JP6483372B2 - Valve assembly for a fuel supply device and fuel supply device - Google Patents

Valve assembly for a fuel supply device and fuel supply device Download PDF

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JP6483372B2
JP6483372B2 JP2014161100A JP2014161100A JP6483372B2 JP 6483372 B2 JP6483372 B2 JP 6483372B2 JP 2014161100 A JP2014161100 A JP 2014161100A JP 2014161100 A JP2014161100 A JP 2014161100A JP 6483372 B2 JP6483372 B2 JP 6483372B2
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pressure
fuel supply
valve
supply device
pressure region
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JP2015034552A (en
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クリスティアン・モンツェルト
アンドレアス・シュティッヒノート
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MAN Energy Solutions SE
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M63/00Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
    • F02M63/0012Valves
    • F02M63/0031Valves characterized by the type of valves, e.g. special valve member details, valve seat details, valve housing details
    • F02M63/005Pressure relief valves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M63/00Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
    • F02M63/02Fuel-injection apparatus having several injectors fed by a common pumping element, or having several pumping elements feeding a common injector; Fuel-injection apparatus having provisions for cutting-out pumps, pumping elements, or injectors; Fuel-injection apparatus having provisions for variably interconnecting pumping elements and injectors alternatively
    • F02M63/0225Fuel-injection apparatus having a common rail feeding several injectors ; Means for varying pressure in common rails; Pumps feeding common rails
    • F02M63/023Means for varying pressure in common rails
    • F02M63/026Means for reducing the pressure in common rails at power off

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Fluid-Pressure Circuits (AREA)

Description

本発明は、内燃機関の燃料供給装置のための弁アセンブリに関する。本発明はさらに、当該弁アセンブリを有する燃料供給装置に関する。   The present invention relates to a valve assembly for a fuel supply device of an internal combustion engine. The present invention further relates to a fuel supply apparatus having the valve assembly.

コモンレール燃料供給装置の基本的な構成は、特許文献1から知られている。コモンレール燃料供給装置は、内燃機関のシリンダごとに、それぞれ少なくとも1つのインジェクタを含んでいる。これらのインジェクタを通して、内燃機関のシリンダのそれぞれに、燃料が噴射可能である。さらに、コモンレール燃料供給装置は、燃料をコモンレール燃料供給装置の低圧領域から高圧領域へ運ぶために、少なくとも1つの低圧ポンプと、少なくとも1つの高圧ポンプと、少なくとも1つの高圧貯蔵装置とを含んでおり、ポンプ装置とインジェクタとの間の高圧領域には、永久に高圧下にある蓄圧システムが設けられている。この永久に高圧下にある蓄圧システムは、コモンレールとも称され、1つ又は複数の貯蔵ユニットを有している。これらの貯蔵ユニットは、永久に高圧下にある高圧導管を通じて、ポンプ装置と接続されていると共に、互いに接続されている。蓄圧システム、すなわち貯蔵ユニットは、さらに、噴射時期に応じて一時的に高圧になる高圧導管を通じてインジェクタと接続されている。インジェクタを貯蔵ユニットと接続する、噴射時期に応じて一時的に高圧になる高圧導管には、切換弁が配設されており、当該切換弁は、噴射時期に応じてインジェクタに燃料を供給する。   The basic configuration of the common rail fuel supply apparatus is known from Patent Document 1. The common rail fuel supply apparatus includes at least one injector for each cylinder of the internal combustion engine. Through these injectors, fuel can be injected into each cylinder of the internal combustion engine. Further, the common rail fuel supply device includes at least one low pressure pump, at least one high pressure pump, and at least one high pressure storage device for transporting fuel from the low pressure region of the common rail fuel supply device to the high pressure region. In the high pressure region between the pump device and the injector, a pressure accumulating system that is permanently under high pressure is provided. This permanent high pressure storage system, also called common rail, has one or more storage units. These storage units are connected to the pump device and to each other through a high-pressure conduit that is permanently under high pressure. The pressure accumulating system, that is, the storage unit, is further connected to the injector through a high-pressure conduit that temporarily becomes high pressure according to the injection timing. A switching valve is disposed in a high-pressure conduit that connects the injector to the storage unit and temporarily becomes high pressure according to the injection timing, and the switching valve supplies fuel to the injector according to the injection timing.

