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公开(公告)号：US06792352B1
公开(公告)日：2004-09-14
申请号：US10088211
申请日：2002-07-26
IPC分类号： G01C2126
CPC分类号： B60R25/102 , B60G2400/204 , B60G2400/40 , B60G2400/824 , B60G2401/16 , B60G2600/0422 , B60G2800/92 , B60G2800/94 , B60R25/33 , B60W2550/402
摘要： A vehicle data bus system includes locating means which comprise a locating computing unit and a locating sensor system which contains at least one GPS receiver with associated GPS antenna and gyro data acquisition means, and a data bus via which connects a plurality of bus users in data communication with one another. The locating means contain a locating module which is embodied as one of the bus users and is configured to receive at least wheel speed data and forward/backward direction of travel data via the data bus, to acquire at least vehicle position data, direction of travel angle data, travel speed data and altitude position data as well as to output this acquired data onto the data bus. For this purpose, the locating module contains the location computing unit, the GPS receiver and a gyroscope or means for the bus-end reception and evaluation of gyro data of a travel dynamics/traction control system.
摘要翻译： 车辆数据总线系统包括定位装置，其包括定位计算单元和定位传感器系统，所述定位传感器系统包含至少一个具有相关联的GPS天线和陀螺仪数据获取装置的GPS接收器，以及通过数据总线连接多个总线用户的数据 相互沟通。 定位装置包含定位模块，该定位模块被实现为总线用户之一，并被配置为经由数据总线至少接收车轮速度数据和行进数据的前向/后向方向，至少获取车辆位置数据，行进方向 角度数据，行驶速度数据和高度位置数据，以及将所获取的数据输出到数据总线上。 为此，定位模块包含位置计算单元，GPS接收器和用于总线端接收和评估行驶动力/牵引力控制系统的陀螺仪数据的陀螺仪或装置。
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公开(公告)号：US20140345662A1
公开(公告)日：2014-11-27
申请号：US13993600
申请日：2011-10-26
申请人： Roland Gauss , Stefan Hoffmann , Karl Stockinger
发明人： Roland Gauss , Stefan Hoffmann , Karl Stockinger
摘要： The invention relates to a device for converting thermal energy to electrical energy, comprising at least one thermoelectric module (19) which has an outer surface having a hot side (20) for contacting a heat source and having a cold side (22) for contacting a heat sink, wherein the hot side of the thermoelectric module is thermally conductively connected to a heat source, in particular an exhaust channel (11) of a combustion engine. The device further comprises a cooling channel (25) through which a cooling fluid can flow and which is thermally conductively connected to the cold side of the thermoelectric module. The cooling channel has at least one opening to the cold side of the thermoelectric module and is sealed in a fluid-tight manner around the opening with respect to the hot side of the thermoelectric module.
摘要翻译： 本发明涉及一种用于将热能转换成电能的装置，包括至少一个热电模块（19），该热电模块具有外表面，该外表面具有热侧（20），用于接触热源并具有用于接触的冷侧（22） 散热器，其中热电模块的热侧热传导连接到热源，特别是内燃机的排气通道（11）。 该装置还包括冷却通道（25），冷却流体可以通过该冷却通道流动，并且热传导连接到热电模块的冷侧。 冷却通道具有至少一个通向热电模块的冷侧的开口，并相对于热电模块的热侧围绕开口以流体密封的方式密封。
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公开(公告)号：US08092175B2
公开(公告)日：2012-01-10
申请号：US12226537
申请日：2007-02-13
CPC分类号： F01D5/145 , F01D5/186 , F01D5/187 , F01D5/189 , F01D9/065 , F02C3/16 , F02K3/08 , F05D2240/122 , F05D2240/124 , F05D2250/25 , F05D2260/204
摘要： The invention relates to a turbine blade comprising a profiled vane around which working gas flows. The working gas cross-flows a front edge of the vane and flows away on a rear edge of the vane. The vane has a first and a second channel system for guiding two media separated from the turbine blade. Combustion taking place inside is reduced in a safe manner to maintain the service life of the turbine blade and to prevent damage in the gas turbine, such that a first outlet connected to the first channel system is arranged in the region of the rear edge for blowing out the first media into the working gas and a second outlet connected to the second channel system is arranged in the region of the rear edge for blowing out the second medium.
