JPS61184360A - Turbo refrigerator - Google Patents

Turbo refrigerator

Info

Publication number
JPS61184360A
JPS61184360A JP60024321A JP2432185A JPS61184360A JP S61184360 A JPS61184360 A JP S61184360A JP 60024321 A JP60024321 A JP 60024321A JP 2432185 A JP2432185 A JP 2432185A JP S61184360 A JPS61184360 A JP S61184360A
Authority
JP
Japan
Prior art keywords
compressor
gas
flange
suction duct
suction
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.)
Granted
Application number
JP60024321A
Other languages
Japanese (ja)
Other versions
JPH042867B2 (en
Inventor
寺崎 政敏
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.)
Hitachi Ltd
Original Assignee
Hitachi 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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP60024321A priority Critical patent/JPS61184360A/en
Priority to DE8585114481T priority patent/DE3584139D1/en
Priority to EP85114481A priority patent/EP0182292B1/en
Priority to KR1019850008583A priority patent/KR890004394B1/en
Priority to US06/799,975 priority patent/US4615184A/en
Priority to CN85109765.0A priority patent/CN1004227B/en
Publication of JPS61184360A publication Critical patent/JPS61184360A/en
Publication of JPH042867B2 publication Critical patent/JPH042867B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Cold Air Circulating Systems And Constructional Details In Refrigerators (AREA)
  • Devices That Are Associated With Refrigeration Equipment (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 〔発明の利用分野〕 本発明は、ターボ冷凍機に関する。[Detailed description of the invention] [Field of application of the invention] The present invention relates to a centrifugal refrigerator.

〔発明の背景〕[Background of the invention]

従来の方法を第1図〜第4図を用いて説明する。 The conventional method will be explained using FIGS. 1 to 4.

蒸発器1.凝縮器2.及び圧縮機3.主電動機4と、蒸
発器からの発生ガスを圧縮機3に導く吸込ダクト5.圧
縮機3からの吐出ガスを凝縮器2に導く吐出ダクト6よ
り構成されるターボ冷凍機において、従来では圧縮機3
の吸込、吐出部の取り合いが、a、bの2面であったた
め、まず吐出部Bに圧縮機3を取り付けた後に吸込部A
を現金する必要があり、製作工数がかかった。
Evaporator 1. Condenser 2. and compressor 3. A main motor 4 and a suction duct 5 that guides generated gas from the evaporator to the compressor 3. Conventionally, in a turbo chiller configured with a discharge duct 6 that guides discharge gas from the compressor 3 to the condenser 2, the compressor 3
Since the suction and discharge parts of 2 were connected to each other on two sides, a and b, first the compressor 3 was attached to the discharge part B, and then the suction part A
It was necessary to pay cash, and it took a lot of man-hours to manufacture.

又、内部ガスの大気側への洩れ(高圧ガスの場合)ある
いは大気からの洩れ(低圧ガスの場合)の発生個所とし
ても比較的大口径のため大きなウェイトを占めていた。
In addition, because of its relatively large diameter, it occupies a large portion of the area where internal gas leaks to the atmosphere (in the case of high-pressure gas) or from the atmosphere (in the case of low-pressure gas).

又、主電動機4を冷却するため、凝縮器底部より冷媒液
を配管7を介して主電動機4に供給し、主電動機4の冷
却により発生した蒸発ガスを、配管8にて蒸発器1に戻
していた。一方圧縮機3において羽根車9の背側ラビリ
ンス1oより洩れたガスを配管11を介して羽根車3の
吸込側に戻していた。これら配管7,8.11と圧縮機
3とは組立の段階で現金取り合いとなり製作工数ががが
った上、内部ガスの洩れ個所が多いという欠点があった
In addition, in order to cool the main motor 4, refrigerant liquid is supplied from the bottom of the condenser to the main motor 4 through a pipe 7, and evaporated gas generated by cooling the main motor 4 is returned to the evaporator 1 through a pipe 8. was. On the other hand, in the compressor 3, gas leaking from the back labyrinth 1o of the impeller 9 was returned to the suction side of the impeller 3 via a pipe 11. These pipes 7, 8, 11 and the compressor 3 had to compete for cash at the assembly stage, which increased the number of manufacturing steps and had the disadvantage that there were many points where internal gas leaked.

さらに、圧縮機3を熱交換器の上に搭載する構造であっ
たため、熱交換器上に取り付け台を設けている。この場
合圧縮機3の水平位置出しを現金取り合いとしたリライ
ナにてレベル調整を行なっていたため製作工数のかかる
欠点があった。
Furthermore, since the compressor 3 was constructed to be mounted on the heat exchanger, a mounting base was provided on the heat exchanger. In this case, the horizontal positioning of the compressor 3 was performed using a reliner, which was used as a cash-for-money method to adjust the level, which had the disadvantage of requiring a lot of manufacturing man-hours.