特許文献1からは、蓄圧システムの貯蔵ユニットの内1つには、安全弁及び逃し弁が配設されていることが知られている。安全弁と逃し弁とは、共に1つの負荷軽減装置を形成する。安全弁及び逃し弁は、唯一の弁要素によっても実現され得る。逃し弁を通じて、原動機を停止した後、燃料供給装置からタンクに向けて除去することが可能であり、特許文献1によると、逃し弁の作動は、固有の制御媒体を通じて、空気圧又は油圧又は電磁気を用いて行われる。   From Patent Document 1, it is known that a safety valve and a relief valve are arranged in one of the storage units of the pressure accumulating system. Together, the safety valve and the relief valve form one load reducing device. Safety valves and relief valves can also be realized with a single valve element. After stopping the prime mover through the relief valve, it is possible to remove it from the fuel supply device toward the tank. According to Patent Document 1, the operation of the relief valve is performed by the pneumatic, hydraulic or electromagnetic through the inherent control medium. Done with.

独国特許発明第10157135号明細書German Patent Invention No. 10157135

ここから出発して、本発明の課題は、燃料供給装置のための新式の弁アセンブリと、当該弁アセンブリを有する燃料供給装置とを創出することにある。   Starting from here, the object of the present invention is to create a new valve assembly for a fuel supply device and a fuel supply device having the valve assembly.

本課題は、請求項1に記載の弁アセンブリによって解決される。本発明に係る弁アセンブリは、パイロット弁、主弁及び圧力調整弁を有しており、主弁は、圧力接続部によって、燃料供給装置の高圧領域と接続可能であり、パイロット弁と圧力調整弁とは、圧力接続部によって、燃料供給装置の低圧領域と接続可能である。すなわち、パイロット弁、主弁及び圧力調整弁は、低圧領域における圧力に応じて、及び/又は、高圧領域における圧力に応じて自動的に作動され得るように接続可能である。   This problem is solved by a valve assembly according to claim 1. The valve assembly according to the present invention includes a pilot valve, a main valve, and a pressure regulating valve, and the main valve can be connected to a high pressure region of the fuel supply device by a pressure connecting portion. Can be connected to the low pressure region of the fuel supply device by means of a pressure connection. That is, the pilot valve, the main valve, and the pressure regulating valve can be connected so that they can be automatically actuated according to the pressure in the low pressure region and / or according to the pressure in the high pressure region.

本発明に係る弁アセンブリは、内燃機関を停止した後、又は、燃料供給装置の低圧ポンプを停止した後の、燃料供給装置の高圧領域の自動的な負荷軽減を機械を用いた方法で可能にするので、空気圧による又は電磁気による又はその他の方法による作動は必要としない。   The valve assembly according to the present invention enables automatic load reduction in the high pressure region of the fuel supply device after stopping the internal combustion engine or after stopping the low pressure pump of the fuel supply device by a method using a machine. Thus, it does not require operation by air pressure, electromagnetic or other methods.

したがって、原動機を停止した後の、制御装置による作動を行わない、燃料供給装置の自動的な減圧が可能になる。制御媒体として、燃料供給装置に存在する燃料の圧力が用いられる。燃料供給装置の減圧は、本発明に係る弁アセンブリを用いて数秒の内に行われ得る。それゆえ、燃料供給装置のインジェクタは、摩耗から効果的に保護され得る。   Therefore, after the prime mover is stopped, the fuel supply device can be automatically depressurized without being operated by the control device. As the control medium, the pressure of the fuel existing in the fuel supply apparatus is used. The depressurization of the fuel supply device can be performed within a few seconds using the valve assembly according to the present invention. Therefore, the injector of the fuel supply device can be effectively protected from wear.

有利なさらなる構成によると、圧力調整弁は、圧力接続部によって、燃料供給装置の低圧領域と、低圧領域に動作圧力が加えられている場合に圧力調整弁がバネ要素の調整可能な弾力に反して自動的に開口するように接続され得る。パイロット弁は、第1の圧力接続部によって、燃料供給装置の低圧領域と、及び、第2の圧力接続部によって、少なくとも1つのチョークを介して燃料供給装置の高圧領域と、低圧領域及び高圧領域に動作圧力が加えられている場合にパイロット弁が自動的に閉口するように接続され得る。主弁は、圧力接続部によって、燃料供給装置の高圧領域と、高圧領域に動作圧力が加えられる前に主弁が自動的に閉口するように接続され得る。そうすると、燃料供給装置の低圧領域における動作圧力が低圧ポンプの停止によって低下した場合に、パイロット弁及び主弁が自動的に開口するので、高圧領域から燃料タンクに向けて除去することができる。このパイロット弁、主弁及び圧力調整弁の接続は好ましいものであり、少ない費用で、内燃機関の停止後又は燃料供給装置の低圧ポンプの停止後における、制御機器による外部からの作動を行わない、燃料噴射システムの機械による自動的な減圧を可能にする。   According to a further advantageous configuration, the pressure regulating valve is operated by the pressure connection so that the pressure regulating valve is against the adjustable elasticity of the spring element when operating pressure is applied to the low pressure region of the fuel supply device and to the low pressure region. And can be connected to automatically open. The pilot valve has a low pressure region of the fuel supply device by the first pressure connection, and a high pressure region, a low pressure region and a high pressure region of the fuel supply device by at least one choke by the second pressure connection. The pilot valve may be connected to automatically close when operating pressure is applied to the valve. The main valve may be connected by a pressure connection to the high pressure region of the fuel supply device so that the main valve automatically closes before operating pressure is applied to the high pressure region. Then, when the operating pressure in the low pressure region of the fuel supply device decreases due to the stop of the low pressure pump, the pilot valve and the main valve are automatically opened, so that it can be removed from the high pressure region toward the fuel tank. The connection of the pilot valve, the main valve and the pressure regulating valve is preferable, and the external operation by the control device is not performed after the stop of the internal combustion engine or the low pressure pump of the fuel supply device at a low cost. Allows automatic depressurization of the fuel injection system.

