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Magnetic levitation ducted fan for electric aircraft

A ducted fan and aircraft technology, applied in the field of aircraft electric propulsion devices, can solve problems such as low efficiency, high noise, and speed influence, and achieve high efficiency

Inactive Publication Date: 2021-04-30
AERO ENGINE ACAD OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, the existing aircraft propulsion device is mainly shafting structure transmission, and the traditional shafting structure power device mainly has the following defects: the traditional electric propulsion device is driven by the shafting system, and the rotational speed is affected by the structure; and the propulsion structure of the traditional shafting structure power device Connected with the shaft system, it will generate huge noise when rotating, causing sound pollution to the environment
The problems of traditional shafting structure power devices such as high noise, low efficiency, and small thrust can no longer meet the society's increasing demand for environmental protection and high efficiency. The research has reached its apex, and if a breakthrough is needed, it can only start from a brand new structure

Method used

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  • Magnetic levitation ducted fan for electric aircraft
  • Magnetic levitation ducted fan for electric aircraft
  • Magnetic levitation ducted fan for electric aircraft

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Embodiment Construction

[0033] The present disclosure will be further described in detail below with reference to the drawings and embodiments. It can be understood that the specific implementation manners described here are only used to explain relevant content, rather than to limit the present disclosure. It should also be noted that, for ease of description, only parts related to the present disclosure are shown in the drawings.

[0034] It should be noted that, in the case of no conflict, the implementation modes and the features in the implementation modes in the present disclosure can be combined with each other. The present disclosure will be described in detail below with reference to the drawings and embodiments.

[0035] like Figures 1 to 7 As shown, a magnetic levitation ducted fan for an electric aircraft includes:

[0036] The casing 100 has an accommodation space inside, and its two ends are hollowed out; the material selection of the casing requires low density and high strength, a...

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Abstract

The invention provides a magnetic levitation ducted fan for an electric aircraft, which comprises a shell, a stator, a first coil, a rotor fan and a permanent magnet, aiming at a high-rotating-speed low-noise electric propulsion mode adopted by an oil-electricity hybrid power aircraft, a magnetic levitation technology is adopted, a traditional shafting power system is decoupled in a shaftless manner, the traditional shafting structure limitation is eliminated, suspension rotation of the rotor fan is achieved through the mixed magnetic suspension bearing, and the low-noise environment-friendly requirement is met. The magnetic levitation ducted fan has higher efficiency, can generate greater thrust under the same power consumption, and realizes high speed, shaftless and environment-friendly effects of the electric propulsion device of the oil-electricity hybrid power aircraft.

Description

technical field [0001] The present disclosure relates to the technical field of aircraft electric propulsion devices, in particular to a magnetic levitation ducted fan for electric aircraft. Background technique [0002] At present, the existing aircraft propulsion device is mainly shafting structure transmission, and the traditional shafting structure power device mainly has the following defects: the traditional electric propulsion device is driven by the shafting system, and the rotational speed is affected by the structure; and the propulsion structure of the traditional shafting structure power device Connected with the shaft system, it will generate huge noise when rotating, causing sound pollution to the environment. The problems of traditional shafting structure power devices such as high noise, low efficiency, and small thrust can no longer meet the society's increasing demand for environmental protection and high efficiency. At the peak of research, if a breakthro...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C11/00B64D27/24F04D25/08F04D19/00F04D29/52F04D29/32F04D29/058
CPCB64C11/001B64D27/24F04D25/08F04D25/0606F04D19/002F04D29/522F04D29/325F04D29/058Y02T50/60
Inventor 姚轩宇蒋承志满运堃
Owner AERO ENGINE ACAD OF CHINA
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