JPH0577794A - Noise reducing device for high-speed flow noise - Google Patents

Noise reducing device for high-speed flow noise

Info

Publication number
JPH0577794A
JPH0577794A JP24136591A JP24136591A JPH0577794A JP H0577794 A JPH0577794 A JP H0577794A JP 24136591 A JP24136591 A JP 24136591A JP 24136591 A JP24136591 A JP 24136591A JP H0577794 A JPH0577794 A JP H0577794A
Authority
JP
Japan
Prior art keywords
noise
jet
flow
speed
trailing edge
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
JP24136591A
Other languages
Japanese (ja)
Inventor
Hiroshi Nagano
宏 永野
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP24136591A priority Critical patent/JPH0577794A/en
Publication of JPH0577794A publication Critical patent/JPH0577794A/en
Withdrawn legal-status Critical Current

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  • Exhaust Silencers (AREA)

Abstract

PURPOSE:To effectively reduce noise generated by a highspeed flow of a jet engine and so on with a simple device. CONSTITUTION:A damping plate 2 is provided at the rear edge of a member in contact with a high-speed fluid, for example, a jet duct 1, along the flow direction of the high-speed fluid, and generation of noise is restricted by relaxing speed fluctuation of the fluid by the damping plate 2.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、ジェットエンジンの噴
流等の高速流の発生する騒音の減音装置に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a noise reduction device for noise generated by a high speed flow such as a jet flow of a jet engine.

【0002】[0002]

【従来の技術】公害問題となっている航空機騒音は、ジ
ェットエンジンの噴流より発生する空気力学的騒音が、
原因の一つとなっており、これを低減することが、現在
強く要望されている。
2. Description of the Related Art Aircraft noise, which is a pollution problem, is generated by the aerodynamic noise generated by the jet flow of a jet engine.
It is one of the causes, and it is strongly desired to reduce it.

【0003】このような要望を満たすため、図3に図示
するサプレッサ・ノズルおよび図4に図示するコラゲー
テッド・ノズルのような形式のものを用いることが考え
られる。
In order to meet such a demand, it is conceivable to use a suppressor nozzle shown in FIG. 3 and a type such as a collaged nozzle shown in FIG.

【0004】図3に示すサプレッサ・ノズルでは、ジェ
ットエンジンの噴流Fがその内部を流れるジェットパイ
プ01の後縁部に後方へ向かって開口する複数のノズル
02を設け、同ノズル02から噴射される噴流によって
外部の空気を吸い込んでジェットエンジン噴流より発生
する騒音を低減する。
In the suppressor nozzle shown in FIG. 3, a jet flow F of a jet engine is provided with a plurality of nozzles 02 opening rearward at the trailing edge of a jet pipe 01 flowing therein, and jetted from the nozzle 02. The jet stream draws in outside air and reduces the noise generated by the jet engine jet stream.

【0005】図4に示すコラゲーテッド・ノズルでは、
ジェットエンジンの噴流Fがその内部を流れるジェット
パイプ01の後縁部にひだ状の開口03を設け、矢印f
に示すように、外部からこの開口03を経て空気をジェ
ットパイプ01の後縁部に流し込んでジェットエンジン
噴流より発生する騒音を低減する。
In the collaged nozzle shown in FIG. 4,
The jet F of the jet engine is provided with a pleated opening 03 at the trailing edge of the jet pipe 01, and the arrow f
As shown in, the air is made to flow from the outside through the opening 03 to the trailing edge of the jet pipe 01 to reduce noise generated by the jet engine jet flow.

【0006】[0006]

【発明が解決しようとする課題】前記図3及び図4に示
すような、外部からジェットパイプの後縁部に空気を吸
い込み又は流し込む形式の減音装置では、外部からの空
気が噴流に混合することによって推進効率が低下するた
めに、その実用化が困難であった。
In the noise reduction device of the type in which air is sucked or poured into the trailing edge of the jet pipe from the outside as shown in FIGS. 3 and 4, the air from the outside is mixed with the jet flow. As a result, the propulsion efficiency is lowered, which makes it difficult to put it into practical use.

【0007】本発明は、前記に鑑みてなされたもので、
推進効率等を極力損なうことなく、効果的に騒音を低下
させることができる高速流騒音の減音装置を提供しよう
とするものである。
The present invention has been made in view of the above,
An object of the present invention is to provide a noise reduction device for high-speed flow noise that can effectively reduce noise without impairing propulsion efficiency and the like as much as possible.

【0008】[0008]

【課題を解決するための手段】本発明の高速流騒音の減
音装置は、高速流体に接する部材の後縁部に、前記高速
流体の流れに沿った減衰板を設けた。
In the noise reduction device for high-speed flow noise according to the present invention, a damping plate is provided at the trailing edge of a member in contact with the high-speed fluid along the flow of the high-speed fluid.

【0009】[0009]

【作用】ジェットパイプ、ダクト等高速流体に接する部
材の後縁部では、該流体の流れ方向に沿った速度成分が
時間的に著しく変動して、その速度変動による剪断力変
化で騒音が発生する。
In the trailing edge portion of a member such as a jet pipe or a duct that is in contact with a high-speed fluid, the velocity component along the flow direction of the fluid fluctuates remarkably with time, and the shearing force changes due to the velocity fluctuation to generate noise. .

【0010】本発明では、前記部材の後縁部における高
速流体の流れの激しい速度変動は、減衰板によって緩和
することができるので、騒音の発生が抑制される。
According to the present invention, the violent velocity fluctuation of the flow of the high-speed fluid at the trailing edge of the member can be alleviated by the damping plate, so that the generation of noise is suppressed.

