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1. 发明授权

US08864073B1 Aeroshell thermal protection system and method 有权
标题翻译： Aeroshell热保护系统及方法
公开(公告)号：US08864073B1
公开(公告)日：2014-10-21
申请号：US13192431
申请日：2011-07-27
申请人： Ben Y. Won , Peter A. Hogenson , Vann Heng , Mary M. Litwinski , Robert J. Perez , Caroline Neri Kim
发明人： Dae H. Kim , Ben Y. Won , Peter A. Hogenson , Vann Heng , Mary M. Litwinski , Robert J. Perez
IPC分类号： B64C1/38 , B64G1/58
CPC分类号： B64C1/38 , B64G1/14 , B64G1/58
摘要： A thermal protection system for a vehicle may include a substantially rigid, relatively thin outer aeroshell, a relatively low density insulation layer, and a resiliently compressible conformal layer. The vehicle may include a substructure. The aeroshell may be configured to be fastened to the substructure. The insulation layer may be disposed against the aeroshell. The conformal layer may be disposable against the insulation layer. The conformal layer may be compressively preloaded against the substructure when the aeroshell is fastened to the substructure.
摘要翻译：用于车辆的热保护系统可以包括基本上刚性的，较薄的外部气囊，相对低密度的绝缘层和可弹性压缩的保形层。车辆可以包括子结构。气囊可以被配置为紧固到子结构。绝缘层可以抵靠气囊设置。保形层可以是一次性抵抗绝缘层。当气溶胶被固定到子结构体上时，共形层可以压缩地预加载到子结构上。

2. 发明授权

US08357258B2 Thermal insulation assemblies and methods for fabricating the same 有权
标题翻译：隔热组件及其制造方法
公开(公告)号：US08357258B2
公开(公告)日：2013-01-22
申请号：US12983918
申请日：2011-01-04
申请人： Vann Heng , Robert A. DiChiara, Jr. , Elizabeth Chu , Dave Zorger
发明人： Vann Heng , Robert A. DiChiara, Jr. , Elizabeth Chu , Dave Zorger
IPC分类号： B29C65/00 , B32B27/00 , B32B37/00 , B32B7/02 , B32B17/06 , B32B9/04 , B32B13/04 , B32B3/26 , B32B9/00 , B32B19/00
CPC分类号： B32B18/00 , C04B35/117 , C04B35/185 , C04B35/803 , C04B41/009 , C04B41/5031 , C04B41/87 , C04B2111/00982 , C04B2235/3217 , C04B2235/3463 , C04B2235/3826 , Y10T29/49826 , Y10T428/166 , Y10T428/24033 , Y10T428/24942 , Y10T428/24999 , C04B41/4539 , C04B41/5037 , C04B35/00 , C04B35/80
摘要： Thermal insulation assemblies, methods for fabricating thermal insulation assemblies, and thermally insulated structures are provided. In an exemplary embodiment, a thermally insulated structure is disclosed that includes a thermal insulation assembly comprises a ceramic tile having a surface coated with an alumina-mullite slurry. A ceramic matrix composite is disposed on the coated surface. The ceramic matrix composite comprises a first ply of a ceramic fiber impregnated with a ceramic matrix.
摘要翻译：提供隔热组件，制造隔热组件的方法和绝热结构。在示例性实施例中，公开了一种绝热结构，其包括绝热组件，其包括具有涂覆有氧化铝 - 莫来石浆料的表面的陶瓷砖。陶瓷基复合材料设置在涂层表面上。陶瓷基复合材料包括浸渍有陶瓷基体的陶瓷纤维的第一层。

