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1. 发明申请

US20130276459A1 RESISTIVE BAND FOR TURBOMACHINE BLADE 有权
标题翻译：涡轮叶片电阻带
公开(公告)号：US20130276459A1
公开(公告)日：2013-10-24
申请号：US13454979
申请日：2012-04-24
申请人： Herbert Chidsey Roberts , Glenn Curtis Taxacher
发明人： Herbert Chidsey Roberts , Glenn Curtis Taxacher
IPC分类号： F01D5/14 , F02C7/00 , F02C3/06
CPC分类号： F01D5/005 , F01D5/282 , F01D5/284 , F05D2300/603 , F05D2300/6033 , Y02T50/672
摘要： A turbomachine system includes a rotor that defines a longitudinal axis of the turbomachine system. A first blade is coupled to the rotor, and the first blade has first and second laminated plies. A first band is coupled to the first blade and is configured to resist separation of the first and second laminated plies.
摘要翻译：涡轮机系统包括限定涡轮机系统的纵向轴线的转子。第一叶片联接到转子，并且第一叶片具有第一和第二层压层。第一带耦合到第一叶片并且被配置为抵抗第一和第二层压层的分离。

2. 发明授权

US09115584B2 Resistive band for turbomachine blade 有权
标题翻译：涡轮机叶片的电阻带
公开(公告)号：US09115584B2
公开(公告)日：2015-08-25
申请号：US13454979
申请日：2012-04-24
申请人： Herbert Chidsey Roberts , Glenn Curtis Taxacher
发明人： Herbert Chidsey Roberts , Glenn Curtis Taxacher
IPC分类号： F01D5/14 , F01D5/00 , F01D5/28
CPC分类号： F01D5/005 , F01D5/282 , F01D5/284 , F05D2300/603 , F05D2300/6033 , Y02T50/672
摘要： A turbomachine system includes a rotor that defines a longitudinal axis of the turbomachine system. A first blade is coupled to the rotor, and the first blade has first and second laminated plies. A first band is coupled to the first blade and is configured to resist separation of the first and second laminated plies.
摘要翻译：涡轮机系统包括限定涡轮机系统的纵向轴线的转子。第一叶片联接到转子，并且第一叶片具有第一和第二层压层。第一带耦合到第一叶片并且被配置为抵抗第一和第二层压层的分离。

3. 发明授权

US08303245B2 Shroud assembly with discourager 有权
标题翻译：护罩装配与沮丧者
公开(公告)号：US08303245B2
公开(公告)日：2012-11-06
申请号：US12576386
申请日：2009-10-09
申请人： Gregory Thomas Foster , Andres Jose Garcia Crespo , Herbert Chidsey Roberts
发明人： Gregory Thomas Foster , Andres Jose Garcia Crespo , Herbert Chidsey Roberts
IPC分类号： F01D11/08
CPC分类号： F01D25/265 , F01D9/04 , F01D11/00 , F05D2240/11 , Y02T50/672
摘要： A turbine shroud assembly is disclosed, the shroud assembly including an outer shroud, at least one inner shroud attached to the outer shroud, and at least one discourager enclosed within the inner shroud. The discourager prevents the hot gas or steam in the turbine from having a direct line of access to the outer shroud. In one embodiment, one inner shroud is provided for the shroud assembly, with one discourager enclosed within the inner shroud, the discourager positioned offset from the inner shroud so as to extend past the inner shroud and into an inner shroud of a neighboring shroud assembly. In another embodiment, a plurality of inner shrouds are provided, each inner shroud enclosing a discourager, the discouragers being adjacent to each other within the inner shrouds and positioned offset from the inner shrouds so as to cover a gap between the inner shrouds.
摘要翻译：公开了一种涡轮机护罩组件，护罩组件包括外护罩，附接到外护罩的至少一个内护罩和封闭在内护罩内的至少一个挡板。防火墙防止涡轮机中的热气体或蒸汽直接进入外护罩。在一个实施例中，为护罩组件提供一个内护罩，其中一个气囊封闭在内护罩内，捣毁器定位成偏离内护罩，以便延伸穿过内护罩并进入相邻护罩组件的内护罩。在另一个实施例中，提供多个内护罩，每个内护罩包围一个挡板，该挡板在该内护罩内彼此相邻并且与该内护罩相偏离，以便覆盖该内护罩之间的间隙。

