RELEASE SYSTEM, AIRCRAFT EVACUATION SLIP ASSEMBLY, AND METHOD FOR POSITIONING AN AIRCRAFT EVACUATION SLIP.

摘要

It is a release system for an aircraft evacuation slide assembly that includes a fluid manifold, a first actuator, and a second actuator. In various embodiments, a fluid is configured to flow inwards and pressurize the fluid delivery piping from a fluid source in response to an evacuation event. In various embodiments, the first actuator is fluidly coupled to the fluid distribution piping, wherein the first actuator is configured to release a blast panel from the fluid response evacuation slide assembly by pressurizing the fluid distribution piping. In various embodiments, the second actuator is fluidly coupled to the fluid delivery tubing, wherein the second actuator is configured to release a soft cover of the fluid response evacuation slide assembly by pressurizing the fluid distribution tubing.