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公开(公告)号：US06908657B2
公开(公告)日：2005-06-21
申请号：US10605241
申请日：2003-09-17
CPC分类号： B23P6/002 , B23P2700/06 , C23C4/00 , F01D5/186 , F01D5/288 , F05D2230/13 , F05D2260/607 , Y10T29/49318 , Y10T29/49339 , Y10T428/12361 , Y10T428/24273 , Y10T428/249953
摘要： A process of removing deposits from through-holes in a component, such as metallic bond coat and ceramic materials from cooling holes in an air-cooled gas turbine engine. The process is particularly effective in removing a TBC material deposited in a cooling hole of a component as a result of depositing a coating of the TBC material on a surface of the component, in which the deposit is removed from the cooling hole without damaging the cooling hole or the TBC coating surrounding the cooling hole on the coated surface of the component. A preferred feature is that the cooling hole, including the entrance to the hole at a surface of the component opposite the coated surface and the coating surrounding the exit of the hole at the coated surface, exhibits improved surface characteristics that increase the discharge coefficient of the cooling hole, as evidenced by an increase in the effective area of the cooling hole.
摘要翻译： 从空气冷却燃气涡轮发动机的冷却孔中除去金属结合层和陶瓷材料等成分的通孔的沉积物的工序。 该方法特别有效地除去沉积在部件的冷却孔中的TBC材料，这是因为在组件的表面上沉积TBC材料的涂层，其中沉积物从冷却孔移除而不损坏冷却 孔或TBC涂层，围绕组件的涂覆表面上的冷却孔。 一个优选的特征是，包括在与涂覆表面相对的部件的表面处的孔的入口和围绕涂覆表面的孔的出口的涂层的冷却孔表现出改进的表面特性，其增加了 如冷却孔的有效面积的增加所证明的。
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公开(公告)号：US06655149B2
公开(公告)日：2003-12-02
申请号：US10321088
申请日：2002-12-17
IPC分类号： F01D2512
CPC分类号： F23R3/06 , Y02T50/675
摘要： A multi-hole cooled combustor liner is provided which reduces hot streaks and associated material distress in the liner. Areas of increased cooling hole density are disposed upstream of the primary dilution holes and in circumferential alignment with fuel cup centers. Additional cooling holes are provided in between primary dilution holes are arranged in alternating pairs of circumferentially angled holes so as to provide a converging cooling air flow in the downstream direction.
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公开(公告)号：US06561872B2
公开(公告)日：2003-05-13
申请号：US09878847
申请日：2001-06-11
IPC分类号： B24B100
摘要： A method of stripping coating from a portion of a coated surface of a component. The method includes fastening a mask sheet to the component over a region adjacent the portion of the coated surface. The mask sheet has a contour generally corresponding to a contour of the surface of the component. A high pressure fluid jet is sprayed from a spray head toward the portion of the coated surface after the mask sheet is fastened to the component to strip the coating from the portion of the surface. After the coating is stripped from the portion of the surface, the mask sheet is removed from the component.
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4.发明授权Venturi for use in the swirl cup package of a gas turbine combustor having water injected therein 失效文丘里管用于其中注入有水的燃气轮机燃烧器的涡流杯组件公开(公告)号：US06286302B1
公开(公告)日：2001-09-11
申请号：US09283428
申请日：1999-04-01
IPC分类号： F02C700
CPC分类号： F23L7/002 , F23D2211/00 , F23R3/14
摘要： A combustion apparatus for a gas turbine engine including a combustor structure having at least one combustion chamber, a dual cone fuel nozzle for injecting both fuel and water to the combustion chamber, and a swirl cup package upstream of and adjacent to the combustion chamber. The swirl cup package further includes a swirler and a venturi extending between the nozzle and the combustion chamber for mixing the fuel and water with air. The venturi is configured to have a non-uniform thickness from an upstream end to a downstream end resulting in a cross-sectional area which provides a heat transfer conduction path that reduces axial stresses imposed on the venturi when water impinges on an upstream portion of the venturi.