本発明に係る燃料供給装置は、請求項9に規定されている。本発明の好ましいさらなる構成は、下位請求項及び以下の説明から明らかである。本発明の実施例は、図面を用いて詳細に説明されるが、当該図面に限定されるものではない。   A fuel supply apparatus according to the present invention is defined in claim 9. Preferred further configurations of the invention are evident from the subclaims and the following description. Embodiments of the present invention will be described in detail with reference to the drawings, but are not limited to the drawings.

本発明に係る燃料供給装置のための弁アセンブリの概略図である。1 is a schematic view of a valve assembly for a fuel supply apparatus according to the present invention.

本発明は、好ましくは大型ディーゼルエンジン又は船舶用ディーゼルエンジンとして構成された内燃機関の燃料供給装置の弁アセンブリと燃料供給装置、特にコモンレール燃料供給装置とに関する。   The present invention relates to a valve assembly and a fuel supply device, in particular a common rail fuel supply device, for a fuel supply device of an internal combustion engine, preferably configured as a large diesel engine or a marine diesel engine.

内燃機関のコモンレール燃料供給装置として構成された燃料供給装置の基本的な構成は、当業者にはよく知られており、すでに特許文献1からも知られている。本発明は、内燃機関の始動に際して、及び、内燃機関が動き始めた後、燃料供給装置の低圧領域及び高圧領域の両方において、所定の動作圧力の調整を支援し、原動機又は低圧ポンプの停止後は、燃料供給装置の機械による自動的な減圧を可能にするような燃料供給装置のための弁アセンブリに関する。   The basic configuration of a fuel supply device configured as a common rail fuel supply device for an internal combustion engine is well known to those skilled in the art, and is already known from Patent Document 1. The present invention supports the adjustment of a predetermined operating pressure at the start of the internal combustion engine and after the internal combustion engine starts to move, both in the low pressure region and the high pressure region of the fuel supply device, and after the prime mover or the low pressure pump is stopped. Relates to a valve assembly for a fuel supply device that allows automatic depressurization by the machine of the fuel supply device.

図1は、本発明に係る船舶用ディーゼルエンジンとして構成された内燃機関の燃料供給装置、特にコモンレール燃料供給装置のための弁アセンブリ10のブロック図である。弁アセンブリ10は、パイロット弁11、主弁12及び圧力調整弁13を含んでいる。図1の弁アセンブリ10は、内燃機関の燃料供給装置の低圧領域14にも高圧領域15にも接続され得る。   FIG. 1 is a block diagram of a valve assembly 10 for a fuel supply device for an internal combustion engine, particularly a common rail fuel supply device, configured as a marine diesel engine according to the present invention. The valve assembly 10 includes a pilot valve 11, a main valve 12 and a pressure regulating valve 13. The valve assembly 10 of FIG. 1 can be connected to both the low pressure region 14 and the high pressure region 15 of the fuel supply system of the internal combustion engine.