3. 发明授权

US07887937B2 Thermal insulation assemblies and methods for fabricating the same 有权
标题翻译：隔热组件及其制造方法
公开(公告)号：US07887937B2
公开(公告)日：2011-02-15
申请号：US11737115
申请日：2007-04-18
申请人： Vann Heng , Robert A. DiChiara, Jr. , Elizabeth Chu , Dave Zorger
发明人： Vann Heng , Robert A. DiChiara, Jr. , Elizabeth Chu , Dave Zorger
IPC分类号： B32B9/00 , B05D3/02
CPC分类号： B32B18/00 , C04B35/117 , C04B35/185 , C04B35/803 , C04B41/009 , C04B41/5031 , C04B41/87 , C04B2111/00982 , C04B2235/3217 , C04B2235/3463 , C04B2235/3826 , Y10T29/49826 , Y10T428/166 , Y10T428/24033 , Y10T428/24942 , Y10T428/24999 , C04B41/4539 , C04B41/5037 , C04B35/00 , C04B35/80
摘要： Thermal insulation assemblies and methods for fabricating thermal insulation assemblies are provided. In an exemplary embodiment, a thermal insulation assembly comprises a ceramic tile having a surface coated with an alumina-mullite slurry. A ceramic matrix composite is disposed on the coated surface. The ceramic matrix composite comprises a first ply of a ceramic fiber impregnated with a ceramic matrix.
摘要翻译：提供隔热组件和制造隔热组件的方法。在示例性实施例中，绝热组件包括具有涂覆有氧化铝 - 莫来石浆料的表面的陶瓷砖。陶瓷基复合材料设置在涂层表面上。陶瓷基复合材料包括浸渍有陶瓷基体的陶瓷纤维的第一层。

4. 发明申请

US20110003077A1 Reworking Ceramic Structures 有权
标题翻译：返修陶瓷结构
公开(公告)号：US20110003077A1
公开(公告)日：2011-01-06
申请号：US12497008
申请日：2009-07-02
申请人： Vann Heng , Elizabeth Chu , Van H. Ngo , Larry D. King
发明人： Vann Heng , Elizabeth Chu , Van H. Ngo , Larry D. King
IPC分类号： B05D3/00
CPC分类号： C04B37/008 , C04B37/001 , C04B37/005 , C04B41/009 , C04B41/5025 , C04B41/87 , C04B2111/00982 , C04B2235/612 , C04B2235/6567 , C04B2235/6581 , C04B2237/04 , C04B2237/062 , C04B2237/064 , C04B2237/08 , C04B2237/083 , C04B2237/32 , C04B2237/341 , C04B2237/343 , C04B2237/365 , C04B2237/368 , C04B2237/52 , C04B2237/62 , C04B2237/88 , F01D5/005 , F05D2300/6033 , Y02T50/672 , B32B18/00 , C04B35/80 , C04B41/4535 , C04B41/457 , C04B41/4572
摘要： A method for reworking a ceramic structure. A number of holes are formed in a portion of the ceramic structure in which a rework of the ceramic structure is desired. The ceramic structure has a plurality of layers in the portion in which the rework is desired. A ceramic bonding material is introduced into the number of holes formed in the portion of the ceramic structure. The ceramic bonding material is cured in the portion of the ceramic structure.
摘要翻译：陶瓷结构的再加工方法。在陶瓷结构的一部分中形成多个孔，其中期望陶瓷结构的返修。陶瓷结构在需要返工的部分中具有多个层。将陶瓷接合材料引入形成在陶瓷结构部分中的孔数。陶瓷接合材料在陶瓷结构的部分被固化。

5. 发明申请

US20140248812A1 RE-USABLE HIGH-TEMPERATURE RESISTANT SOFTGOODS FOR AEROSPACE APPLICATIONS 有权
标题翻译：用于航空应用的可用的高温抗性软件
公开(公告)号：US20140248812A1
公开(公告)日：2014-09-04
申请号：US13629782
申请日：2012-09-28
申请人： Adam J. Lang , Leanne L. Lehman , Vann Heng , Kenneth R. Stempel
发明人： Adam J. Lang , Leanne L. Lehman , Vann Heng , Kenneth R. Stempel
IPC分类号： B32B9/04 , B32B5/02 , B05D7/24
CPC分类号： C04B41/5031 , B32B5/02 , B32B9/04 , C04B41/009 , C04B41/5059 , C04B41/5089 , C04B41/52 , C04B2111/00982 , Y10T442/20 , Y10T442/2984 , C04B14/4625 , C04B30/02 , C04B14/4693 , C04B41/4539 , C04B2103/54 , C04B41/4535 , C04B41/4554
摘要： High-temperature fabrics with a coatings to provide oxidation protection at high temperatures, and capable of being formed into a variety of softgoods parts, and methods for their manufacture are disclosed.
摘要翻译：公开了具有涂层以在高温下提供氧化保护并且能够形成各种软质部件的高温织物及其制造方法。

