JPH0240073A - Muffling mechanism for engine driven air conditioner - Google Patents

Muffling mechanism for engine driven air conditioner

Info

Publication number
JPH0240073A
JPH0240073A JP18803588A JP18803588A JPH0240073A JP H0240073 A JPH0240073 A JP H0240073A JP 18803588 A JP18803588 A JP 18803588A JP 18803588 A JP18803588 A JP 18803588A JP H0240073 A JPH0240073 A JP H0240073A
Authority
JP
Japan
Prior art keywords
intake
engine
engines
length
pulsations
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.)
Pending
Application number
JP18803588A
Other languages
Japanese (ja)
Inventor
Yoshihisa Kato
嘉久 加藤
Eiji Morita
栄治 森田
Michinao Takahashi
道尚 高橋
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.)
Aisin Corp
Original Assignee
Aisin Seiki Co 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 Aisin Seiki Co Ltd filed Critical Aisin Seiki Co Ltd
Priority to JP18803588A priority Critical patent/JPH0240073A/en
Publication of JPH0240073A publication Critical patent/JPH0240073A/en
Pending legal-status Critical Current

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  • Exhaust Silencers (AREA)

Abstract

PURPOSE:To reduce an engine noise sharply by setting up each draft tube between two engines and the atmospheric air after being branched off from a common draft tube source, and selecting each length of respective draft tubes so as to cause the pulsation of gas being produced in these draft tubes to become such a phase relationship as being offset with each other. CONSTITUTION:A pressure differential in front and in the rear of an intake valve of and engine and pressure fluctuations according to the opening are produced by drive of both first and second engines 1a, 1b, whereby intake pulsa tion conformed to this engine drive is produced each in both first and second intake pipes 6-1, 6-2, and thereby respective intake noises are brought forth. Since each intake pulsation in both these intake pipes 6-1, 6-2 is selected to length so as to cause each length, l1, l2, of the intake pipes 6-1, 6-2 to offset these pulsations, namely, each wavelength of these pulsations is set to lambda, or l1=2/3lambda, l2=lambda, it is offset in an ideal state, thus intake noises in these engines 1a, 1b will not occur at all.

Description

【発明の詳細な説明】 〈産業上の利用分野〉 本発明はエンジンの消音装置、特に複数のエンジンを並
設して駆動する空調装置の消音機構に関する。
DETAILED DESCRIPTION OF THE INVENTION <Industrial Application Field> The present invention relates to an engine muffling device, and particularly to a muffling mechanism for an air conditioner in which a plurality of engines are arranged in parallel and driven.

〈従来の技術〉 従来、エンジン駆動式空調装置において複数のエンジン
を並設して駆動する場合には、それぞれのエンジンの吸
気管路又は排気管路にマフラーサイレンサなどを配設し
、それぞれのエンジンごとに消音を行なっていた。例え
ば実開昭58−154832号公報には、エンジンルー
ムのパネルの一面に吸気口を設け、この吸気口から吸気
管によってエンジンに燃焼用の吸入空気を供給し、この
吸気管に消音器と空気清浄器を設け、エンジンからの排
気ガスをカップリングを介してパネルの他の面に設けた
排気口から外部に放出する方式のものが提案されている
<Prior art> Conventionally, when multiple engines are installed in parallel and driven in an engine-driven air conditioner, a muffler silencer or the like is installed in the intake pipe or exhaust pipe of each engine. The sound was muted every time. For example, in Japanese Utility Model Application Publication No. 58-154832, an intake port is provided on one side of a panel in the engine room, intake air for combustion is supplied to the engine from this intake port through an intake pipe, and a silencer and an air filter are connected to the intake pipe. A system has been proposed in which a purifier is provided and exhaust gas from the engine is discharged to the outside from an exhaust port provided on the other side of the panel via a coupling.

エンジンを並設して駆動する場合には、この提案の方式
のものを複数使用して、エンジンの騒音を低減すること
が出来る。
When engines are installed in parallel and driven, a plurality of the proposed methods can be used to reduce engine noise.

