Vibration reduction mechanism and flight equipment

The embodiment of the utility model discloses a vibration reduction mechanism and flight equipment. The vibration reduction mechanism comprises a containing unit, a mandrel and a first vibration reduction part. The interior of the containing unit is hollow to form a containing chamber, the first vibration reduction part and at least part of the mandrel are arranged in the containing chamber, the mandrel and the first vibration reduction part are sequentially arranged in the vertical direction, and the mandrel is fixedly connected with the first vibration reduction part; wherein the first vibration reduction part is made of a rubber element, the first vibration reduction part is provided with a corner angle, at least two first vibration reduction grooves are formed in the corner angle of the first vibration reduction part, and a vibration reduction space is formed between each first vibration reduction groove and the containing unit. According to the damping device, it is guaranteed that deformation spaces are