-
公开(公告)号：US08108979B2
公开(公告)日：2012-02-07
申请号：US11789268
申请日：2007-04-24
CPC分类号： B64D33/02 , B29C73/06 , B64D2033/0206 , B64F5/40 , Y10T29/49732 , Y10T29/49734 , Y10T29/49746 , Y10T29/49748
摘要： A method of repairing a part, which has a first side, a second side opposite of the first side, and an aperture that makes the part susceptible to cracking, includes the steps of forming a slot in the first side of the part near the aperture, inserting a stiffener into the slot, and attaching at least one repair ply onto the first side of the part to cover the stiffener.
摘要翻译： 修复具有第一侧，与第一侧相反的第二侧的部件和使部件易于破裂的孔的方法包括以下步骤：在靠近孔的部分的第一侧中形成槽 将加强件插入槽中，以及将至少一个修复层附接到部件的第一侧以覆盖加强件。
-
公开(公告)号：US20080263844A1
公开(公告)日：2008-10-30
申请号：US11789268
申请日：2007-04-24
IPC分类号： B23P6/04
CPC分类号： B64D33/02 , B29C73/06 , B64D2033/0206 , B64F5/40 , Y10T29/49732 , Y10T29/49734 , Y10T29/49746 , Y10T29/49748
摘要： A method of repairing a part, which has a first side, a second side opposite of the first side, and an aperture that makes the part susceptible to cracking, includes the steps of forming a slot in the first side of the part near the aperture, inserting a stiffener into the slot, and attaching at least one repair ply onto the first side of the part to cover the stiffener.
摘要翻译： 修复具有第一侧，与第一侧相反的第二侧的部件和使部件易于破裂的孔的方法包括以下步骤：在靠近孔的部分的第一侧中形成槽 将加强件插入槽中，以及将至少一个修复层附接到部件的第一侧以覆盖加强件。
-
3.发明申请Method and assembly for bonding metal layers in a gas turbine engine using a polyimide adhesive 审中-公开用于使用聚酰亚胺粘合剂在燃气涡轮发动机中接合金属层的方法和组件公开(公告)号：US20090165926A1
公开(公告)日：2009-07-02
申请号：US11977283
申请日：2007-10-24
CPC分类号： F01D5/005 , C09J5/00 , C09J2400/163 , C09J2479/00 , F05D2230/236 , F05D2230/80 , F16B11/006 , Y02T50/673
摘要： A method and system is described herein for using a polyimide adhesive to bond a first metal layer to a second metal layer used in a gas turbine engine. The polyimide adhesive may be a film or a paste and is able to withstand operating temperatures in excess of 600 degrees Fahrenheit (315 degrees Celsius). In an exemplary embodiment, the second metal layer is an outer face skin of an exhaust nozzle and the first metal layer is a metal doubler configured to cover a damaged portion of the outer face skin. In some embodiments, the first and second metal layers may be formed of titanium.
摘要翻译： 本文描述了使用聚酰亚胺粘合剂将第一金属层粘合到燃气涡轮发动机中使用的第二金属层的方法和系统。 聚酰亚胺粘合剂可以是膜或糊料，并且能够承受超过华氏600度（315摄氏度）的工作温度。 在示例性实施例中，第二金属层是排气喷嘴的外表皮，并且第一金属层是构造成覆盖外表皮的损坏部分的金属倍增器。 在一些实施例中，第一和第二金属层可以由钛形成。
-
公开(公告)号：US08128100B2
公开(公告)日：2012-03-06
申请号：US11999355
申请日：2007-12-05
IPC分类号： F16J15/12
CPC分类号： F02K1/805 , F01D11/005 , F05D2240/55 , F16J15/3284 , Y02T50/672 , Y10T428/25
摘要： A laminate air seal for a gas turbine engine includes at least one fabric layer made of fiberglass, ceramic fiber, basalt and/or carbon, and a polymeric resin that is stable at an operating temperature of the gas turbine engine. The resin may be preimpregnated into the fabric layers, or introduced into the fabric during assembly and formation of the laminate. The resin may be polyimide, bismaelimide (BMI) or cyanate ester. A particular resin selected may depend, in part, on the operating temperatures in that region of the gas turbine engine. In some embodiments, the laminate seal may include a coating to increase lubricity of the seal. In one embodiment, the laminate air seal is used to seal a gap between a pylon fairing and an exhaust nozzle of the turbine engine.
