专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

51. 发明授权

US08475120B2 Exhaust gas turbocharger for an internal combustion engine 有权
标题翻译：用于内燃机的废气涡轮增压器
公开(公告)号：US08475120B2
公开(公告)日：2013-07-02
申请号：US12661637
申请日：2010-03-22
申请人： Peter Fledersbacher , Torsten Hirth
发明人： Peter Fledersbacher , Torsten Hirth
IPC分类号： F01D17/00
CPC分类号： F01D17/143 , F02B37/22 , F02C6/12 , F05D2220/40
摘要： In an exhaust gas turbocharger for an internal combustion engine, including a turbine housing and a rotor, the housing having an exhaust gas guide section and the rotor including a turbine wheel and a shaft connected to the turbine wheel which is driven by exhaust gas, and a control device for controlling the exhaust gas flow to the turbine wheel comprising an annular guide vane structure and an axial slide supported on a contour sleeve mounted to the turbine housing remote from the rotor and extending toward the rotor and forming also the turbine exhaust gas discharge duct, the axial slide includes a cavity accommodating the guide vane structure.
摘要翻译：在具有涡轮壳体和转子的内燃机的排气涡轮增压器中，所述壳体具有排气导引部，所述转子包括涡轮机叶轮和与所述涡轮机叶轮连接的轴，所述涡轮机叶轮由废气驱动，以及用于控制到涡轮机叶轮的废气流的控制装置，包括环形引导叶片结构和支撑在轮廓套筒上的轴向滑动件，轮廓套筒安装到远离转子的涡轮机壳体上，并且朝向转子延伸并且还形成涡轮机废气排放轴向滑动件包括容纳导叶结构的空腔。

52. 发明申请

US20100183434A1 Exhaust gas turbocharger for an internal combustion engine 有权
标题翻译：用于内燃机的废气涡轮增压器
公开(公告)号：US20100183434A1
公开(公告)日：2010-07-22
申请号：US12661637
申请日：2010-03-22
申请人： Peter Fledersbacher , Torsten Hirth
发明人： Peter Fledersbacher , Torsten Hirth
IPC分类号： F04D29/44
CPC分类号： F01D17/143 , F02B37/22 , F02C6/12 , F05D2220/40
摘要： In an exhaust gas turbocharger for an internal combustion engine, including a turbine housing and a rotor, the housing having an exhaust gas guide section and the rotor including a turbine wheel and a shaft connected to the turbine wheel which is driven by exhaust gas, and a control device for controlling the exhaust gas flow to the turbine wheel comprising an annular guide vane structure and an axial slide supported on a contour sleeve mounted to the turbine housing remote from the rotor and extending toward the rotor and forming also the turbine exhaust gas discharge duct, the axial slide includes a cavity accommodating the guide vane structure.
摘要翻译：在具有涡轮壳体和转子的内燃机的排气涡轮增压器中，所述壳体具有排气导引部，所述转子包括涡轮机叶轮和与所述涡轮机叶轮连接的轴，所述涡轮机叶轮由废气驱动，以及用于控制到涡轮机叶轮的废气流的控制装置，包括环形引导叶片结构和支撑在轮廓套筒上的轴向滑动件，轮廓套筒安装到远离转子的涡轮机壳体上，并且朝向转子延伸并且还形成涡轮机废气排放轴向滑动件包括容纳导叶结构的空腔。

