JP2006348940A - Exhaust-driven supercharger of internal combustion engine - Google Patents

Exhaust-driven supercharger of internal combustion engine Download PDF

Info

Publication number
JP2006348940A
JP2006348940A JP2006164428A JP2006164428A JP2006348940A JP 2006348940 A JP2006348940 A JP 2006348940A JP 2006164428 A JP2006164428 A JP 2006164428A JP 2006164428 A JP2006164428 A JP 2006164428A JP 2006348940 A JP2006348940 A JP 2006348940A
Authority
JP
Japan
Prior art keywords
inlet chamber
exhaust
cleaning nozzle
turbine
internal combustion
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
JP2006164428A
Other languages
Japanese (ja)
Other versions
JP5063937B2 (en
Inventor
Michael Spengler
シュプレングラー ミヒァエル
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.)
MAN Energy Solutions France SAS
Original Assignee
MAN Diesel SA
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 MAN Diesel SA filed Critical MAN Diesel SA
Publication of JP2006348940A publication Critical patent/JP2006348940A/en
Application granted granted Critical
Publication of JP5063937B2 publication Critical patent/JP5063937B2/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/002Cleaning of turbomachines
    • 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
    • F02B39/16Other safety measures for, or other control of, pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/40Application in turbochargers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supercharger (AREA)
  • Exhaust Silencers (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To provide an exhaust-driven supercharger of an internal combustion engine comprising a turbine expanding an exhaust gas flow from the engine of the internal combustion engine and a compressor for compressing a combustion air flow to be supplied to the engine of the internal combustion engine, and having an inlet chamber 10 formed as a bend to introduce the exhaust gas flow to be expanded in the turbine into a turbine rotor, and a washing nozzle installed in the inlet chamber 10 to supply a washing medium to the inlet chamber 10 at a low engine load operating point. <P>SOLUTION: The washing nozzle is disposed on a line or a straight line aligned with the rotating axis 14 of the turbine rotor. <P>COPYRIGHT: (C)2007,JPO&INPIT

Description

本発明は請求項1の前文に記載の内燃機関の排気駆動過給機に関する。   The present invention relates to an exhaust-drive supercharger for an internal combustion engine according to the preamble of claim 1.

内燃機関の効率を高めるために、内燃機関に排気駆動過給機を装備することが既に従来において知られている。排気駆動過給運転ないしターボチャージ運転の場合、エンジンから出る排気ガスが排気駆動過給機のタービンにおいて膨張され、その際、タービンがエンジンに供給すべき燃焼空気を圧縮する圧縮機を駆動する。その圧縮済み燃焼空気を所定の温度に冷却するために、排気駆動過給機の圧縮機とエンジンとの間にインタクーラ(過給空気冷却器)が挿入接続されている。そのような排気駆動過給運転ないしターボチャージ運転によって、内燃機関の効率が向上される。   In order to increase the efficiency of an internal combustion engine, it is already conventionally known to equip an internal combustion engine with an exhaust-drive supercharger. In the case of the exhaust drive supercharging operation or the turbo charge operation, the exhaust gas emitted from the engine is expanded in the turbine of the exhaust drive supercharger, and the turbine drives a compressor that compresses the combustion air to be supplied to the engine. In order to cool the compressed combustion air to a predetermined temperature, an intercooler (supercharged air cooler) is inserted and connected between the compressor of the exhaust drive supercharger and the engine. The efficiency of the internal combustion engine is improved by such an exhaust drive supercharging operation or turbocharge operation.

