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1. 发明授权

US06802121B2 Method for producing a cylinder block for an internal combustion engine 失效
标题翻译：一种用于制造用于内燃机的气缸体的方法
公开(公告)号：US06802121B2
公开(公告)日：2004-10-12
申请号：US10203415
申请日：2002-08-09
申请人： Antonio Fuganti , Paolo Barban , Ezio Merlo , Stefano Plano
发明人： Antonio Fuganti , Paolo Barban , Ezio Merlo , Stefano Plano
IPC分类号： B23P1500
CPC分类号： F02F1/004 , B22D19/0009 , B22D19/0081 , F02F2007/009 , F05C2201/021 , Y10T29/49231 , Y10T29/4927 , Y10T29/49272
摘要： Method for making a cylinder block for internal combustion engine, in which at least one cylinder liner (10) is arranged inside a mould and aluminium-based material is cast into the mould and cooled, so that the cylinder liner (10) is incorporated in the cylinder block. The cylinder liner (10) is made of aluminium-based material and has protuberances destined to melt in contact with the molten material cast into the mould arranged on its external surface.
摘要翻译：一种用于制造内燃机的气缸体的方法，其中在模具内布置至少一个气缸套（10），并将铝基材料浇铸到模具中并被冷却，使得气缸套（10）被引入气缸体。气缸套（10）由铝基材料制成，并且具有预定熔化的铸件与铸造在其外表面上的模具中的熔融材料接触。

2. 发明授权

US06789315B2 Establishing a throat area of a gas turbine nozzle, and a technique for modifying the nozzle vanes 有权
标题翻译：建立燃气轮机喷嘴的喉部区域以及用于改变喷嘴叶片的技术
公开(公告)号：US06789315B2
公开(公告)日：2004-09-14
申请号：US10104757
申请日：2002-03-21
申请人： Marcio Lins Tinoco Marques , Tathiana Carneiro de Rezende , Andreas Martin von Montfort , David Edwin Budinger , William G. Messelling
发明人： Marcio Lins Tinoco Marques , Tathiana Carneiro de Rezende , Andreas Martin von Montfort , David Edwin Budinger , William G. Messelling
IPC分类号： B23P1500
CPC分类号： B23P6/002 , F01D5/005 , F01D5/147 , F01D9/02 , F05D2230/23 , F05D2240/80 , Y02T50/67 , Y02T50/673 , Y10T29/49318 , Y10T29/49323 , Y10T29/49771 , Y10T29/49778
摘要： A final throat area of a gas turbine nozzle circumferential structure is established by providing at least two gas turbine nozzle vanes, and determining a pairwise initial throat area between each pair of gas turbine nozzle vanes. For each pair of gas turbine nozzle vanes whose pairwise initial throat area is not within the final pairwise throat area target range, a trailing edge of at least one of the gas turbine nozzle vanes is extended responsive to the step of determining the initial pairwise throat area, so that a final pairwise throat area is within a final pairwise throat area target range. A nozzle plurality of pairs of gas turbine nozzle vanes that together comprise the gas turbine nozzle circumferential structure may be selected so that a sum of their final pairwise throat areas is within a final total throat area target range. The trailing edge may be extended for this or other purposes by affixing an extension wire to the trailing edge extending lengthwise along the trailing edge, applying a braze material to the extension wire and the trailing edge, and heating the braze material to a brazing temperature to melt at least a portion of the braze material and, upon cooling, to bond the extension wire and the braze material to the trailing edge.
摘要翻译：通过设置至少两个燃气涡轮喷嘴叶片并确定每对燃气轮机喷嘴叶片之间的成对初始喉部区域来建立燃气涡轮喷嘴周向结构的最终喉部区域。对于其成对初始喉部区域不在最终成对喉部区域目标范围内的每对燃气轮机喷嘴叶片，响应于确定初始成对喉部区域的步骤来延伸至少一个燃气涡轮喷嘴叶片的后缘，使得最终成对喉部区域在最终成对喉部区域目标范围内。可以选择共同组成燃气轮机喷嘴周向结构的多对燃气涡轮喷嘴叶片，使得它们的最终成对喉部区域的总和在最终总喉部区域目标范围内。后缘可以通过将延伸线固定到沿着后缘沿纵向延伸的后缘，将延伸线施加到延伸线和后缘，并将钎焊材料加热至钎焊温度以延伸以达到或其它目的熔化钎焊材料的至少一部分，并且在冷却时将延伸线和钎焊材料粘合到后缘。

