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公开(公告)号：US20110138574A1
公开(公告)日：2011-06-16
申请号：US12638410
申请日：2009-12-15
申请人： William Bogue , Michael J. Madel
发明人： William Bogue , Michael J. Madel
CPC分类号： B64D29/06 , B64F5/40 , Y10T16/52 , Y10T16/537 , Y10T16/557 , Y10T29/24 , Y10T29/49318 , Y10T29/49718 , Y10T29/49732 , Y10T29/49735 , Y10T408/03 , Y10T408/557 , Y10T408/56245 , Y10T409/303808
摘要： A hinge arm having a hinge pin hole having a worn bore, for example a hinge arm of a hinge assembly of an access door on a gas turbine engine, is repaired by forming in the worn hinge arm a new hole with a keyway extending outwardly from the new hole. A keyed bushing is provided having a cylindrical body having a central bore extending axially therethrough and a key extending outwardly from the cylindrical hole. The keyed bushing is inserted into the new hole and keyway formed in the hinge arm thereby preventing rotation of the bushing relative to the hinge arm.
摘要翻译： 铰链臂具有具有磨损孔的铰链销孔，例如燃气涡轮发动机上的进入门的铰链组件的铰链臂，通过在磨损的铰链臂中形成一个新的孔，其中的一个新的孔由从 新的洞。 提供了一种带键衬套，其具有圆柱形本体，其具有轴向延伸穿过的中心孔和从该圆柱形孔向外延伸的键。 带键衬套插入在铰链臂中形成的新孔和键槽中，从而防止衬套相对于铰链臂的旋转。
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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。
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3.发明申请DEVICE AND METHOD FOR REPAIRING A FORWARD FRAME V-BLADE IN AN AIRCRAFT ENGINE 有权用于修复飞机发动机中的前向叶片V形叶片的装置和方法公开(公告)号：US20110000086A1
公开(公告)日：2011-01-06
申请号：US12828836
申请日：2010-07-01
IPC分类号： B23P6/00
CPC分类号： F01D5/005 , B23P6/005 , F01D5/141 , F05B2260/301 , Y10T29/49316 , Y10T29/49318 , Y10T29/4932 , Y10T29/49321 , Y10T29/49721
摘要： A repair device and method for repairing a forward frame v-blade on an aircraft engine are described in which the repair device replaces a section of the forward frame v-blade. In one embodiment, the repair device includes a supplemental part, which is secured to the forward frame v-blade. The supplemental part includes a central web and a pair of legs with a leg thickness that is greater than the thickness of corresponding flanges on the forward frame v-blade. Fasteners such as rivets are used to couple the supplemental part to the forward frame v-blade.
摘要翻译： 描述了用于修复飞机发动机上的前方叶片V形叶片的修理装置和方法，其中修理装置取代前方叶片V形叶片的一部分。 在一个实施例中，修理装置包括固定到前框架叶片的补充部件。 辅助部件包括中央腹板和一对腿部，其腿部厚度大于前部框架v形叶片上的对应凸缘的厚度。 诸如铆钉的紧固件用于将补充部件连接到前框架叶片。
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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。
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公开(公告)号：US08661667B2
公开(公告)日：2014-03-04
申请号：US12638410
申请日：2009-12-15
申请人： William Bogue , Michael J. Madel
发明人： William Bogue , Michael J. Madel
CPC分类号： B64D29/06 , B64F5/40 , Y10T16/52 , Y10T16/537 , Y10T16/557 , Y10T29/24 , Y10T29/49318 , Y10T29/49718 , Y10T29/49732 , Y10T29/49735 , Y10T408/03 , Y10T408/557 , Y10T408/56245 , Y10T409/303808
摘要： A hinge arm having a hinge pin hole having a worn bore, for example a hinge arm of a hinge assembly of an access door on a gas turbine engine, is repaired by forming in the worn hinge arm a new hole with a keyway extending outwardly from the new hole. A keyed bushing is provided having a cylindrical body having a central bore extending axially therethrough and a key extending outwardly from the cylindrical hole. The keyed bushing is inserted into the new hole and keyway formed in the hinge arm thereby preventing rotation of the bushing relative to the hinge arm.
摘要翻译： 铰链臂具有具有磨损孔的铰链销孔，例如燃气涡轮发动机上的进入门的铰链组件的铰链臂，通过在磨损的铰链臂中形成一个新的孔，其中的一个新的孔由从 新的洞。 提供了一种带键衬套，其具有圆柱形本体，其具有轴向延伸穿过的中心孔和从该圆柱形孔向外延伸的键。 带键衬套插入在铰链臂中形成的新孔和键槽中，从而防止衬套相对于铰链臂的旋转。
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6.发明授权Device and method for repairing a forward frame V-blade in an aircraft engine 有权用于修理飞机发动机中的前方V形叶片的装置和方法公开(公告)号：US08769814B2
公开(公告)日：2014-07-08
申请号：US12828836
申请日：2010-07-01
IPC分类号： B23P6/00
CPC分类号： F01D5/005 , B23P6/005 , F01D5/141 , F05B2260/301 , Y10T29/49316 , Y10T29/49318 , Y10T29/4932 , Y10T29/49321 , Y10T29/49721
摘要： A repair device and method for repairing a forward frame v-blade on an aircraft engine are described in which the repair device replaces a section of the forward frame v-blade. In one embodiment, the repair device includes a supplemental part, which is secured to the forward frame v-blade. The supplemental part includes a central web and a pair of legs with a leg thickness that is greater than the thickness of corresponding flanges on the forward frame v-blade. Fasteners such as rivets are used to couple the supplemental part to the forward frame v-blade.
摘要翻译： 描述了用于修复飞机发动机上的前方叶片V形叶片的修理装置和方法，其中修理装置取代前方叶片V形叶片的一部分。 在一个实施例中，修理装置包括固定到前框架叶片的补充部件。 辅助部件包括中央腹板和一对腿部，其腿部厚度大于前部框架v形叶片上的对应凸缘的厚度。 诸如铆钉的紧固件用于将补充部件连接到前框架叶片。
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