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1. 发明授权

US6032361A Gas turbine multi-hole film cooled combustor liner and method of manufacturing 失效
标题翻译：燃气轮机多孔薄膜冷却燃烧器衬管及其制造方法
公开(公告)号：US6032361A
公开(公告)日：2000-03-07
申请号：US989650
申请日：1997-12-12
申请人： Yoshinobu Makino , Kiyoshi Yamada , Hiroshi Matsui , Yoshihiro Aburatani , Yamato Kaminaka , Hiroshi Kubo , Hiroaki Okamoto
发明人： Yoshinobu Makino , Kiyoshi Yamada , Hiroshi Matsui , Yoshihiro Aburatani , Yamato Kaminaka , Hiroshi Kubo , Hiroaki Okamoto
IPC分类号： F02C7/00 , B23K26/24 , B23K26/28 , B23K26/38 , F23R3/00 , F23R3/06 , F23R3/42 , B23P15/00
CPC分类号： F23R3/002 , B23K26/244 , B23K26/282 , B23K26/384 , B23K26/388 , B23K26/389 , B23K26/40 , B23K2201/001 , B23K2203/26 , B23P2700/13 , F05B2260/202 , Y10T29/4932 , Y10T29/49346
摘要： Provided are a gas turbine multi-hole film-cooled combustor liner, which can be manufactured with improved accuracy in shape and position of cooling holes in a very short time, ensuring desirable buckling strength and satisfactory cooling performance. A planar flat member is curved to form a liner shell of a cylindrical shape, the cylindrical member is welded in the longitudinal direction thereof to form a cylindrical shell. Then a wavy configuration and a corrugated configuration are formed on the cylindrical shell by a hydro-bulging method, cooling holes are formed through the liner shell by laser drilling at or near wave crest portions of the wavy configuration of the liner shell, and inner rings are attached to the liner shell by resistance spot welding or vacuum brazing.
摘要翻译：本发明提供一种燃气轮机多孔薄膜冷却燃烧器衬套，能够在非常短的时间内提高冷却孔的形状和位置的精度，确保理想的翘曲强度和令人满意的冷却性能。平面平面构件弯曲以形成圆柱形的衬套，圆柱形构件沿其纵向方向焊接以形成圆柱形壳体。然后通过水力膨胀方法在圆柱形壳体上形成波状结构和波纹状结构，通过在衬套壳的波状构造的波峰部分处或附近通过激光钻孔在衬套壳体上形成冷却孔，并且内圈通过电阻点焊或真空钎焊连接到衬套外壳。

2. 发明授权

US5826431A Gas turbine multi-hole film cooled combustor liner and method of manufacture 失效
标题翻译：燃气轮机多孔薄膜冷却燃烧器衬管及其制造方法
公开(公告)号：US5826431A
公开(公告)日：1998-10-27
申请号：US596827
申请日：1996-02-05
申请人： Yoshinobu Makino , Kiyoshi Yamada , Hiroshi Matsui , Yoshihiro Aburatani , Yamato Kaminaka , Hiroshi Kubo , Hiroaki Okamoto
发明人： Yoshinobu Makino , Kiyoshi Yamada , Hiroshi Matsui , Yoshihiro Aburatani , Yamato Kaminaka , Hiroshi Kubo , Hiroaki Okamoto
IPC分类号： F02C7/00 , B23K26/24 , B23K26/28 , B23K26/38 , F23R3/00 , F23R3/06 , F23R3/42 , F02G3/00
CPC分类号： F23R3/002 , B23K26/244 , B23K26/282 , B23K26/384 , B23K26/388 , B23K26/389 , B23K26/40 , B23K2201/001 , B23K2203/26 , B23P2700/13 , F05B2260/202 , Y10T29/4932 , Y10T29/49346
摘要： Provided are a gas turbine multi-hole film-cooled combustor liner, which can be manufactured with improved accuracy in shape and position of cooling holes in a very short time, ensuring desirable buckling strength and satisfactory cooling performance. A planar flat member is curved to form a liner shell of a cylindrical shape, the cylindrical member is welded in the longitudinal direction thereof to form a cylindrical shell. Then a wavy configuration and a corrugated configuration are formed on the cylindrical shell by a hydro-bulging method, cooling holes are formed through the liner shell by laser drilling at or near wave crest portions of the wavy configuration of the liner shell, and inner rings are attached to the liner shell by resistance spot welding or vacuum brazing.
摘要翻译：本发明提供一种燃气轮机多孔薄膜冷却燃烧器衬套，能够在非常短的时间内提高冷却孔的形状和位置的精度，确保理想的翘曲强度和令人满意的冷却性能。平面平面构件弯曲以形成圆柱形的衬套，圆柱形构件沿其纵向方向焊接以形成圆柱形壳体。然后通过水力膨胀方法在圆柱形壳体上形成波状结构和波纹状结构，通过在衬套壳的波状构造的波峰部分处或附近通过激光钻孔在衬套壳体上形成冷却孔，并且内圈通过电阻点焊或真空钎焊连接到衬套外壳。

3. 发明授权

US06348232B1 Spraying robot system and spraying method wherein spray conditions are determined by using computer 失效
标题翻译：喷涂机器人系统和喷涂方法，其中通过使用计算机确定喷雾条件
公开(公告)号：US06348232B1
公开(公告)日：2002-02-19
申请号：US09284474
申请日：1999-04-21
申请人： Itaru Chida , Masayuki Itoh , Keizoh Honda , Takeshi Takahara , Yamato Kaminaka
发明人： Itaru Chida , Masayuki Itoh , Keizoh Honda , Takeshi Takahara , Yamato Kaminaka
IPC分类号： C23C412
CPC分类号： C23C4/12
摘要： An object of the present invention is to provide a thermal spraying robot system capable of automatically determining spraying conditions according to the shape of a workpiece. Shape data on a workpiece (9) and material data on a thermal spray material are entered by operating a data input unit (1). A spray condition database 3 stores a plurality of spray parameters for kinds of thermal spray materials and for qualities of sprayed coatings. A path calculating unit (4) selects values of spray parameters from the spray condition database (3), and then calculates a path for a thermal spraying gun (14) according to a predetermined program on the basis of the shape data on the workpiece and the selected values of the spray parameters. The path calculating unit (4) decides whether or not a thermal spraying operation can be carried out by moving the thermal spraying gun along a calculated path. If it is decided that the thermal spraying operation is feasible, a thermal spraying apparatus 10 carries out the thermal spraying operation in which the thermal spraying gun is moved along the calculated path.
摘要翻译：本发明的目的是提供一种能够根据工件的形状自动确定喷涂条件的热喷涂机器人系统。通过操作数据输入单元（1）输入工件（9）上的形状数据和热喷涂材料上的材料数据。喷雾条件数据库3存储用于各种热喷涂材料的多个喷雾参数和喷涂涂层的质量。路径计算单元（4）从喷雾条件数据库（3）中选择喷射参数值，然后根据工件上的形状数据根据预定程序计算热喷枪（14）的路径，喷雾参数的选定值。路径计算单元（4）通过沿着计算的路径移动热喷枪来判定热喷涂操作是否可以进行。如果确定热喷涂操作是可行的，则热喷涂装置10执行热喷涂操作，其中热喷枪沿所计算的路径移动。

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