JPH0240180B2 - TAABOCHAAJANOKAKYUTOKUSEISOKUTEISOCHI - Google Patents

TAABOCHAAJANOKAKYUTOKUSEISOKUTEISOCHI

Info

Publication number
JPH0240180B2
JPH0240180B2 JP11813782A JP11813782A JPH0240180B2 JP H0240180 B2 JPH0240180 B2 JP H0240180B2 JP 11813782 A JP11813782 A JP 11813782A JP 11813782 A JP11813782 A JP 11813782A JP H0240180 B2 JPH0240180 B2 JP H0240180B2
Authority
JP
Japan
Prior art keywords
turbine
compressor
turbocharger
side passage
exhaust side
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.)
Expired - Lifetime
Application number
JP11813782A
Other languages
Japanese (ja)
Other versions
JPS599538A (en
Inventor
Teruhisa Katsumata
Masao Nitsuta
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.)
Honda Motor Co Ltd
Original Assignee
Honda Motor 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 Honda Motor Co Ltd filed Critical Honda Motor Co Ltd
Priority to JP11813782A priority Critical patent/JPH0240180B2/en
Publication of JPS599538A publication Critical patent/JPS599538A/en
Publication of JPH0240180B2 publication Critical patent/JPH0240180B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B39/00Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Testing Of Engines (AREA)

Description

【発明の詳細な説明】 本発明は、ターボチヤージヤのタービンとコン
プレツサとを各介在させる排気側と吸気側の通路
を備え、該タービンを該排気側通路に流す気体で
回転駆動して、該コンプレツサに流れる空気流量
や圧縮比を測定するようにしたターボチヤージヤ
の過給特性測定装置に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention comprises passages on the exhaust side and intake side in which a turbine and a compressor of a turbocharger are respectively interposed, and the turbine is rotationally driven by gas flowing through the exhaust side passage. The present invention relates to a turbocharger supercharging characteristic measuring device that measures the flow rate and compression ratio of flowing air.

従来この種装置においては、タービンを介在さ
せる排気側通路とコンプレツサを介在させる吸気
側通路とをエンジンの排気ポートと吸気ポートと
に接続して、エンジン実装状態でターボチヤージ
ヤの過給特性を測定するか、或いは排気側通路に
バーナや電気ヒータ等で熱した空気を送り込んで
タービンを回転駆させることにより過給特性を測
定するを一般としているが、前者においては、 (i) エンジンを安定して運転しその出力を吸収す
るため高価なダイナモ器が必要である。
Conventionally, in this type of device, the supercharging characteristics of the turbocharger are measured with the engine installed by connecting an exhaust side passage with a turbine in between and an intake side passage with a compressor in between to the exhaust port and intake port of the engine. Alternatively, it is common to measure the supercharging characteristics by feeding air heated by a burner or electric heater into the exhaust passage to rotate the turbine. An expensive dynamo is required to absorb the output.

(ii) タービン側は900℃以上になるためガソリン、
オイル等が漏れると火災を起こす危険がある。
(ii) Because the temperature on the turbine side is over 900℃, gasoline
There is a risk of fire if oil etc. leaks.

(iii) エンジンを運転するための補助部材類が多く
なり、作業性が悪く、装置の組立に手数がかか
る。
(iii) A large number of auxiliary parts are needed to operate the engine, which results in poor workability and requires time and effort to assemble the device.

等の不都合を伴い、又後者においても、 (i) タービンへの加熱空気の流量、温度を一定に
保つための制御機構が複雑且つ高価となる。
In the latter case as well, (i) the control mechanism for keeping the flow rate and temperature of heated air to the turbine constant is complicated and expensive;

(ii) 高温(約800℃)の空気を長時間流すため、
装置の断熱、排熱関係設備が複雑となり、且つ
安全上の配慮が必要となる。
(ii) To flow high temperature (approximately 800℃) air for a long time,
The equipment's insulation and heat exhaust equipment become complicated, and safety considerations are required.

等の不都合を伴う。It is accompanied by other inconveniences.

