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1. 发明授权

US09022743B2 Segmented thermally insulating coating 有权
标题翻译：分段绝热涂层
公开(公告)号：US09022743B2
公开(公告)日：2015-05-05
申请号：US13307295
申请日：2011-11-30
申请人： James A. Dierberger
发明人： James A. Dierberger
IPC分类号： F01D25/08 , F01D25/14 , C23C4/00
CPC分类号： F01D25/08 , C23C4/00 , F01D5/288 , F01D25/145 , Y10T29/49229
摘要： A gas turbine article includes a substrate and a thermally insulating topcoat disposed on a surface of the substrate. The surface of the substrate includes a surface pattern defining first surface regions and second surface regions. The first surface regions include incubation sites that are favorable for deposition of the thermally insulating topcoat and the second surface regions are less favorable for deposition of the topcoat. The topcoat includes segmented portions that are separated by faults extending through the topcoat from the second regions.
摘要翻译：燃气轮机制品包括设置在基板的表面上的基板和绝热顶涂层。衬底的表面包括限定第一表面区域和第二表面区域的表面图案。第一表面区域包括有利于沉积隔热顶涂层的孵育位点，第二表面区域不利于顶涂层的沉积。顶涂层包括由第二区域延伸通过顶涂层的断层分开的分段部分。

2. 发明申请

US20120324894A1 STRAIN TOLERANT COMBUSTOR PANEL FOR GAS TURBINE ENGINE 有权
标题翻译：用于气体涡轮发动机的耐腐蚀混凝土面板
公开(公告)号：US20120324894A1
公开(公告)日：2012-12-27
申请号：US13168258
申请日：2011-06-24
申请人： James A. Dierberger
发明人： James A. Dierberger
IPC分类号： F02C3/14
CPC分类号： F23R3/002 , F23R3/005 , F23R2900/00018 , Y02T50/675
摘要： A combustor component of a gas turbine engine includes a substrate with a cold side, a central core section and a hot side, the cold side and the hot side have a porosity different than the central core section.
摘要翻译：燃气涡轮发动机的燃烧器部件包括具有冷侧，中心芯部和热侧的基板，冷侧和热侧具有不同于中心芯部的孔隙率。

3. 发明申请

US20100178165A1 WELDING REPAIR METHOD FOR FULL HOOP STRUCTURES 有权
标题翻译：全套结构焊接维修方法
公开(公告)号：US20100178165A1
公开(公告)日：2010-07-15
申请号：US12731183
申请日：2010-03-25
申请人： James A. Dierberger
发明人： James A. Dierberger
IPC分类号： F04D29/40 , B32B15/01
CPC分类号： B23K31/00 , B23K2101/001 , B23P6/002 , C21D9/50 , Y10T428/12
摘要： A unique heat treat method for relieving stresses caused by a repairing weld joint in a full hoop part heat treats locally, at the location of the weld joint, and at a diametrically opposed location. By providing the diametrically opposed heat treat location, the present invention relieves stresses caused by the weld joint, without creating any additional residual stress in the weld joint.
摘要翻译：一种独特的热处理方法，用于在整个箍部分中修复焊接接头引起的应力消除局部热处理，在焊接接头的位置和直径相对的位置。通过提供直径相对的热处理位置，本发明减轻了由焊接接头引起的应力，而不会在焊接接头中产生任何额外的残余应力。

4. 发明授权

US09534783B2 Insert adjacent to a heat shield element for a gas turbine engine combustor 有权
标题翻译：插入燃气涡轮发动机燃烧器的隔热元件附近
公开(公告)号：US09534783B2
公开(公告)日：2017-01-03
申请号：US13188442
申请日：2011-07-21
申请人： James A. Dierberger , Masamichi Hongoh , Dennis J. Sullivan
发明人： James A. Dierberger , Masamichi Hongoh , Dennis J. Sullivan
IPC分类号： F23R3/00 , F23R3/06
CPC分类号： F23R3/002 , F23R3/007 , F23R3/06 , F23R2900/03042 , Y02T50/675
摘要： A combustor of a gas turbine engine includes a heat shield panel mounted to a support shell and an insert at least partially between opposed surfaces of the support shell and the heat shield panel, the insert exposed to a combustion chamber, and the insert being flush with a hot side of the heat shield.
摘要翻译：燃气涡轮发动机的燃烧器包括安装到支撑壳体和至少部分地在支撑壳体和隔热板的相对表面之间的插入件的隔热板，所述插入件暴露于燃烧室，并且所述插入件与热屏的热边。

