Abstract: The invention relates to a winding, particularly a winch, arrangement (100) comprising a two speed manually operable winding member (10) and a drive unit (20) comprising a motor (21). The drive unit (20) comprises a transmission arrangement connected to a motor shaft (25), an outgoing shaft (22) with an outer gear wheel (23). The transmission arrangement is adapted to allow the outgoing shaft gear wheel (23) rotate in the same direction but at different speeds depending on rotational direction of the motor (21). The manual winch (10) is adapted for reception of the outgoing shaft (22) allowing the winch drum (1) to be motor (21) driven. The drive unit (20) comprises means (67,68) allowing engagement/disengagement of the outgoing shaft gear wheel (23) from the manually operable winding member (10) and the winding arrangement can be used as a two-speed manual or a two speed motor driven winding arrangement.

Abstract: A breech for noise reduction in a recoil-less weapon is described. The breech is adapted to be arranged in fluid communication with a launcher of the weapon to release exhaust gas. The breech comprises a venturi tube. The venturi tube has an inlet at a first end adapted to be connected to the launcher, and an outlet for releasing the exhaust gas at a second end, wherein the area of the outlet is larger than the area of the inlet. The venturi tube further comprises an exhaust gas controlling element formed at the venturi tube structure. The exhaust gas controlling element is arranged to control the release of exhaust gas so as to decrease a sound pressure peak at the weapon. The inner envelope surface of the venturi tube is configured, such that the inner envelope surface does not alter or at least has a very small influence on recoil characteristics of the weapon.

Abstract: The invention relates to a method for launching a projectile and a launcher comprising a barrel (1) accommodating a. a projectile (2); b. a rocket motor (13) at the rear end of the projectile (2) comprising a first compartment containing a first propellant; c. a countermass (3) at the rear end of the barrel (1); and d. a second compartment between the rocket motor (13) and the countermass (3) containing a second propellant, wherein said first and second compartments form a high pressure chamber (6) subsequent to firing of the projectile (2).

Abstract: A breech for noise reduction in a recoil-less weapon is described. The breech is adapted to be arranged in fluid communication with a launcher of the weapon to release exhaust gas. The breech comprises a venturi tube. The venturi tube has an inlet at a first end adapted to be connected to the launcher, and an outlet for releasing the exhaust gas at a second end, wherein the area of the outlet is larger than the area of the inlet. The venturi tube further comprises an exhaust gas controlling element formed at the venturi tube structure. The exhaust gas controlling element is arranged to control the release of exhaust gas so as to decrease a sound pressure peak at the weapon. The inner envelope surface of the venturi tube is configured, such that the inner envelope surface does not alter or at least has a very small influence on recoil characteristics of the weapon.

Abstract: The invention relates to a method for launching a projectile and a launcher comprising a barrel (1) accommodating a. a projectile (2); b. a rocket motor (13) at the rear end of the projectile (2) comprising a first compartment containing a first propellant; c. a countermass (3) at the rear end of the barrel (1); and d. a second compartment between the rocket motor (13) and the countermass (3) containing a second propellant, wherein said first and second compartments form a high pressure chamber (6) subsequent to firing of the projectile (2).

Abstract: The invention relates to a device (10) at a cleat (1) for a sailing boat in order to provide detachable locking of the line (3) to a sail, a rig or the like, where the line (3) runs over a sheave (2) on an elevated level and having cleat (1) for locking the line (3) situated at a distance from the deck of the boat. According to the invention, the line (3) is arranged to run over a sheave (2), which is provided with ratchet back stop (5). The line (3) is in that connection arranged to directly co-operate with a movably actuatable mechanism (14), which is arranged to activate the ratchet back stop (5).

Abstract: The invention relates to a device (10) at a cleat (1) for a sailing boat in order to provide detachable locking of the line (3) to a sail, a rig or the like, where the line (3) runs over a sheave (2) on an elevated level and having cleat (1) for locking the line (3) situated at a distance from the deck of the boat. According to the invention, the line (3) is arranged to run over a sheave (2), which is provided with ratchet back stop (5). The line (3) is in that connection arranged to directly co-operate with a movably actuatable mechanism (14), which is arranged to activate the ratchet back stop (5).

Abstract: An arrangement for a sail for sailing boats to connect the sail to a mast (4) on the sailing boat by means of a number of mast track slides (6) distributed along one edge of the sail, which are so arranged as to be connected by means of rolling devices to a track extending along the mast. The rolling devices are accommodated jointly in a channel-shaped track (9) integrated with the mast (4), with the edges (18,19;21,28;22,29) of which the aforementioned rolling devices are so arranged as to interact. A channel-shaped opening (16) extends along the aforementioned track (9) to permit the track slides (6) to extend out from the aforementioned track (9) with a narrower part for attachment to the sail with a broader part.

Abstract: The invention relates to an arrangement for the detachable locking of a line (2) which is led out through an opening in, for example, a mast (55) on a sailing boat (6) in question and for enabling the line (2) to be led further to an existing winch on board. In accordance with the invention, a tension release device (1A) and a ferrule (1B) for the line (2) are formed by a common component. Each part of this common component (1) can be situated to either side (A and B respectively) of the wall (12) in the mast (5) and or a cockpit, through which a lead-in (11) for the line (2) extends.