〈発明の解決しようとする課題〉 しかし、大容量のエンジン駆動式空気調和装置では、 
 一つのエンジンルーム内に複数のエンジンを収容して
、これら並設された複数のエンジンを同時に駆動するこ
とが必要となる。
<Problems to be solved by the invention> However, in large-capacity engine-driven air conditioners,
It is necessary to house a plurality of engines in one engine room and drive these plurality of engines arranged in parallel at the same time.

この場合に、前述の提案の方式を用いるとエンジン室が
大型化し、 大気とエンジン間に配設され る吸気管及び排気管の配置が複雑なものとなり、装置が
大型化し製造コストも上昇する。
In this case, if the above-mentioned proposed method is used, the engine room will become larger, the arrangement of the intake pipe and exhaust pipe placed between the atmosphere and the engine will become complicated, the device will become larger, and the manufacturing cost will increase.

本発明の目的は、全体の構成を簡易化小型化し、製造コ
ストを低減することができ、エンジンの騒音を大幅に低
下させうるエンジン消音装置を提供することにある。
SUMMARY OF THE INVENTION An object of the present invention is to provide an engine silencer that can simplify and downsize the overall configuration, reduce manufacturing costs, and significantly reduce engine noise.

く課題を解決するための手段〉 本発明においては、複数の各エンジンへの通気管内に生
じる気体の脈動が、互いに相殺されるような位相関係と
なるように、各通気管の長さが選択されている。
Means for Solving the Problems> In the present invention, the length of each vent pipe is selected so that the pulsations of gas generated in the vent pipes to each of the plurality of engines have a phase relationship that cancels each other out. has been done.

即ち、本発明は、複数のエンジンを並設して駆動させる
場合に生じるエンジンの騒音を低減するエンジンの消音
装置であり、複数のエンジンと大気間の通気管を共通の
通気管源がら分岐してそれぞれ配設し、複数のエンジン
の駆動に伴ってこれら複数の通気管内に生じる気体の脈
動が、互いに相殺されるような位相関係となるように、
各通気管の長さが選択された構成になっている。
That is, the present invention is an engine silencing device that reduces engine noise generated when a plurality of engines are installed in parallel and driven, and in which vent pipes between the plurality of engines and the atmosphere are branched from a common vent pipe source. so that the gas pulsations generated in the plurality of vent pipes due to the driving of the plurality of engines have a phase relationship that cancels each other out.
Each vent tube has a selected length configuration.

く作 用〉 本発明では、複数のエンジンの駆動に伴って共通の通気
管源から分岐して各エンジンに供給されている各通気管
内に生じる気体の脈動は、互いに相殺される。即ち、こ
れらの気体の脈動が互いに相殺されるような位相関係と
なるように、各通気管の長さが選択されている。このた
めに、各通気管内に生じる脈動が互いに相殺され、これ
によってエンジンの騒音が低減することになる。
Effects> In the present invention, the gas pulsations generated in the respective vent pipes that are branched from a common vent pipe source and supplied to each engine due to the driving of a plurality of engines cancel each other out. That is, the length of each vent pipe is selected so that the pulsations of these gases have a phase relationship that cancels each other out. For this reason, the pulsations occurring in each vent pipe cancel each other out, thereby reducing engine noise.

く実 施 例〉 以下、本発明を吸気系に適用した実施例を図面を用いて
詳細に説明する。
Embodiments Hereinafter, embodiments in which the present invention is applied to an intake system will be described in detail with reference to the drawings.

第1図は、実施例の構成を示すブロック図であり、燃焼
用の吸入空気がエアクリーナ7を介して通気管源8に供
給され、この通気管源8から分岐した第1の吸気管6−
1が、ガスミキサ3a及びインテークマニホールド2a
を介して、第1のエンジン1aに接続され、第1のエン
ジン1aの燃焼用の吸気がこの第1の吸気管6−1によ
ってガスミキサー3aに供給される。
FIG. 1 is a block diagram showing the configuration of an embodiment, in which intake air for combustion is supplied to a ventilation pipe source 8 via an air cleaner 7, and a first intake pipe 6-- which branches from this ventilation pipe source 8.
1 is a gas mixer 3a and an intake manifold 2a
The intake pipe 6-1 is connected to the first engine 1a through the first intake pipe 6-1, and intake air for combustion of the first engine 1a is supplied to the gas mixer 3a through the first intake pipe 6-1.