53. 发明申请

US20090110547A1 Method for producing a contoured gap, and turbo-engine comprising contoured gap 审中-公开
标题翻译：用于产生轮廓间隙的方法，以及包括轮廓间隙的涡轮发动机
公开(公告)号：US20090110547A1
公开(公告)日：2009-04-30
申请号：US11661477
申请日：2005-07-11
申请人： Peter Fledersbacher , Wolfgang Ruff , Martin Schlegl , Holger Stark
发明人： Peter Fledersbacher , Wolfgang Ruff , Martin Schlegl , Holger Stark
IPC分类号： F01D11/12 , B23P15/00
CPC分类号： F01D11/22 , F01D11/122 , F05D2220/40 , F05D2230/10 , F05D2250/41 , Y10T29/49236
摘要： A method for producing a contoured gap between a rotor and a stator of a turbo-engine is provided. A first turbo-engine drives a second turbo-engine by means of a common shaft, the shaft being mounted in a bearing housing by means of a bearing. The aim of the invention is to enable the contoured gap to be created in a simple and reliable manner. To this end, the contoured gap is formed between a contoured surface of the rotor and a contoured surface of an engine housing associated with the rotor, by grinding the contoured surfaces against each other, using the axial play of the bearing.
摘要翻译：提供了一种用于在涡轮发动机的转子和定子之间产生轮廓间隙的方法。第一涡轮发动机通过公共轴驱动第二涡轮发动机，轴通过轴承安装在轴承壳体中。本发明的目的是能够以简单和可靠的方式产生轮廓间隙。为此，通过使用轴承的轴向游隙，轮廓间隙形成在转子的轮廓表面和与转子相关联的发动机壳体的轮廓表面之间，通过相对于彼此磨削轮廓表面。

54. 发明授权

US07438529B2 Compressor and turbine wheel for a secondary air feed device 有权
标题翻译：用于二次空气供给装置的压缩机和涡轮机叶轮
公开(公告)号：US07438529B2
公开(公告)日：2008-10-21
申请号：US11399686
申请日：2006-04-06
申请人： Peter Fledersbacher , Hans-Georg Lehmann , Martin Schlegl , Holger Stark
发明人： Peter Fledersbacher , Hans-Georg Lehmann , Martin Schlegl , Holger Stark
IPC分类号： F01D5/14 , F01D15/08 , F01N3/32 , F04D25/04
CPC分类号： F04D25/045 , F01D15/08 , F01N3/32 , Y02T10/20
摘要： In a compressor and turbine wheel for a secondary air feed device formed as a single component, a rotor which includes a center disc structure consisting of at least two discs of different materials is provided at one side with compressor blades and on the opposite side with turbine blades, and the discs consist of an alloy based on Al, Mg, Ti, Fe, or Ni and are preferably arranged in axially spaced relationship with a disc carrier of a plastic material disposed in the space between the two bladed discs.
摘要翻译：在形成为单个部件的二次空气供给装置的压缩机和涡轮机叶轮中，包括由至少两个不同材料的盘构成的中心盘结构的转子在一侧设置有压缩机叶片，并且在与涡轮相反的一侧叶片，并且盘由基于Al，Mg，Ti，Fe或Ni的合金组成，并且优选地与设置在两个叶片盘之间的空间中的塑料材料的盘式载体轴向间隔开地布置。

55. 发明申请

US20050265822A1 Method of operating a compressor near the compressor pumping limit and compressor 失效
标题翻译：在压缩机泵送极限和压缩机附近操作压缩机的方法
公开(公告)号：US20050265822A1
公开(公告)日：2005-12-01
申请号：US11110965
申请日：2005-04-20
申请人： Peter Fledersbacher , Gernot Hertweck , Steffen Schiedt , Guido Vent , Jurgen Willand
发明人： Peter Fledersbacher , Gernot Hertweck , Steffen Schiedt , Guido Vent , Jurgen Willand
IPC分类号： F01D17/06 , F01D17/16 , F02B37/24 , F02C7/042 , F02C7/057 , F04D25/04 , F04D27/02 , F01D1/00
CPC分类号： F02B37/12 , F01D17/06 , F01D17/16 , F02B37/24 , F02C7/042 , F02C7/057 , F04D25/04 , F04D27/02 , F05D2220/40 , F05D2270/101 , Y02T10/144
摘要： In a method of operating a compressor near the compressor pumping limit wherein the compressor includes a control arrangement for adjusting the momentary operating state of the compressor, the flow velocity of a mass flow through the compressor in the boundary layer along the wall of the flow passage is determined for detecting operation of the compressor close to the pumping limit from a reversal of the direction of the mass flow vector in the boundary layer and the control arrangement is actuated so as to prevent the compressor from transgressing the pumping limit.
摘要翻译：在压缩机泵送极限附近操作压缩机的方法中，其中压缩机包括用于调节压缩机的瞬时操作状态的控制装置，沿着流动通道的壁在边界层中通过压缩机的质量流的流速被确定为从边界层中的质量流矢量的方向反转来检测靠近泵送极限的压缩机的操作，并且控制装置被致动以防止压缩机超过泵送极限。