6. 发明授权

US06866733B1 Method of forming a flexible insulation blanket having a ceramic matrix composite outer layer 有权
标题翻译：形成具有陶瓷基复合外层的柔性绝缘毯的方法
公开(公告)号：US06866733B1
公开(公告)日：2005-03-15
申请号：US10611493
申请日：2003-07-01
申请人： Jerry Denham , Robert A. Dichiara, Jr. , Vann Heng , Leanne L. Lehman , David Zorger
发明人： Jerry Denham , Robert A. Dichiara, Jr. , Vann Heng , Leanne L. Lehman , David Zorger
IPC分类号： B32B3/06 , B32B5/02 , B32B5/26 , B32B5/30 , B32B9/00 , B32B17/02 , B32B18/00 , B64C1/00 , C04B35/00 , C04B35/447 , C04B35/80 , F16L59/02 , B32B31/20 , B32B31/26
CPC分类号： B32B18/00 , B32B5/02 , B32B5/26 , B32B5/30 , B32B17/02 , C04B35/447 , C04B35/6263 , C04B35/803 , C04B2235/3224 , C04B2235/5224 , C04B2235/5228 , C04B2235/5232 , C04B2235/5244 , C04B2235/5256 , F16L59/026 , Y10S428/92 , Y10T428/24033 , Y10T428/249928 , Y10T428/26
摘要： A flexible insulation blanket having a ceramic matrix composite (CMC) outer layer, and a method of producing a flexible insulation blanket having a smooth, aerodynamically suitable, outer surface by infiltrating ceramic material within the outer ceramic fabric layer of the flexible insulation blanket and curing the ceramic material to form a CMC layer. The CMC layer is cured while the blanket is under compression such that the resulting CMC layer has a smooth surface.
摘要翻译：一种具有陶瓷基复合材料（CMC）外层的柔性绝缘毯，以及通过在柔性绝缘毯的外陶瓷织物层内渗透陶瓷材料并固化而制备具有光滑，空气动力学适合的外表面的柔性绝缘毯的方法陶瓷材料形成CMC层。当层压缩时，CMC层被固化，使得所得的CMC层具有光滑的表面。

7. 发明授权

US06716782B2 Rigid insulation and method of producing same 有权
标题翻译：刚性绝缘及其制造方法
公开(公告)号：US06716782B2
公开(公告)日：2004-04-06
申请号：US10222622
申请日：2002-08-16
申请人： Vann Heng , Karrie Ann Hinkle , Mary Ann Santos
发明人： Vann Heng , Karrie Ann Hinkle , Mary Ann Santos
IPC分类号： C04B3580
CPC分类号： C04B35/806 , C04B30/02 , C04B35/62635 , C04B38/0038 , C04B2111/00379 , C04B2111/00982 , C04B2235/3821 , C04B2235/5224 , C04B2235/5232 , C04B2235/526 , C04B2235/5264 , C04B2235/5268 , C04B2235/77 , C04B2235/94 , C04B2235/9607 , Y10T428/249928 , Y10T428/249929 , C04B14/323 , C04B14/4625 , C04B14/4631 , C04B40/0071 , C04B40/0268
摘要： A porous ceramic fiber insulating material and method of making a material having a combination of silica (SiO2) and alumina (Al2O3) fibers, and boron-containing powders is the topic of the new invention. The insulative material is composed of about 60 wt % to about 80 wt % silica fibers, about 20 wt % to about 40 wt % alumina fibers, and about 0.1 wt % to about 1.0 wt % boron-containing powders. A specific boron-containing powder used for this invention is boron carbide powder which provide boron-containing by-products, which aid in fusion and sintering of the silica and alumina fibers. The material is produced by forming an aqueous slurry, blending and chopping the fibers via a shear mixer, orienting the fibers in the in-plane direction, draining water from the fibers, pressing the fibers into a billet, heating the fibers to remove residual water, and firing the billet to fuse the fibers of the material. After sintering, bulk density of the new insulation material ranges from 6 to 20 lb/ft3.
摘要翻译：多孔陶瓷纤维绝缘材料和制备具有二氧化硅（SiO 2）和氧化铝（Al 2 O 3）纤维和含硼粉末的组合的材料的方法是本发明的主题。绝缘材料由约60重量％至约80重量％的二氧化硅纤维，约20重量％至约40重量％的氧化铝纤维和约0.1重量％至约1.0重量％的含硼粉末组成。用于本发明的特定的含硼粉末是提供含硼副产物的碳化硼粉末，其有助于二氧化硅和氧化铝纤维的熔融和烧结。该材料通过形成含水浆料，通过剪切混合器共混和切割纤维来制造，将纤维定向在面内方向，从纤维中排出水，将纤维压制成坯料，加热纤维以除去残留的水，并烧制坯料以熔化材料的纤维。烧结后，新型绝缘材料的体积密度范围为6至20磅/英尺3。

