Honeycomb elastic lining for aircraft shell

The invention relates to a honeycomb elastic lining for an aircraft shell, and can be applied to shell protection of aircrafts such as aircrafts spacecrafts, and satellites. In order to resist impact from foreign objects, such as birds, hail and space debris, a method that a layer of honeycomb elastic lining is additionally arranged on the inner side of the aircraft shell is adopted by a technique, namely a layer of concave honeycomb lining is arranged on the inner side of the aircraft shell; honeycomb chambers uniformly distributed are formed between the honeycomb lining and the aircraft shell; a dynamic protective layer is arranged at a top opening of each honeycomb chamber; the plane of the dynamic protective layer is approximately in parallel to and close to the aircraft shell; the shape size of the dynamic protective layer is basically matched with a top opening of the honeycomb chamber, but is slightly smaller than the top opening, so that the dynamic protective layer can make reciprocating movement in