5. 发明授权

US08256223B2 Ceramic combustor liner panel for a gas turbine engine 有权
标题翻译：用于燃气涡轮发动机的陶瓷燃烧器衬板
公开(公告)号：US08256223B2
公开(公告)日：2012-09-04
申请号：US11872782
申请日：2007-10-16
申请人： James A. Dierberger , Kevin W. Schlichting , Melvin Freling
发明人： James A. Dierberger , Kevin W. Schlichting , Melvin Freling
IPC分类号： F02C1/00
CPC分类号： F23R3/007 , F23R3/60 , F23R2900/00017 , F23R2900/00018 , Y10T29/49348
摘要： A combustor assembly includes a support structure and at least one combustor liner panel selectively attached to the support structure. The combustor liner panel includes an uncooled ceramic portion, a cooled ceramic portion and a support that receives the cooled ceramic portion.
摘要翻译：燃烧器组件包括支撑结构和选择性地附接到支撑结构的至少一个燃烧器衬套面板。燃烧器衬套板包括非制冷陶瓷部分，冷却的陶瓷部分和接收冷却的陶瓷部分的支撑件。

6. 发明申请

US20100176185A1 WELDING REPAIR METHOD FOR FULL HOOP STRUCTURES 有权
公开(公告)号：US20100176185A1
公开(公告)日：2010-07-15
申请号：US12731189
申请日：2010-03-25
申请人： James A. Dierberger
发明人： James A. Dierberger
IPC分类号： B23K31/02
CPC分类号： B23K31/00 , B23K2101/001 , B23P6/002 , C21D9/50 , Y10T428/12
摘要： A unique heat treat method for relieving stresses caused by a repairing weld joint in a full hoop part heat treats locally, at the location of the weld joint, and at a diametrically opposed location. By providing the diametrically opposed heat treat location, the present invention relieves stresses caused by the weld joint, without creating any additional residual stress in the weld joint.

7. 发明授权

US4655044A Coated high temperature combustor liner 失效
标题翻译：涂层高温燃烧器衬管
公开(公告)号：US4655044A
公开(公告)日：1987-04-07
申请号：US563848
申请日：1983-12-21
申请人： James A. Dierberger , Thomas F. Tumicki
发明人： James A. Dierberger , Thomas F. Tumicki
IPC分类号： F23R3/08 , F23R3/00 , F23R3/06 , F23R3/42 , F02C1/00 , F02G3/00
CPC分类号： F23R3/002 , F05B2260/202
摘要： Each panel of the louver liner of the combustor of a gas turbine engine is coated with a ceramic composition on the surface adjacent the combustion zone with a tapered end at the lip of the cooling air film generating mechanism. A second taper may be incorporated at the back side of the lip of the next adjacent cooling air film generating mechanism.
摘要翻译：燃气涡轮发动机的燃烧器的百叶板衬套的每个面板在邻近燃烧区的表面上涂覆有陶瓷组合物，在冷却空气膜产生机构的唇缘处具有锥形端。可以在下一个相邻的冷却空气膜产生机构的唇缘的背面处并入第二锥形。