本発明は、かかる不都合を解消した測定装置を
提供することをその目的とするもので、ターボチ
ヤージヤのタービンとコンプレツサとを各介在さ
せる排気側と吸気側の通路を備え、該タービンを
該排気側通路に流す気体で回転駆動して、該該コ
ンプレツサに流れる空気流量や圧縮比を測定する
ようにしたターボチヤージヤの過給特性測定装置
において、該排気側通路の上流端を圧搾空気源に
接続して該タービンを該空気源からの圧搾空気で
回転駆動するようにし、該排気側通路の該タービ
ンの入口上流側と、該吸気側通路のコンプレツサ
の出口下流側とに夫々設定の異る複数のソニツク
ノズルを配置して、該両通路のソニツクノズルを
互に所定の組合せで選的に作させるようにしたこ
とを特徴とする。
An object of the present invention is to provide a measuring device that eliminates such inconveniences, and is provided with a passageway on the exhaust side and an intake side in which the turbine and compressor of a turbocharger are interposed, respectively, and the turbine is connected to the exhaust side passageway. In a turbocharger supercharging characteristic measuring device that is rotatably driven by gas flowing through the compressor and measures the air flow rate and compression ratio flowing through the compressor, the upstream end of the exhaust side passage is connected to a compressed air source. The turbine is rotationally driven by compressed air from the air source, and a plurality of sonic nozzles with different settings are provided on the upstream side of the turbine inlet in the exhaust side passage and on the downstream side of the compressor outlet in the intake side passage. The invention is characterized in that the sonic nozzles in both passages are arranged so that the sonic nozzles in both passages are selectively produced in a predetermined combination.

次いで本発明を図示の実施例に付説明する。 Next, the present invention will be explained with reference to the illustrated embodiments.

図面で1はターボチヤージヤAを収納する測定
ケース、2,3は該ターボチヤージヤAのタービ
ンTとコンプレツサCとを各介在させた排気側と
吸気側の通路を示し、該排気側通路2は、該ター
ビンTの入口を工場エア源その他の圧搾空気源4
に接続する上流側の管路2aと、その出口を消音
器5を介して該ケース1内に開放する下流側の管
路2bとで構成され、又該吸気側通路3は、該コ
ンプレツサCの入口をエアフイルタ6を介して該
ケース1内に開放する上流側の管路3aと、その
出口を該ケース1内に開放する下流側の管路3b
とで構成され、該排気側通路2の上流側管路2a
と、該吸気側通路3の下流側管路3bとに夫々設
定の異る複数のソニツクノズル7,8を配置し、
これら両通路2,3のソニツクノズル7,8を互
に所定の組合せで選択的に作動させるようにし
た。
In the drawings, reference numeral 1 indicates a measurement case that houses the turbocharger A, and 2 and 3 indicate passages on the exhaust side and intake side in which the turbine T and compressor C of the turbocharger A are interposed, respectively. Connect the inlet of T to the factory air source or other compressed air source 4.
The intake passage 3 is composed of an upstream pipe line 2a connected to the compressor C, and a downstream pipe line 2b whose outlet is opened into the case 1 via a silencer 5. An upstream pipe line 3a whose inlet is opened into the case 1 via the air filter 6, and a downstream pipe line 3b whose outlet is opened into the case 1.
and an upstream pipe line 2a of the exhaust side passage 2.
and a plurality of sonic nozzles 7, 8 with different settings are arranged in the downstream pipe line 3b of the intake passage 3,
The sonic nozzles 7, 8 in both passages 2, 3 are selectively operated in a predetermined combination.

これを更に詳述するに、これらソニツクノズル
7,8は夫々ノズルチヤンバ9,10内に互に並
列に配置されて、シリンダー7a,8aに連動す
るノズル7b,8bの開弁で選択的に作されるも
ので、この場合排気側通路2に備えるソニツクノ
ズル7は、タービンTに供給する圧搾空気の流量
を規定すべく作動し、図示のものではこれを第1
乃至第3の3個に設けて、第1ソニツクノズル7
−1はターボチヤージヤの起動性測定用としてエ
ンジン実装時の排気ガス流量より少ない流量設定
のものとし、第2ソニツクノズル7−2はエンジ
ンの過給運転の任意所定の回転数で流れる排気ガ
ス流量に対応した流量設定のものとし、又第3ソ
ニツクノズル7−3は、ウエストゲートバルブ開
始直前の最大過給圧となる排気ガス流量に対応し
た流量設定のものとした。
To explain this in more detail, these sonic nozzles 7 and 8 are arranged in parallel in nozzle chambers 9 and 10, respectively, and are selectively activated by opening the nozzles 7b and 8b that are linked to the cylinders 7a and 8a. In this case, the sonic nozzle 7 provided in the exhaust side passage 2 operates to regulate the flow rate of compressed air supplied to the turbine T;
The first sonic nozzle 7 is provided in the third to third sonic nozzles.
-1 is set to a flow rate lower than the exhaust gas flow rate when the engine is installed for measuring the startability of the turbocharger, and the second sonic nozzle 7-2 corresponds to the flow rate of exhaust gas flowing at an arbitrary predetermined rotation speed during supercharging operation of the engine. The flow rate of the third sonic nozzle 7-3 was set to correspond to the exhaust gas flow rate that corresponds to the maximum boost pressure immediately before the start of the waste gate valve.