排気駆動過給機のタービンは、タービン内で膨張すべきエンジンの排気ガス流をタービンロータに導入するために、入口室(流入ハウジング)を利用している。二サイクルエンジンの場合、その入口室はベンド(曲がり管)として形成される。タービン内で膨張された排気ガス流は排気室(流出ハウジング)を通してタービンから排出される。排気駆動過給機を洗浄するために、従来実際に、低いエンジン負荷運転点で排気駆動過給機の入口室に洗浄媒体を導入することが知られ、そのために、実際に1つあるいは複数の洗浄ノズルが用いられる。それらの洗浄ノズルは従来において入口室に不定位置ないし任意位置に付設されている。このために、洗浄ノズルの具体的位置に関係して、種々の配管敷設が必要である。   The turbine of an exhaust drive supercharger utilizes an inlet chamber (inflow housing) to introduce an exhaust gas flow of an engine to be expanded in the turbine into the turbine rotor. In the case of a two-cycle engine, the inlet chamber is formed as a bend. The exhaust gas stream expanded in the turbine is exhausted from the turbine through an exhaust chamber (outflow housing). In order to clean the exhaust-driven supercharger, it is conventionally known to introduce a cleaning medium into the inlet chamber of the exhaust-driven supercharger in practice, at a low engine load operating point, so that actually one or more A cleaning nozzle is used. These cleaning nozzles are conventionally attached to the inlet chamber at an indefinite or arbitrary position. For this reason, various piping laying is necessary in relation to the specific position of the cleaning nozzle.

上述の点から出発して、本発明の課題は、内燃機関の新しい排気駆動過給機を提供することにある。   Starting from the above points, an object of the present invention is to provide a new exhaust-drive supercharger for an internal combustion engine.

この課題は請求項1に記載の内燃機関の排気駆動過給機によって解決される。本発明に基づいて、洗浄ノズルが、タービンロータの回転軸線と一致する線上ないし直線上に配置されている。   This problem is solved by the exhaust-drive supercharger for an internal combustion engine according to claim 1. According to the invention, the cleaning nozzle is arranged on a line or a straight line that coincides with the rotational axis of the turbine rotor.

本発明の目的において、洗浄ノズルを入口室に所定の位置に付設すること、詳しくは、タービンロータないし排気駆動過給機の延長回転軸線が入口室ないしベンドの壁と交差する位置に付設することを提案する。それに応じて、洗浄ノズルは、タービンロータの回転軸線と一致する線上ないし直線上に配置され、即ち、その直線が入口室の壁と交差する場所に配置されている。これによって、ベンドとして形成された入口室の角度位置に相当するいわゆる接続短管位置に無関係に、洗浄ノズルに対する常に同じ接続管敷設を利用することが可能となる。   For the purpose of the present invention, the cleaning nozzle is attached to the inlet chamber at a predetermined position, more specifically, the extended rotation axis of the turbine rotor or the exhaust drive supercharger is attached to the inlet chamber or the bend wall. Propose. Accordingly, the cleaning nozzle is arranged on a line or straight line that coincides with the axis of rotation of the turbine rotor, i.e., where the straight line intersects the wall of the inlet chamber. This makes it possible to always use the same connecting pipe laying for the cleaning nozzle, irrespective of the so-called connecting short pipe position corresponding to the angular position of the inlet chamber formed as a bend.

本発明の有利な実施態様において、入口室に、タービンロータの回転軸線と一致する線上ないし直線上に配置された唯一の洗浄ノズルが付設されている。その場合、洗浄媒体を入口室に流入する洗浄ノズルの出口領域ないし出口孔は、入口室の内面に対してほぼ垂直に延びている。洗浄ノズルの出口領域ないし出口孔の長手軸線および洗浄ノズルが配置された延長回転軸線は、入口室に注入された洗浄媒体が入口室を貫流する排気ガス流によって転向された後で入口室のバルブ形デフレクタに衝突するように、互いに角度を成している。その角度は好適には30°〜35°である。   In a preferred embodiment of the invention, the inlet chamber is provided with a single cleaning nozzle which is arranged on a line or a straight line that coincides with the rotational axis of the turbine rotor. In that case, the outlet region or outlet hole of the cleaning nozzle for flowing the cleaning medium into the inlet chamber extends substantially perpendicular to the inner surface of the inlet chamber. The longitudinal axis of the outlet region or outlet hole of the cleaning nozzle and the extended rotational axis in which the cleaning nozzle is arranged are the valves of the inlet chamber after the cleaning medium injected into the inlet chamber is turned by the exhaust gas flow flowing through the inlet chamber They are angled with respect to each other so as to collide with the shape deflector. The angle is preferably 30 ° to 35 °.