図1の実施例において2/2方向制御弁として構成されている主弁12は、2つの圧力接続部16及び17を有している。両方の圧力接続部16及び17によって、主弁12を燃料供給装置の高圧領域15に接続することが可能であり、両方の圧力接続部16及び17は、その押圧面に関して異なっている。チョーク18を介して燃料供給装置の高圧領域15に接続され得る第1の圧力接続部16は、主弁12の第2の圧力接続部17よりも大きな押圧面を有しており、主弁12は、圧力接続部17を通じて、チョークを介することなく燃料供給装置の高圧領域15に直接接続され得る。燃料供給装置の高圧領域15が非加圧の場合、バネ要素19は主弁12を図1に示した閉口位置に押圧する。このバネ要素19は、比較的少ない弾力を有するように構成され得る。なぜなら、バネ要素19は実質的には、非加圧状態における主弁12の位置決めにのみ用いられるからである。高圧領域15内に少なくとも1つの高圧ポンプによって動作圧力が加えられる場合、主弁12の第1の圧力接続部16が圧力接続部17よりも大きい押圧面を有するということによって、主弁12も同様に図1に示された閉口位置に押圧される。   The main valve 12, which is configured as a 2/2 direction control valve in the embodiment of FIG. 1, has two pressure connections 16 and 17. Both pressure connections 16 and 17 make it possible to connect the main valve 12 to the high pressure region 15 of the fuel supply device, both pressure connections 16 and 17 being different with respect to their pressing surfaces. The first pressure connection 16 that can be connected to the high pressure region 15 of the fuel supply device via the choke 18 has a larger pressing surface than the second pressure connection 17 of the main valve 12, and the main valve 12. Can be directly connected to the high pressure region 15 of the fuel supply device through the pressure connection 17 without a choke. When the high pressure region 15 of the fuel supply device is not pressurized, the spring element 19 presses the main valve 12 to the closed position shown in FIG. The spring element 19 can be configured to have relatively little elasticity. This is because the spring element 19 is substantially used only for positioning the main valve 12 in the non-pressurized state. When the operating pressure is applied by at least one high-pressure pump in the high-pressure region 15, the main valve 12 has the same pressure surface as the first pressure connection 16 of the main valve 12 has a larger pressing surface than the pressure connection 17. 1 to the closed position shown in FIG.

パイロット弁11及び圧力調整弁13は、圧力接続部20、21によって、燃料供給装置の低圧領域14に接続され得る。低圧領域14のチョーク22は、低圧領域14における圧力振動を減衰させる。低圧領域14が非加圧の場合、パイロット弁11はバネ要素23によって図1に示した閉口位置に押圧される。パイロット弁11のバネ要素23は、主弁12のバネ要素19と同様に、少ない弾力を有するように構成されており、パイロット弁11の場合は、専ら、非加圧状態におけるパイロット弁11の位置決めを行うために用いられる。場合によっては、バネ要素23を完全に省略しても良い。   The pilot valve 11 and the pressure regulating valve 13 can be connected to the low pressure region 14 of the fuel supply apparatus by the pressure connecting portions 20 and 21. The choke 22 in the low pressure region 14 attenuates pressure vibration in the low pressure region 14. When the low pressure region 14 is not pressurized, the pilot valve 11 is pressed to the closed position shown in FIG. Similar to the spring element 19 of the main valve 12, the spring element 23 of the pilot valve 11 is configured to have less elasticity. In the case of the pilot valve 11, the positioning of the pilot valve 11 in the non-pressurized state is exclusively performed. Used to do In some cases, the spring element 23 may be omitted completely.

図1に示された実施例において主弁12と同様に2/2方向制御弁として構成されているパイロット弁11は、パイロット弁11を燃料供給装置の低圧領域14に接続できる圧力接続部21の他に、さらなる圧力接続部24を有しており、圧力接続部24を通じてパイロット弁11は、少なくとも1つのチョークを介して高圧領域15に接続され得る。図1では、パイロット弁11の圧力接続部24と高圧領域15との間には、すでに言及したチョーク18とさらなるチョーク25とが接続されている。パイロット弁11の両方の圧力接続部21及び24もやはり異なる押圧面を有しており、第1の圧力接続部21の押圧面は、第2の圧力接続部24の押圧面よりも大きいので、低圧領域14及び高圧領域15において、それぞれ対応する動作圧力が加えられている場合に、パイロット弁11は図1に示された閉口位置に押圧される。   In the embodiment shown in FIG. 1, the pilot valve 11 configured as a 2 / 2-directional control valve, like the main valve 12, has a pressure connection portion 21 that can connect the pilot valve 11 to the low pressure region 14 of the fuel supply device. In addition, it has a further pressure connection 24 through which the pilot valve 11 can be connected to the high pressure region 15 via at least one choke. In FIG. 1, the choke 18 and the further choke 25 already mentioned are connected between the pressure connection 24 of the pilot valve 11 and the high pressure region 15. Both pressure connecting parts 21 and 24 of the pilot valve 11 also have different pressing surfaces, and the pressing surface of the first pressure connecting part 21 is larger than the pressing surface of the second pressure connecting part 24. In the low pressure region 14 and the high pressure region 15, when the corresponding operating pressure is applied, the pilot valve 11 is pressed to the closed position shown in FIG.

