing station that is pre-heated to a curing temperature and curing the at least one resin-infused fiber reinforcement layer in the molding tool to form a composite panel member; and moving or transferring the molding tool to a cooling station that is provided at a cooling temperature and cooling the composite panel member in the molding tool.