4. 发明申请

US20110256358A1 CERAMIC COMPOSITE COMPONENTS AND METHODS OF FABRICATING THE SAME 有权
标题翻译：陶瓷复合材料及其制造方法
公开(公告)号：US20110256358A1
公开(公告)日：2011-10-20
申请号：US12761932
申请日：2010-04-16
申请人： Herbert Chidsey Roberts , Paul Stephen DiMascio
发明人： Herbert Chidsey Roberts , Paul Stephen DiMascio
IPC分类号： B32B3/10 , B29C65/00
CPC分类号： F01D25/12 , B32B18/00 , C04B35/632 , C04B35/63476 , C04B35/653 , C04B37/008 , C04B2237/32 , C04B2237/62 , F01D25/005 , F05C2203/08 , F05C2253/04
摘要： A method for fabricating a ceramic composite includes forming a first ceramic composite layer (CCL), positioning a form against the first CCL, positioning a second CCL against the form such that the form is at least partially circumscribed by the first CCL and the second CCL. The method also includes coupling the first CCL to the second CCL, such that at least a first passage extends in a first direction across at least a portion of the ceramic composite component and is defined at least partially by the first CCL and the second CCL in a location vacated by the first form.
摘要翻译：一种制造陶瓷复合材料的方法包括：形成第一陶瓷复合层（CCL），将形状定位成抵靠第一CCL，将第二CCL定位成使形状至少部分地被第一CCL和第二CCL限定。该方法还包括将第一CCL耦合到第二CCL，使得至少第一通道跨过陶瓷复合部件的至少一部分沿第一方向延伸，并且至少部分地由第一CCL和第二CCL限定由第一个表格腾出的位置。

5. 发明授权

US09290836B2 Crack-resistant environmental barrier coatings 有权
标题翻译：耐破坏环境屏障涂层
公开(公告)号：US09290836B2
公开(公告)日：2016-03-22
申请号：US13588051
申请日：2012-08-17
申请人： James Zhang , Herbert Chidsey Roberts , Rupak Das
发明人： James Zhang , Herbert Chidsey Roberts , Rupak Das
IPC分类号： B05D5/00 , C23C4/02 , C23C4/18 , C23C16/02 , C23C16/56 , C23C30/00 , C04B41/89 , C04B41/00 , C04B41/52 , F01D5/28
CPC分类号： C23C4/02 , C04B41/009 , C04B41/52 , C04B41/89 , C23C4/18 , C23C16/02 , C23C16/56 , C23C30/00 , F01D5/288 , F05D2240/121 , F05D2240/122 , F05D2240/125 , F05D2240/303 , F05D2240/304 , F05D2240/307 , Y10T428/24793 , C04B35/565 , C04B35/806 , C04B41/5096 , C04B41/5059 , C04B41/522 , C04B41/5066 , C04B41/5024 , C04B41/5042
摘要： Methods suitable for reducing corner cracking of environmental barrier coating systems. The methods include forming at least one layer of a first portion of the environmental barrier coating system on at least a first region of the component, performing a first heat treatment, forming at least one layer of a second portion of the environmental barrier coating system on a second region of the component, and performing a second heat treatment to the component. Edges of the first portion and edges of the second portion form an angle of at most 60° with respect to a surface of the first region of the component. During the second heat treatment, the second portion of the EBC system expands and the expansion of the second portion of the EBC system is at least partially constrained by the first portion of the EBC system to reduce tensile interfacial stresses in the EBC system.
摘要翻译：适用于减少环境屏障涂层系统的角裂纹的方法。所述方法包括在所述部件的至少第一区域上形成环境阻挡涂层系统的第一部分的至少一层，进行第一热处理，将环境阻挡涂层系统的至少一层第二部分形成在所述部件的第二区域，并且对所述部件进行第二热处理。第一部分的边缘和第二部分的边缘相对于部件的第一区域的表面形成至多60°的角度。在第二热处理期间，EBC系统的第二部分膨胀并且EBC系统的第二部分的膨胀至少部分地被EBC系统的第一部分约束，以减少EBC系统中的拉伸界面应力。