すでに説明したように、圧力調整弁13は、圧力接続部20によって低圧領域14に接続可能であり、低圧領域14が非加圧の場合、その弾力に関して調整可能なバネ要素26は、圧力調整弁13を、図1に示した閉口位置に押圧する。次に、低圧領域14に動作圧力が加えられている場合、当該動作圧力は圧力接続部20に存在し、バネ要素26の調整された弾力に応じて、圧力調整弁13を、閉口位置から押圧する。つまり、圧力接続部20及び21では、圧力調整弁13及びパイロット弁11によって、一定の圧力が生じるように押圧する。したがって、圧力調整弁13及び調整可能なバネ要素26を用いて、燃料供給システム内で圧力が変動した場合においても主弁12のために一定の開口圧力を保証することが可能であり、圧力接続部20及びそれに伴って圧力接続部21における高すぎる圧力は、圧力調整弁13のチョーク27における圧力が所望の値に低下するまでの間は、圧力調整弁13の開口につながる。ここで、圧力調整弁13をパイロット弁11のピストンに組み込むことが可能であることを指摘しておく。   As already described, the pressure regulating valve 13 can be connected to the low pressure region 14 by the pressure connection 20, and when the low pressure region 14 is unpressurized, the spring element 26 that can be adjusted with respect to its elasticity is a pressure regulating valve. 13 is pressed to the closing position shown in FIG. Next, when an operating pressure is applied to the low pressure region 14, the operating pressure exists in the pressure connection portion 20, and the pressure adjustment valve 13 is pressed from the closed position according to the adjusted elasticity of the spring element 26. To do. That is, in the pressure connection parts 20 and 21, the pressure adjusting valve 13 and the pilot valve 11 are pressed so as to generate a constant pressure. Thus, the pressure regulating valve 13 and the adjustable spring element 26 can be used to guarantee a constant opening pressure for the main valve 12 even when the pressure fluctuates in the fuel supply system, and the pressure connection The pressure that is too high at the part 20 and the pressure connecting part 21 leads to the opening of the pressure regulating valve 13 until the pressure at the choke 27 of the pressure regulating valve 13 drops to a desired value. Here, it is pointed out that the pressure regulating valve 13 can be incorporated in the piston of the pilot valve 11.

停止した内燃機関において、つまり、低圧領域17の低圧ポンプ及び高圧領域15の高圧ポンプが停止した結果、燃料供給装置が非加圧である場合、弁アセンブリ10の弁11、12及び13は、図1に示した位置をとる。   In a stopped internal combustion engine, that is, as a result of the low pressure pump in the low pressure region 17 and the high pressure pump in the high pressure region 15 being stopped, the fuel supply device is non-pressurized, the valves 11, 12 and 13 of the valve assembly 10 are The position shown in 1 is taken.

内燃機関の始動の際、及び、燃料供給装置の低圧領域14の低圧ポンプの始動の際、圧力接続部20及び21では、圧力調整弁13及びパイロット弁11によって、圧力が生成され、当該圧力は、圧力調整弁13によって一定に保たれ、パイロット弁11を図1に示した閉口位置に押圧する。内燃機関が始動する際、高圧領域15の1つ又は各高圧ポンプも始動する。圧力接続部16及び17の構成によって、主弁12は、高圧領域15に動作圧力が存在する場合に、燃料供給装置の高圧領域15を閉じた状態で保つ。すでに説明したように、燃料供給装置の低圧領域14における圧力変動は、チョーク22によって減衰され、圧力調整弁13は、燃料供給装置内の圧力変動の際に、主弁12のために開口圧力を一定に保っている。   When the internal combustion engine is started and when the low pressure pump in the low pressure region 14 of the fuel supply device is started, pressure is generated by the pressure regulating valve 13 and the pilot valve 11 at the pressure connecting portions 20 and 21, and the pressure is The pilot valve 11 is pressed to the closed position shown in FIG. When the internal combustion engine is started, one or each high pressure pump in the high pressure region 15 is also started. Due to the configuration of the pressure connections 16 and 17, the main valve 12 keeps the high pressure region 15 of the fuel supply device closed when there is an operating pressure in the high pressure region 15. As already explained, pressure fluctuations in the low pressure region 14 of the fuel supply device are attenuated by the choke 22 and the pressure regulating valve 13 reduces the opening pressure for the main valve 12 during pressure fluctuations in the fuel supply device. Kept constant.

内燃機関の始動後、並びに、対応して動作圧力が、低圧領域14の低圧ポンプ及び高圧領域15の1つ又は各高圧ポンプによって低圧領域14及び高圧領域15内に生成された後、燃料供給装置の図示されていないインジェクタには、対応する噴射圧力が存在している。チョーク18を介して、主弁12の圧力接続部16は満たされ、すでに言及したように、圧力接続部16は圧力接続部17よりも大きな押圧面を有しているので、主弁12は、内燃機関の始動後、確実に閉止した状態で保たれる。   After starting the internal combustion engine and correspondingly, after the operating pressure has been generated in the low pressure zone 14 and the high pressure zone 15 by one or each high pressure pump in the low pressure zone 14 and the high pressure zone 15, the fuel supply device A corresponding injection pressure exists in an injector (not shown). Via the choke 18, the pressure connection 16 of the main valve 12 is filled and, as already mentioned, the pressure connection 16 has a larger pressing surface than the pressure connection 17, so that the main valve 12 After the internal combustion engine is started, it is kept securely closed.