56. 发明申请

US20050207915A1 Motor vehicle drive arrangement 失效
标题翻译：机动车装置
公开(公告)号：US20050207915A1
公开(公告)日：2005-09-22
申请号：US11110969
申请日：2005-04-20
申请人： Peter Fledersbacher , Gernot Hertweck , Steffen Schiedt , Guido Vent , Jurgen Willand
发明人： Peter Fledersbacher , Gernot Hertweck , Steffen Schiedt , Guido Vent , Jurgen Willand
IPC分类号： F04B17/00 , F04B35/00 , F04D13/02 , F04D13/06
CPC分类号： F16H57/04 , F04D13/022 , F04D13/06 , F16H61/0028 , Y10T74/2186
摘要： In a motor vehicle drive arrangement having an electric motor with a rotor for driving an oil pump and being supported in an air space of a housing by a rotor disk of the rotor of the electric motor which is permanently connected to a pump rotor of the oil pump, a freewheeling mechanism for a mechanical drive of the pump rotor of the oil pump is provided for coupling the oil pump to a vehicle travel drive train of the vehicle drive arrangement when the travel drive train rotates faster than the electric motor.
摘要翻译：在一种具有电机的机动车辆驱动装置中，所述电动机具有用于驱动油泵的转子，并且通过电动机的转子的转子盘被支撑在壳体的空气空间中，转子盘永久地连接到油的泵转子提供了一种用于油泵的泵转子的机械驱动的续流机构，用于当行驶传动系转动比电动机更快时将油泵连接到车辆驱动装置的车辆行驶传动系。

57. 发明申请

US20090277171A1 Exhaust gas turbocharger turbine 失效
标题翻译：废气涡轮增压器涡轮机
公开(公告)号：US20090277171A1
公开(公告)日：2009-11-12
申请号：US12387144
申请日：2009-04-28
申请人： Peter Fledersbacher , Torsten Hirth
发明人： Peter Fledersbacher , Torsten Hirth
IPC分类号： F02D23/00
CPC分类号： F01D17/141 , F02B37/24 , F02C6/12 , F05D2220/40
摘要： In an exhaust gas turbocharger turbine for an internal combustion engine having a housing including a turbine wheel rotatably supported in the housing, wherein the housing has an exhaust gas flow guide section including an exhaust gas flow control arrangement with a guide vane structure for directing exhaust gas onto the turbine rotor, an adjustment mechanism with an axially movable control slide is provided which is movable by an operating fork which is slidably supported on a guide element and engages the control slide at opposite sides so as to prevent cogging of the movable control slide during movement into, and out of, the exhaust gas flow guide section.
摘要翻译：在一种用于内燃机的排气涡轮增压器涡轮机中，该涡轮增压器具有壳体，该外壳包括可旋转地支撑在壳体中的涡轮机叶轮，其中壳体具有排气流引导部分，该排气气体引导部分包括排气流动控制装置，提供具有可轴向移动的控制滑块的调节机构，其可通过可滑动地支撑在引导元件上的操作叉移动，并且在相对侧接合控制滑块，以防止可移动控制滑块在齿轮进入和离开废气流动引导部分的运动。