本発明の有利な実施態様は従属請求項および以下の説明から理解できる。次に図を参照して本発明の実施例を詳細に説明するが、本発明はこれに限定されるものではない。   Advantageous embodiments of the invention can be seen from the dependent claims and the following description. Next, examples of the present invention will be described in detail with reference to the drawings, but the present invention is not limited to these.

以下図1〜図3を参照して本発明を詳細に説明する。   Hereinafter, the present invention will be described in detail with reference to FIGS.

図1には、排気駆動過給機のいわゆる90°ベンド(曲がり管)として形成された入口室(流入ハウジング)10が断面図で示されている。その場合、排気ガス流が入口開口11を通して入口室10に導入され90°転向されて入口室10のバルブ(電球)形デフレクタ12に到達する。バルブ形デフレクタ12の領域において、排気ガス流はもう一度転向され、いわゆる環状ノズル13を通して、バルブ形デフレクタ12の下流側に位置された排気駆動過給機のタービンロータ(図示せず)に向けて導かれる。タービンロータの領域で膨張された排気ガスは、入口室10につながる排気室(図示せず)を通して排気駆動過給機から排出される。タービンロータについてその回転軸線14しか示されていない。そのタービンロータは軸を介して排気駆動過給機の圧縮機ロータに連結され、この圧縮機ロータを駆動する。   FIG. 1 shows a sectional view of an inlet chamber (inflow housing) 10 formed as a so-called 90 ° bend (bent tube) of an exhaust-driven supercharger. In that case, the exhaust gas flow is introduced into the inlet chamber 10 through the inlet opening 11 and turned 90 ° to reach the bulb (bulb) -shaped deflector 12 in the inlet chamber 10. In the region of the valve deflector 12, the exhaust gas flow is once again turned and directed through a so-called annular nozzle 13 towards the turbine rotor (not shown) of the exhaust-driven supercharger located downstream of the valve deflector 12. It is burned. The exhaust gas expanded in the region of the turbine rotor is discharged from the exhaust driving supercharger through an exhaust chamber (not shown) connected to the inlet chamber 10. Only the axis of rotation 14 is shown for the turbine rotor. The turbine rotor is connected to a compressor rotor of an exhaust drive supercharger via a shaft, and drives the compressor rotor.

既に述べたように、入口室10は90°ベンドとして形成され、それに応じて、湾曲壁15を有している。低いエンジン負荷運転点で排気駆動過給機を洗浄するために洗浄媒体つまり洗浄水を入口室10に注入するために、入口室10の壁15に、図1および図2に示されていない洗浄ノズルが付設されている。図1および図2には洗浄ノズルのホルダ16しか示されていない。そのホルダ16は壁15にねじ止めされ、洗浄ノズルを受けるための孔17を規定している。   As already mentioned, the inlet chamber 10 is formed as a 90 ° bend and has a curved wall 15 accordingly. Washing not shown in FIGS. 1 and 2 on the wall 15 of the inlet chamber 10 for injecting a cleaning medium or wash water into the inlet chamber 10 to clean the exhaust-driven supercharger at low engine load operating points A nozzle is attached. Only the holder 16 of the cleaning nozzle is shown in FIGS. The holder 16 is screwed to the wall 15 and defines a hole 17 for receiving a cleaning nozzle.