6. 发明授权

US08807931B2 System for impact zone reinforcement 有权
标题翻译：冲击带加固系统
公开(公告)号：US08807931B2
公开(公告)日：2014-08-19
申请号：US12652031
申请日：2010-01-04
申请人： Herbert Chidsey Roberts
发明人： Herbert Chidsey Roberts
IPC分类号： F01D9/02 , F01D5/28
CPC分类号： F01D5/282 , F01D5/147 , F05D2240/122 , F05D2240/304 , F05D2300/603 , Y02T50/672 , Y02T50/673 , Y10T428/249933 , Y10T428/249938 , Y10T428/249939 , Y10T428/249949 , Y10T428/24995
摘要： A system may include a structure having a leading edge and a fiber-reinforced composite cover. The fiber-reinforced composite cover may include a protective portion and a retaining portion, wherein the retaining portion extends about the structure to self-retain the protective portion along the leading edge, and the protective portion is different from the retaining portion.
摘要翻译：系统可以包括具有前缘的结构和纤维增强的复合覆盖物。纤维增强复合材料盖可以包括保护部分和保持部分，其中保持部分围绕结构延伸以沿着前缘自我保持保护部分，并且保护部分与保持部分不同。

7. 发明授权

US07951464B2 Composite material with fiber alignment 失效
标题翻译：复合材料与光纤对准
公开(公告)号：US07951464B2
公开(公告)日：2011-05-31
申请号：US12553032
申请日：2009-09-02
申请人： Herbert Chidsey Roberts
发明人： Herbert Chidsey Roberts
IPC分类号： H01F3/02
CPC分类号： B29C70/14 , B29C70/88 , H01F1/37 , Y10T428/12063 , Y10T428/12465 , Y10T428/249924 , Y10T428/249942 , Y10T428/249944
摘要： A composite material may be provided with unique alignment characteristics. The composite material may include a matrix material and a plurality of fibers disposed in the matrix material, wherein the plurality of fibers is magnetically aligned in a uniform spacing within the matrix material.
摘要翻译：复合材料可以具有独特的对准特性。复合材料可以包括基体材料和布置在基体材料中的多个纤维，其中多个纤维以基体材料内均匀的间隔磁性排列。

8. 发明申请

US20140037969A1 Hybrid Air Plasma Spray and Slurry Method of Environmental Barrier Deposition 审中-公开
标题翻译：混合空气等离子体喷雾和泥浆环境阻挡沉积法
公开(公告)号：US20140037969A1
公开(公告)日：2014-02-06
申请号：US13565946
申请日：2012-08-03
申请人： Joshua Lee Margolies , Herbert Chidsey Roberts , Don Mark Lipkin , Glen Harold Kirby , Nicholas Edward Antolino
发明人： Joshua Lee Margolies , Herbert Chidsey Roberts , Don Mark Lipkin , Glen Harold Kirby , Nicholas Edward Antolino
IPC分类号： B05D1/36 , C23C4/12 , B32B9/00
CPC分类号： C23C4/12 , C04B41/009 , C04B41/52 , C04B41/89 , C23C4/02 , C23C4/18 , C23C28/00 , F01D5/282 , F01D5/288 , F05D2220/32 , F05D2230/312 , F05D2240/30 , F05D2300/15 , F05D2300/6033 , Y02T50/672 , C04B35/565 , C04B35/806 , C04B35/58092 , C04B35/584 , C04B35/52 , C04B35/83 , C04B41/4531 , C04B41/5096 , C04B41/4527 , C04B41/5071 , C04B41/522 , C04B41/5024 , C04B41/4539 , C04B41/526
摘要： A bond layer may be applied to the substrate of an article and a first layer may be applied to the bond layer by thermal spray. A second layer may be applied above the first layer by slurry coating.
摘要翻译：可以将粘合层施加到制品的基底上，并且可以通过热喷涂将第一层施加到接合层。可以通过浆料涂覆在第一层上方施加第二层。

