An evacuation slide for an aircraft may be deployable in a slide mode and a raft mode. The evacuation slide includes a head end and a toe end, with the head end having a mounting feature and the toe end being longitudinally opposite the head end. In response to the evacuation slide being in the slide mode, the head end of the evacuation slide is mounted to the aircraft via the mounting feature. In response to the evacuation slide being in the raft mode, the evacuation slide is detached from the aircraft and the mounting feature is a boarding aid, according to various embodiments.

An evacuation system (10) includes an electrically insulating inflatable conveyance (11), which is stowed within, and deployed from, a framework (21) attached to an interior structure (45) or exterior structure (43) of an industrial vehicle (38). The inflatable conveyance (11) preferably has a flexible base (12) affixed to, and dependently supported by, longitudinally disposed closed tubular members (15), and may take the form of a chute that may be configured to function as a slide or as a ladder. The chute may be enclosed with a canopy (17), or may be open but provided with upwardly extending side walls (16). In implementations of a canopy (17), transparent egress windows (19) may be provided. Transversely oriented straps (14) form safety steps and/or hand rails in a “ladder” configuration of the chute.

A power source for inflation systems. Specific embodiments relate to inflation systems that use an electrically-powered inflation system, wherein the power source of the inflation system is a solid state battery. Particular embodiments may find use in connection with inflating evacuation slides or life rafts on board a passenger transportation vehicle, such as an aircraft or marine vessel. Other embodiments may be used for inflating shelters, life vests, or any other inflatable safety device that requires a rapid inflation.

A combination adaptive energy absorption and emergency flotation device for positioning beneath a plurality of seat pans of a seat assembly in an aircraft seating application. The device includes a plurality of fluidly coupled inflatable elastic bladders, at least one constrictor valve fluidly coupling at least two adjacent ones of the plurality of inflatable elastic bladders allowing fluid flow therethrough in response to predetermined pressure on the device from the plurality of seat pans, and a fluid supply source fluidly coupled to the plurality of inflatable elastic bladders for outputting a positive flow of fluid to the plurality of inflatable elastic bladders, wherein the adaptive energy absorption device is detached from the plurality of seat pans to allow removal from beneath the plurality of seat pans for use as an emergency flotation device.

An escape system comprises a passage (1), a platform (3) and at least one craft (4), the platform (3) and the craft (4) being deployable from a structure (2) to water to facilitate evacuation of the structure via the passage. The passage is mounted to the platform such that the platform is urged towards the structure when deployed. The passage may be mounted to the platform such that movement of the passage relative to the platform is restricted in at least one direction. A plate (64) may support the passage, platform and/or craft during deployment, and/or stabilises the passage, platform and/or craft after deployment in the water.

A travel case includes a case body defining an interior cavity in which to carry articles and an exterior shell; an inflatable floatation aid fixed to the exterior shell; an inflator in communication with the inflatable floatation aid, for inflation of the inflatable floatation aid; and a locator beacon fixed to the exterior shell, including a communications transmitter capable of signaling a remote party and a geo-locating apparatus.

A device comprises a spring and a sleeve. The spring is configured to form a closed loop. The spring is moveable between a coiled configuration when the spring is collapsed and an uncoiled configuration when the spring is expanded. The spring defines a circumference while in the uncoiled configuration. The spring is disposed within the sleeve.

The conformable pressure vessel having: a plurality of individual pressure vessels, the individual pressure vessels each having an outer wall enclosing an inner volume. The inner volumes are fluidly connected to each other. The individual pressures vessels are oriented parallel to each other.

A personal flotation device capable of providing buoyancy and preventing hypothermia and death caused by loss of body heat by supporting the individual's entire body out of the water. Special design features increase the ease of use to ensure successful deployment and boarding, even among injured, weak, and/or physically exhausted individuals. This personal flotation device is small and compact, so that it may be used in a prophylactic manner from low-risk to high-risk applications.

This application relates to inflatable flotation devices that support an infant, and having first, second and third inflatable members. The first member has an outer and an inner perimeter and a first and second diameters at first and second end portions. The second member is at least partially within the inner perimeter of the first member. At least a portion of the upper surface of the second member is recessed with respect to an upper surface of the first member. The third member has an inner perimeter disposed about at least a portion of the outer perimeter of the first member. The third member has a maximum height, when inflated, that is less than the maximum height of the first member, at least a portion of the inner perimeter of the third member being spaced apart from the outer perimeter of the first member.