又、吸気側通路3に備えるソニツクノズル8
は、コンプレツサCの出口側の抵抗を上記第1乃
至第3ソニツクノズル7−1,7−2,7−3で
夫々設定される流量の排気ガス流量が流れるエン
ジン回転数の時のエンジンの吸入抵抗に設定すべ
く、該各ソニツノズル7−1,7−2,7−3に
連動して作動される第1乃至第3の3個8−1,
8−2,8−3に設けられる。
In addition, a sonic nozzle 8 provided in the intake passage 3
is the resistance on the outlet side of the compressor C when the engine rotational speed is such that the exhaust gas flow rate is set by the first to third sonic nozzles 7-1, 7-2, and 7-3, respectively. three first to third nozzles 8-1, which are operated in conjunction with the respective Sonitz nozzles 7-1, 7-2, 7-3 to set the
8-2 and 8-3.

而して、排気側通路2と吸気側通路3とのソニ
ツクノズル7,8を第1のものから第2、第3の
ものに順次切換作動して、該吸気側通路3に備え
る差圧流量計11によりコンプレツサCに流れる
空気流量CQと、又該コンプレツサCの入口側と
出口側の圧力CP1,CP2から圧縮比(CP2/CP1
とを測定するもので、これによればエンジン実装
時をシユミレートしての種々の運転状態での過給
特性を知ることが出来る。
Thus, the sonic nozzles 7 and 8 in the exhaust side passage 2 and the intake side passage 3 are sequentially switched from the first one to the second and third ones, and the differential pressure flowmeter provided in the intake side passage 3 is activated. 11, the air flow rate CQ flowing into the compressor C, and the pressures CP 1 and CP 2 on the inlet side and outlet side of the compressor C, the compression ratio ( CP 2 / CP 1 ) is calculated.
According to this, it is possible to know the supercharging characteristics under various operating conditions by simulating the time when the engine is installed.

尚、図示のものでは上記データCQ,CP1,CP2
に加えて、コンプレツサCの入口側と出口側の温
度CT1,CT2、タービンの入口側と出口側の圧力
TP1,TP2と温度TT1,TT2、ソニツクノズル7
の上流側の圧力TP0と温度TT0、ターボチヤージ
ヤAの回転数N、測定ケース1内の圧力PAと温
度TA等の各種データをA−D変換器12を介し
て演算処理装置13に入力し、該装置13により
データのプリンタ14への打出しと、データを演
算処理してターボチヤージヤを予定のエンジンに
塔載可能か否かの合否判定ランプ15の点灯とを
行わせるようにした。
In addition, in the diagram, the above data CQ, CP 1 , CP 2
In addition to the temperatures CT 1 and CT 2 on the inlet and outlet sides of the compressor C, and the pressures on the inlet and outlet sides of the turbine.
TP 1 , TP 2 and temperature TT 1 , TT 2 , Sonic nozzle 7
Various data such as pressure TP 0 and temperature TT 0 on the upstream side of The device 13 outputs the data to the printer 14, processes the data, and lights up a pass/fail judgment lamp 15 to determine whether the turbocharger can be installed on the intended engine.

図面で16はソニツクノズル7の上流側の圧力
TP0を圧力調節器17からの指令によつて所定圧
に保持すべく作動する調圧弁、18は測定ケース
1内の圧力PAを圧力調節器19からの指令で所
定気圧に保持すべく作動する調圧弁を示す。
In the drawing, 16 is the pressure on the upstream side of Sonic nozzle 7.
A pressure regulating valve operates to maintain TP 0 at a predetermined pressure according to a command from the pressure regulator 17, and a pressure regulating valve 18 operates to maintain the pressure P A in the measurement case 1 at a predetermined pressure according to a command from the pressure regulator 19. This shows the pressure regulating valve.

又、図面で20はターボチヤージヤAの潤滑油
の循環系を示し、これに温度調節器21で温度管
理されたオイルバン22、ポンプ23、レギユレ
ータ24、流量計25、圧力計26を配置した。
Further, in the drawing, 20 indicates a lubricating oil circulation system of the turbocharger A, in which an oil bun 22 whose temperature is controlled by a temperature controller 21, a pump 23, a regulator 24, a flow meter 25, and a pressure gauge 26 are arranged.

