Multi-rotor unmanned aerial vehicle emergency parachuting device with adaptive ejection angle adjustment function and method
A multi-rotor UAV and self-adaptive adjustment technology, applied in the field of agricultural UAV research, can solve problems such as crashes, bombings, and reducing the success rate of UAV self-rescue.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Publication Date
- 2017-06-23
Smart Images

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Abstract
Description
technical field
[0001] The invention relates to a UAV parachute device and method, in particular to a multi-rotor UAV emergency parachute device and method for adaptively adjusting the ejection angle, and belongs to the field of agricultural UAV research. Background technique
[0002] Multi-rotor UAV is a special unmanned helicopter with three or more rotor shafts. It is a hot spot in the field of aviation research. There are a lot of demands in practical applications, such as: reconnaissance and rescue missions, scientific data collection , geological and forestry exploration, agricultural pest control, video surveillance, film and television production, etc. Using unmanned aerial vehicles to complete the above tasks can greatly reduce costs and improve personnel safety. Therefore, unmanned aerial vehicles have developed rapidly in military, civilian, and especially agricultural fields in recent years. However, at present, various unexpected risks are prone to occur due t...
Examples
Embodiment 1
[0042] Such as figure 1 As shown, the present embodiment provides a multi-rotor unmanned aerial vehicle emergency parachute device, which device includes an umbrella compartment 1, an umbrella compartment cover 2, a parachute 3, a parachute throwing spring 4, a lock bolt 5, an unlocking steering gear 6, a micro Controller 7, inertial motion measurement unit 8 and spring support rotation device.
[0043] There are two locking bolts 5 and two unlocking steering gears 6 respectively, and the two unlocking steering gears 6 are respectively fixed on the side walls of the umbrella compartment 1. The two locking bolts 5 are respectively located above the two unlocking steering gears 6, and respectively The two unlocking steering gears 6 are connected, and the umbrella cover 2 is fixed on the umbrella housing 1 under the joint action of the lock bolt 5 and the unlocking steering gear 6, and the umbrella housing 1 is fixed on the multi-rotor UAV.
[0044] Described parachute 3, parachut...