主弁12の圧力接続部16は、完全には密封されていないので、主弁12のいわゆる隙間経路(Spaltfuehrung)に起因して、一定量の燃料が、燃料タンク又は回収タンク28に向かうに従って損失する。主弁12の圧力接続部16の漏れは、図1では概略的に、チョーク29を通じて示されているが、ここでは、構造的に完成されたチョークではなく、単に、主弁12の圧力接続部16の漏れの結果としての第2の圧力接続部16から回収タンク28の方向への燃料の損失が対象になっている。しかしながら、チョーク18を通じて、原理的なチョーク29に関して圧力接続部16の漏れの結果として回収タンク28の方向に排出されるよりも多くの燃料が補充されるので、主弁12の圧力接続部16における圧力は維持され、燃料供給装置の高圧領域15は閉じた状態で維持され得る。   Since the pressure connection 16 of the main valve 12 is not completely sealed, a certain amount of fuel is lost toward the fuel tank or the recovery tank 28 due to the so-called gap path (Spaltfuehrung) of the main valve 12. To do. The leakage of the pressure connection 16 of the main valve 12 is shown schematically in FIG. 1 through the choke 29, but here the pressure connection of the main valve 12 is simply not a structurally completed choke. The loss of fuel in the direction of the recovery tank 28 from the second pressure connection 16 as a result of 16 leaks is of interest. However, since more fuel is replenished through the choke 18 than is discharged in the direction of the recovery tank 28 as a result of leakage of the pressure connection 16 with respect to the basic choke 29, the pressure connection 16 of the main valve 12 is refilled. The pressure is maintained and the high pressure region 15 of the fuel supply can be maintained closed.

内燃機関が停止され、したがって低圧領域14の低圧ポンプと高圧領域15の1つ又は各高圧ポンプとが停止された場合、燃料供給装置内の圧力は急速に低下する。それによって、パイロット弁11の圧力接続部21における圧力が低下し、燃料供給装置の高圧領域15に依然として存在する比較的高い圧力であって、チョーク18及び25を介してパイロット弁11の圧力接続部24に存在する圧力の結果、パイロット弁11が自動的に開口する。これによって、燃料供給装置内の圧力状況を利用して、内燃機関の停止後数秒の内に、自動的に低圧領域14から回収タンク28に向けて除去又は換気させることができる。   When the internal combustion engine is shut down and thus the low pressure pump in the low pressure zone 14 and one or each high pressure pump in the high pressure zone 15 are shut down, the pressure in the fuel supply system drops rapidly. As a result, the pressure at the pressure connection 21 of the pilot valve 11 decreases and is a relatively high pressure still present in the high pressure region 15 of the fuel supply device, which is connected via the chokes 18 and 25 to the pressure connection of the pilot valve 11. As a result of the pressure present at 24, the pilot valve 11 opens automatically. As a result, the pressure state in the fuel supply device can be used to automatically remove or ventilate from the low pressure region 14 toward the recovery tank 28 within a few seconds after the internal combustion engine is stopped.

この関連において、チョーク25はチョーク18よりも大きいので、チョーク25を介しては、チョーク18を介して圧力接続部16に送られるよりも多くの燃料が圧力接続部16から流出可能であることを留意すべきである。   In this connection, the choke 25 is larger than the choke 18, so that more fuel can flow out of the pressure connection 16 via the choke 25 than is sent to the pressure connection 16 via the choke 18. It should be noted.

主弁12の圧力接続部16における圧力が減少することによって、主弁12も圧力接続部17における圧力によって自動的に開口するので、それによって、燃料供給装置の高圧領域15も、内燃機関停止後数秒の内に、機械的かつ自動的に、回収タンク28に向けて除去又は換気させることができる。   As the pressure at the pressure connection 16 of the main valve 12 is reduced, the main valve 12 is also automatically opened by the pressure at the pressure connection 17, so that the high pressure region 15 of the fuel supply device is also Within a few seconds, it can be removed or vented towards the collection tank 28 mechanically and automatically.

図1に示されたチョーク30は、回収タンク28への圧力損失を示している。   The choke 30 shown in FIG. 1 indicates a pressure loss to the recovery tank 28.