このように本発明によるときは、排気側通路に
圧搾空気を流してタービンを駆動するもので、作
業性、安全性が向上されると共に、排気側通路と
吸気側通路とに夫々設定の異る複数のソニツクノ
ズルを配設して、これら両通路のソニツクノズル
を所定の組合わせで選択的に作動させ、タービン
への流量とコンプレツサ出口側の抵抗とをエンジ
ン実装時の各種運転状態に対する値にシユミレー
トして、ターボチヤージヤの過給特性を測定出
来、且つソニツクノズルを用いるため動作が定し
て、実装時との相関性の高い正確な過給特性が測
定される効果を有する。
In this way, according to the present invention, the turbine is driven by flowing compressed air through the exhaust side passage, and workability and safety are improved, and the settings are different between the exhaust side passage and the intake side passage. A plurality of sonic nozzles are arranged, and the sonic nozzles in both passages are selectively operated in a predetermined combination to simulate the flow rate to the turbine and the resistance at the compressor outlet side to values corresponding to various operating conditions when the engine is installed. Therefore, the supercharging characteristics of the turbocharger can be measured, and since the sonic nozzle is used, the operation is constant, and accurate supercharging characteristics with high correlation with the time of mounting can be measured.

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

図面は本発明装置の1例の系統線図である。 A……ターボチヤージヤ、T……タービン、C
……コンプレツサ、2……排気側通路、3……吸
気側通路、4……圧搾空気源、7,8……ソニツ
クノズル。
The drawing is a system diagram of an example of the device of the present invention. A...Turbo charger, T...Turbine, C
...Compressor, 2...Exhaust side passage, 3...Intake side passage, 4...Compressed air source, 7, 8...Sonic nozzle.

Claims (1)

【特許請求の範囲】[Claims] 1 ターボチヤージヤのタービンとコンプレツサ
とを各介在させる排気側と吸気側の通路を備え、
該タービンを該排気側通路に流す気体で回転駆動
して、該コンプレツサに流れる空気流量や圧縮比
を測定するようにしたターボチヤージヤの過給特
性測定装置において、該排気側通路の上流端を圧
搾空気源に接続して該タービンを該空気源からの
圧搾空気で回転駆動するようにし、該排気側通路
の該タービンの入口上流側と、該吸気側通路の該
コンプレツサの出口下流側とに夫々設定の異る複
数のソニツクノズルを配置して、該両通路のソニ
ツクノズルを互に所定の組合せで選択的に作動さ
せるようにしたことを特徴とするターボチヤージ
ヤの過給特性測定装置。
1. It is provided with passages on the exhaust side and the intake side in which the turbine and compressor of the turbocharger are interposed, respectively,
In a turbocharger supercharging characteristic measuring device that measures the flow rate and compression ratio of air flowing to the compressor by rotationally driving the turbine with gas flowing through the exhaust side passage, the upstream end of the exhaust side passage is driven by compressed air. The turbine is connected to a power source so that the turbine is rotationally driven by compressed air from the air source, and is set respectively at the upstream side of the inlet of the turbine in the exhaust side passage and the downstream side of the outlet of the compressor in the intake side passage. 1. An apparatus for measuring supercharging characteristics of a turbocharger, characterized in that a plurality of sonic nozzles having different characteristics are arranged, and the sonic nozzles in both passages are selectively operated in a predetermined combination.
JP11813782A 1982-07-07 1982-07-07 TAABOCHAAJANOKAKYUTOKUSEISOKUTEISOCHI Expired - Lifetime JPH0240180B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11813782A JPH0240180B2 (en) 1982-07-07 1982-07-07 TAABOCHAAJANOKAKYUTOKUSEISOKUTEISOCHI

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11813782A JPH0240180B2 (en) 1982-07-07 1982-07-07 TAABOCHAAJANOKAKYUTOKUSEISOKUTEISOCHI

Publications (2)

Publication Number Publication Date
JPS599538A JPS599538A (en) 1984-01-18
JPH0240180B2 true JPH0240180B2 (en) 1990-09-10

Family

ID=14728966

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11813782A Expired - Lifetime JPH0240180B2 (en) 1982-07-07 1982-07-07 TAABOCHAAJANOKAKYUTOKUSEISOKUTEISOCHI

Country Status (1)

Country Link
JP (1) JPH0240180B2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5164203A (en) * 1985-02-13 1992-11-17 Mitsubishi Denki Kabushiki Kaisha Plastic molding device for a semiconductor element
KR100925914B1 (en) 2007-10-23 2009-11-09 현대자동차주식회사 Turbo charger tester

Also Published As

Publication number Publication date
JPS599538A (en) 1984-01-18

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