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Auxiliary propulsion device for aircraft

A technology for auxiliary propulsion and aircraft, which is applied in the direction of aircraft, auxiliary power equipment, aircraft power plant, etc., and can solve the problems of increasing the weight of components and fuselage resistance, reducing the amount of passenger space and aircraft resistance, etc.

Pending Publication Date: 2022-06-28
HYUNDAI MOTOR CO LTD +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, there are disadvantages of increasing the weight and airframe drag of components mounted on the aircraft and reducing the amount of space for passengers and aircraft drag

Method used

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  • Auxiliary propulsion device for aircraft
  • Auxiliary propulsion device for aircraft
  • Auxiliary propulsion device for aircraft

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Embodiment Construction

[0030] Reference will now be made in detail to various embodiments of the present invention, examples of which are illustrated in the accompanying drawings and described below. While the invention will be described in conjunction with exemplary embodiments of the invention, it should be understood that this description is not intended to limit the invention to these exemplary embodiments. On the other hand, the invention is intended to cover not only the exemplary embodiments of the invention, but also various alternatives, modifications, equivalents, and other embodiments included within the spirit and scope of the invention as defined by the appended claims .

[0031] The specific structural and functional descriptions of the embodiments of the invention disclosed herein are for purposes of illustration only of exemplary embodiments of the invention. The present invention may encompass various forms without departing from the essential or distinctive characteristics of the ...

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PUM

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Abstract

An auxiliary propulsion device for an aircraft may include an engine mounted in a fuselage of the aircraft; a generator configured to be driven using power from the engine; a compressor configured to be driven by the engine or the generator; a battery configured to store power generated by the generator; a power distributor connected to the generator, the battery, and the main propulsion device and configured to distribute power generated by the generator to the battery and the main propulsion device; and at least one nozzle device configured to inject the high-pressure gas supplied from the compressor to the outside of the machine body.

Description

technical field [0001] The present invention relates to an auxiliary propulsion device applicable to an aircraft, such as urban air mobility (UAM). Background technique [0002] In the event of a malfunction of the aircraft, safety can be greatly improved when an air vehicle, such as a UAM, is provided with auxiliary propulsion means capable of providing the aircraft with independent or auxiliary thrust. However, there are disadvantages of increasing the weight and airframe drag of components mounted on the aircraft and reducing the amount of space for passengers and aircraft drag. [0003] The information disclosed in this Background section of the invention is only for enhancement of understanding of the overall background of the invention and should not be taken as forming an acknowledgement or any suggestion that this information already is already known to a person skilled in the art. SUMMARY OF THE INVENTION [0004] Aspects of the present invention are directed to ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D27/16B64D41/00B64D45/04
CPCB64D27/16B64D41/00B64D45/04F16D2500/5114F16D2500/306F16D2500/70424F16D21/00F16D48/10F16D48/06B64C15/14B64C29/0016B64D31/09B64D27/34B64D31/18B64D35/025B64D27/24B64C29/0091B05B1/30B64D2221/00Y02T50/60Y02T50/50B64D31/06F16D21/02B64D35/024
Inventor 郑遇锡金贵泽全伦哲赵现起
Owner HYUNDAI MOTOR CO LTD