摘要翻译： 一种用于燃气涡轮发动机的燃烧装置，其包括具有至少一个燃烧室的燃烧器结构，用于将燃料和水喷射到燃烧室的双锥形燃料喷嘴，以及在燃烧室上游和邻近燃烧室的涡流杯组件。 涡流杯包装还包括在喷嘴和燃烧室之间延伸的旋流器和文氏管，用于将燃料和水与空气混合。 文丘里管构造成具有从上游端到下游端的不均匀的厚度，从而产生横截面积，该横截面面积提供传热传导路径，当水冲击在文丘里管的上游部分时，该导热路径减小施加在文氏管上的轴向应力 文丘里
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公开(公告)号：US2743883A
公开(公告)日：1956-05-01
申请号：US49759355
申请日：1955-03-29
申请人： GILBERT FARMER
发明人： GILBERT FARMER
CPC分类号： B65H49/325 , B65H49/32 , B65H49/327 , B65H75/20 , B65H75/22
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公开(公告)号：US07022940B2
公开(公告)日：2006-04-04
申请号：US10722101
申请日：2003-11-24
IPC分类号： B23K26/00
CPC分类号： F23R3/002 , B23K26/244 , B23K2101/001
摘要： A combustor liner is provided having first and second annular bands which define an overlapping circumferential joint area, wherein a weld is disposed in the joint area encompassing substantially all of the axial length of the joint area. A method for producing such a combustor liner is also provided.
摘要翻译： 燃烧器衬套设置有第一和第二环形带，其限定重叠的圆周接合区域，其中在包围接头区域的基本上所有轴向长度的接头区域中设置焊缝。 还提供了一种用于制造这种燃烧器衬套的方法。
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7.发明授权Process of removing a coating deposit from a through-hole in a component and component processed thereby 失效从被处理的部件和部件中的通孔中去除涂层沉积物的过程公开(公告)号：US06663919B2
公开(公告)日：2003-12-16
申请号：US10086266
申请日：2002-03-01
IPC分类号： C23C418
CPC分类号： B23P6/002 , B23P2700/06 , C23C4/00 , F01D5/186 , F01D5/288 , F05D2230/13 , F05D2260/607 , Y10T29/49318 , Y10T29/49339 , Y10T428/12361 , Y10T428/24273 , Y10T428/249953
摘要： A process of removing deposits from through-holes in a component, such as metallic bond coat and ceramic materials from cooling holes in an air-cooled gas turbine engine. The process is particularly effective in removing a TBC material deposited in a cooling hole of a component as a result of depositing a coating of the TBC material on a surface of the component, in which the deposit is removed from the cooling hole without damaging the cooling hole or the TBC coating surrounding the cooling hole on the coated surface of the component. A preferred feature is that the cooling hole, including the entrance to the hole at a surface of the component opposite the coated surface and the coating surrounding the exit of the hole at the coated surface, exhibits improved surface characteristics that increase the discharge coefficient of the cooling hole, as evidenced by an increase in the effective area of the cooling hole.
摘要翻译： 从空气冷却燃气涡轮发动机的冷却孔中除去金属结合层和陶瓷材料等成分的通孔的沉积物的工序。 该方法特别有效地除去沉积在部件的冷却孔中的TBC材料，这是因为在组件的表面上沉积TBC材料的涂层，其中沉积物从冷却孔移除而不损坏冷却 孔或TBC涂层，围绕组件的涂覆表面上的冷却孔。 一个优选的特征是，包括在与涂覆表面相对的部件的表面处的孔的入口和围绕涂覆表面的孔的出口的涂层的冷却孔表现出改进的表面特性，其增加了 如冷却孔的有效面积的增加所证明的。
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公开(公告)号：US06408610B1
公开(公告)日：2002-06-25
申请号：US09618571
申请日：2000-07-18
IPC分类号： F02C712
CPC分类号： F01D5/186 , B23P2700/06 , C23C14/046 , F01D5/18 , F01D5/288 , Y10T29/4932
摘要： A method of adjusting airflow through a plurality of cooling holes by depositing a thermal barrier coating on an exterior surface and/or an interior surface of the component by a physical vapor deposition process. The cooling holes are not masked. Thus, a portion of the thermal barrier coating partially obstructs airflow through the cooling holes and reduces airflow through the cooling holes. A predetermined pressure drop is developed across the cooling holes and airflow through the cooling holes is measured. The measured airflow is compared to a preselected range of desired cooling hole airflows and the steps of depositing the thermal barrier coating, developing the predetermined pressure drop, calculating airflow and comparing the measured airflow to the preselected range are repeated until the measured airflow is within the preselected range of desired cooling hole airflows.
