Abstract: The invention provides a drug mixing and injection system, in particular an adapter for said system enabling the preparation of drug formulations. In a first aspect, the invention relates to an adapter for a drug mixing and injection system comprising a first subunit (110) adapted to hold a vial (113) and a reservoir (115) with injectable liquid, a second subunit (120) comprising a valve (115) and an outlet port (122), at least one internal adapter channel (131), a first cannula (134) between the vial (113) and the internal adapter channel (131), wherein the adapter (100) has a resting position and an activated position. In another aspect, the invention relates to a drug mixing and injection system (200) comprising the adapter of the first aspect of the invention, a vial and a reservoir with injectable liquid.

Abstract: An airscrew for propelling an aircraft has a hub, a jacket and a plurality of propeller blades secured by blade necks to the hub. These blade necks are secured to the hub with symmetric or equal angular spacings around the hub between neighboring radial blade neck axes. Each propeller blade has a longitudinal axis. At least certain of these longitudinal blade axes extend at different sweep angles relative to the respective radial blade neck axis. When the sweep angle is positive the respective sweep of the blade is a positive sweepback with a trailing sweep of the respective blade relative to a rotational direction of the airscrew. When the sweep angle is negative the respective sweep of the blade is a negative sweep forward with a leading sweep of the respective blade relative to a rotational direction of the airscrew. These differing sweep angles achieve a substantial noise reduction compared to conventional airscrews having a completely symmetrical construction.

Abstract: In combination with a propeller disposed in an aircraft, aft from the nose portion of the craft, an improvement is provided for reducing noise, as well as mechanical load on the propeller blade, and includes a construction part situated upstream from the propeller and being exposed to the oncoming air flow prior to reaching the propeller, thus being an obstacle that has a particular contour in a plane transversely to an axis of rotation of the propeller, so that at least the rear edge, as seen in peripheral direction of rotation of the propeller, forms an angle that is not zero in relation to a leading edge of the propeller, when the propeller as a whole is in a horizontal disposition.

Abstract: The vehicle is constructed from a flat disc recessed in a slot in a thin, pencil-like fuselage having aft and front propulsion engines and mounted for rotating about the center of the disc and about an axis extending transversely to the disc and to the direction of extension of the fuselage.