本発明の目的において、洗浄ノズルはタービンロータの延長回転軸線14上に配置され、詳しくは、タービンロータの延長回転軸線14が入口室10の壁15と交差する場所に配置されている。ここで本発明の目的において、入口室10に唯一の洗浄ノズルが付設されている。この洗浄ノズルは、図1および図2の実施例において、タービンロータの延長回転軸線14が壁15と交差する位置で壁15にねじ止めされたホルダ16に収納されている。それに応じて、洗浄ノズルはタービンロータの回転軸線14と一致する直線上ないし線上に配置されている。   For the purposes of the present invention, the cleaning nozzle is disposed on the turbine rotor's extended rotational axis 14, in particular, where the turbine rotor's extended rotational axis 14 intersects the wall 15 of the inlet chamber 10. Here, for the purpose of the present invention, a single cleaning nozzle is attached to the inlet chamber 10. 1 and 2, the cleaning nozzle is accommodated in a holder 16 screwed to the wall 15 at a position where the extended rotation axis 14 of the turbine rotor intersects the wall 15. Accordingly, the cleaning nozzle is arranged on a straight line or line that coincides with the rotational axis 14 of the turbine rotor.

図1および図2の実施例において、図示されていない洗浄ノズルはホルダ16の孔17の中に、洗浄媒体を入口室10に流入ないし注入する洗浄ノズルの出口領域ないし出口孔が、入口室10の壁15の内面18に対してほぼ垂直に延びているように、収納されている。図1および図2の実施例において、ホルダ16ないし孔17の長手軸線19と一致している洗浄ノズルの出口孔の長手軸線は、タービンロータの延長回転軸線14に対して、入口室10に注入された洗浄媒体が入口室を貫流する排気ガス流により転向ないし引き連れられた後、入口室10のバルブ形デフレクタ12に衝突し、そのバルブ形デフレクタ12への衝突によって霧化されるように、角度αを成している。   In the embodiment of FIGS. 1 and 2, the cleaning nozzle (not shown) has an outlet region or outlet hole of the cleaning nozzle through which the cleaning medium flows into or injects into the inlet chamber 10 in the hole 17 of the holder 16. The wall 15 is accommodated so as to extend substantially perpendicular to the inner surface 18 of the wall 15. In the embodiment of FIGS. 1 and 2, the longitudinal axis of the outlet hole of the cleaning nozzle, which coincides with the longitudinal axis 19 of the holder 16 or hole 17, is injected into the inlet chamber 10 with respect to the extended rotational axis 14 of the turbine rotor. So that the cleaned cleaning medium is turned or drawn by the exhaust gas flow flowing through the inlet chamber and then collides with the valve-shaped deflector 12 of the inlet chamber 10 and is atomized by the collision with the valve-shaped deflector 12. α is formed.

その洗浄ノズルの出口孔の長手軸線19は、タービンロータの延長回転軸線14と20°〜40°の角度α、特に30°〜35°の角度αを成している。有利な実施例においてその角度αは約33°である。   The longitudinal axis 19 of the outlet hole of the cleaning nozzle forms an angle α of 20 ° to 40 °, in particular an angle α of 30 ° to 35 °, with the extended axis of rotation 14 of the turbine rotor. In the preferred embodiment, the angle α is about 33 °.

図1および図2の実施例において、洗浄ノズルのホルダ16は別個の部品として形成され、入口室10の壁15にねじ止めされている。このホルダ16に、即ちその孔17の中に、洗浄ノズルがはめ込まれている。   In the embodiment of FIGS. 1 and 2, the cleaning nozzle holder 16 is formed as a separate piece and is screwed to the wall 15 of the inlet chamber 10. A cleaning nozzle is fitted in the holder 16, that is, in the hole 17.

図1および図2の実施例と異なって、図3には、洗浄ノズルのホルダ16が壁15と一体構造部品であり、即ち、入口室10の壁15に一体鋳造されている実施例が示されている。洗浄ノズルはホルダ16に設けられた孔20、21によって規定され、即ち、入口孔20および出口孔21によって規定されている。その洗浄ノズルの出口孔21の長手軸線19は、既に図1および図2の実施例に関連して述べたように、壁15の内面18に対してほぼ垂直に延び、タービンロータの延長回転軸線14と角度αを成している。これに対して、入口孔20の長手軸線はタービンロータの延長回転軸線14と一致している。   Unlike the embodiment of FIGS. 1 and 2, FIG. 3 shows an embodiment in which the cleaning nozzle holder 16 is an integral part of the wall 15, that is, is integrally cast on the wall 15 of the inlet chamber 10. Has been. The cleaning nozzle is defined by the holes 20 and 21 provided in the holder 16, that is, by the inlet hole 20 and the outlet hole 21. The longitudinal axis 19 of the outlet hole 21 of the cleaning nozzle extends substantially perpendicular to the inner surface 18 of the wall 15, as already described in connection with the embodiment of FIGS. 14 and an angle α. In contrast, the longitudinal axis of the inlet hole 20 coincides with the extended rotation axis 14 of the turbine rotor.

