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1. 发明申请

US20130045093A1 METHOD FOR THE MANUFACTURE OF A COMPONENT FOR HIGH THERMAL LOADS, A COMPONENT PRODUCIBLE BY THIS METHOD AND AN AIRCRAFT ENGINE PROVIDED WITH THE COMPONENT 有权
标题翻译：用于制造高热负荷的组件的方法，通过该方法制造的组件和由组件提供的飞机发动机
公开(公告)号：US20130045093A1
公开(公告)日：2013-02-21
申请号：US13588133
申请日：2012-08-17
申请人： Thomas WUNDERLICH , Dan ROTH-FAGARASEANU , Susanne GEBHARD
发明人： Thomas WUNDERLICH , Dan ROTH-FAGARASEANU , Susanne GEBHARD
IPC分类号： B23K26/00 , F01D1/00
CPC分类号： C23C24/10 , B22F3/1055 , B22F7/04 , B23K26/32 , B23K26/342 , B23K35/0244 , B23K35/3033 , B23K35/3607 , B23K35/361 , B23K2101/006 , B23K2103/08 , B23K2103/18 , B23K2103/26 , B23K2103/50 , B33Y10/00 , B33Y70/00 , B33Y80/00 , C22C19/055 , C22C19/056 , C22C19/057 , C23C26/00 , F01D25/005 , Y02P10/295
摘要： A method for manufacturing a thermally deformable component for high thermal loads, includes: providing a first area of the component with a first metallic material by a generative laser process, or making the first area of the first metallic material; providing a second area of the component with a second metallic material by a generative laser process, or making the second area of the second metallic material; where at least one of the metallic materials is deposited by the generative laser process, and a ratio of a linear expansion coefficient α1 of the first metallic material and of a linear expansion coefficient α2 of the second metallic material is as: α 2  ( T 2 ) α 1  ( T 1 ) = x   T 1 - T 0   T 2 - T 0  , where x=0.5 to 1; T1=mean operating temperature on a hot side; T0=reference temperature; T2=mean operating temperature on a cold side.
摘要翻译：一种用于制造用于高热负荷的热变形部件的方法，包括：通过生成激光工艺为部件的第一区域提供第一金属材料，或者制造第一金属材料的第一区域; 通过生成激光处理提供具有第二金属材料的部件的第二区域，或者制造第二金属材料的第二区域; 其中通过生成激光处理沉积至少一种金属材料，并且第一金属材料的线性膨胀系数α1与第二金属材料的线性膨胀系数α2的比率为：α2（T 2）α1（T 1）= x T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T T1 =热侧平均工作温度; T0 =参考温度; T2 =冷侧平均工作温度。

2. 发明授权

US07780174B2 Door seal for a turbomachine 有权
标题翻译：涡轮机的门密封
公开(公告)号：US07780174B2
公开(公告)日：2010-08-24
申请号：US11783751
申请日：2007-04-11
申请人： Thomas Wunderlich , Hans-Frieder Vogt
发明人： Thomas Wunderlich , Hans-Frieder Vogt
IPC分类号： F16J15/02
CPC分类号： F01D11/005 , F01D9/023 , F02C7/28
摘要： With a door seal for a gas turbine engine, a gap (3) existing between an axially symmetrical component (1) and an assembly formed by several segments (2) is sealed by seal doors (11), which are held via retaining holes (10) at retaining bolts (9) on one of the components, the seal doors (11) being pressed against sealing edges (5, 7) of the two components, with the sealing edges (5, 7) being disposed at a certain distance from each other. The retaining bolts and holes are located outside the pressure surface (A) of the seal doors, formed between the two sealing edges, thus preventing cooling air losses via a gap remaining between the retaining bolts and bores.
摘要翻译：利用用于燃气涡轮发动机的门密封件，存在于轴向对称部件（1）和由多个段（2）形成的组件之间的间隙（3）由密封门（11）密封，密封门通过保持孔如图10所示，在其中一个部件上的固定螺栓（9）上，密封门（11）被按压在两个部件的密封边缘（5,7）上，密封边缘（5,7）以一定距离从彼此。固定螺栓和孔位于形成在两个密封边缘之间的密封门的压力表面（A）的外侧，从而通过留在保持螺栓和孔之间的间隙来防止冷却空气损失。