3. 发明授权

US06785961B1 Turbine nozzle segment and method of repairing same 失效
标题翻译：涡轮喷嘴段及其修理方法
公开(公告)号：US06785961B1
公开(公告)日：2004-09-07
申请号：US09438969
申请日：1999-11-12
申请人： James W. Caddell, Jr. , James M. Caldwell
发明人： James W. Caddell, Jr. , James M. Caldwell
IPC分类号： B23P1500
CPC分类号： B23P6/002 , F01D5/005 , F05D2240/10 , Y02T50/67 , Y10T29/49318 , Y10T29/49721 , Y10T29/4973
摘要： A method for repairing a turbine nozzle segment having at least two vanes disposed between outer and inner bands includes the steps of separating the nozzle segment into a first singlet containing a repairable vane and a second singlet containing a non-repairable vane, and joining the first singlet to a newly manufactured singlet having a configuration that is similar to the second singlet.
摘要翻译：一种用于修复具有设置在外部和内部带之间的至少两个叶片的涡轮喷嘴段的方法包括以下步骤：将喷嘴段分离成包含可修复叶片的第一单瓣瓣和包含不可修复叶片的第二单瓣形，并将第一单峰到具有类似于第二单峰的构造的新制造的单线态。

4. 发明授权

US06782605B1 Accumulator forming installation 失效
标题翻译：蓄电池成型安装
公开(公告)号：US06782605B1
公开(公告)日：2004-08-31
申请号：US10110529
申请日：2002-04-15
申请人： Franco Stocchiero
发明人： Franco Stocchiero
IPC分类号： B23P1500
CPC分类号： H01M4/0447 , H01M2/362 , H01M10/128 , Y10T29/49108 , Y10T29/53113 , Y10T29/53135 , Y10T29/53435
摘要： An installation for manufacturing accumulators employs a plurality of pallets for supporting the accumulators, a loading station (3), an unloading station (4), a power supply (5), and an electrolyte feeder (6). A casing (7) with projecting supports (8) is positioned side by side and aligned in vertical direction for supporting the pallets to create the same number of accumulator (A) manufacturing stations, and a handler (10) moves the pallets (2).
摘要翻译：用于制造蓄能器的装置采用多个用于支撑蓄能器的托盘，装载站（3），卸载站（4），电源（5）和电解液供给器（6）。具有突出支撑件（8）的壳体（7）并排设置并在垂直方向上对准以支撑托盘以产生相同数量的蓄能器（A）制造站，并且处理器（10）使托盘（2）移动，。

5. 发明授权

US06760971B2 Method of making a gas turbine engine diffuser 有权
标题翻译：制造燃气轮机发动机扩散器的方法
公开(公告)号：US06760971B2
公开(公告)日：2004-07-13
申请号：US10194556
申请日：2002-07-15
申请人： Ioan Sasu , Bertrand Gendreau , Robert Francois Lanoue
发明人： Ioan Sasu , Bertrand Gendreau , Robert Francois Lanoue
IPC分类号： B23P1500
CPC分类号： B23B41/00 , F04D29/444 , F05D2250/52 , Y10T29/49316 , Y10T29/4932 , Y10T29/49995 , Y10T29/49996 , Y10T408/03
摘要： A method of machining a plurality of circumferentially spaced bores in an object, each of the bores extending generally tangentially and inwardly and being positioned in the object so as to generally asymmetrically intersect two adjacent bores, comprises the steps of: providing an object; determining a plurality of bore positions generally around a circumference of the object; machining a first bore and performing at least one subsequent machining operation on the first bore to substantially complete the first bore; machining a second bore immediately adjacent to the completed first bore, wherein the second bore is machined so as to intersect the completed first bore, and performing at least one subsequent machining operation on the second bore to substantially complete the second bore; sequentially machining a remaining plurality of bores except a final bore, wherein each said bore is machined so as to intersect an immediately adjacent completed bore; and machining the final bore immediately intermediate the first bore and a second-final bore wherein the final bore is machined so as to intersect the first and second-final bores.
摘要翻译：一种在物体中加工多个周向间隔开的孔的方法，每个孔大体上切向和向内延伸并且被定位在物体中，以便大体上不对称地相交两个相邻的孔，包括以下步骤：提供物体; 通常围绕物体的圆周确定多个孔位置; 加工第一孔并在所述第一孔上执行至少一个随后的加工操作以基本上完成所述第一孔; 加工紧邻完成的第一孔的第二孔，其中第二孔加工成与完成的第一孔相交，并且在第二孔上执行至少一个随后的加工操作以基本上完成第二孔; 依次加工除了最终孔之外的剩余多个孔，其中每个所述孔加工成与紧邻的完成孔相交; 并且立即在第一孔的中间加工最终孔，以及第二最终孔，其中最终孔加工成与第一和第二最终孔相交。