〔発明の目的〕[Purpose of the invention]

本発明の目的は、圧縮機の吸込部と吐出部、さらにはそ
の他冷媒液、ガスの供受を同−取り合いフランジ面で行
なうことにより、ガス洩れ箇所を削減し、ガス洩れによ
る弊害を予防しまた、製作工数の低減化をはかったター
ボ冷凍機を提供することにある。
The purpose of the present invention is to reduce the number of gas leakage points and prevent the harmful effects caused by gas leakage by supplying and receiving the suction and discharge parts of the compressor, as well as other refrigerant liquid and gas on the same mating flange surface. Another object of the present invention is to provide a centrifugal chiller that reduces manufacturing man-hours.

〔発明の概要〕[Summary of the invention]

本発明は、ターボ圧縮機のスクロールから出た後のガス
の流れを圧縮機のケーシング内にて吸込ダクト側に曲げ
ることにより、圧縮機の吸込ダクトとの取り合い面上で
ガスの吸込、吐出を行なわせることができる他に、吸込
ダクトと圧縮機の取り合い面で圧縮機を支持することに
よりオーバハング構造が可能となる。
The present invention bends the flow of gas after exiting from the scroll of the turbo compressor toward the suction duct within the casing of the compressor, thereby controlling the suction and discharge of gas on the interface with the suction duct of the compressor. In addition to this, an overhang structure is also possible by supporting the compressor at the interface between the suction duct and the compressor.

〔発明の実施例〕[Embodiments of the invention]

以下、本発明の一実施例を第5図〜第8図により説明す
る。
An embodiment of the present invention will be described below with reference to FIGS. 5 to 8.

本図に示すターボ冷凍機は、蒸発器1と凝縮器2が1ケ
のシュルを2分割することにより構成された熱交換器3
と、圧縮機4と、蒸発器1からの蒸発ガスを圧縮機4に
導く吸込ダクト5と、圧縮機4からの吐出ガスを凝縮器
2に導く吐出ダクト6から構成される。
The centrifugal refrigerator shown in this figure has a heat exchanger 3 in which an evaporator 1 and a condenser 2 are constructed by dividing one cell into two.
, a compressor 4 , a suction duct 5 that leads evaporated gas from the evaporator 1 to the compressor 4 , and a discharge duct 6 that leads the discharged gas from the compressor 4 to the condenser 2 .

同図に示す圧縮機4は、スクロールから出た後のガス流
路に関し吸込ダクトlに向いて流れを曲げた形状を有し
てしる。圧縮機4と吸込ダクト5との取り合いはフラン
ジ7を介して行なわれ、このフランジ7には、圧縮機4
の吐出ガスの通過に必要な切り欠きdが形成されており
、シートパツキンにて圧縮機の吸込部Cと吐出部dとの
境界をシールする。一方吸込ダクト5の内部には、−例
として吸込ダクトの壁を一部利用して吐出ダクト6を形
成し、凝縮器2に設けたガス通過穴に通じている。ガス
の流れは第5図、第6図の中で白抜きの矢印にて示しで
ある通りである。
The compressor 4 shown in the figure has a shape in which the gas flow path after exiting the scroll is bent toward the suction duct 1. The compressor 4 and the suction duct 5 are connected via a flange 7, and the compressor 4 is connected to the flange 7.
A notch d necessary for passage of the discharged gas is formed, and the boundary between the suction part C and the discharge part d of the compressor is sealed with a sheet packing. On the other hand, inside the suction duct 5, for example, a discharge duct 6 is formed using a part of the wall of the suction duct, and communicates with a gas passage hole provided in the condenser 2. The gas flow is as shown by the white arrows in FIGS. 5 and 6.

主電動機8を冷媒冷却するための冷媒液は、凝縮器2の
底部より供給されるが、この配管9は吸込ダクト5のフ
ランジ部7まで導がれでいる。一方圧縮機ケーシング側
には、主電動機へ冷媒液を供給するための通路が設けら
れ、吸込ダクト5のフランジ7に設けられた冷媒液通過
穴〇を通じて冷媒液の供給が行なわれる。さらに、主電
動機8の冷却により発生した蒸発ガスは、やはり圧縮機
ケーシングに設けられた通路を介して、フランジ7に設
けられた通過穴fを通じて吸込ダクト内に戻している。
A refrigerant liquid for refrigerant cooling the main motor 8 is supplied from the bottom of the condenser 2, and this piping 9 is led to the flange portion 7 of the suction duct 5. On the other hand, on the compressor casing side, a passage for supplying refrigerant liquid to the main motor is provided, and the refrigerant liquid is supplied through the refrigerant liquid passage hole 〇 provided in the flange 7 of the suction duct 5. Further, the evaporated gas generated by cooling the main motor 8 is returned into the suction duct through a passage hole f provided in the flange 7, also via a passage provided in the compressor casing.