それに応じて本発明の目的において、ベンドとして形成された入口室を有し、この入口室に洗浄ノズルが付設され、その場合、唯一の洗浄ノズルが、タービンロータの回転軸線がベンドとして形成された入口室の壁と交差する位置に配置されている排気駆動過給機を提案する。   Accordingly, for the purposes of the present invention, it has an inlet chamber formed as a bend, and a cleaning nozzle is attached to this inlet chamber, in which case the only cleaning nozzle is formed with the rotational axis of the turbine rotor as a bend. We propose an exhaust-driven supercharger that is located at a position that intersects the wall of the entrance chamber.

洗浄ノズルの出口孔は入口室の壁の内面に対してほぼ垂直に延び、その出口孔の長手軸線はタービンロータの回転軸線と、入口室に注入された洗浄媒体が排気ガス流による方向転換によって入口室のバルブ形デフレクタに衝突し、そのバルブ形デフレクタの領域において霧化されるような角度を成している。洗浄媒体はそれから入口室の環状ノズルの領域に全周にわたって一様に到達する。   The outlet hole of the cleaning nozzle extends substantially perpendicular to the inner surface of the wall of the inlet chamber. The longitudinal axis of the outlet hole is the axis of rotation of the turbine rotor and the direction of the cleaning medium injected into the inlet chamber is changed by the exhaust gas flow. The angle is such that it strikes the valve deflector in the inlet chamber and is atomized in the area of the valve deflector. The cleaning medium then reaches the area of the annular nozzle in the inlet chamber uniformly over the entire circumference.

内燃機関の本発明に基づく排気駆動過給機のタービンの入口室の概略断面図。1 is a schematic sectional view of an inlet chamber of a turbine of an exhaust drive supercharger according to the present invention of an internal combustion engine. 図1の部分IIの詳細図。FIG. 2 is a detailed view of part II of FIG. 1. 異なった実施例の図2に相当した詳細図。FIG. 3 is a detailed view corresponding to FIG. 2 of a different embodiment.

符号の説明Explanation of symbols

10 入口室(流入ハウジング)
11 入口開口
12 バルブ(電球)形デフレクタ
13 環状ノズル
14 回転軸線
15 壁
16 ホルダ
17 孔
18 内面
19 長手軸線
20 入口孔
21 出口孔
10 Inlet chamber (inflow housing)
DESCRIPTION OF SYMBOLS 11 Entrance opening 12 Valve | bulb (light bulb) -shaped deflector 13 Annular nozzle 14 Rotating axis 15 Wall 16 Holder 17 Hole 18 Inner surface 19 Longitudinal axis 20 Inlet hole 21 Outlet

Claims (9)