3. 发明授权

US07524164B2 Arrangement for the automatic running gap control on a two or multi-stage turbine 有权
标题翻译：在两级或多级涡轮机上进行自动运行间隙控制的布置
公开(公告)号：US07524164B2
公开(公告)日：2009-04-28
申请号：US11088840
申请日：2005-03-25
申请人： Thomas Wunderlich , Harald Schiebold , Peter Broadhead
发明人： Thomas Wunderlich , Harald Schiebold , Peter Broadhead
IPC分类号： F01D11/16 , F01D9/00 , F01D25/26
CPC分类号： F01D11/24 , F01D11/18 , F01D25/26 , F05D2240/11
摘要： On a two or multi-stage turbine, expansion rings are provided in all stages at the sides of the rotors for passive, continuous running gap control whose thermal expansion and contraction behavior corresponds to that of the rotors and which are connected to radially moveable upstream and downstream stator vanes (5, 7). The downstream stator vanes are assembled to the upstream stator vanes via a bridge (16; 17, 18) which is axially and circumferentially fixed and located flexibly in the radial direction on the outer casing (10) of the turbine. The stator vanes (6) arranged between the rotor disks are integrally connected to the bridge or, as separate components, held axially and circumferentially on the bridge to take up rolling and tilting moments.
摘要翻译：在两级或多级涡轮机上，在转子侧面的所有阶段都设有膨胀环，用于被动连续运行间隙控制，其热膨胀和收缩行为对应于转子的膨胀和收缩行为，并且连接到径向可移动的上游和下游定子叶片（5,7）。下游定子叶片经由桥（16; 17,18）组装到上游定子叶片上，所述桥（16; 17,18）沿涡轮机的外壳（10）沿径向方向轴向和周向地固定和定位。布置在转子盘之间的定子叶片（6）一体地连接到桥上，或者作为单独的部件轴向和周向地保持在桥上以卷取滚动和倾斜力矩。

4. 发明授权

US07306428B2 Gas turbine with running gap control 有权
标题翻译：燃气轮机运行间隙控制
公开(公告)号：US07306428B2
公开(公告)日：2007-12-11
申请号：US10933257
申请日：2004-09-03
申请人： Harald Schiebold , Olaf Mistareck , Thomas Wunderlich
发明人： Harald Schiebold , Olaf Mistareck , Thomas Wunderlich
IPC分类号： F01D11/22 , F01D11/08
CPC分类号： F01D11/18
摘要： A gas turbine with several shroud segments (1) which enclose rotor blades (3) of a turbine wheel (5) as a seal, with the shroud segments (1) having at least a front and a rear attachment at the radially outward area of stator vane segments (7, 12), and with each of the stator vane segments (7, 12) being located at their radially inner area on a control ring (9, 10), wherein the stator vane segments (7, 12) are located on the control ring (9, 10) in a radially adjustable manner.
摘要翻译：一种燃气轮机，其具有围绕涡轮机叶轮（5）的转子叶片（3）封闭的几个护罩段（1），其中护罩段（1）至少具有前部和后部附件在径向向外的区域定子叶片段（7,12），并且每个定子叶片段（7,12）位于控制环（9,10）的径向内部区域，其中定子叶片段（7,12）是以可径向调节的方式位于控制环（9,10）上。