また羽根車の背面側からラビリンスを通じて洩れたガス
もフランジ7に設けられた通過穴gを通じて吸込ダクト
側にバランスしている。
Further, gas leaking from the back side of the impeller through the labyrinth is also balanced to the suction duct side through the passage hole g provided in the flange 7.

吸込、吐出の取り合いばかりでなく、その他の冷媒液、
ガスの取り合いも同−取り合いフランジ上にて行なうこ
とができる。
Not only the suction and discharge, but also other refrigerant liquids,
Gas connection can also be performed on the same connection flange.

吸込ダクト5と圧縮機4とはフランジ7にて取り合いと
なっており側面で圧縮機を支持することができるため、
圧縮機を軽量化することによりオーバハング支持が可能
となる。第5図に示す圧縮機にはフランジ面次外にサポ
ートがない構造となっている。
The suction duct 5 and the compressor 4 are connected to each other at the flange 7, and the compressor can be supported on the side.
By reducing the weight of the compressor, overhang support becomes possible. The compressor shown in FIG. 5 has a structure in which there is no support outside the flange surface.

上記のように一実施例を説明したが1本実施例では、吸
込ダクト5の内部の壁を一部利分して吐出ダクト6を形
成できるので必要部片が減り製作費の低減がはかれる他
、フランジ7が熱交換器から直接溶接にて固定されてい
るため、圧縮機をこのフランジ7にてオーババンク支持
するのに十分な剛性を得ることができる。又このような
吸込ダクト5が圧縮機4の取り合いフランジ7と同等か
それより小さければ、長手方向に長くても占有スペース
としては変わらない。
One embodiment has been described above, but in this embodiment, the discharge duct 6 can be formed by using a portion of the inner wall of the suction duct 5, which reduces the number of required parts and reduces manufacturing costs. Since the flange 7 is directly fixed to the heat exchanger by welding, sufficient rigidity can be obtained to support the compressor in an overbank manner by the flange 7. Further, if such a suction duct 5 is equal to or smaller than the connecting flange 7 of the compressor 4, the occupied space remains the same even if it is longer in the longitudinal direction.

〔発明の効果〕〔Effect of the invention〕

以上のように本発明によれば、圧縮機のガス吸込部と吐
出部さらには、その他必要冷媒液、ガスを、吸込ダクト
と圧縮機の取り付けフランジ面上にて取り合うことがで
きるため、現金作業が不要となり大幅な製作工数の低減
がはかれるとともに。
As described above, according to the present invention, the gas suction part and the discharge part of the compressor, as well as other necessary refrigerant liquid and gas, can be exchanged between the suction duct and the mounting flange surface of the compressor. This eliminates the need for this, and significantly reduces manufacturing man-hours.

ガス洩れの可能性のある個所を8ケ所から1N2i所に
削減したことによりガス洩れに対する信頼性が向上する
効果がある。また圧縮機の軽量化をはかることにより吸
込ダクトとオーバハング支持が可能になるため組立工数
及び不要なサポートの廃止により製作費の低減化がはか
れる。
Reliability against gas leaks is improved by reducing the number of locations where gas leaks may occur from 8 to 1N2i locations. In addition, by reducing the weight of the compressor, it becomes possible to support the suction duct and overhang, thereby reducing manufacturing costs by eliminating assembly man-hours and unnecessary supports.

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

第1図は、従来のターボ冷凍機の外観図、第2図は、第
1図のA−AI5面図、第3図は、B矢視図、第4図は
、要部断面、第5図は本発明の一実施例の正面図、第6
図は、第5図の平面図、第7図は、第5図のC−C断面
図、第8図は、圧縮機取合い部の断面図である。 1・・・蒸発器、2・・・凝縮器、3・・・熱交換器、
4・・・圧    “縮機、5・・・吸込ダクト、6・
・・吐出ダクト、7・・・フランジ、8・・・主電動機
、9,11・・・配管、10・・・オイルセパレータ、
C・・・吸込側切欠、d・・・吐出側切欠、e・・・冷
媒液供給穴、fig・・・冷媒ガス戻シネ  1  口 l ¥35 図
Fig. 1 is an external view of a conventional centrifugal chiller, Fig. 2 is a 5-plane view taken along line A-AI in Fig. The figure is a front view of one embodiment of the present invention.
5 is a plan view of FIG. 5, FIG. 7 is a sectional view taken along the line C--C of FIG. 5, and FIG. 8 is a sectional view of the compressor joint. 1... Evaporator, 2... Condenser, 3... Heat exchanger,
4... Compressor, 5... Suction duct, 6...
...Discharge duct, 7...Flange, 8...Main motor, 9, 11...Piping, 10...Oil separator,
C... Suction side notch, d... Discharge side notch, e... Refrigerant liquid supply hole, fig... Refrigerant gas return cine 1 port ¥35 Diagram