内燃機関のエンジンから出る排気ガス流を膨張するためのタービンと、内燃機関のエンジンに供給すべき燃焼空気流を圧縮するための圧縮機とを備え、タービン内で膨張すべき排気ガス流をタービンロータに導入するために、タービンがベンドとして形成された入口室(10)を有し、低いエンジン負荷運転点で入口室(10)に洗浄媒体を供給するために、入口室(10)に洗浄ノズルが付設されている内燃機関の排気駆動過給機において、洗浄ノズルが、タービンロータの回転軸線(14)と一致する線上ないし直線上に配置されていることを特徴とする内燃機関の排気駆動過給機。   A turbine for expanding an exhaust gas flow coming out of an engine of an internal combustion engine, and a compressor for compressing a combustion air flow to be supplied to the engine of the internal combustion engine, the exhaust gas flow to be expanded in the turbine being a turbine For introduction into the rotor, the turbine has an inlet chamber (10) formed as a bend, and the inlet chamber (10) is cleaned to supply cleaning medium to the inlet chamber (10) at a low engine load operating point. An exhaust drive supercharger for an internal combustion engine provided with a nozzle, wherein the cleaning nozzle is arranged on a line or a straight line that coincides with the rotational axis (14) of the turbine rotor. Turbocharger. 入口室(10)に、タービンロータの回転軸線(14)と一致する線上ないし直線上に配置された唯一の洗浄ノズルが付設されていることを特徴とする請求項1記載の排気駆動過給機。   The exhaust-drive supercharger according to claim 1, wherein the inlet chamber (10) is provided with a single cleaning nozzle arranged on a line or straight line that coincides with the rotational axis (14) of the turbine rotor. . 洗浄媒体が入口室(10)に流入する洗浄ノズルの出口領域が、入口室(10)の内面(18)に対してほぼ垂直に延びていることを特徴とする請求項1又は2に記載の排気駆動過給機。   3. The outlet region of the cleaning nozzle, into which the cleaning medium flows into the inlet chamber (10), extends substantially perpendicular to the inner surface (18) of the inlet chamber (10). Exhaust-driven supercharger. 洗浄ノズルの出口孔(21)の長手軸線(19)および洗浄ノズルが配置された延長回転軸線(14)が、20°〜40°の角度を成していることを特徴とする請求項3記載の排気駆動過給機。   4. The longitudinal axis (19) of the outlet hole (21) of the cleaning nozzle and the extended rotation axis (14) in which the cleaning nozzle is arranged form an angle of 20 [deg.] To 40 [deg.]. Exhaust-driven supercharger. 洗浄ノズルの出口孔(21)の長手軸線(19)および洗浄ノズルが配置された延長回転軸線(14)が、30°〜35°の角度を成していることを特徴とする請求項4記載の排気駆動過給機。   5. The longitudinal axis (19) of the outlet hole (21) of the cleaning nozzle and the extended rotational axis (14) in which the cleaning nozzle is arranged form an angle of 30 [deg.] To 35 [deg.]. Exhaust-driven supercharger. 洗浄ノズルの出口領域ないし出口孔(21)の長手軸線(19)および洗浄ノズルが配置された延長回転軸線(14)が、入口室(10)に注入された洗浄媒体が入口室(10)によって案内される排気ガス流の方向転換によって入口室(10)のバルブ形デフレクタ(12)に衝突するように、角度を成していることを特徴とする請求項3ないし5のいずれか1つに記載の排気駆動過給機。   The longitudinal axis (19) of the outlet region of the cleaning nozzle or the outlet hole (21) and the extended rotation axis (14) in which the cleaning nozzle is disposed are used to allow the cleaning medium injected into the inlet chamber (10) to be introduced by the inlet chamber (10). 6. An angle according to claim 3, characterized in that it is angled so as to impinge on the valve-shaped deflector (12) of the inlet chamber (10) by changing the direction of the guided exhaust gas flow. Exhaust-driven supercharger as described. 洗浄ノズルが、入口室(10)にねじ止めされたホルダ(16)に収納されていることを特徴とする請求項1ないし6のいずれか1つに記載の排気駆動過給機。   The exhaust-driven supercharger according to any one of claims 1 to 6, characterized in that the cleaning nozzle is housed in a holder (16) screwed into the inlet chamber (10). 洗浄ノズルが、入口室(10)の一体構造部品であるホルダ(16)に収納されていることを特徴とする請求項1ないし6のいずれか1つに記載の排気駆動過給機。   The exhaust-drive supercharger according to any one of claims 1 to 6, wherein the cleaning nozzle is accommodated in a holder (16) which is an integral part of the inlet chamber (10). ホルダ(16)が入口室(10)に一体鋳造され、洗浄ノズルがホルダ(16)に設けられた孔(20、21)によって形成されていることを特徴とする請求項8記載の排気駆動過給機。

The exhaust drive overload according to claim 8, characterized in that the holder (16) is integrally cast in the inlet chamber (10) and the cleaning nozzle is formed by holes (20, 21) provided in the holder (16). Feeder.

