Silencer for heavy fixed-wing unmanned aerial vehicle

A muffler and fixed-wing technology, which is applied in the field of UAV muffler design, can solve the problems of low structural space utilization efficiency and large volume, and achieve the effects of lightweight design, high space utilization, and reduced power impact

Pending Publication Date: 2021-03-26
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] In order to avoid the deficiencies in the prior art and to overcome the problems of relatively large volume and low structural space utilization efficiency of the mufflers of small and medium-sized drones, the present invention proposes a muffler for heavy-duty fixed-wing unmanned aerial vehicles; the muffler Through the coiled structure, resistive noise reduction is designed on the upper and lower end surfaces of the muffler, and the resistance noise reduction is involved in the pipeline, so that the airflow can flow in the unobstructed pipeline, and at the same time realize the resistive noise reduction, so as to reduce the airflow resistance. The dynamic impact of small displacement engines; the muffler has the characteristics of simple structure, light weight, smaller airflow resistance and higher space utilization

Method used

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  • Silencer for heavy fixed-wing unmanned aerial vehicle
  • Silencer for heavy fixed-wing unmanned aerial vehicle

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Embodiment Construction

[0022] This embodiment is a muffler for heavy-duty fixed-wing drones.

[0023] This embodiment is aimed at the muffler design requirement of small-sized piston engine:

[0024] ① Due to the relatively small exhaust pressure of low-power internal combustion engines, the contradiction between noise attenuation and airflow resistance is more prominent.

[0025] ②The requirements for shape space are far greater than those for ordinary internal combustion engines.

[0026] ③The sensitivity to weight is much higher than that of ordinary muffler design.

[0027] refer to figure 1 , figure 2 , the present embodiment is used for the muffler of the heavy-duty fixed-wing unmanned aerial vehicle, consists of an upper casing 1, an upper resistive sound-absorbing material plate 2, an upper exhaust flow channel 3, a lower exhaust flow channel 4, and a lower resistive sound-absorbing material plate 5. The lower shell 6 and the muffler body 8 are composed; among them, the muffler body 8 a...

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Abstract

The invention discloses a silencer for a heavy fixed-wing unmanned aerial vehicle. The silencer is composed of a silencer body, an impedance material and a coiled pipeline. The silencer body is of a coiled structure, resistive noise reduction is designed on the upper end face and the lower end face of the silencer, resistance noise reduction is involved in the pipeline, a honeycomb core is arranged on the inner surface of the pipeline, airflow can flow in the smooth pipeline, meanwhile, resistive resistance noise reduction is achieved, and therefore the power influence of airflow resistance ona small-displacement engine is reduced. The silencer has the advantages that the structure is simple, so that the space utilization structure of the silencer is compact; and meanwhile, an exhaust guide pipe is short, so that the silencer is lighter in weight and smaller in airflow resistance. Under the condition that special application environment requirements exist, the strict requirements forthe weight, the installation space and the exhaust resistance of the silencer when the silencer is applied to the unmanned aerial vehicle are effectively met; and the silencer can also be used as a silencing device of an automobile, and can be used in other occasions where flowing gas is silenced.

Description

technical field [0001] The invention relates to the technical field of UAV noise reduction device design, in particular to a noise reduction device for heavy-duty fixed-wing UAVs. Background technique [0002] Unmanned aircraft is an aircraft mainly controlled by radio remote control or by its own program. It has the characteristics of small size, low cost and easy to use. In terms of military affairs, drones are favored by armies all over the world because of their low requirements on the combat environment and strong battlefield survivability. In terms of civilian use, drones are also widely used in fields such as aerial photography, geophysical prospecting, disaster monitoring, and coastal anti-smuggling. But for a long time, drones have been one of the main problems affecting their performance due to noise. [0003] The noise of drones is mainly composed of aerodynamic noise and power system noise. At present, the most commonly used low-speed, medium and low-altitude d...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F01N13/00F01N1/12F01N1/10B64D33/04
CPCF01N13/007F01N1/125B64D33/06F01N2590/00B64U50/11Y02T50/40
Inventor 李晋吴亚锋张佳琪种泽中苏元
Owner NORTHWESTERN POLYTECHNICAL UNIV
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