摘要翻译： 通过物理气相沉积工艺在组件的外表面和/或内表面上沉积热障涂层，来调节通过多个冷却孔的气流的方法。 冷却孔未被遮蔽。 因此，热障涂层的一部分部分阻碍通过冷却孔的空气流并且减少通过冷却孔的气流。 在冷却孔之间产生预定的压降，并测量通过冷却孔的气流。 将测量的气流与期望的冷却孔气流的预选范围进行比较，并重复沉积热障涂层，显影预定压降，计算气流并将测量的气流与预选范围进行比较的步骤，直到所测量的气流在 所需冷却孔气流的预选范围。
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公开(公告)号：US06205763B1
公开(公告)日：2001-03-27
申请号：US09317243
申请日：1999-05-24
IPC分类号： F02C1310
CPC分类号： F23C7/002 , F23R3/14 , Y02T50/675 , Y10T29/49229
摘要： A method for determining the appropriate hole parameters to achieve the desired airflow in a swirler with as-cast air jet holes includes the steps of determining the desired airflow through the holes and selecting a hole angle for the holes. Next, the ratio of the hole exit area to the hole inlet area is calculated based on the desired airflow and the selected hole angle using a regression equation. Then a value is determined for either of the hole exit area or the hole inlet area, and the other area is calculated from the known ratio. Once the hole angle, hole exit area and hole inlet area have been determined, then a swirler can be cast with as-cast holes using these hole parameters.
摘要翻译： 用于确定适当的孔参数以在具有铸态空气喷射孔的旋流器中实现所需气流的方法包括以下步骤：确定通过孔的所需气流并选择孔的孔角。 接下来，使用回归方程，基于期望的气流和所选择的孔角计算出孔面积与孔入口面积的比率。 然后为孔出口区域或孔入口区域中的任一个确定值，并且从已知比例计算另一区域。 一旦确定了孔角度，孔出口面积和孔入口面积，则可以使用这些孔参数用旋转器铸造旋流器。
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10.发明授权Method of protecting gas turbine combustor components against water erosion and hot corrosion 失效保护燃气轮机燃烧器部件防止水侵蚀和热腐蚀的方法
公开(公告)号：US6047539A
公开(公告)日：2000-04-11
申请号：US70053
申请日：1998-04-30
申请人： Gilbert Farmer
发明人： Gilbert Farmer
CPC分类号： F23R3/007 , F23M5/00 , F23R3/002 , F23L2900/07008 , F23M2900/05001
摘要： A method of preventing water erosion and hot corrosion in a combustor of a gas turbine engine, wherein water is injected into said combustor for NOx abatement, which involves the step of applying a dense vertically cracked thermal barrier coating to certain components thereof The dense vertically cracked thermal barrier coating has a porosity of less than approximately 8% and a tensile strength in the range of approximately 4-7 ksi. The dense vertically cracked thermal barrier coating is applied to such combustor components so as to produce a segmented ceramic structure having macrocracks formed therein which are oriented substantially perpendicular to an interface of the combustor component and the segmented ceramic structure.
摘要翻译： 一种防止燃气涡轮发动机的燃烧器中的水侵蚀和热腐蚀的方法，其中将水注入到所述燃烧器中用于NOx减排，其涉及向其某些组分施加致密的垂直裂纹热障涂层的步骤。致密的垂直裂纹 热障涂层的孔隙率小于约8％，拉伸强度在约4-7ksi的范围内。 致密的垂直裂纹热障涂层被施加到这种燃烧器部件上，以便产生一个分段的陶瓷结构，其中形成有宏观裂纹，其中基本垂直于燃烧器部件和分段陶瓷结构的界面。
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