9. 发明申请

US20110164986A1 SYSTEM FOR IMPACT ZONE REINFORCEMENT 有权
标题翻译：影响区域加固系统
公开(公告)号：US20110164986A1
公开(公告)日：2011-07-07
申请号：US12652031
申请日：2010-01-04
申请人： Herbert Chidsey Roberts
发明人： Herbert Chidsey Roberts
IPC分类号： F01D5/28
CPC分类号： F01D5/282 , F01D5/147 , F05D2240/122 , F05D2240/304 , F05D2300/603 , Y02T50/672 , Y02T50/673 , Y10T428/249933 , Y10T428/249938 , Y10T428/249939 , Y10T428/249949 , Y10T428/24995
摘要： A system may include a structure having a leading edge and a fiber-reinforced composite cover. The fiber-reinforced composite cover may include a protective portion and a retaining portion, wherein the retaining portion extends about the structure to self-retain the protective portion along the leading edge, and the protective portion is different from the retaining portion.
摘要翻译：系统可以包括具有前缘的结构和纤维增强的复合覆盖物。纤维增强复合材料盖可以包括保护部分和保持部分，其中保持部分围绕结构延伸以沿着前缘自我保持保护部分，并且保护部分与保持部分不同。

10. 发明申请

US20110085899A1 SHROUD ASSEMBLY WITH DISCOURAGER 有权
公开(公告)号：US20110085899A1
公开(公告)日：2011-04-14
申请号：US12576386
申请日：2009-10-09
申请人： Gregory Thomas Foster , Andres Jose Garcia Crespo , Herbert Chidsey Roberts
发明人： Gregory Thomas Foster , Andres Jose Garcia Crespo , Herbert Chidsey Roberts
IPC分类号： F01D11/00 , F01D9/04 , F01D25/26
CPC分类号： F01D25/265 , F01D9/04 , F01D11/00 , F05D2240/11 , Y02T50/672
摘要： A turbine shroud assembly is disclosed, the shroud assembly including an outer shroud, at least one inner shroud attached to the outer shroud, and at least one discourager enclosed within the inner shroud. The discourager prevents the hot gas or steam in the turbine from having a direct line of access to the outer shroud. In one embodiment, one inner shroud is provided for the shroud assembly, with one discourager enclosed within the inner shroud, the discourager positioned offset from the inner shroud so as to extend past the inner shroud and into an inner shroud of a neighboring shroud assembly. In another embodiment, a plurality of inner shrouds are provided, each inner shroud enclosing a discourager, the discouragers being adjacent to each other within the inner shrouds and positioned offset from the inner shrouds so as to cover a gap between the inner shrouds.
摘要翻译：公开了一种涡轮机护罩组件，护罩组件包括外护罩，附接到外护罩的至少一个内护罩和封闭在内护罩内的至少一个挡板。防火墙防止涡轮机中的热气体或蒸汽直接进入外护罩。在一个实施例中，为护罩组件提供一个内护罩，其中一个气囊封闭在内护罩内，捣毁器定位成偏离内护罩，以便延伸穿过内护罩并进入相邻护罩组件的内护罩。在另一个实施例中，提供多个内护罩，每个内护罩包围一个挡板，该挡板在该内护罩内彼此相邻并且与该内护罩相偏离，以便覆盖该内护罩之间的间隙。

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