58. 发明授权

US07428815B2 Method of operating a compressor near the compressor pumping limit and compressor 失效
标题翻译：在压缩机泵送极限和压缩机附近操作压缩机的方法
公开(公告)号：US07428815B2
公开(公告)日：2008-09-30
申请号：US11110965
申请日：2005-04-20
申请人： Peter Fledersbacher , Gernot Hertweck , Steffen Schiedt , Guido Vent , Jürgen Willand
发明人： Peter Fledersbacher , Gernot Hertweck , Steffen Schiedt , Guido Vent , Jürgen Willand
IPC分类号： F02B33/44
CPC分类号： F02B37/12 , F01D17/06 , F01D17/16 , F02B37/24 , F02C7/042 , F02C7/057 , F04D25/04 , F04D27/02 , F05D2220/40 , F05D2270/101 , Y02T10/144
摘要： In a method of operating a compressor near the compressor pumping limit wherein the compressor includes a control arrangement for adjusting the momentary operating state of the compressor, the flow velocity of a mass flow through the compressor in the boundary layer along the wall of the flow passage is determined for detecting operation of the compressor close to the pumping limit from a reversal of the direction of the mass flow vector in the boundary layer and the control arrangement is actuated so as to prevent the compressor from transgressing the pumping limit.
摘要翻译：在压缩机泵送极限附近操作压缩机的方法中，其中压缩机包括用于调节压缩机的瞬时操作状态的控制装置，沿着流动通道的壁在边界层中通过压缩机的质量流的流速被确定为从边界层中的质量流矢量的方向反转来检测靠近泵送极限的压缩机的操作，并且控制装置被致动以防止压缩机超过泵送极限。

59. 发明申请

US20060222503A1 Compressor and turbine wheel for a secondary air feed device 有权
标题翻译：用于二次空气供给装置的压缩机和涡轮机叶轮
公开(公告)号：US20060222503A1
公开(公告)日：2006-10-05
申请号：US11399686
申请日：2006-04-06
申请人： Peter Fledersbacher , Hans-Georg Lehmann , Martin Schlegl , Holger Stark
发明人： Peter Fledersbacher , Hans-Georg Lehmann , Martin Schlegl , Holger Stark
IPC分类号： F01D5/14
CPC分类号： F04D25/045 , F01D15/08 , F01N3/32 , Y02T10/20
摘要： In a compressor and turbine wheel for a secondary air feed device formed as a single component, a rotor which includes a center disc structure consisting of at least two discs of different materials is provided at one side with compressor blades and on the opposite side with turbine blades, and the discs consist of an alloy based on Al, Mg, Ti, Fe, or Ni and are preferably arranged in axially spaced relationship with a disc carrier of a plastic material disposed in the space between the two bladed discs.
摘要翻译：在形成为单个部件的二次空气供给装置的压缩机和涡轮机叶轮中，包括由至少两个不同材料的盘构成的中心盘结构的转子在一侧设置有压缩机叶片，并且在与涡轮相反的一侧叶片，并且盘由基于Al，Mg，Ti，Fe或Ni的合金组成，并且优选地与设置在两个叶片盘之间的空间中的塑料材料的盘式载体轴向间隔开地布置。

60. 发明授权

US08230683B2 Turbocharger including variable geometry turbine with improved guide element and operating fork 失效
标题翻译：涡轮增压器包括具有改进的引导元件和操作叉的可变几何涡轮机
公开(公告)号：US08230683B2
公开(公告)日：2012-07-31
申请号：US12387144
申请日：2009-04-28
申请人： Peter Fledersbacher , Torsten Hirth
发明人： Peter Fledersbacher , Torsten Hirth
IPC分类号： F02B37/10
CPC分类号： F01D17/141 , F02B37/24 , F02C6/12 , F05D2220/40
摘要： In an exhaust gas turbocharger turbine for an internal combustion engine having a housing including a turbine wheel rotatably supported in the housing, wherein the housing has an exhaust gas flow guide section including an exhaust gas flow control arrangement with a guide vane structure for directing exhaust gas onto the turbine rotor, an adjustment mechanism with an axially movable control slide is provided which is movable by an operating fork which is slidably supported on a guide element and engages the control slide at opposite sides so as to prevent cogging of the movable control slide during movement into, and out of, the exhaust gas flow guide section.
摘要翻译：在一种用于内燃机的排气涡轮增压器涡轮机中，该涡轮增压器具有壳体，该外壳包括可旋转地支撑在壳体中的涡轮机叶轮，其中壳体具有排气流引导部分，该排气气体引导部分包括排气流动控制装置，提供具有可轴向移动的控制滑块的调节机构，其可通过可滑动地支撑在引导元件上的操作叉移动，并且在相对侧接合控制滑块，以防止可移动控制滑块在齿轮进入和离开废气流动引导部分的运动。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式