摘要翻译： 用于燃气涡轮发动机的层压空气密封件包括由玻璃纤维，陶瓷纤维，玄武岩和/或碳制成的至少一个织物层和在燃气涡轮发动机的工作温度下是稳定的聚合物树脂。 树脂可以预先浸渍到织物层中，或者在组装和形成层压体期间引入织物。 树脂可以是聚酰亚胺，双马来酰亚胺（BMI）或氰酸酯。 所选择的特定树脂可以部分地取决于燃气涡轮发动机的该区域中的操作温度。 在一些实施例中，层压密封件可以包括用于增加密封件的润滑性的涂层。 在一个实施例中，层压空气密封件用于密封塔架整流罩和涡轮发动机的排气喷嘴之间的间隙。
-
公开(公告)号：US20090148275A1
公开(公告)日：2009-06-11
申请号：US11999355
申请日：2007-12-05
CPC分类号： F02K1/805 , F01D11/005 , F05D2240/55 , F16J15/3284 , Y02T50/672 , Y10T428/25
摘要： A laminate air seal for a gas turbine engine includes at least one fabric layer made of fiberglass, ceramic fiber, basalt and/or carbon, and a polymeric resin that is stable at an operating temperature of the gas turbine engine. The resin may be preimpregnated into the fabric layers, or introduced into the fabric during assembly and formation of the laminate. The resin may be polyimide, bismaelimide (BMI) or cyanate ester. A particular resin selected may depend, in part, on the operating temperatures in that region of the gas turbine engine. In some embodiments, the laminate seal may include a coating to increase lubricity of the seal. In one embodiment, the laminate air seal is used to seal a gap between a pylon fairing and an exhaust nozzle of the turbine engine.
摘要翻译： 用于燃气涡轮发动机的层压空气密封件包括至少一个由玻璃纤维，陶瓷纤维，玄武岩和/或碳制成的织物层和在燃气涡轮发动机的工作温度下是稳定的聚合物树脂。 树脂可以预先浸渍到织物层中，或者在组装和形成层压体期间引入织物。 树脂可以是聚酰亚胺，双马来酰亚胺（BMI）或氰酸酯。 所选择的特定树脂可以部分地取决于燃气涡轮发动机的该区域中的操作温度。 在一些实施例中，层压密封件可以包括用于增加密封件的润滑性的涂层。 在一个实施例中，层压空气密封件用于密封塔架整流罩和涡轮发动机的排气喷嘴之间的间隙。
-
公开(公告)号：US07622178B2
公开(公告)日：2009-11-24
申请号：US11396479
申请日：2006-04-03
CPC分类号： B29C73/04 , B29C73/10 , Y10T428/20
摘要： An assembly includes a composite flange, an insert, an adhesive and a support. The composite flange has at least one damaged aperture. The insert is positioned in the damaged aperture and extends therefrom to provide compressive load transfer through the composite flange. The adhesive is positioned directly on at least a portion of the composite flange proximate the damaged aperture. The support is positioned over the adhesive and contacts the insert.
摘要翻译： 组件包括复合凸缘，插入件，粘合剂和支撑件。 复合凸缘具有至少一个损坏的孔。 插入件位于损坏的孔中并从其延伸以提供通过复合凸缘的压缩载荷传递。 粘合剂直接位于邻近损坏的孔的复合凸缘的至少一部分上。 支撑件位于粘合剂上方并与插入物接触。
-
公开(公告)号：US07981519B2
公开(公告)日：2011-07-19
申请号：US12082455
申请日：2008-04-11
CPC分类号： B29C73/10 , B29C73/06 , B29L2031/608 , Y10T29/49618 , Y10T29/4973 , Y10T29/49734 , Y10T428/1234 , Y10T428/24149
摘要： A method and system of repairing an engine part having a cracked metal skin bonded to a honeycomb core includes removing a portion of the honeycomb that corresponds to a cracked portion of the metal skin. A crack in the metal skin originates from an edge of the engine part. A portion of the honeycomb is removed to form a slot in the honeycomb beginning at the edge of the part. A doubler is inserted into the slot in the honeycomb and is attached to an underside of the metal skin to form a lap joint between the doubler and the metal skin. In one embodiment, the portion of the metal skin that includes the crack remains. In an alternative embodiment, the cracked portion of the metal skin is removed and a metal patch is attached to the doubler such that the patch replaces the removed metal skin.
