Multi-rotor-wing oil-electricity hybrid power aircraft

A hybrid power and aircraft technology, applied in the field of flight, can solve problems such as aircraft constraints, and achieve the effects of large load capacity, low motor power, and strong endurance.

Inactive Publication Date: 2017-09-01
徐成
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The technical problem to be solved by the present invention is to provide a multi-rotor oil-electric hybrid air

Method used

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  • Multi-rotor-wing oil-electricity hybrid power aircraft
  • Multi-rotor-wing oil-electricity hybrid power aircraft

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Embodiment Construction

[0021] The following examples can enable those skilled in the art to understand the present invention more comprehensively, but the present invention is not limited to the scope of the described examples.

[0022] Such as Figure 1 to Figure 2 A kind of multi-rotor oil-electric hybrid aircraft shown, comprises rotor assembly 1, fuselage support 2, engine 3, drive motor 4, control box 5, battery box 6, fuel tank 7 and landing gear 8; Said rotor assembly 1 is vertically distributed and installed at both ends of the fuselage support 2 according to the direction of the rotor rotation axis, the control box 5, the battery box 6 and the fuel tank 7 are installed on the fuselage support 1, and the landing gear 8 is connected and installed on the fuselage support 2 below.

[0023] The rotor assembly 1 includes a pair of engine rotors 11 and two pairs of motor rotors 12; the engine rotor 11 is composed of the engine 3 and the rotors connected thereto, and the motor rotor 12 is composed...

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Abstract

The invention relates to a multi-rotor-wing oil-electricity hybrid power aircraft. The multi-rotor-wing oil-electricity hybrid power aircraft is characterized in that the aircraft comprises a rotor wing assembly, an aircraft body support, an engine, a driving motor, a control box, a battery box, an oil tank and an undercarriage; and the rotor wing assembly is vertically distributed and mounted at the two ends of the aircraft body support in the directions of rotor wing rotary shafts, the control box, the battery box and the oil tank are mounted on the aircraft body support, and the undercarriage is connected and mounted below the aircraft body support. Compared with a traditional oil drive multi-rotor-wing helicopter, in an oil drive multi-rotor-wing helicopter, a rotor wing orientation adjustment structure is omitted, so that the multi-rotor-wing oil-electricity hybrid power aircraft is greatly simplified in structure, convenient to maintain, low in failure rate and low in manufacturing cost; the multi-rotor-wing oil-electricity hybrid power aircraft is easy to achieve, the adjusting mode is simple in advancing, the structure is simple and reasonable, and components are easy to obtain; and a hybrid power aircraft driving system of the multi-rotor-wing oil-electricity hybrid power aircraft can achieve the remote navigation effect and the large load capacity and is applicable to serving as a driving system of the multi-rotor-wing helicopter.

Description

technical field [0001] The invention relates to the technical field of flight, in particular to a multi-rotor oil-electric hybrid aircraft. Background technique [0002] Multi-rotor aircraft is an aircraft with simple structure, flexible control and stable flight attitude. Generally, there are different types such as three-axis, four-axis, six-axis, and eight-axis. Thanks to the development of micro-electromechanical and sensor technologies in recent years, multi-rotor aircraft have been widely used in fields such as model aircraft and aerial photography platforms. The multi-rotor aircraft perceives the flight state through various sensors, and sends speed instructions to the rotor motor through the microprocessor to adjust different flight attitudes of the aircraft. [0003] There are currently two types of power source drives for multi-rotor helicopters. One is oil-powered multi-rotor helicopters. This type of helicopter uses a fuel engine to transmit power to each rotor...

Claims

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Application Information

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IPC IPC(8): B64D27/02
CPCB64D27/02B64D2027/026B64U50/11B64U10/10B64U50/19
Inventor 徐成
Owner 徐成
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