Multi-rotor aircraft elevating turnover device and carrying and elevating device thereof

The technology of a multi-rotor aircraft and a turning device is applied in the field of aircraft, which can solve the problems of cumbersome loading process, high damage rate of aircraft, and easy crushing of aircraft, etc., and achieves the effect of improving efficiency, simple structure and improving lifting effect.

CN107336655AInactive Publication Date: 2017-11-10成都鑫晨航空科技有限公司
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Publication Date
2017-11-10
Estimated Expiration
Not applicable · inactive patent

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Abstract

The invention discloses a multi-rotor aircraft elevating turnover device and a carrying and elevating device thereof, and belongs to the technical field of aircrafts. According to the multi-rotor aircraft elevating turnover device and the carrying and elevating device thereof, the elevating efficiency is higher, the aircraft finished product elevating and turnover efficiency is improved, and therefore the aircraft finished product truck loading efficiency is improved. The elevating turnover device comprises a rail and a guide part; a rotating assembly and a rotating drive assembly are connected to the rail, a rotating rod is connected to the rotating assembly, a connecting rod is hinged to the end of the rotating rod, a first elevating rod is hinged to the other end of the connecting rod, one end of the first elevating rod is in fit connection with the guide part, the first elevating rod can move on the guide part along the track of the guide part, and a turnover plate is connected to the first elevating rod. The carrying and elevating device comprises a compartment, the elevating turnover device and a containing mechanism; the elevating turnover device is adopted, and the multi-rotor aircraft elevating turnover device and the carrying and elevating device thereof are suitable for storing and transporting multi-rotor aircrafts.
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Description

technical field

[0001] The invention belongs to the technical field of aircraft, relates to a multi-rotor aircraft, in particular to the transportation of the multi-rotor aircraft. Background technique

[0002] In recent years, multi-rotor aircraft has broad application prospects in military and civilian fields due to its low cost, high cost-effectiveness ratio, no risk of casualties, and the ability to enter many unreachable areas, such as low-altitude reconnaissance, meteorological survey, Aerial photography, traffic patrol, etc. With the needs of the development of the industry, many professional multi-axis and long-wheelbase multi-rotor aircraft have appeared on the market. The long-wheelbase multi-axis multi-rotor aircraft meets the needs of many customers. Due to the long wheelbase and the large size of the aircraft, the packaging size is also large and the weight is heavy.

[0003] However, during the transportation of the aircraft, the first problem is to load the ...

Examples

Embodiment 1

[0026]A lifting and flipping device for a multi-rotor aircraft includes rails 1 installed on a compartment 8, two groups of rails 1 are arranged, and two groups of rails 1 are arranged side by side along the length direction of the compartment 8 at a certain distance in parallel. Also be provided with guide piece on track 1, can guide some parts by guide piece. The guide member may be a groove provided on the side of the guide rail 67, and some parts are located in the groove, so as to realize movement along the track direction of the groove. This track 1 becomes L-shaped structure, and one side of this L-shaped track 1 is connected on the top surface of compartment 8, and the other side of this L-shaped track 1 is positioned on compartment 8 side, and is connected with compartment 8 side. A rotary assembly 2 is arranged between the L-shaped rails 1 on the top surface of the compartment 8, and a rotary drive assembly 3 is provided on the top surface of the compartment 8 or the...

Embodiment 2

[0028] On the basis of Embodiment 1, the other end of the first lifting rod 5 is also hinged with a second lifting rod, which is an L-shaped second lifting rod, and the end of the long side of the second lifting rod is connected to The end of the long side of the first lifting rod 5 is hinged, and the end of the short side of the second lifting rod is connected with the guide and can move along the track of the guide on the guide. And under the action of the second lifting rod, the turning angle of the first lifting rod 5 can be prevented from being too large.

Embodiment 3

[0030] A multi-rotor aircraft handling and lifting device includes a compartment 8 for storing and transporting finished aircraft products 10 . A lifting and turning device 9 is connected to the compartment 8, and the lifting and turning device 9 is mainly used for turning. The lifting and turning device 9 can be arranged corresponding to each compartment 8, that is, the lifting and turning device 9 is fixedly connected to the car body of the compartment 8; of course, the compartment 8 can also be reused with multiple compartments 8, that is, the lifting and turning device 9 is detachable Ground is connected on the car body of compartment 8. An accommodating mechanism is provided on the lifting and turning device 9, and the accommodating mechanism is mainly used for placing the finished aircraft 10 and effectively preventing the finished aircraft 10 from being crushed.

[0031] Lifting and flipping device comprises track 1 installed on the compartment 8, two groups of tracks ...