| 摘要 |
An unmanned aircraft is provided to emit high temperature heat over 1000°C by burning the incompletely burned gas included in exhaust heat and to generate smoke by burning smoke liquid with the exhaust heat emitted from the turbine. An unmanned aircraft(1) comprises an aircraft body(10), a fuel storage(20) which is installed on one side of the aircraft body and in which fuel is stored, a smoke liquid storage(30) which is installed on the other side of the aircraft body and in which smoke liquid is stored, a turbine(40) which is installed on one side of the aircraft body and provides the power to rotate wings, a body(50) having one open end and a connection pipe connected to the exhaust chamber of the turbine, a smoke liquid injection pipe(60) which is formed on the upper side of the body and guides the smoke liquid to the body inside, and an oxidation catalyst mesh mounted on the open one end of the body.
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