The disclosure relates to an unmanned aerial vehicle that is characterized in that the unmanned aerial vehicle comprises a
machine shell, a cabin is defined by the
machine shell, the cabin is provided with a closed sub-chamber, a first ventilation opening and a second ventilation opening which communicate with the sub-chamber are formed in the
machine shell, and a first cabin air opening and a second cabin air opening which communicate with the space outside the sub-chamber in the cabin are formed in the machine shell; besides, the unmanned aerial vehicle includes a first
electronic component disposed in the cabin, a first heat dissipation
assembly, and a second heat dissipation
assembly; the first heat dissipation
assembly comprises a heat dissipation structure and a first heat dissipation fan which are arranged in the sub-chamber, the heat dissipation structure is used for exchanging heat with the first
electronic component, the first heat dissipation fan is used for enabling an
airflow flowing through the heat dissipation structure to be generated in the sub-chamber, and the
airflow enters from one of the first ventilation opening and the second ventilation opening and flows out from the other one; and the second heat dissipation assembly comprises a second heat dissipation fan arranged at the air opening of the first cabin, and the second heat dissipation fan is used for enabling the space outside the sub-chamber in the cabin to generate
airflow.