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Patent Agency Ranking
公开(公告)号：WO2014099160A1
公开(公告)日：2014-06-26
申请号：PCT/US2013/068745
申请日：2013-11-06
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： BOGUE, William , PRIHAR, Ron, I.P.E.
CPC classification number: F02C7/12 , B23P6/002 , B23P2700/06 , C23C4/00 , C25D7/04 , F01D5/18 , F01D5/284 , F01D5/288 , F01D25/12 , F05D2230/90 , Y02T50/675
Abstract: A method for filling cooling holes in a component of a gas turbine engine is disclosed. The component may include a plurality of first cooling holes penetrating the wall of the component. The method may comprise the steps of exposing the outer surface of the component, filling the plurality of first cooling holes of the component with a filling agent, curing the filling agent to block the passage of air through the cooling holes, and applying a thermal barrier coating over the surface of the component. The method may further include installing a second plurality of cooling holes, the second plurality of cooling holes penetrating the thermal barrier coating and the wall of the component and allow air to pass therethrough.
Abstract translation: 公开了一种用于填充燃气涡轮发动机的部件中的冷却孔的方法。 该部件可以包括穿过部件的壁的多个第一冷却孔。 该方法可以包括以下步骤：暴露组件的外表面，用填充剂填充组件的多个第一冷却孔，固化填充剂以阻止空气通过冷却孔，并且施加热障碍 涂覆在组件的表面上。 该方法可以进一步包括安装第二多个冷却孔，第二多个冷却孔穿过热障涂层和部件的壁并允许空气通过。
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公开(公告)号：WO2014099161A1
公开(公告)日：2014-06-26
申请号：PCT/US2013/068750
申请日：2013-11-06
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： BOGUE, William , PRIHAR, Ron, I.P.E.
CPC classification number: B05D7/22 , B23P6/007 , B23P2700/06 , B23P2700/13 , C23C4/02 , F01D5/005 , F01D5/288 , F05D2230/42 , F05D2230/80 , F05D2230/90 , F05D2300/434 , F23R3/002 , F23R2900/00016 , F23R2900/00019
Abstract: A method for filling cooling holes in a component of a gas turbine engine is disclosed. The component may include a plurality of first cooling holes extending through the wall of the component. The method may comprise the steps of exposing the outer surface of the component, filling the plurality of first cooling holes with a polyimide, curing the polyimide to block the passage of cooling fluid through the plurality of first cooling holes, and applying a thermal barrier coating over the outer surface of the component. The method may further include the step of installing a second plurality of cooling holes in the wall of the component wherein the plurality of second cooling holes penetrate the thermal barrier coating and the wall of the component and allow cooling fluid to pass therethrough.
Abstract translation: 公开了一种用于填充燃气涡轮发动机的部件中的冷却孔的方法。 部件可以包括延伸穿过部件的壁的多个第一冷却孔。 该方法可以包括以下步骤：暴露部件的外表面，用聚酰亚胺填充多个第一冷却孔，固化聚酰亚胺以阻止冷却流体通过多个第一冷却孔，并施加热障涂层 在组件的外表面上。 该方法还可以包括在组件的壁中安装第二多个冷却孔的步骤，其中多个第二冷却孔穿过热障涂层和部件的壁并允许冷却流体通过。
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公开(公告)号：EP2935951B1
公开(公告)日：2019-09-11
申请号：EP13864840.7
申请日：2013-11-06
Applicant: United Technologies Corporation
Inventor： BOGUE, William , PRIHAR, Ron, I.P.E.
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公开(公告)号：EP2935951A1
公开(公告)日：2015-10-28
申请号：EP13864840.7
申请日：2013-11-06
Applicant: United Technologies Corporation
Inventor： BOGUE, William , PRIHAR, Ron, I.P.E.
CPC classification number: B05D7/22 , B23P6/007 , B23P2700/06 , B23P2700/13 , C23C4/02 , F01D5/005 , F01D5/288 , F05D2230/42 , F05D2230/80 , F05D2230/90 , F05D2300/434 , F23R3/002 , F23R2900/00016 , F23R2900/00019 , Y02T50/6765
Abstract: A method for filling cooling holes in a component of a gas turbine engine is disclosed. The component may include a plurality of first cooling holes extending through the wall of the component. The method may comprise the steps of exposing the outer surface of the component, filling the plurality of first cooling holes with a polyimide, curing the polyimide to block the passage of cooling fluid through the plurality of first cooling holes, and applying a thermal bather coating over the outer surface of the component. The method may further include the step of installing a second plurality of cooling holes in the wall of the component wherein the plurality of second cooling holes penetrate the thermal barrier coating and the wall of the component and allow cooling fluid to pass therethrough.
Abstract translation: 公开了一种用于填充燃气涡轮发动机的部件中的冷却孔的方法。 部件可以包括延伸穿过部件的壁的多个第一冷却孔。 该方法可以包括暴露所述部件的外表面，填充所述多个与聚酰亚胺第一冷却孔的步骤，固化该聚酰亚胺以阻止冷却流体通过多个第一冷却孔，并且施加热障涂层的通道 在部件的外表面上。 该方法可以进一步包括在部件的壁中安装第二多个冷却孔的步骤，其中多个第二冷却孔穿透热障涂层和部件的壁并且允许冷却流体通过其中。
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5.发明公开
公开(公告)号：EP2935836A1
公开(公告)日：2015-10-28
申请号：EP13864805.0
申请日：2013-11-06
Applicant: United Technologies Corporation
Inventor： BOGUE, William , PRIHAR, Ron, I.P.E.
CPC classification number: F02C7/12 , B23P6/002 , B23P2700/06 , C23C4/00 , C25D7/04 , F01D5/18 , F01D5/284 , F01D5/288 , F01D25/12 , F05D2230/90 , Y02T50/675
Abstract: a plurality of second cooling holes penetrating the thermal barrier coating and extending between the outer surface and the inner surface, the plurality of second cooling holes allowing cooling fluid to pass therethrough.
Abstract translation: 公开了一种用于填充燃气涡轮发动机的部件中的冷却孔的方法。 该部件可以包括穿过部件的壁的多个第一冷却孔。 该方法可以包括以下步骤：暴露组件的外表面，用填充剂填充组件的多个第一冷却孔，固化填充剂以阻止空气通过冷却孔，并且施加热障碍 涂覆在组件的表面上。 该方法还可以包括安装第二多个冷却孔，第二多个冷却孔穿过热障涂层和部件的壁并允许空气通过。
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