摘要翻译： 本发明涉及一种涡轮叶片，其包括工作气体围绕其流动的异型叶片。 工作气体交叉流动叶片的前边缘并在叶片的后边缘上流走。 叶片具有用于引导从涡轮叶片分离的两种介质的第一和第二通道系统。 在内部进行的燃烧以安全的方式被减少以维持涡轮机叶片的使用寿命并且防止燃气轮机中的损坏，使得连接到第一通道系统的第一出口布置在用于吹送的后边缘的区域中 将第一介质排出到工作气体中，并且连接到第二通道系统的第二出口布置在后边缘的区域中以吹出第二介质。
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公开(公告)号：US20090081048A1
公开(公告)日：2009-03-26
申请号：US12226534
申请日：2007-03-09
IPC分类号： F01D5/18
CPC分类号： F23R3/14 , F01D5/18 , F01D9/065 , F02C3/16 , F02K3/08 , F02K3/10 , F23C2900/07001 , F23R3/286
摘要： The invention relates to a blade for a turbine comprising a blade wall, a first channel for guiding a first medium and a second channel for guiding a second medium that can be supplied to the turbine blade separately from the first medium. In order to combine both media, which are supplied separately, into one mixture, a turbine blade has least one chamber which is arranged in the interior or in the blade wall and said chamber is connected to said channels via a respective connection line. In order to provide a particularly simple component that is economical to produce, the chamber and/or the outlet conduit are a least partially delimited and/or formed by an insert accommodated in the wall.
摘要翻译： 本发明涉及一种用于涡轮机的叶片，其包括叶片壁，用于引导第一介质的第一通道和用于引导可与第一介质分开供应到涡轮叶片的第二介质的第二通道。 为了将分别供应的两种介质组合成一种混合物，涡轮机叶片具有布置在内部或叶片壁中的至少一个室，并且所述室经由相应的连接线连接到所述通道。 为了提供生产经济的特别简单的部件，腔室和/或出口导管由容纳在壁中的插入件至少部分地界定和/或形成。
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5.发明申请Open cooled component for a gas turbine, combustion chamber, and gas turbine 失效用于燃气轮机，燃烧室和燃气轮机的开式冷却部件公开(公告)号：US20070101722A1
公开(公告)日：2007-05-10
申请号：US10561641
申请日：2004-06-16
申请人： Stefan Hoffmann
发明人： Stefan Hoffmann
IPC分类号： F02C1/00
CPC分类号： F23R3/30 , F01D5/186 , F01D25/12 , F05D2260/202 , F05D2260/221 , F23M5/085 , F23R3/002
摘要： The invention relates to an open-cooled component for a gas turbine having an outer wall (20) which is subjected to hot gas and which at least partly defines a first cavity (15) for a first medium and in which through-openings (3, 12) are arranged, which through-openings (3, 12) open into the cavity (15) on the one side and into the hot-gas space (21) on the other side, and having at least one second cavity for admixing a second medium, this second cavity being fluidically connected to the through-openings (3, 12). In order to specify a component for a gas turbine with which flashback and spontaneous ignition during feeding of fuel into the cooling air can be reduced, it is proposed that the second cavity be formed by supply passages (9, 13) which are provided in the outer wall (20) and are connected via transverse passages (4) to the through-openings (3, 12) designed as through-bores, so that the two media cannot be mixed until inside the through-bores. A combustion chamber for a gas turbine and a gas turbine having such a component are also proposed.