5. 发明授权

US07588414B2 Arrangement for internal passive turbine blade tip clearance control in a high pressure turbine 有权
标题翻译：高压涡轮机内部被动涡轮叶片顶端间隙控制的布置
公开(公告)号：US07588414B2
公开(公告)日：2009-09-15
申请号：US11403809
申请日：2006-04-14
申请人： Thomas Wunderlich , Peter Broadhead
发明人： Thomas Wunderlich , Peter Broadhead
IPC分类号： F01D11/18
CPC分类号： F01D11/18 , F01D9/041
摘要： A passive internal control system for rotor blade tip clearance of a high-pressure turbine is based on inner rings that expand in a radial direction under the influence of heat and radially adjust the clearance delimited by liner segments (9) on the casing side. It comprises a radially expandable U-shaped downstream inner ring (10) mounted to inner platforms (7b) of guide vanes (7) on a side where the rotor does not have a static bearing, said ring providing expansion compensation in the axial and peripheral directions and forming a torsion box (8) with struts (13, 14) that absorbs rolling and tilting moments.
摘要翻译：用于高压涡轮机的转子叶片顶端间隙的被动内部控制系统基于在热影响下在径向方向上膨胀的内环，并且径向地调节由套管侧上的衬套段（9）限定的间隙。它包括安装在导向叶片（7）的内平台（7b）上的径向可膨胀的U形下游内圈（10），转子不具有静态轴承，所述环在轴向和周边提供膨胀补偿方向并且形成具有吸收滚动和倾斜力矩的支柱（13,14）的扭转箱（8）。

6. 发明申请

US20090010758A1 Suspension arrangement for the casing shroud segments 有权
标题翻译：套管护罩段的悬挂装置
公开(公告)号：US20090010758A1
公开(公告)日：2009-01-08
申请号：US12216459
申请日：2008-07-03
申请人： Thomas Wunderlich
发明人： Thomas Wunderlich
IPC分类号： F04D29/40
CPC分类号： F01D25/246 , F01D11/08 , F05D2230/60 , F05D2240/11 , Y02T50/671
摘要： A suspension arrangement for the casing shroud segments of the high-pressure turbine of a jet engine with inclination or graduation of the rotor blade tips (4) includes spaced apart attaching hooks (11) formed onto the casing shroud segments (2) which engage an axial retaining groove (13) on the turbine casing (1) on the upstream side and which are axially retained in the downstream direction by a retaining ring (14) arranged in a retaining ring groove (15) formed onto the turbine casing. In the retaining ring groove (15), assembly pockets (19) are provided on the downstream side, with the assembly pockets (19) agreeing with the distance and dimensioning of the attaching hooks (11), so that—with the rotor installed—axial travel (s2) of the casing shroud segments (2) is reduced and handling clearance is increased, when the casing shroud segments (2) are installed.
摘要翻译：用于具有转子叶片尖端（4）的倾斜或分级的喷气发动机的高压涡轮机的壳体护罩部分的悬挂装置包括形成在壳体护罩部分（2）上的间隔开的附接钩（11），其接合轴向保持槽（13），位于上游侧的涡轮机壳体（1）上并且通过设置在形成于涡轮机壳体上的保持环槽（15）中的保持环（14）沿下游方向轴向保持。在保持环槽（15）中，组装袋（19）设置在下游侧，组装袋（19）与安装钩（11）的距离和尺寸一致，因此，当安装壳体护罩段（2）时，壳体护罩区段（2）的轴向行程（s2）减小并且操纵间隙增大。