本発明に係る弁アセンブリ10は、燃料供給装置の低圧領域14及び高圧領域15における圧力状況を利用することによって、内燃機関の起動又は始動の際にはパイロット弁11及び主弁12を自動的に閉口させ、内燃機関の停止後にはパイロット弁11及び主弁12を数秒の内に自動的に開口させる。これによって、別個の制御機器の作動を行わない、内燃機関の停止後の燃料供給装置の自動的な減圧が確実化される。空気圧若しくは油圧による圧力空気の供給又は電磁気若しくはその他の種類の作動は不要である。制御媒体は動作媒体、すなわち燃料に相当するので、望ましくない異なる媒体の混合が生じず、例えば、空気圧による作動の際に燃料と圧力空気とが混合することはない。原動機の停止後の、本発明に係る弁アセンブリ10のパイロット弁11及び主弁12の開口と、それに伴う燃料供給装置の減圧とは、数秒の内に行われるので、例えば燃料インジェクタの負荷を迅速に軽減することができる。主弁12及びパイロット弁11のバネ要素19及び23は、少ない弾力を有するように構成されている。なぜなら、これらのバネ要素は、非加圧の状態では実質的に、対応する弁11、12の位置決めにのみ用いられるからである。   The valve assembly 10 according to the present invention automatically uses the pressure conditions in the low pressure region 14 and the high pressure region 15 of the fuel supply device to automatically switch the pilot valve 11 and the main valve 12 when the internal combustion engine is started or started. The pilot valve 11 and the main valve 12 are automatically opened within a few seconds after the internal combustion engine is stopped. This ensures automatic depressurization of the fuel supply device after the internal combustion engine is stopped without the operation of a separate control device. There is no need for pneumatic or hydraulic pressure air supply or electromagnetic or other types of actuation. Since the control medium corresponds to the working medium, i.e. fuel, there is no undesired mixing of the different media, e.g. fuel and pressurized air are not mixed during operation by pneumatic pressure. After stopping the prime mover, the opening of the pilot valve 11 and the main valve 12 of the valve assembly 10 according to the present invention and the accompanying pressure reduction of the fuel supply device are performed within a few seconds. Can be reduced. The spring elements 19 and 23 of the main valve 12 and the pilot valve 11 are configured to have a small elasticity. This is because these spring elements are substantially only used for positioning the corresponding valves 11, 12 in the non-pressurized state.

10 弁アセンブリ
11 パイロット弁
12 主弁
13 圧力調整弁
14 低圧領域
15 高圧領域
16 圧力接続部
17 圧力接続部
18 チョーク
19 バネ要素
20 圧力接続部
21 圧力接続部
22 チョーク
23 バネ要素
24 圧力接続部
25 チョーク
26 バネ要素
27 チョーク
28 回収タンク
29 チョーク
30 チョーク
DESCRIPTION OF SYMBOLS 10 Valve assembly 11 Pilot valve 12 Main valve 13 Pressure adjustment valve 14 Low pressure area 15 High pressure area 16 Pressure connection part 17 Pressure connection part 18 Choke 19 Spring element 20 Pressure connection part 21 Pressure connection part 22 Choke 23 Spring element 24 Pressure connection part 25 Choke 26 Spring element 27 Choke 28 Collection tank 29 Choke 30 Choke

Claims (6)

