Title:
AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2023/142769
Kind Code:
A1
Abstract:
An aircraft, comprising a housing, wherein an inner cavity is formed in the housing, a driving mechanism (3) and a control unit (4) are provided in the inner cavity, and a camera assembly (2) is provided in the housing; an air inlet (215) is provided on the camera assembly (2), a first air outlet (121) is provided on the housing, and an airflow enters the inner cavity from the air inlet (215), flows through the driving mechanism (3) to the control unit (4), and then is discharged from the first air outlet (121). In the flight process of the aircraft, the inner cavity can form a heat dissipation airflow, and the airflow enters the inner cavity from the air inlet (215), flows through the driving mechanism (3) to the control unit (4), and then is discharged from the first air outlet (121), which facilitates heat dissipation of internal elements of the aircraft and discharge of hot airflow in the inner cavity, especially the heat dissipation speed of the driving mechanism and the control unit is accelerated, the heat dissipation effect is improved, the possibility of damaging the internal elements of the aircraft due to overheating is reduced, and the service life of the aircraft is prolonged.
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Inventors:
LI ZHIGUO (CN)
DAI YIN (CN)
WANG YANWEI (CN)
DAI YIN (CN)
WANG YANWEI (CN)
Application Number:
PCT/CN2022/139735
Publication Date:
August 03, 2023
Filing Date:
December 16, 2022
Export Citation:
Assignee:
HANWANG TECH CO LTD (CN)
International Classes:
B64D47/08; B64C1/06; H05K7/20
Foreign References:
| CN217100494U | 2022-08-02 | |||
| CN217100445U | 2022-08-02 | |||
| CN217456362U | 2022-09-20 | |||
| CN211442748U | 2020-09-08 | |||
| CN209994469U | 2020-01-24 | |||
| CN113443156A | 2021-09-28 | |||
| US20110249386A1 | 2011-10-13 | |||
| CN215188002U | 2021-12-14 |
Attorney, Agent or Firm:
BEIJING MIZAR STAR INTELLECTUAL PROPERTY AGENCY CO., LTD. (CN)
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