7. 发明授权

US06719361B1 Truck sleeper cab to day cab conversion kit assembly 有权
标题翻译：卡车卧铺驾驶室到日间驾驶室转换套件组装
公开(公告)号：US06719361B1
公开(公告)日：2004-04-13
申请号：US10282059
申请日：2002-10-29
申请人： David Scott Adams , James Thomas Wunderlich , Donald Michael Reed
发明人： David Scott Adams , James Thomas Wunderlich , Donald Michael Reed
IPC分类号： B62D3306
CPC分类号： B62D33/0612
摘要： A conversion kit assembly for converting a sleeper truck cab with a modular sleeper/cab into a day cab includes a sleeper truck cab including a rear sill, two laterally spaced walls, and a roof, with each of the walls having a B-pillar assembly at a rearward end of the sleeper truck cab. The B-pillar assemblies are coupled together at their upper ends by the roof, and at their lower ends by a lower member such as a lower panel or a rear sill such that the rearward end of the sleeper truck cab is substantially square. The sleeper truck cab further has a plurality of attachment points at the rearward end for attaching the modular sleeper. A first plurality of fasteners, which connect the modular sleeper to the sleeper truck cab, are removed. The modular sleeper is removed from the sleeper truck cab thereby creating a rearward opening at rearward end of modular truck cab. A closeoff panel assembly comprising a frame sub-assembly and an outer panel welded to the frame sub-assembly is then attached to the sleeper truck cab by fasteners disposed at locations corresponding to at least some of the plurality of attachment points. The closeoff panel assembly is provided to close the rearward opening created by removal of the modular sleeper from the sleeper truck cab. First and second reinforcement members connect the closeoff panel assembly to the B-pillar assemblies of the sleeper truck cab, and third and fourth reinforcement members connect the closeoff panel assembly to the lower panel or rear sill of the sleeper truck cab, to distribute loads from the closeoff panel to the sleeper truck cab, and thence to the vehicle chassis. A load is distributed from the closeoff panel assembly to the sleeper truck cab with the reinforcement members. A gasket is also used between the sleeper truck cab and the closeoff panel assembly to seal moisture from the cab.
摘要翻译：用于将具有模块化卧铺机/驾驶室的卧铺车厢转换成日间驾驶室的转换套件组件包括包括后门槛，两个横向间隔开的壁和屋顶的卧铺车，其中每个壁具有B柱组件在卧铺车厢的后端。 B柱组件在其上端由屋顶联接在一起，并且在其下端由诸如下面板或后梁的下部构件联接在一起，使得卧铺车厢的后端基本上是正方形的。卧铺车厢还在后端具有多个附接点，用于连接模块化的卧铺。去除了将模块化卧铺连接到卧铺车厢的第一组紧固件。将模块化的卧铺从卧铺卡车驾驶室中取出，从而在模块化卡车驾驶室的后端形成向后的开口。然后，将包括框架子组件和焊接到框架子组件的外板的闭合面板组件通过设置在对应于多个附接点中的至少一些的位置处的紧固件附接到轨枕卡车驾驶室。提供闭路面板组件以关闭通过从卧铺车厢移除模块化的卧铺而产生的向后开口。第一和第二加强构件将闭路面板组件连接到卧铺驾驶室的B柱组件，并且第三和第四加强构件将闭路面板组件连接到卧铺车厢的下板或后梁，以将负载从卧铺车厢的接近面板，然后到车辆底盘。负载从紧急面板组件分配到具有加强构件的卧铺车厢。卧铺车和闭路面板组件之间也使用垫圈来密封驾驶室的水分。

8. 发明授权

US08152455B2 Suspension arrangement for the casing shroud segments 有权
标题翻译：套管护罩段的悬挂装置
公开(公告)号：US08152455B2
公开(公告)日：2012-04-10
申请号：US12216459
申请日：2008-07-03
申请人： Thomas Wunderlich
发明人： Thomas Wunderlich
IPC分类号： F01D5/20 , F01D11/08
CPC分类号： F01D25/246 , F01D11/08 , F05D2230/60 , F05D2240/11 , Y02T50/671
摘要： A suspension arrangement for the casing shroud segments of the high-pressure turbine of a jet engine with inclination or graduation of the rotor blade tips (4) includes spaced apart attaching hooks (11) formed onto the casing shroud segments (2) which engage an axial retaining groove (13) on the turbine casing (1) on the upstream side and which are axially retained in the downstream direction by a retaining ring (14) arranged in a retaining ring groove (15) formed onto the turbine casing. In the retaining ring groove (15), assembly pockets (19) are provided on the downstream side, with the assembly pockets (19) agreeing with the distance and dimensioning of the attaching hooks (11), so that—with the rotor installed—axial travel (s2) of the casing shroud segments (2) is reduced and handling clearance is increased, when the casing shroud segments (2) are installed.
摘要翻译：用于具有转子叶片尖端（4）的倾斜或分级的喷气发动机的高压涡轮机的壳体护罩部分的悬挂装置包括形成在壳体护罩部分（2）上的间隔开的附接钩（11），其接合轴向保持槽（13），位于上游侧的涡轮机壳体（1）上并且通过设置在形成于涡轮机壳体上的保持环槽（15）中的保持环（14）沿下游方向轴向保持。在保持环槽（15）中，组装袋（19）设置在下游侧，组装袋（19）与安装钩（11）的距离和尺寸一致，因此，当安装壳体护罩段（2）时，壳体护罩区段（2）的轴向行程（s2）减小并且操纵间隙增大。