6. 发明授权

US06748655B2 Method for profiling the outer circumferential face of cylinder liners 失效
标题翻译：气缸套外周面成型方法
公开(公告)号：US06748655B2
公开(公告)日：2004-06-15
申请号：US10270257
申请日：2002-10-11
申请人： Thomas Dickmann , Udo Kempken , Erik Mertner , Rolf Schattevoy
发明人： Thomas Dickmann , Udo Kempken , Erik Mertner , Rolf Schattevoy
IPC分类号： B23P1500
CPC分类号： F02F1/004 , B21J5/12 , F02F1/16 , F02F1/18 , Y10T29/4927 , Y10T29/49272
摘要： A method for producing, by forming techniques, an undercut profile in the outer circumferential face of cylinder liners to be cast in place in a crankcase, characterized by the introduction of a bracing inner core into the cavity of a cylinder liner, the introduction of the cylinder liner equipped with bracing inner core into a first forming die equipped on its working faces with a serrated profile, the pressing of the first forming die against the outer circumferential face of the cylinder liner, thus producing a complementary profile in the outer circumferential face, the introduction of the cylinder liner equipped with bracing inner core into a second forming die equipped on its working faces with a smooth surface, and the pressing of the second forming die against the outer circumferential face of the cylinder liner equipped with the complementary profile.
摘要翻译：通过形成技术来生产待铸造的汽缸套的外周面中的底切轮廓的方法，该曲轴在曲轴箱中就位，其特征在于将支撑内芯引入气缸套的空腔中，引入气缸衬套，其具有支撑内芯，在其工作面上装配有锯齿形轮廓的第一成形模具，将第一成形模压在气缸套的外周面上，从而在外圆周面上产生互补的轮廓，将配备有支撑内芯的气缸套引入装配在其工作面上的平滑表面的第二成型模具中，并且将第二成形模压在装配有补充轮廓的气缸套的外周面上。

7. 发明授权

US06739049B2 Method of manufacturing an article by diffusion bonding and superplastic forming 有权
标题翻译：通过扩散粘结和超塑性成型制造制品的方法
公开(公告)号：US06739049B2
公开(公告)日：2004-05-25
申请号：US10360804
申请日：2003-02-10
申请人： Stephen Nicholson
发明人： Stephen Nicholson
IPC分类号： B23P1500
CPC分类号： B21D26/055 , B21D53/78 , B23P15/04 , Y10T29/49336 , Y10T29/49339 , Y10T29/49341 , Y10T29/49805 , Y10T29/49885 , Y10T29/49995
摘要： A method of manufacturing a gas turbine engine fan blade (10) comprises forming three metal workpieces (50,52,54). A metal slab (30) is upset forged at both ends (32,34) to produce a metal block (40) with increased thickness (42,44) extending from opposite surfaces (36,38). The metal block (40) is cut in an inclined path to form two of the metal workpieces (50,52). The metal workpieces (50,52,54) are assembled into a stack (56) so that the flat surfaces (38,42,46,48) are in mating abutment. Heat and pressure is applied across the thickness of the metal workpieces (50,52,54) to diffusion bond the metal workpieces (53,52,54) together to form an integral structure (100). The integral structure (100) is hot creep formed and superplastically formed to produce the required aerofoil shape and the thickened end is machined to form the blade root (26). The method enables thinner metallic workpieces with better microstructure to be used and increases the yield of metallic workpieces.
摘要翻译：一种制造燃气涡轮发动机风扇叶片（10）的方法包括形成三个金属工件（50,52,54）。金属板坯（30）在两端（32,34）锻造，以产生具有从相对表面（36,38）延伸的厚度增加的（42,44）的金属块（40）。金属块（40）以倾斜路径切割以形成两个金属工件（50,52）。金属工件（50,52,54）组装成堆叠（56），使得平坦表面（38,42,46,48）处于配合邻接处。在金属工件（50,52,54）的厚度上施加热和压力以将金属工件（53,52,54）扩散连接在一起以形成整体结构（100）。整体结构（100）是热蠕变形成并被超塑性地形成以产生所需的机翼形状，并且加厚端被机加工以形成叶根（26）。该方法使得能够使用具有更好的微观结构的较薄的金属工件并增加金属工件的产量。