摘要翻译： 本发明涉及一种用于燃气轮机的开式冷却部件，其具有经受热气体的外壁（20），并且至少部分地限定用于第一介质的第一空腔（15），并且其中通孔 ，12），所述通孔（3,12）在一侧开口到所述空腔（15）中并进入另一侧的热气体空间（21）中，并且具有至少一个用于混合的第二腔 第二介质，该第二腔流体地连接到通孔（3,12）。 为了指定用于燃料供给到冷却空气中的回火和自发点燃的燃气轮机的部件，可以提供第二空腔由供应通道（9,13）形成，供应通道（9,13）设置在 外壁（20）并且经由横向通道（4）连接到设计为通孔的通孔（3,12），使得两个介质不能混合直到通孔内部。 还提出了一种用于燃气轮机的燃烧室和具有这种部件的燃气轮机。
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公开(公告)号：US08047001B2
公开(公告)日：2011-11-01
申请号：US12226534
申请日：2007-03-09
CPC分类号： F23R3/14 , F01D5/18 , F01D9/065 , F02C3/16 , F02K3/08 , F02K3/10 , F23C2900/07001 , F23R3/286
摘要： The invention relates to a blade for a turbine comprising a blade wall, a first channel for guiding a first medium and a second channel for guiding a second medium that can be supplied to the turbine blade separately from the first medium. In order to combine both media, which are supplied separately, into one mixture, a turbine blade has least one chamber which is arranged in the interior or in the blade wall and said chamber is connected to said channels via a respective connection line. In order to provide a particularly simple component that is economical to produce, the chamber and/or the outlet conduit are a least partially delimited and/or formed by an insert accommodated in the wall.
摘要翻译： 本发明涉及一种用于涡轮机的叶片，其包括叶片壁，用于引导第一介质的第一通道和用于引导可与第一介质分开供应到涡轮叶片的第二介质的第二通道。 为了将分别供应的两种介质组合成一种混合物，涡轮机叶片具有布置在内部或叶片壁中的至少一个室，并且所述室经由相应的连接线连接到所述通道。 为了提供生产经济的特别简单的部件，腔室和/或出口导管由容纳在壁中的插入件至少部分地界定和/或形成。
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7.发明申请Open-cooled component for a gas turbine, combustion chamber, and gas turbine 失效用于燃气轮机，燃烧室和燃气轮机的开式冷却部件公开(公告)号：US20100083665A1
公开(公告)日：2010-04-08
申请号：US12631940
申请日：2009-12-07
申请人： Stefan Hoffmann
发明人： Stefan Hoffmann
CPC分类号： F23R3/30 , F01D5/186 , F01D25/12 , F05D2260/202 , F05D2260/221 , F23M5/085 , F23R3/002
摘要： An open-cooled component for a gas turbine is provided. The component includes an outer wall that is subjected to a hot gas and at least partially defines a first cavity for a first means. The outer wall is provided with through-openings which open up into the cavity on one side and into a hot gas chamber on the other. The inventive component also includes at least one second cavity for admixing a second means, said second cavity is connected to the through-openings in a fluid-connected manner. A combustion chamber for a gas turbine, and to a gas turbine including one such component is also provided.