9. 发明申请

US20100018425A1 METHOD FOR OPERATING A WEB-FED PRINTING PRESS 失效
标题翻译：操作WEB-FED印刷机的方法
公开(公告)号：US20100018425A1
公开(公告)日：2010-01-28
申请号：US12509179
申请日：2009-07-24
申请人： Ralf Schaedlich , Klaus Toepfer , Thomas Wunderlich
发明人： Ralf Schaedlich , Klaus Toepfer , Thomas Wunderlich
IPC分类号： B41F33/00
CPC分类号： B41F33/12 , B41P2233/10
摘要： A method for starting up a web-fed printing press is disclosed. In an embodiment, the method includes: a) a first start-up sequence is executed while using predetermined preset parameters that are specific to the printing press and/or the print job for the color register adjustment, cut-off compensator control and the ink density control; b) the web-fed printing press is subsequently stopped, where copies printed during the first start-up sequence are evaluated with respect to the color register, the cut-off compensator and the ink density, and where the preset parameters are adjusted as a function of this evaluation while the printing press is stopped; c) following this, a second start-up sequence is executed, where the preset parameters that are adjusted during the standstill are not used for printing until defined printing press speeds are reached and/or exceeded.
摘要翻译：公开了一种启动卷筒纸式印刷机的方法。在一个实施例中，该方法包括：a）使用特定于印刷机的预定预设参数和/或用于颜色寄存器调整，切断补偿器控制和墨水的打印作业执行第一启动顺序密度控制 b）随后停止卷筒纸式印刷机，其中在第一启动顺序期间打印的副本相对于颜色寄存器，截止补偿器和墨水密度进行评估，并且将预设参数调整为当打印机停止时，该评估的功能; c）之后，执行第二启动顺序，其中在停止期间调整的预设参数不被用于打印，直到达到和/或超过定义的印刷速度。

10. 发明申请

US20090269190A1 Arrangement for automatic running gap control on a two or multi-stage turbine 审中-公开
标题翻译：在两级或多级涡轮机上自动运行间隙控制的布置
公开(公告)号：US20090269190A1
公开(公告)日：2009-10-29
申请号：US12453010
申请日：2009-04-27
申请人： Thomas Wunderlich , Harald Schiebold , Peter Broadhead
发明人： Thomas Wunderlich , Harald Schiebold , Peter Broadhead
IPC分类号： F01D11/00
CPC分类号： F01D11/24 , F01D11/18 , F01D25/26 , F05D2240/11
摘要： On a two or multi-stage turbine, expansion rings are provided in all stages at the sides of the rotors for passive, continuous running gap control whose thermal expansion and contraction behavior corresponds to that of the rotors and which are connected to radially moveable upstream and downstream stator vanes (5, 7). The downstream stator vanes are assembled to the upstream stator vanes via a bridge (16; 17, 18) which is axially and circumferentially fixed and located flexibly in the radial direction on the outer casing (10) of the turbine. The stator vanes (6) arranged between the rotor disks are integrally connected to the bridge or, as separate components, held axially and circumferentially on the bridge to take up rolling and tilting moments.
摘要翻译：在两级或多级涡轮机上，在转子侧面的所有阶段都设有膨胀环，用于被动连续运行间隙控制，其热膨胀和收缩行为对应于转子的膨胀和收缩行为，并且连接到径向可移动的上游和下游定子叶片（5,7）。下游定子叶片经由桥（16; 17,18）组装到上游定子叶片上，所述桥（16; 17,18）沿涡轮机的外壳（10）沿径向方向轴向和周向地固定和定位。布置在转子盘之间的定子叶片（6）一体地连接到桥上，或者作为单独的部件轴向和周向地保持在桥上以卷取滚动和倾斜力矩。

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