JP2006164428A 2005-06-18 2006-06-14 Exhaust-driven supercharger for internal combustion engines Expired - Fee Related JP5063937B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102005028296.2 2005-06-18
DE102005028296A DE102005028296B4 (en) 2005-06-18 2005-06-18 Exhaust gas turbocharger for an internal combustion engine

Publications (2)

Publication Number Publication Date
JP2006348940A true JP2006348940A (en) 2006-12-28
JP5063937B2 JP5063937B2 (en) 2012-10-31

Family

ID=37513428

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2006164428A Expired - Fee Related JP5063937B2 (en) 2005-06-18 2006-06-14 Exhaust-driven supercharger for internal combustion engines

Country Status (5)

Country Link
JP (1) JP5063937B2 (en)
KR (1) KR20060132463A (en)
CN (1) CN1880738B (en)
CH (1) CH698807B1 (en)
DE (1) DE102005028296B4 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014181717A (en) * 2013-03-19 2014-09-29 Abb Turbo Systems Ag Cleaning device of exhaust gas turbine

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8602721B2 (en) * 2009-12-02 2013-12-10 Wartsila Finland Oy Method of operating turbocharged piston engine
EP2722495B1 (en) * 2012-10-17 2015-03-11 ABB Turbo Systems AG Gas entry housing and corresponding exhaust gas turbine
SG10201707125YA (en) * 2017-08-31 2019-03-28 United Technologies Corp Directional water jet cleaning of engine blades

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5844438U (en) * 1981-09-19 1983-03-25 石川島播磨重工業株式会社 Turbine cleaning equipment for non-cooled turbochargers
JPS59119929U (en) * 1982-09-27 1984-08-13 三菱重工業株式会社 Exhaust gas turbine supercharger turbine side cleaning device
JPS6216737U (en) * 1985-07-16 1987-01-31
JPH07269302A (en) * 1994-03-30 1995-10-17 Mitsubishi Heavy Ind Ltd Blade washing method of axial flow compressor and device thereof
JPH0814196A (en) * 1994-06-30 1996-01-16 Hitachi Ltd Gas turbine compressor washing device
JPH08312363A (en) * 1995-05-17 1996-11-26 Niigata Eng Co Ltd Cleaning method and device of exhaust turbosupercharger
JPH10176540A (en) * 1996-12-11 1998-06-30 Asea Brown Boveri Ag Axial turbine for turbosupercharger
JPH10220251A (en) * 1997-02-03 1998-08-18 Nkk Corp Method of eliminating dust stuck to turbine
WO2005049972A1 (en) * 2003-11-24 2005-06-02 Abb Turbo Systems Ag Cleaning device
JP2007146694A (en) * 2005-11-24 2007-06-14 Ishikawajima Harima Heavy Ind Co Ltd Supercharger

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4548040A (en) * 1984-05-11 1985-10-22 Elliott Turbomachinery Company, Inc. Method and apparatus for determining when to initiate cleaning of turbocharger turbine blades
DE3724385A1 (en) * 1987-07-23 1989-02-02 Man B & W Diesel Gmbh Exhaust turbocharger with device for the removal of solids