同様にして、通気管源8から分岐した第2の吸M%F6
2がガスミキサ3a及びインテークマニホールド2bを
介して、第2のエンジン1bに接続され、第2のエンジ
ンlbの燃焼用の吸気がこの第2の吸気管6−2によっ
てガスミキサー3bに供給されている。
Similarly, a second absorption M%F6 branched from the ventilation pipe source 8
2 is connected to the second engine 1b via a gas mixer 3a and an intake manifold 2b, and the intake air for combustion of the second engine lb is supplied to the gas mixer 3b through this second intake pipe 6-2. .

それぞれのガスミキサー3a、3bには、それぞれガス
レギュレータ5a、5bを介して燃料パイプ4a、4b
が接続され、ガスミキサー3 a。
Each gas mixer 3a, 3b is connected to a fuel pipe 4a, 4b via a gas regulator 5a, 5b, respectively.
is connected to the gas mixer 3a.

3bで吸気と混合された燃料が、それぞれ第1及び第2
のエンジン1a、1bに供給されるようになっている。
3b, the fuel mixed with the intake air flows into the first and second
The fuel is supplied to the engines 1a and 1b.

実施例においては、複数のエンジン駆動によって、エン
ジンの吸気弁前後の圧力差とその開度に応じて、第1及
び第2の吸気管6−1.6−2内に圧力変動を伴う吸気
脈動が生じるが、これらの吸気脈動が互いに相殺される
ような位相関係となるように第1及び第2の吸気管6−
1.6−2の長さJl、 j2が、それぞれ選択されて
いる。実施例においては、脈動の波長をλとしてJ2−
λ、J2/3λに設定されている。
In the embodiment, by driving a plurality of engines, intake pulsation with pressure fluctuation occurs in the first and second intake pipes 6-1, 6-2 according to the pressure difference before and after the engine intake valve and its opening degree. However, the first and second intake pipes 6-
The lengths Jl and j2 of 1.6-2 are selected, respectively. In the example, J2-
λ, J2/3λ.

二のような構成の実施例の動作を次に説明する。The operation of the embodiment having the configuration as described in 2 will now be described.

エアクリーナ7を介して、第1及び第2の吸気管6−1
.6−2からガスミキサー3a13bに供給された吸気
は、ガスミキサー3a、3bで燃料バイブ4a、4bか
ら供給される燃料と混合されて、それぞれ第1及び第2
のエンジン1a、1bに供給される。第1及び第2のエ
ンジンの1a、1bの駆動によって、エンジンの吸気弁
前後の圧力差とその開度に応じて圧力変動が生じ、エン
ジンの駆動に対応した吸気脈動が、第1及び第2の吸気
管6−1.6−2内にそれぞれ発生し、それぞれの吸気
騒音が生ずる。
Via the air cleaner 7, the first and second intake pipes 6-1
.. The intake air supplied from the gas mixer 6-2 to the gas mixer 3a13b is mixed with the fuel supplied from the fuel vibrators 4a and 4b by the gas mixers 3a and 3b, and is mixed with the fuel supplied from the fuel vibrators 4a and 4b, respectively.
is supplied to the engines 1a and 1b. By driving 1a and 1b of the first and second engines, pressure fluctuations occur depending on the pressure difference before and after the engine's intake valve and its opening degree, and the intake pulsation corresponding to the driving of the engine The noise is generated in the intake pipes 6-1 and 6-2, respectively, resulting in respective intake noises.

第1の吸気管6−1内及び第2の吸気管6−2内の吸気
脈動は、それぞれ第2図に示すような波形となり第1及
び第2の吸気管6−1.6−2の長さJl、 j2が、
これらの脈動を相殺させるような長さ、即ちこれらの脈
動の波長なλとして、凌=2/3λ、J、二λに選択さ
れているので、理想的な状態では脈動が相殺され、エン
ジンla、■bの吸気騒音は発生しない。
The intake pulsations in the first intake pipe 6-1 and the second intake pipe 6-2 have waveforms as shown in FIG. 2, respectively. The lengths Jl and j2 are
The length λ that cancels out these pulsations, that is, the wavelength of these pulsations, is selected to be L = 2/3 λ, J, 2 λ, so in an ideal state the pulsations are canceled and the engine la , ■b The intake noise is not generated.

