US 12,202,633 B2
Heat dissipation structure, heat dissipation method and device, aerial vehicle, and readable storage medium
Zhiwei Cai, Shenzhen (CN); and Yawen Zhang, Shenzhen (CN)
Assigned to SZ DJI TECHNOLOGY CO., LTD., Shenzhen (CN)
Filed by SZ DJI TECHNOLOGY CO., LTD., Shenzhen (CN)
Filed on Nov. 20, 2023, as Appl. No. 18/514,744.
Application 18/514,744 is a continuation of application No. 16/931,251, filed on Jul. 16, 2020, granted, now 11,820,496.
Application 16/931,251 is a continuation of application No. PCT/CN2018/073510, filed on Jan. 19, 2018.
Prior Publication US 2024/0083571 A1, Mar. 14, 2024
This patent is subject to a terminal disclaimer.
Int. Cl. B64U 30/20 (2023.01); B64U 10/14 (2023.01); B64U 20/87 (2023.01); B64U 50/19 (2023.01); B64U 70/90 (2023.01); B64U 101/30 (2023.01)
CPC B64U 30/20 (2023.01) [B64U 10/14 (2023.01); B64U 20/87 (2023.01); B64U 50/19 (2023.01); B64U 70/90 (2023.01); B64U 2101/30 (2023.01)] 20 Claims
OG exemplary drawing
 
1. A heat dissipation structure comprising:
a housing configured to accommodate a heating element of an aerial vehicle, the housing including:
a first air vent configured to guide an airflow into the housing, the airflow including a propeller-generated airflow generated by a propeller of the aerial vehicle during rotation;
a second air vent configured to guide the airflow out of the housing;
wherein:
the housing is located at an end of an arm of the aerial vehicle, away from the propeller in a longitudinal direction of the arm; and
a projection of the housing on a plane on which an area of rotation of the propeller lies at least partially overlaps the area of rotation of the propeller.