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5844438U (en) * 1981-09-19 1983-03-25 石川島播磨重工業株式会社 Turbine cleaning equipment for non-cooled turbochargers
JPS59119929U (en) * 1982-09-27 1984-08-13 三菱重工業株式会社 Exhaust gas turbine supercharger turbine side cleaning device
JPS6216737U (en) * 1985-07-16 1987-01-31
JPH07269302A (en) * 1994-03-30 1995-10-17 Mitsubishi Heavy Ind Ltd Blade washing method of axial flow compressor and device thereof
JPH0814196A (en) * 1994-06-30 1996-01-16 Hitachi Ltd Gas turbine compressor washing device
JPH08312363A (en) * 1995-05-17 1996-11-26 Niigata Eng Co Ltd Cleaning method and device of exhaust turbosupercharger
JPH10176540A (en) * 1996-12-11 1998-06-30 Asea Brown Boveri Ag Axial turbine for turbosupercharger
JPH10220251A (en) * 1997-02-03 1998-08-18 Nkk Corp Method of eliminating dust stuck to turbine
WO2005049972A1 (en) * 2003-11-24 2005-06-02 Abb Turbo Systems Ag Cleaning device
JP2007146694A (en) * 2005-11-24 2007-06-14 Ishikawajima Harima Heavy Ind Co Ltd Supercharger

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014181717A (en) * 2013-03-19 2014-09-29 Abb Turbo Systems Ag Cleaning device of exhaust gas turbine

Also Published As

Publication number Publication date
DE102005028296A1 (en) 2006-12-28
CH698807B1 (en) 2009-10-30
CN1880738A (en) 2006-12-20
JP5063937B2 (en) 2012-10-31
CN1880738B (en) 2011-07-06
KR20060132463A (en) 2006-12-21
DE102005028296B4 (en) 2007-03-29

Similar Documents

Publication Publication Date Title
JP4309446B2 (en) Piston internal combustion engine
ATE426090T1 (en) TURBO COMPRESSOR SYSTEM FOR AN INTERNAL COMBUSTION ENGINE HAVING A CENTRAL COMPRESSOR PROVIDED WITH AN IMPELLER WITH SHARED BLADES
KR20160083964A (en) Compressor of an exhaust-gas turbocharger
JP2009047163A (en) Internal combustion engine system having power turbine with broad efficiency range
JP2006529016A5 (en)
JP5369723B2 (en) Centrifugal compressor
EP1903184A3 (en) Combustion transition duct providing stage 1 tangential turning for turbine engines
JP2010101320A (en) Inlet system for egr system
KR101907139B1 (en) Noise reduction type intake / exhaust device for enhancing output of internal combustion engine
JP2008157235A (en) Low-restriction turbine outlet housing
RU2007129434A (en) TWO-CIRCUIT TURBOCHARGE WITH INDIRECT CHANGE OF THE NECK FOR THE EXHAUST OF GASES
JP2012107551A (en) Low-pressure-loop egr device
US20090196739A1 (en) Axial flow fluid device
JP5063937B2 (en) Exhaust-driven supercharger for internal combustion engines
KR100853583B1 (en) Counterflow control circulation exhaust device of engine
RU2006110656A (en) GAS TURBINE ENGINE
EA022179B1 (en) A turbocharger with an increasing cross-section exhaust casing and a method for turbocharging
KR20060038317A (en) Exhaust for automobile
US6360731B1 (en) Axial-type supercharger
KR20180120757A (en) A turbine structure comprising a continuously decreasing flow area having a continuously decreasing valley
JP2006348939A (en) Exhaust-driven supercharger of internal combustion engine
CN110080830A (en) A kind of radial-flow type supercharging device of included back disk impinging cooling
US10920719B2 (en) Internal combustion engine
JP2010281281A (en) Supercharger and multistage supercharging device having the same
CN2816359Y (en) Gas intaking shell for wormgear booster

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20090415

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20101109

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20101111

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20110208

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20110705

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20111004

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20120124

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20120417

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20120710

A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20120808

R150 Certificate of patent or registration of utility model

Ref document number: 5063937

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

Free format text: JAPANESE INTERMEDIATE CODE: R150

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20150817

Year of fee payment: 3

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

S533 Written request for registration of change of name

Free format text: JAPANESE INTERMEDIATE CODE: R313533

R350 Written notification of registration of transfer

Free format text: JAPANESE INTERMEDIATE CODE: R350

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

LAPS Cancellation because of no payment of annual fees