摘要 |
The present invention provides an aircraft housing and an aircraft with the same. The aircraft housing includes an upper housing and a lower housing. The upper and lower housings are connected through ultrasonic welding or gluing. The aircraft housing has a cavity therein which is communicated with at least one opening of the lower housing. A power system is located within the cavity through the opening. In the present invention, the upper and lower housings of the aircraft are connected through ultrasonic welding, and the aircraft is formed by one step and is high in good product rate. Meanwhile, the aircraft housing is processed through welding, so that the upper and lower housing are in seamless connection with each other, the contact surface suffers from stress, and the strength is substantially increased. |