摘要翻译： 提供了一种用于燃气轮机的开式冷却部件。 该部件包括经受热气体的外壁，并且至少部分地限定第一装置的第一腔体。 外壁设有通孔，该开口在一侧开口进入空腔，并在另一侧开口进入热气室。 本发明的部件还包括用于混合第二装置的至少一个第二腔，所述第二腔以流体连接的方式连接到通孔。 还提供了一种用于燃气轮机的燃烧室和包括一个这种部件的燃气涡轮机。
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8.发明授权Open cooled component for a gas turbine, combustion chamber, and gas turbine 失效用于燃气轮机，燃烧室和燃气轮机的开式冷却部件公开(公告)号：US07658076B2
公开(公告)日：2010-02-09
申请号：US10561641
申请日：2004-06-16
申请人： Stefan Hoffmann
发明人： Stefan Hoffmann
IPC分类号： F02C1/00
CPC分类号： F23R3/30 , F01D5/186 , F01D25/12 , F05D2260/202 , F05D2260/221 , F23M5/085 , F23R3/002
摘要： The invention relates to an open-cooled component for a gas turbine having an outer wall which is subjected to hot gas and which at least partly defines a first cavity for a first medium and in which through-openings are arranged, which through-openings open into the cavity on the one side and into the hot-gas space on the other side, and having at least one second cavity for admixing a second medium, this second cavity being fluidically connected to the through-openings. In order to specify a component for a gas turbine with which flashback and spontaneous ignition during feeding of fuel into the cooling air can be reduced, it is proposed that the second cavity be formed by supply passages which are provided in the outer wall and are connected via transverse passages (4) to the through-openings designed as through-bores, so that the two media cannot be mixed until inside the through-bores.
摘要翻译： 本发明涉及一种用于燃气轮机的开式冷却部件，其具有经受热气体的外壁，并且至少部分地限定用于第一介质的第一空腔，并且其中布置有通孔，该通孔开口 进入一侧的空腔并进入另一侧的热气体空间，并具有用于混合第二介质的至少一个第二空腔，该第二空腔与通孔流体连接。 为了指定用于燃料供给到冷却空气中的回火和自发点燃的燃气轮机的部件，建议第二腔由设置在外壁中并连接的供应通道形成 通过设计为通孔的通孔的横向通道（4），使得两个介质不能混合直到通孔内部。
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公开(公告)号：US20080228490A1
公开(公告)日：2008-09-18
申请号：US12126507
申请日：2008-05-23
IPC分类号： G10L21/06
CPC分类号： G06F17/30056 , G06F17/30746 , G06F17/30855 , Y10S707/912
摘要： A method and apparatus for creating links between a representation, (e.g. text data,) and a realization, (e.g. corresponding audio data,) is provided. According to the invention the realization is structured by combining a time-stamped version of the representation generated from the realization with structural information from the representation. Thereby so called hyper links between representation and realization are created. These hyper links are used for performing search operations in realization data equivalent to those which are possible in representation data, enabling an improved access to the realization (e.g. via audio databases).
摘要翻译： 提供了用于在表示（例如文本数据）和实现之间创建链接（例如相应的音频数据）的方法和装置。 根据本发明，实现通过将从实现产生的表示的时间戳版本与来自表示的结构信息组合而构成。 从而创建所谓的表示和实现之间的超链接。 这些超链接用于执行与在表示数据中可能的那些相当的实现数据中的搜索操作，使得能够改进对实现的访问（例如，经由音频数据库）。
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公开(公告)号：US07412643B1
公开(公告)日：2008-08-12
申请号：US09447871
申请日：1999-11-23
CPC分类号： G06F17/30056 , G06F17/30746 , G06F17/30855 , Y10S707/912
摘要： A method and apparatus for creating links between a representation, (e.g. text data,) and a realization, (e.g. corresponding audio data,) is provided. According to the invention the realization is structured by combining a time-stamped version of the representation generated from the realization with structural information from the representation. Thereby so called hyper links between representation and realization are created. These hyper links are used for performing search operations in realization data equivalent to those which are possible in representation data, enabling an improved access to the realization (e.g. via audio databases).
摘要翻译： 提供了用于在表示（例如文本数据）和实现之间创建链接（例如相应的音频数据）的方法和装置。 根据本发明，实现通过将从实现产生的表示的时间戳版本与来自表示的结构信息组合而构成。 从而创建所谓的表示和实现之间的超链接。 这些超链接用于执行与在表示数据中可能的那些相当的实现数据中的搜索操作，使得能够改进对实现的访问（例如，经由音频数据库）。
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