船舶用ディーゼルエンジンとして構成された内燃機関の燃料供給装置、特にコモンレール燃料供給装置のための弁アセンブリ(10)であって、パイロット弁(11)、主弁(12)及び圧力調整弁(13)を有する弁アセンブリにおいて、
前記パイロット弁(11)、前記主弁(12)及び前記圧力調整弁(13)が、低圧領域(14)における圧力に応じて、及び/又は、高圧領域(15)における圧力に応じて、自動的に作動可能であるように、前記主弁(12)は、圧力接続部(16、17)によって前記燃料供給装置の前記高圧領域(15)と接続可能であり、前記パイロット弁(11)も前記圧力調整弁(13)も、圧力接続部(20、21)によって前記燃料供給装置の前記低圧領域(14)と接続可能であり、前記主弁(12)が、前記高圧領域(15)に動作圧力が加えられている場合に前記主弁(12)が自動的に閉口するように、2つの圧力接続部(16、17)によって前記燃料供給装置の前記高圧領域(15)と接続されることが可能であり、比較的大きな押圧面を有する、第1の、閉口方向に作用する前記主弁(12)の圧力接続部(16)が、少なくとも1つのチョーク(18)を介して、前記燃料供給装置の前記高圧領域(15)に接続されることが可能であり、比較的小さな押圧面を有する、第2の、開口方向に作用する前記主弁(12)の圧力接続部(17)が、前記燃料供給装置の前記高圧領域(15)に直接接続されることが可能であることを特徴とする弁アセンブリ(10)。
A fuel supply device for an internal combustion engine configured as a marine diesel engine, in particular a valve assembly (10) for a common rail fuel supply device, comprising a pilot valve (11), a main valve (12) and a pressure regulating valve (13) A valve assembly having:
Said pilot valve (11), said main valve (12) and said pressure regulating valve (13), in response to the pressure in the low pressure region (14), and / or, depending on the pressure in the high pressure area (15), automatically so as to be operated, the main valve (12) is connectable the said high pressure region of the fuel supply device (15) by a pressure connection (16, 17), said pilot valve (11 ) And the pressure regulating valve (13) can be connected to the low pressure region (14) of the fuel supply device by a pressure connection (20, 21), and the main valve (12) is connected to the high pressure region (15). ) Is connected to the high pressure region (15) of the fuel supply device by two pressure connections (16, 17) so that the main valve (12) automatically closes when operating pressure is applied to Can be relatively large The pressure connection (16) of the first main valve (12) acting in the closing direction, which has a pressing surface, is connected to the high-pressure region (of the fuel supply device) via at least one choke (18). 15), and having a relatively small pressing surface, a second, pressure connection (17) of the main valve (12) acting in the opening direction is connected to the fuel supply device. A valve assembly (10) characterized in that it can be connected directly to the high-pressure region (15 ).
前記圧力調整弁(13)が、前記低圧領域(14)に動作圧力が加えられている場合に前記圧力調整弁(13)がバネ要素(26)の調整可能な弾力に反して前記低圧領域(14)における一定の動作圧力を保証した上で自動的に開口するように、圧力接続部(20)によって前記低圧領域(14)と接続され得ることを特徴とする請求項1に記載の弁アセンブリ(10)。   When the operating pressure is applied to the low pressure region (14), the pressure adjusting valve (13) is opposed to the adjustable elasticity of the spring element (26) and the low pressure region (14) The valve assembly according to claim 1, characterized in that it can be connected to the low pressure region (14) by means of a pressure connection (20) so as to open automatically with a guarantee of a constant operating pressure in 14). (10). 前記パイロット弁(11)が、第1の圧力接続部(21)によって前記燃料供給装置の前記低圧領域(14)と、及び、第2の圧力接続部(24)によって少なくとも1つのチョーク(18、25)を介して前記燃料供給装置の前記高圧領域(15)と、前記低圧領域(14)に動作圧力が加えられている場合、及び、前記高圧領域(15)に動作圧力が加えられている場合に前記パイロット弁(11)が自動的に閉口するように接続され得ることを特徴とする請求項1又は2に記載の弁アセンブリ(10)。   The pilot valve (11) is connected to the low pressure region (14) of the fuel supply device by a first pressure connection (21) and at least one choke (18, 18) by a second pressure connection (24). 25), when the operating pressure is applied to the high pressure region (15) and the low pressure region (14) of the fuel supply device, and the operating pressure is applied to the high pressure region (15). 3. The valve assembly (10) according to claim 1 or 2, characterized in that in some cases the pilot valve (11) can be connected to automatically close. 前記燃料供給装置の前記低圧領域(14)における動作圧力が低下した場合に、前記パイロット弁(11)及び前記主弁(12)が自動的に開口するので、前記低圧領域(14)及び前記高圧領域(2)から燃料タンク(28)に向けて除去することができることを特徴とする請求項1からのいずれか一項に記載の弁アセンブリ(10)。 When the operating pressure in the low pressure region (14) of the fuel supply device decreases, the pilot valve (11) and the main valve (12) automatically open, so the low pressure region (14) and the high pressure region the valve assembly according to any one of claims 1 to 3, characterized in that it can be removed toward the area (2) fuel tank from (28) (10). 前記パイロット弁(11)及び前記主弁(12)が2/2方向制御弁として構成されていることを特徴とする請求項1からのいずれか一項に記載の弁アセンブリ(10)。 The valve assembly (10) according to any one of claims 1 to 4 , characterized in that the pilot valve (11) and the main valve (12) are configured as 2 / 2-way control valves. 船舶用ディーゼルエンジンとして構成された内燃機関の燃料供給装置、特にコモンレール燃料供給装置であって、低圧領域(14)と高圧領域(15)とを有する燃料供給装置において、請求項1からのいずれか一項に記載の弁アセンブリ(10)を備えているを特徴とする燃料供給装置。 The fuel supply device of internal combustion engine formed as a marine diesel engine, in particular common rail fuel supply system, a fuel supply system having a low pressure region (14) and the high-pressure region (15), one of claims 1 to 5 A fuel supply device comprising the valve assembly (10) according to claim 1.
JP2014161100A 2013-08-08 2014-08-07 Valve assembly for a fuel supply device and fuel supply device Expired - Fee Related JP6483372B2 (en)

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EP2835526A1 (en) 2015-02-11
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DE102013013231A1 (en) 2015-02-12
CN104454277B (en) 2019-10-18
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KR102125102B1 (en) 2020-06-19
JP2015034552A (en) 2015-02-19

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