Claims (1)

【特許請求の範囲】 1、蒸発器と凝縮器が1つの容器内に納められた熱交換
器と、ターボ圧縮機と主電動機により構成されたターボ
冷凍機において、蒸発器で発生する蒸発ガスを圧縮機の
ガス吸入口に導く吸込ダクトと、吸込ダクト内に、圧縮
機の吐出ガスを凝縮器に導くように形成された吐出ダク
トを有し、吸込ダクトと圧縮機との取り合いは、吸込ダ
クト側に設けられたフランジ上で行なわれることを特徴
とするターボ冷凍機。 2、冷媒にて冷却される主電動機を有する特許請求の範
囲第1項記載のターボ冷凍機において、主電動機へ供給
される冷媒液と、主電機の冷却により発生する冷媒ガス
と、圧縮機の羽根車背側からラビリンスを介して洩れ、
羽根車の吸込側に戻されるガスを圧縮機と吸込ダクト側
フランジの取り付け面にて受け渡しできるように、圧縮
機側フランジ面上には、上記冷媒液、冷媒ガスの通過穴
を設け、吸込ダクト側フランジには、それらの穴に対応
する位置に切欠穴を設け、配管にて所定の場所に通路を
導びいたことを特徴とするターボ冷凍機。 3、特許請求の範囲第1項または第2項に記載のターボ
冷凍機において、圧縮機の支持部を吸込ダクト側フラン
ジ面のみとし圧縮機の支持方式をオーバハング構造とし
たことを特徴とするターボ冷凍機。
[Claims] 1. In a turbo chiller composed of a heat exchanger in which an evaporator and a condenser are housed in one container, a turbo compressor, and a main electric motor, evaporative gas generated in the evaporator is It has a suction duct that leads to the gas inlet of the compressor, and a discharge duct that is formed within the suction duct to lead the discharge gas of the compressor to the condenser. A turbo chiller characterized by being operated on a flange provided on the side. 2. In the centrifugal chiller according to claim 1, which has a main motor cooled by a refrigerant, the refrigerant liquid supplied to the main motor, the refrigerant gas generated by cooling the main motor, and the compressor Leakage from the back side of the impeller through the labyrinth,
The passage holes for the refrigerant liquid and refrigerant gas are provided on the flange surface of the compressor side so that the gas returned to the suction side of the impeller can be transferred between the mounting surface of the compressor and the suction duct side flange. A turbo chiller characterized in that the side flange is provided with notched holes at positions corresponding to those holes, and a passage is guided to a predetermined location by piping. 3. A turbo chiller according to claim 1 or 2, characterized in that the supporting portion of the compressor is only the flange surface on the suction duct side, and the compressor is supported in an overhung structure. refrigerator.
JP60024321A 1984-02-13 1985-02-13 Turbo refrigerator Granted JPS61184360A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
JP60024321A JPS61184360A (en) 1985-02-13 1985-02-13 Turbo refrigerator
DE8585114481T DE3584139D1 (en) 1984-11-22 1985-11-14 COMPRESSOR REFRIGERATOR WITH A LIQUID VAPOR SEPARATOR.
EP85114481A EP0182292B1 (en) 1984-11-22 1985-11-14 Compressor refrigerating machine with vapor-liquid separator
KR1019850008583A KR890004394B1 (en) 1984-02-13 1985-11-16 Compression refrigerating machine with vapor-liquid seperator
US06/799,975 US4615184A (en) 1984-11-22 1985-11-20 Compression refrigerating machine with vapor-liquid separator
CN85109765.0A CN1004227B (en) 1984-11-22 1985-11-22 Compression refrigeration machines with separator of vapours-liquid

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP60024321A JPS61184360A (en) 1985-02-13 1985-02-13 Turbo refrigerator

Publications (2)

Publication Number Publication Date
JPS61184360A true JPS61184360A (en) 1986-08-18
JPH042867B2 JPH042867B2 (en) 1992-01-21

Family

ID=12134915

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60024321A Granted JPS61184360A (en) 1984-02-13 1985-02-13 Turbo refrigerator

Country Status (1)

Country Link
JP (1) JPS61184360A (en)

Also Published As

Publication number Publication date
JPH042867B2 (en) 1992-01-21

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