BRENNKRAFTMASCHINE
    1.
    发明公开
    BRENNKRAFTMASCHINE 审中-公开
    内燃机

    公开(公告)号:EP2049774A1

    公开(公告)日:2009-04-22

    申请号:EP07801521.1

    申请日:2007-08-06

    CPC classification number: F01L13/06

    Abstract: An internal combustion engine has a camshaft (23) which acts on inlet and outlet valves (5, 7), wherein the lift curve (EV, AV) of the inlet and outlet valves (5, 7) is determined by the shape of the cams (24, 25) of the camshaft (23). Arranged on the camshaft (23) is an additional auxiliary cam which acts on the outlet valve (7), as a result of which a phase-offset auxiliary lift curve (AVz) is imparted to the outlet valve (7).

    VERDICHTER IM ANSAUGTRAKT EINER BRENNKRAFTMASCHINE
    4.
    发明公开
    VERDICHTER IM ANSAUGTRAKT EINER BRENNKRAFTMASCHINE 有权
    压缩机进气内燃机

    公开(公告)号:EP1673525A1

    公开(公告)日:2006-06-28

    申请号:EP04740250.8

    申请日:2004-06-24

    CPC classification number: F02B37/24 F02B37/225 F02D2009/0283 Y02T10/144

    Abstract: The invention relates to a compressor (5) in the induction tract (6) of an internal combustion engine, comprising a compressor wheel that is rotatably mounted in a compressor inlet channel (9) and that is used to compress supplied combustion air to an increased boost pressure. The compressor is also equipped with an adjustable conductor grid device (12) in the flow path to the compressor wheel, said device comprising two separate, co-operating conductor grids (27, 31), each containing a plurality of guide vanes (33, 34) that are distributed around the periphery. The flow cross-section between the guide vanes (33, 34) of the two conductor grids (27, 31) can be adjusted by means of the displacement of at least one conductor grid (27, 31).

    ABGASTURBOLADER FÜR EINE BRENNKRAFTMASCHINE MIT VARIABLER TURBINENGEOMETRIE
    5.
    发明授权
    ABGASTURBOLADER FÜR EINE BRENNKRAFTMASCHINE MIT VARIABLER TURBINENGEOMETRIE 有权
    涡轮增压器与可变几何涡轮的内燃发动机

    公开(公告)号:EP1334262B1

    公开(公告)日:2006-03-22

    申请号:EP01978369.5

    申请日:2001-09-14

    CPC classification number: F01D17/165 F02B37/025 F02C6/12 Y02T10/144

    Abstract: An exhaust gas turbocharger (1) for an internal combustion engine comprises an exhaust gas turbine and a compressor (3) which is connected to said turbine (2) by a shaft (4). The turbine (2) is configured in the form of a radial turbine (2) with a radial supply channel (5) and a radial flow entry cross-section (6) to the turbine wheel (9). A variable turbine geometry (7) is provided, enabling the cross-sectional adjustment of the radial flow entry cross-section (6). The variable turbine geometry (7) is supported between two support walls (11, 14) that are fixed to the housing. One of said support walls (14) projects into the supply channel (5) in such a way that the rear side of this support wall (14) that faces away from the variable turbine geometry (7) is at a distance from the inner wall (12) of the supply channel (5) and the exhaust gas located in the supply channel (5) can flow against said rear side.

    ABGASTURBOLADER FÜR EINE BRENNKRAFTMASCHINE
    6.
    发明公开
    ABGASTURBOLADER FÜR EINE BRENNKRAFTMASCHINE 有权
    涡轮增压器的内燃发动机

    公开(公告)号:EP1576265A1

    公开(公告)日:2005-09-21

    申请号:EP03775381.1

    申请日:2003-11-21

    Abstract: Disclosed is an exhaust gas turbocharger (2) for an internal combustion engine (1), comprising a compressor (5) in the intake pipe system (6) and an exhaust gas turbine (3) in the exhaust gas leg (4). The exhaust gas turbine (3) is provided with an exhaust gas collection chamber located inside a turbine housing (24). The exhaust gas of said exhaust gas collection chamber can be fed to the turbine wheel (27) via a cross section of a turbine inlet. The inventive exhaust gas turbocharger (2) further comprises an exhaust gas by-pass (31) which bridges the cross section of the turbine inlet and connects the exhaust gas collection chamber to a discharge area (28) of the exhaust gas turbine (3). The exhaust gas turbine (3) forms a pump for a gas-feeding device while a gas-feeding conduit (18, 21) that is assigned to the gas-feeding device extends into the exhaust gas by-pass (31).

    ABGASTURBOLADER FÜR EINE BRENNKRAFTMASCHINE MIT VARIABLER TURBINENGEOMETRIE
    8.
    发明公开
    ABGASTURBOLADER FÜR EINE BRENNKRAFTMASCHINE MIT VARIABLER TURBINENGEOMETRIE 有权
    涡轮增压器与可变几何涡轮的内燃发动机

    公开(公告)号:EP1334262A1

    公开(公告)日:2003-08-13

    申请号:EP01978369.5

    申请日:2001-09-14

    CPC classification number: F01D17/165 F02B37/025 F02C6/12 Y02T10/144

    Abstract: An exhaust gas turbocharger (1) for an internal combustion engine comprises an exhaust gas turbine and a compressor (3) which is connected to said turbine (2) by a shaft (4). The turbine (2) is configured in the form of a radial turbine (2) with a radial supply channel (5) and a radial flow entry cross-section (6) to the turbine wheel (9). A variable turbine geometry (7) is provided, enabling the cross-sectional adjustment of the radial flow entry cross-section (6). The variable turbine geometry (7) is supported between two support walls (11, 14) that are fixed to the housing. One of said support walls (14) projects into the supply channel (5) in such a way that the rear side of this support wall (14) that faces away from the variable turbine geometry (7) is at a distance from the inner wall (12) of the supply channel (5) and the exhaust gas located in the supply channel (5) can flow against said rear side.

    ABGASTURBOLADER FÜR EINE BRENNKRAFTMASCHINE UND BRENNKRAFTMASCHINE
    10.
    发明公开
    ABGASTURBOLADER FÜR EINE BRENNKRAFTMASCHINE UND BRENNKRAFTMASCHINE 有权
    涡轮增压器的内燃发动机和内燃机

    公开(公告)号:EP2049771A2

    公开(公告)日:2009-04-22

    申请号:EP07801544.3

    申请日:2007-08-08

    CPC classification number: F02C6/12 F02B37/00 F02B37/025 F05D2220/40 Y02T10/144

    Abstract: The invention relates to an exhaust-gas turbocharger for an internal combustion engine, having a housing (2) and having a rotor (6), wherein the housing (2) has an air guiding section (3) through which flow can pass, an exhaust-gas guiding section (4) through which flow can pass, and a bearing section (5), and the rotor (6) comprises a compressor wheel (7) for sucking in and compressing air, a turbine wheel (8) for expanding exhaust gas, and a shaft (9) for rotationally fixedly connecting the compressor wheel (7) to the turbine wheel (8), wherein the compressor wheel (7) is arranged so as to be rotatable in the air guiding section (3), and the turbine wheel (8) is positioned so as to be rotatable in the exhaust-gas guiding section (4), and the shaft (9) is rotatably mounted in the bearing section (5). According to the invention, a ratio M of a first mass (mVer) of the compressor wheel (7) and a second mass (mTur) of the turbine wheel (8) follows the function M = mVer/mTur, wherein the ratio M lies in the following value range: 0.8

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