摘要翻译： 修复具有结合到蜂窝芯的裂纹金属表皮的发动机部件的方法和系统包括去除与金属表皮的裂纹部分对应的一部分蜂窝体。 金属皮肤的裂纹起源于发动机部件的边缘。 去除蜂窝体的一部分，从而在该部件的边缘开始形成蜂窝状的槽。 将倍增器插入到蜂窝中的狭槽中并且附着到金属皮肤的下侧，以在倍增器和金属皮肤之间形成搭接接头。 在一个实施例中，包含裂纹的金属皮肤的部分残留。 在替代实施例中，去除金属表皮的裂纹部分并且将金属贴片附接到倍增器，使得贴片代替去除的金属表皮。
-
公开(公告)号：US20090258185A1
公开(公告)日：2009-10-15
申请号：US12082455
申请日：2008-04-11
CPC分类号： B29C73/10 , B29C73/06 , B29L2031/608 , Y10T29/49618 , Y10T29/4973 , Y10T29/49734 , Y10T428/1234 , Y10T428/24149
摘要： A method and system of repairing an engine part having a cracked metal skin bonded to a honeycomb core includes removing a portion of the honeycomb that corresponds to a cracked portion of the metal skin. A crack in the metal skin originates from an edge of the engine part. A portion of the honeycomb is removed to form a slot in the honeycomb beginning at the edge of the part. A doubler is inserted into the slot in the honeycomb and is attached to an underside of the metal skin to form a lap joint between the doubler and the metal skin. In one embodiment, the portion of the metal skin that includes the crack remains. In an alternative embodiment, the cracked portion of the metal skin is removed and a metal patch is attached to the doubler such that the patch replaces the removed metal skin.
摘要翻译： 修复具有结合到蜂窝芯的裂纹金属表皮的发动机部件的方法和系统包括去除与金属表皮的裂纹部分对应的一部分蜂窝体。 金属皮肤的裂纹起源于发动机部件的边缘。 去除蜂窝体的一部分，从而在该部件的边缘开始形成蜂窝状的槽。 将倍增器插入到蜂窝中的狭槽中并且附着到金属皮肤的下侧，以在倍增器和金属皮肤之间形成搭接接头。 在一个实施例中，包含裂纹的金属皮肤的部分残留。 在替代实施例中，去除金属表皮的裂纹部分并且将金属贴片附接到倍增器，使得贴片代替去除的金属表皮。
-
公开(公告)号：US07727349B2
公开(公告)日：2010-06-01
申请号：US11897887
申请日：2007-08-31
CPC分类号： B29C73/04 , B29C73/10 , Y10T428/20
摘要： A doubler assembly repairs at least one damaged aperture of a composite flange. The doubler assembly includes an insert, an adhesive, and a support. The insert is positioned in the damaged aperture to provide compressive load transfer through the composite flange. The adhesive is positioned directly on at least a portion of the composite flange proximate the damaged aperture. The support is positioned over the adhesive.
摘要翻译： 双组件修复复合法兰的至少一个损坏的孔。 倍增器组件包括插入件，粘合剂和支撑件。 插入件位于损坏的孔中，以通过复合凸缘提供压缩载荷传递。 粘合剂直接位于邻近损坏的孔的复合凸缘的至少一部分上。 支撑件位于粘合剂上。
-
10.发明申请Replacement of a lubricant layer bonded to a part of a gas turbine engine 审中-公开更换粘合到燃气涡轮发动机的一部分的润滑剂层公开(公告)号：US20090038739A1
公开(公告)日：2009-02-12
申请号：US11891253
申请日：2007-08-09
IPC分类号： B32B43/00
CPC分类号： B23P6/005 , B29C73/10 , F01D5/005 , F01D17/162 , F05D2230/80 , F05D2230/90 , F05D2300/43 , F05D2300/603 , Y10T156/1116 , Y10T156/1928 , Y10T428/3154
摘要： A method and system is described herein for repairing a part used in a gas turbine engine, which has a damaged or worn lubricant layer bonded to a surface of the part. After removing the damaged or worn lubricant layer, a polymeric adhesive may be used to attach a replacement lubricant layer to the metal surface. The polymeric adhesive may be a film or a paste. In some embodiments, the adhesive includes a non-metallic filler. The polymeric adhesive is stable at an operating temperature of the part to which it is attached. In one embodiment, the adhesive is polyimide, which is well-suited for use in a high pressure compressor of the gas turbine engine that operates at high temperatures. In other embodiments, the adhesive is bismaleimide (BMI) or cyanate ester.
摘要翻译： 本文描述了一种用于修理燃气涡轮发动机中使用的部件的方法和系统，其具有结合到部件的表面上的损坏或磨损的润滑剂层。 在去除损坏或磨损的润滑剂层之后，可以使用聚合物粘合剂将替换的润滑剂层附着到金属表面。 聚合物粘合剂可以是膜或糊料。 在一些实施方案中，粘合剂包括非金属填料。 聚合物粘合剂在其所连接部分的操作温度下是稳定的。 在一个实施方案中，粘合剂是聚酰亚胺，其非常适用于在高温下操作的燃气轮机的高压压缩机。 在其它实施方案中，粘合剂是双马来酰亚胺（BMI）或氰酸酯。
-
-
-
-
-
-
-
-
-
搜索结果
14 条记录 (耗时 0.023 秒)
