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公开(公告)号：US20120275873A1
公开(公告)日：2012-11-01
申请号：US13095498
申请日：2011-04-27
CPC分类号： F01D25/243 , B23B35/00 , B23B41/00 , B23B2215/76 , B23B2270/30 , B23B2270/62 , B23Q11/0046 , F05D2230/80 , F05D2260/607 , Y10T408/03 , Y10T408/50
摘要： A method of drilling one or more holes, substantially in situ, in a turbomachine casing includes locating piping including at least one vacuum head within the turbomachine casing in proximity to a hole to be drilled; drilling at least one hole in the casing such that drill chips or shavings caused by the drilling are collected in the vacuum head; and applying a vacuum through the piping to the at least one vacuum head to thereby remove the drill chips or shavings collected in the vacuum head to a location outside the turbomachine casing.
摘要翻译： 在涡轮机壳体中基本上原位钻一个或多个孔的方法包括将涡轮机壳体内的至少一个真空头定位在靠近待钻孔的位置， 在壳体中钻出至少一个孔，使得由钻孔引起的钻屑或刨屑被收集在真空头中; 以及通过所述管道将真空施加到所述至少一个真空头，从而将收集在所述真空头中的钻屑或切屑除去到所述涡轮机壳体外部的位置。
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公开(公告)号：US08636449B2
公开(公告)日：2014-01-28
申请号：US13095498
申请日：2011-04-27
IPC分类号： B23B47/34
CPC分类号： F01D25/243 , B23B35/00 , B23B41/00 , B23B2215/76 , B23B2270/30 , B23B2270/62 , B23Q11/0046 , F05D2230/80 , F05D2260/607 , Y10T408/03 , Y10T408/50
摘要： A method of drilling one or more holes, substantially in situ, in a turbomachine casing includes locating piping including at least one vacuum head within the turbomachine casing in proximity to a hole to be drilled; drilling at least one hole in the casing such that drill chips or shavings caused by the drilling are collected in the vacuum head; and applying a vacuum through the piping to the at least one vacuum head to thereby remove the drill chips or shavings collected in the vacuum head to a location outside the turbomachine casing.
摘要翻译： 在涡轮机壳体中基本上原位钻一个或多个孔的方法包括将涡轮机壳体内的至少一个真空头定位在靠近待钻孔的位置， 在壳体中钻出至少一个孔，使得由钻孔引起的钻屑或刨屑被收集在真空头中; 以及通过所述管道将真空施加到所述至少一个真空头，从而将收集在所述真空头中的钻屑或切屑除去到所述涡轮机壳体外部的位置。
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公开(公告)号：US20130171611A1
公开(公告)日：2013-07-04
申请号：US13342655
申请日：2012-01-03
IPC分类号： G09B25/00
CPC分类号： G09B25/02
摘要： This disclosure describes a training apparatus, wherein embodiments of the training apparatus simulate operation of fan blades in a turbine engine. An advantage that practice of some disclosed embodiments of the training apparatus is to provide a platform to train skills for maintaining and servicing turbine engines without placing the individual and/or customer hardware in jeopardy.
摘要翻译： 本公开描述了训练装置，其中训练装置的实施例模拟涡轮发动机中的风扇叶片的操作。 培训设备的一些公开的实施例的实践的优点是提供一个平台来训练维护和维修涡轮发动机的技能，而不会使个人和/或客户硬件处于危险之中。
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