この場合、一般には、mを整数としてJ、、−zJ21
/2λmに選択するとよい。実施例ではm=1に設定さ
れている。
In this case, in general, J, , -zJ21 where m is an integer
/2λm may be selected. In the embodiment, m is set to 1.

このように上述の実施例によると、第1及び第2のエン
ジンla、Ibを共通のエンジンルーム内に配設した場
合の吸気管の配管構成が簡単となり、少ない構成部品で
全体を小型化することができると共に、第1及び第2の
吸気管6−1.62の長さを所定条件に選定するだけで
、吸気騒音を大幅に低減することが出来る。
According to the embodiment described above, when the first and second engines la and Ib are arranged in a common engine room, the piping configuration of the intake pipe is simplified, and the overall size is reduced with fewer components. In addition, by simply selecting the lengths of the first and second intake pipes 6-1.62 to meet predetermined conditions, intake noise can be significantly reduced.

なお、上述の実施例では本発明の吸気系に適用した場合
について説明したが、本発明は排気系に適用することも
、或は排気系及び吸気系の直方に適用することも出来る
In the above-described embodiments, the case where the present invention is applied to an intake system has been described, but the present invention can also be applied to an exhaust system, or directly between an exhaust system and an intake system.

〈発明の効果〉 以上詳細に説明したように、本発明によると部品点数の
少ない簡単な構成で、複数のエンジンな並設駆動させた
場合のエンジン騒音を大幅に低減出来るエンジンの消音
装置が提供される。
<Effects of the Invention> As described in detail above, the present invention provides an engine silencer that has a simple configuration with a small number of parts and can significantly reduce engine noise when a plurality of engines are driven in parallel. be done.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明の実施例の構成を示すブロック図、第2
図は本発明の実施例の動作を示す波形図である。 la、lb・・・エンジン 3a、3b・・・ガスミキサー 4a、4b・・・燃料パイプ 5a、5b・・拳ガスレギュレータ 6−1・・・第1の吸気管 6−2・・・第2の吸気管
FIG. 1 is a block diagram showing the configuration of an embodiment of the present invention, and FIG.
The figure is a waveform diagram showing the operation of the embodiment of the present invention. la, lb...Engine 3a, 3b...Gas mixer 4a, 4b...Fuel pipe 5a, 5b...Fist gas regulator 6-1...First intake pipe 6-2...Second intake pipe

Claims (1)

【特許請求の範囲】[Claims] 並設された複数のエンジンによつて駆動されるエンジン
駆動式空調装置において、各エンジンと大気を結ぶ通気
管が大気側における1本の共通通気管から分岐して配設
され、各通気管の長さは、前記複数のエンジンの駆動に
伴つて各分岐通気管内に生じる気体の脈動が互いに相殺
される位相関係となるように選択されていることを特徴
とする、エンジン駆動式空調装置の消音機構。
In an engine-driven air conditioner that is driven by multiple engines installed in parallel, a vent pipe connecting each engine to the atmosphere is arranged by branching from a single common vent pipe on the atmosphere side. The length is selected such that the gas pulsations generated in each branch ventilation pipe due to the driving of the plurality of engines have a phase relationship that cancels each other out. mechanism.
JP18803588A 1988-07-29 1988-07-29 Muffling mechanism for engine driven air conditioner Pending JPH0240073A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18803588A JPH0240073A (en) 1988-07-29 1988-07-29 Muffling mechanism for engine driven air conditioner

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18803588A JPH0240073A (en) 1988-07-29 1988-07-29 Muffling mechanism for engine driven air conditioner

Publications (1)

Publication Number Publication Date
JPH0240073A true JPH0240073A (en) 1990-02-08

Family

ID=16216529

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18803588A Pending JPH0240073A (en) 1988-07-29 1988-07-29 Muffling mechanism for engine driven air conditioner

Country Status (1)

Country Link
JP (1) JPH0240073A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5372340A (en) * 1991-11-05 1994-12-13 Hitachi, Ltd. Spacecraft system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5372340A (en) * 1991-11-05 1994-12-13 Hitachi, Ltd. Spacecraft system

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