The present invention provides a life jacket case which can achieve weight reduction as well as seal the inside. Provided is a life jacket case for housing a life jacket, wherein a cover of an opening, through which the life jacket is taken in and out, is made of a first material which is hard enough to keep the shape of the cover, and a region other than or larger than the region made of the first material is made of a second material which is more lightweight than the first material. It is preferable that the life jacket case is fitted with a security tag which indicates whether or not the cover has been opened.

A method at a Unmanned Aerial Vehicle (UAV), and a UAV, adapted therefore, is adapted for enabling assisting in a rescue mission, where the method comprise: initiating a first localization of at least one body or object; initiating an analysis, for determining, at least partly based on the first localization of the at least one body or object, a need for activities, and initiating the determined activities, comprising applying floatable foam to an area on or in close proximity to the at least one body or object, while applying, to the floatable foam, a recognizable means capable of assisting in a second localization of the at least one body or object.

A method at a Unmanned Aerial Vehicle (UAV), and a UAV, adapted therefore, is adapted for enabling assisting in a rescue mission, where the method comprise: initiating a first localization of at least one body or object; initiating an analysis, for determining, at least partly based on the first localization of the at least one body or object, a need for activities, and initiating the determined activities, comprising applying floatable foam to an area on or in close proximity to the at least one body or object, while applying, to the floatable foam, a recognizable means capable of assisting in a second localization of the at least one body or object.

A stationary life-saving unit launcher. The stationary life-saving unit launcher includes: a base; a compressed gas tank mounted to an upper portion of the base and supplying compressed gas; a frame mounted above the base by being spaced apart by a predetermined distance therefrom; and a launch unit mounted to the frame and firing a life-saving unit by using the impact force of the compressed gas supplied from the compressed gas tank. The launch unit is capable of firing a projectile without a loading motion for firing the life-saving unit after the mounting thereof.

A stationary life-saving unit launcher. The stationary life-saving unit launcher includes: a base; a compressed gas tank mounted to an upper portion of the base and supplying compressed gas; a frame mounted above the base by being spaced apart by a predetermined distance therefrom; and a launch unit mounted to the frame and firing a life-saving unit by using the impact force of the compressed gas supplied from the compressed gas tank. The launch unit is capable of firing a projectile without a loading motion for firing the life-saving unit after the mounting thereof.

A marker and recovery device comprising: an enclosure adapted to be secured to a wearer; a bladder configured to fit within the enclosure in an uninflated state, the bladder comprising: an elongate tube; a first upper tube fluidly connected to the elongate tube at a first end of the elongate tube; and a second upper tube fluidly connected to the elongate tube at a second end of the elongate tube; and an inflation mechanism to inflate the bladder to extend the bladder from the uninflated state to a deployed state in which the first upper tube and second upper tube join to form a handle portion at the end of the elongate tube.

A marker and recovery device comprising: an enclosure adapted to be secured to a wearer; a bladder configured to fit within the enclosure in an uninflated state, the bladder comprising: an elongate tube; a first upper tube fluidly connected to the elongate tube at a first end of the elongate tube; and a second upper tube fluidly connected to the elongate tube at a second end of the elongate tube; and an inflation mechanism to inflate the bladder to extend the bladder from the uninflated state to a deployed state in which the first upper tube and second upper tube join to form a handle portion at the end of the elongate tube.

An inline for an inflatable assembly may comprise a first end defining a primary gas inlet and a second end defining a primary gas outlet. An internal surface may define a flow path extending from the primary gas inlet to the primary gas outlet. An orifice may be located between the first end and the second end. The orifice may be defined, at least partially, by a radial wall extending from the internal surface to the external surface. The orifice may be configured to entrain ambient air with a primary gas flowing from the primary gas inlet to the primary gas outlet.

An inline for an inflatable assembly may comprise a first end defining a primary gas inlet and a second end defining a primary gas outlet. An internal surface may define a flow path extending from the primary gas inlet to the primary gas outlet. An orifice may be located between the first end and the second end. The orifice may be defined, at least partially, by a radial wall extending from the internal surface to the external surface. The orifice may be configured to entrain ambient air with a primary gas flowing from the primary gas inlet to the primary gas outlet.

An evacuation system may comprise an evacuation slide configured to be deployed from an aircraft, first strap coupled to the evacuation slide, a second strap coupled to the evacuation slide, and a releasable restraint extending through the first strap and the second strap, the releasable restraint comprising a first stem connected to a first bead and a second stem connected to a second bead, where a diameter of the second stem is different from a diameter of the first stem.