8. 发明授权

US4605452A Single crystal articles having controlled secondary crystallographic orientation 失效
标题翻译：具有受控次级晶体取向的单晶制品
公开(公告)号：US4605452A
公开(公告)日：1986-08-12
申请号：US330757
申请日：1981-12-14
申请人： Anthony E. Gemma , James A. Dierberger
发明人： Anthony E. Gemma , James A. Dierberger
IPC分类号： F01D5/14 , C22C1/02 , C22C19/03 , C30B11/00 , C30B11/14 , C30B21/02 , C30B29/52 , F01D5/28 , C22C19/05
CPC分类号： C30B11/14 , C30B11/00 , C30B29/52
摘要： Alignment of the [001] crystal axis of a face centered cubic metal with the primary z axis of a single crystal article provides good thermal fatigue resistance along the z axis, and minimizes cracking transverse to the axis. However, significant cracking is still observed parallel the z axis in severe applications. This cracking can be reduced by controlling the secondary crystallographic orientation (i.e., orientation of crystal axes within x-y planes transverse to the z axis), to make the [110] crystal axis tangent to the article surface in the region most prone to thermal fatigue cracking. Algorithims derived from empirical relationships enable calculation of the orientation likely to produce improved fatigue resistance. More durable single crystal gas turbine blades result when the [110] crystal axis is made tangent to the blade surface in the critical crack prone regions just behind the leading edge of the airfoil at about 40-80% of the airfoil span. A representative improved gas turbine blade will have a secondary orientation angle .alpha. of -10 to +20 degrees, where .alpha. is the angle between the [100] crystal axis and the y axis.
摘要翻译：面心立方金属的[001]晶轴与单晶制品的主z轴的对准提供了沿z轴的良好的耐热疲劳性，并且使横向于轴的裂纹最小化。然而，在严重应用中，平行于z轴仍然发现明显的裂纹。可以通过控制二次晶体取向（即，横向于z轴的xy平面内的晶轴的取向），使得[110]晶轴与最容易发生热疲劳裂纹的区域中的物品表面相切，可以减少这种裂纹。衍生自经验关系的算法可以计算可能产生改善的抗疲劳性的方向。在翼型前缘的正后方的[110]晶轴相对于叶片表面在叶片表面相对于翼型跨度的大约40-80％时产生更耐用的单晶燃气轮机叶片。代表性的改进燃气轮机叶片将具有-10至+20度的次方向角α，其中α是[100]晶轴和y轴之间的角度。

9. 发明授权

US4380906A Combustion liner cooling scheme 失效
标题翻译：燃烧衬管冷却方案
公开(公告)号：US4380906A
公开(公告)日：1983-04-26
申请号：US227317
申请日：1981-01-22
申请人： James A. Dierberger
发明人： James A. Dierberger
IPC分类号： F23R3/06 , F23R3/08 , F02C7/12 , F02C1/00
CPC分类号： F23R3/08 , Y02T50/675
摘要： A louvered liner construction for a gas turbine engine combustor comprises a film cooling system that includes a double pass cool air film producing means having the cooling air inlet facing compressor discharge air to impinge on a depending lip extending from the hot wall of the louver disposed intermediate to the cooling air inlet and the discharge slot. The cooling air is directed to impinge on the depending wall, change directions in a double loop configuration and heat the stiffening ring prior to discharging into the combustor in a film of uniform cooling air.
摘要翻译：用于燃气涡轮发动机燃烧器的百叶窗衬套结构包括膜冷却系统，其包括双通冷空气膜产生装置，其具有面向压缩机排放空气的冷却空气入口，以冲击从设置中间体的百叶窗的热壁延伸的悬垂唇缘到冷却空气入口和排放槽。冷却空气被引向冲击在垂直壁上，改变双重环形结构的方向，并且在均匀冷却空气的膜中排放到燃烧器中之前加热加强环。

10. 发明授权

US08800293B2 Floatwell panel assemblies and related systems 有权
标题翻译： Floatwell面板组件及相关系统
公开(公告)号：US08800293B2
公开(公告)日：2014-08-12
申请号：US11775398
申请日：2007-07-10
申请人： James A. Dierberger , Kevin W. Schlichting , Melvin Freling
发明人： James A. Dierberger , Kevin W. Schlichting , Melvin Freling
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F23R3/007
摘要： Floatwall panel assemblies and related systems are provided. A floatwall panel assembly includes a panel formed of porous ceramic material, the porous ceramic material exhibiting a porosity gradient along at least one of a length, a width and a depth of the panel, the panel lacking a substrate, formed of a material other than porous ceramic material, for supporting the porous ceramic material.
摘要翻译：提供了Floatwall面板组件和相关系统。浮法面板组件包括由多孔陶瓷材料形成的面板，所述多孔陶瓷材料沿着所述面板的长度，宽度和深度中的至少一个表现出孔隙度梯度，所述面板缺少衬底，所述衬底由除了多孔陶瓷材料，用于支撑多孔陶瓷材料。

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