Fixed wing type hybrid power motorplane

A hybrid, fixed-wing technology, applied in the fuel tank of the power unit, driven by multiple power units with a transmission, the type of power plant, etc., to reduce pollution, reduce flight costs, and meet performance indicators.

Inactive Publication Date: 2017-01-11
中电科芜湖通用航空产业技术研究院有限公司
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  • Description
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  • Application Information

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Problems solved by technology

However, the above-mentioned technical requirements cannot be met in the prior art.

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  • Fixed wing type hybrid power motorplane
  • Fixed wing type hybrid power motorplane

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Embodiment Construction

[0021] Below with reference to the accompanying drawings, through the description of the embodiments, the specific embodiments of the present invention, such as the shape, structure, mutual position and connection relationship between the various parts, the role and working principle of the various parts, etc., will be further described. Detailed instructions:

[0022] as attached figure 1 , attached figure 2 As shown, the present invention is a fixed-wing hybrid aircraft. The fixed-wing hybrid aircraft includes a fuselage 1 and a wing 2. A propeller 3 is installed on the fuselage 1, and the propeller 3 is connected with a drive motor 4 to drive The motor 4 is connected with the power battery 5, and the drive motor 4 is connected with the drive motor control part 6 capable of controlling the start and stop of the drive motor 4, the speed and the size of the torque. An engine 7 is also arranged in the fuselage 1, and the engine 7 is connected with the generator 8 to generate ...

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Abstract

The invention provides a fixed wing type hybrid power motorplane applied to the technical field of engine products. A propeller (3) is installed on a fuselage (1) of the fixed wing type hybrid power motorplane and is connected with a driving motor (4), and the driving motor (4) is connected with a power battery (5) and further connected with a driving motor control component (6) capable of controlling the driving motor (4). An engine (7) is further arranged in the fuselage (1) and is connected with a generator (8), the generator (8) is connected with the power battery (5) and connected with the driving motor control component (6) at the same time, and the engine (7) is connected with an engine control component (9) capable of controlling the engine (7). According to fixed wing type hybrid power motorplane, electric energy and fuel oil can be alternately used, various plane performance indexes can be effectively met, energy consumption can be reduced, flying cost can be reduced, and environmental pollution can be relieved.

Description

technical field [0001] The invention belongs to the technical field of aircraft products, and more specifically relates to a fixed-wing hybrid aircraft. Background technique [0002] With the increasingly serious energy crisis and environmental pollution, the development of new energy aircraft is an inevitable trend, and electricity as a clean energy is the first choice. Due to the constraints of battery technology, there is a need for a transitional solution, which results in a hybrid electric system solution. At present, gasoline-electric hybrid aircraft is basically still in a blank stage in China, and there is no actual promotion and application abroad, and it is basically in the research and development stage. The technical difficulty of this solution is mainly to replace the traditional powertrain composed of engines with an oil-electric hybrid power drive system, and it is required to meet various performance indicators of the aircraft. However, the above-mentioned ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D35/08B64D27/24B64D37/04
CPCB64D27/24B64D35/08B64D37/04Y02T50/60
Inventor 平丽浩曾锐李慧颖周义张会勤吴天睿
Owner 中电科芜湖通用航空产业技术研究院有限公司
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