8. 发明授权

US06708407B2 Method for manufacturing a thermoroll for a paper/board machine or a finishing machine 失效
标题翻译：制造纸/纸机或精整机的热辊的方法
公开(公告)号：US06708407B2
公开(公告)日：2004-03-23
申请号：US10379085
申请日：2003-03-04
申请人： Erkki Leinonen , Mika Viljanmaa
发明人： Erkki Leinonen , Mika Viljanmaa
IPC分类号： B23P1500
CPC分类号： D21F5/022 , D21G1/0266 , Y10T29/49563
摘要： A thermoroll for a paper/board machine or a finishing machine, the thermoroll having a shell of metallic, ceramic or composite material, and the shell having ducts for passing a heating medium from one axial end of the thermoroll to the other axial end of the thermoroll. The shell is made by casting or by powder metallurgical methods, and the ducts are formed in the matrix material of the shell which is metal and/or ceramic.
摘要翻译：一种用于纸/纸机或整理机的加热棒，该热棒具有金属，陶瓷或复合材料的壳体，并且该壳体具有用于将加热介质从热棒的一个轴向端部传递到另一轴向端部的管道加热棒壳体通过铸造或通过粉末冶金方法制成，并且管道形成在壳体的基体材料中，其为金属和/或陶瓷。

9. 发明授权

US06702908B1 Method of making a cylinder block with unlined piston bores 有权
标题翻译：制造具有无衬里活塞孔的气缸体的方法
公开(公告)号：US06702908B1
公开(公告)日：2004-03-09
申请号：US10050728
申请日：2002-01-16
申请人： Henry R. Vanderzyden
发明人： Henry R. Vanderzyden
IPC分类号： B23P1500
CPC分类号： F04B1/2035 , B23P15/00 , F01B3/0064 , F01B3/0091 , Y10T29/49231 , Y10T29/4927
摘要： A cylinder block for an axial piston pump or motor is formed from a steel material. The block includes a plurality of bores that each have an internal bore surface of a predefined final material surface finish. The bores are subjected to various machining and heat treating processes to provide a bore surface formed from the same material as the cylinder block, and which has the desired final surface finish. Pistons are mounted within each of the bores for axial movement relative to the cylinder block. Each of the pistons is formed from a steel material and has an exterior surface that is in sliding contact with the internal bore surface. The subject cylinder block is processed to provide a steel-to-steel interface between the bore and piston and eliminates the need for liners to be specially formed or installed within each piston bore.
摘要翻译：用于轴向柱塞泵或马达的气缸体由钢材料形成。该块包括多个孔，每个孔具有预定的最终材料表面光洁度的内孔表面。孔经受各种加工和热处理工艺以提供由与气缸体相同的材料形成的孔表面，并且具有期望的最终表面光洁度。活塞安装在每个孔内，用于相对于气缸体的轴向移动。每个活塞由钢材制成并具有与内孔表面滑动接触的外表面。主体缸体被处理以在孔和活塞之间提供钢 - 钢接口，并且不需要在每个活塞孔内特别形成或安装衬垫。

10. 发明授权

US06691410B2 Method of inspecting a geometry and dimensional accuracy of a circular recuperator inspection fixture 有权
标题翻译：检查圆形换热器检查夹具的几何形状和尺寸精度的方法
公开(公告)号：US06691410B2
公开(公告)日：2004-02-17
申请号：US09999711
申请日：2001-10-31
申请人： Charles W. Bucey , Gregory D. Gleason
发明人： Charles W. Bucey , Gregory D. Gleason
IPC分类号： B23P1500
CPC分类号： G01B3/30 , F28D9/0018 , G01B3/50 , Y10T29/49357 , Y10T29/49771 , Y10T29/49778 , Y10T29/53043
摘要： An inspection fixture and line is used to accurately determine the geometry and dimensional accuracy of a circular recuperator core. With the fixture and line inspection of a length, an inner diameter and an outer diameter of the circular recuperator core are completed. The method of using the fixture and the line further insures the concentricity of a donor inlet duct and a donor outlet duct.
摘要翻译：检查夹具和线用于准确地确定圆形换热器芯的几何形状和尺寸精度。通过长度的夹具和线检查，完成圆形换热器芯的内径和外径。使用夹具和管线的方法进一步确保了供体入口管和供体出口管的同心度。

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