【0011】[0011]

【実施例】以下本発明の一実施例を、図1及び図2によ
って説明する。1はジェットエンジンの噴流Fが内部を
流れる円筒状のジェットパイプで、同ジェットパイプ1
の後縁周囲に一定間隔をおいて複数の減衰板2が配設さ
れている。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of the present invention will be described below with reference to FIGS. Reference numeral 1 is a cylindrical jet pipe through which a jet F of a jet engine flows.
A plurality of damping plates 2 are arranged around the trailing edge at regular intervals.

【0012】同減衰板2は、図2に示すように、前方の
部分がやや尖った水滴状の形状を有し、その軸方向の中
心線に沿って、ジェットパイプ1にジェットエンジンの
噴流Fの流れ方向、即ち、ジェットパイプ1の軸方向に
取付けられ、かつ、その後端部はジェットパイプ1の後
縁より突出するように配置されている。
As shown in FIG. 2, the attenuating plate 2 has a water drop-like shape in which the front portion is slightly pointed, and the jet F of the jet engine is jetted to the jet pipe 1 along the axial center line. In the flow direction of the jet pipe 1, that is, in the axial direction of the jet pipe 1, and its rear end portion is arranged so as to project from the rear edge of the jet pipe 1.

【0013】本実施例では、ジェットパイプ1後縁部に
おけるジェットエンジン噴流Fの速度変動は、同ジェッ
トパイプ1の後縁周囲に設けられた複数の減衰板2によ
って緩和され、騒音の発生を抑制することができる。
In this embodiment, fluctuations in the velocity of the jet engine jet F at the trailing edge of the jet pipe 1 are alleviated by a plurality of damping plates 2 provided around the trailing edge of the jet pipe 1, thus suppressing noise generation. can do.

【0014】また、ジェットパイプ1内には外部からの
空気が流し込まれることがなく、推進効率が低下するこ
ともない。
Further, the air from the outside is not poured into the jet pipe 1, and the propulsion efficiency is not lowered.

【0015】本実施例は、ジェットパイプに本発明を適
用したものであるが、本発明は高速流体に接する部材、
例えば翼型の後縁部、管路のオリフィス等に広く適用す
ることができる。
In this embodiment, the present invention is applied to a jet pipe, but the present invention is a member contacting a high speed fluid.
For example, it can be widely applied to a blade-shaped trailing edge portion, an orifice of a conduit, and the like.

【0016】[0016]

【発明の効果】本発明は、簡単な構成によって、外部か
ら空気等の流体が流入することなく、高速流体に接する
ジェットパイプ、ダクト等の部材の後縁部より発生する
高速流騒音を効果的に低減することができる。
According to the present invention, with a simple structure, high-speed flow noise generated from the trailing edge of a member such as a jet pipe or a duct which comes into contact with a high-speed fluid can be effectively prevented without inflowing a fluid such as air from the outside. Can be reduced to

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明の一実施例の斜視図である。FIG. 1 is a perspective view of an embodiment of the present invention.

【図2】同実施例のジェットパイプ後縁部の断面図であ
る。
FIG. 2 is a cross-sectional view of a trailing edge portion of a jet pipe of the same embodiment.

【図3】従来の高速流騒音の減音装置の1例の斜視図で
ある。
FIG. 3 is a perspective view of an example of a conventional noise reduction device for high-speed flow noise.

【図4】従来の高速流騒音の減音装置の他の例の斜視図
である。
FIG. 4 is a perspective view of another example of a conventional noise reduction device for high-speed flow noise.

【符号の説明】[Explanation of symbols]

1 ジェットパイプ 2 減衰板 F ジェットエンジンの噴流 1 Jet pipe 2 Damping plate F Jet engine jet

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 高速流体に接する部材の後縁部に、前記
高速流体の流れに沿った減衰板を設けたことを特徴とす
る高速流騒音の減音装置。
1. A noise reduction device for high-speed flow noise, characterized in that a damping plate along the flow of the high-speed fluid is provided at the trailing edge of a member that contacts the high-speed fluid.
JP24136591A 1991-09-20 1991-09-20 Noise reducing device for high-speed flow noise Withdrawn JPH0577794A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP24136591A JPH0577794A (en) 1991-09-20 1991-09-20 Noise reducing device for high-speed flow noise

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP24136591A JPH0577794A (en) 1991-09-20 1991-09-20 Noise reducing device for high-speed flow noise

Publications (1)

Publication Number Publication Date
JPH0577794A true JPH0577794A (en) 1993-03-30

Family

ID=17073209

Family Applications (1)

Application Number Title Priority Date Filing Date
JP24136591A Withdrawn JPH0577794A (en) 1991-09-20 1991-09-20 Noise reducing device for high-speed flow noise

Country Status (1)

Country Link
JP (1) JPH0577794A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7516815B2 (en) * 2004-03-03 2009-04-14 Roll-Royce Deutschland Ltd & Co Kg Arrangement for the generation of sonic fields of a specific modal composition

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7516815B2 (en) * 2004-03-03 2009-04-14 Roll-Royce Deutschland Ltd & Co Kg Arrangement for the generation of sonic fields of a specific modal composition

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Legal Events

Date Code Title Description
A300 Withdrawal of application because of no request for examination

Free format text: JAPANESE INTERMEDIATE CODE: A300

Effective date: 19981203