An airplane emergency escape drone is shown and described. The airplane emergency escape drone includes a housing. The housing is made from a planar base, a plurality of sidewalk rising from the base, and a planar top secured to the top of the sidewalls. A door is located within one of the plurality of sidewalk. A motor is secured to the exterior of the planar top. A propeller is rotatably secured to the motor. A plurality of feet is secured to the exterior of the planar base.

An airplane emergency escape drone is shown and described. The airplane emergency escape drone includes a housing. The housing is made from a planar base, a plurality of sidewalk rising from the base, and a planar top secured to the top of the sidewalls. A door is located within one of the plurality of sidewalk. A motor is secured to the exterior of the planar top. A propeller is rotatably secured to the motor. A plurality of feet is secured to the exterior of the planar base.

An evacuation system may comprise a packboard, an evacuation slide configured to deploy from the packboard, and a lane dividing apparatus attached to the evacuation slide, the lane dividing apparatus comprising a strap having flexible material. The lane dividing apparatus may be a dual wall lane divider. The lane dividing apparatus may be a single lane dividing apparatus. The lane dividing apparatus may comprise a first patch disposed at a proximal end of the evacuation slide and a second patch disposed at a second end distal to the proximal end. The lane dividing apparatus may extend from the proximal end to the second end. The lane dividing apparatus may be taut upon deployment of the evacuation slide.

An evacuation system may comprise a packboard, an evacuation slide configured to deploy from the packboard, and a lane dividing apparatus attached to the evacuation slide, the lane dividing apparatus comprising a strap having flexible material. The lane dividing apparatus may be a dual wall lane divider. The lane dividing apparatus may be a single lane dividing apparatus. The lane dividing apparatus may comprise a first patch disposed at a proximal end of the evacuation slide and a second patch disposed at a second end distal to the proximal end. The lane dividing apparatus may extend from the proximal end to the second end. The lane dividing apparatus may be taut upon deployment of the evacuation slide.

A protective system to make drones and unmanned aerial vehicles retrievable in an event of a crash. The protective system also reduces damage from impact during a crash. The protective system will deploy automatically or manually in an event of a crash to reduce the physical impact and provide floatation on the surface of a water body. Several onboard location indicating devices for indicating the location of crashed drone or unmanned aerial vehicle are also part of the protective system.

A protective system to make drones and unmanned aerial vehicles retrievable in an event of a crash. The protective system also reduces damage from impact during a crash. The protective system will deploy automatically or manually in an event of a crash to reduce the physical impact and provide floatation on the surface of a water body. Several onboard location indicating devices for indicating the location of crashed drone or unmanned aerial vehicle are also part of the protective system.

An evacuation system may comprise a first plurality of tubes configured to inflate by an aspirator and pressure cylinder upon deployment from an aircraft. The evacuation system may further comprise a second plurality of tubes coupled to the first plurality of tubes. The second plurality of tubes may be configured to be in deflated state when the evacuation system is in a slide configuration. The second plurality of tubes may be configured to be in an inflated state when the evacuation system is in a raft configuration.

An evacuation system may comprise a first plurality of tubes configured to inflate by an aspirator and pressure cylinder upon deployment from an aircraft. The evacuation system may further comprise a second plurality of tubes coupled to the first plurality of tubes. The second plurality of tubes may be configured to be in deflated state when the evacuation system is in a slide configuration. The second plurality of tubes may be configured to be in an inflated state when the evacuation system is in a raft configuration.

An evacuation system may comprise an inflatable slide, a raft compartment, and an evacuation raft. The evacuation raft may be disposed within the raft compartment. The evacuation raft may be configured to deploy in response to a water landing of an aircraft.

An evacuation system may comprise an inflatable slide, a raft compartment, and an evacuation raft. The evacuation raft may be disposed within the raft compartment. The evacuation raft may be configured to deploy in response to a water landing of an aircraft.