8. 发明授权

US06367740B1 Air foil having a hybrid leading edge construction 失效
标题翻译：具有混合前缘结构的气翼
公开(公告)号：US06367740B1
公开(公告)日：2002-04-09
申请号：US09572382
申请日：2000-05-16
申请人： Scott E. Johnson , Vann Heng , Guillermo Mas
发明人： Scott E. Johnson , Vann Heng , Guillermo Mas
IPC分类号： B64C338
CPC分类号： B64C3/36 , B64C3/28
摘要： A leading edge component for reducing drag and improving heat sink properties of an air foil. The leading edge component includes a composite tile component with a predetermined aerodynamic shape and a metallic lip portion with high thermal conductivity. The metallic lip portion is secured to a forwardmost edge portion of the composite tile component to thereby form a leading edge of the air foil. The leading edge component is better able to withstand the structural stresses and extremely high temperatures that result while travelling at hypersonic speeds, without a significant increase in weight to the air foil with which the leading edge component is used.
摘要翻译：用于减少阻力并改善气翼的散热性能的前沿部件。前缘部件包括具有预定空气动力学形状的复合瓦片部件和具有高导热性的金属唇部分。金属唇部固定在复合瓷砖部件的最前缘部分上，从而形成空气箔的前缘。前缘部件能够更好地承受在超音速行驶时产生的结构应力和极高的温度，而不会使用前缘部件使用的气翼的重量显着增加。

9. 发明授权

US08894919B1 Method for incorporation of insulators and bulk absorbers in high temperature sandwich structures after fabrication 有权
标题翻译：制造后在高温三明治结构中掺入绝缘子和体积吸收体的方法
公开(公告)号：US08894919B1
公开(公告)日：2014-11-25
申请号：US13552235
申请日：2012-07-18
申请人： Leanne L. Lehman , Vann Heng , James Philip Ledesma, Jr. , Jonathan David Embler
发明人： Leanne L. Lehman , Vann Heng , James Philip Ledesma, Jr. , Jonathan David Embler
IPC分类号： C04B41/65
CPC分类号： F16L59/04 , C04B35/111 , C04B35/624 , C04B35/803 , C04B38/0045 , C04B2111/00612 , C04B2235/3218 , C04B2235/3804 , C04B2235/5224 , C04B2235/5228 , C04B2235/5232 , C04B2235/6027 , C04B2235/606 , C04B35/10 , C04B38/08
摘要： A method for adding insulation or bulk absorbers into high temperature sandwich structures following fabrication is presented. A slurry of ceramic fibers and/or particles, opacified particles, fugitive fibers, organic binders and inorganic binders is prepared as an aqueous solution. The slurry is cast within a prepared sandwich structure, dried, and heated to form a low density ceramic core material to provide insulation or noise absorption. Following incorporation of the ceramic material, aerogels or phase change materials may also be added to provide additional thermal management benefits.
摘要翻译：提出了一种在绝缘或体积吸收体制造后加入高温三明治结构的方法。制备陶瓷纤维和/或颗粒，不透明颗粒，短纤维，有机粘合剂和无机粘合剂的浆料作为水溶液。将浆料浇铸在制备的夹层结构中，干燥并加热以形成低密度陶瓷芯材料以提供绝缘或噪声吸收。在加入陶瓷材料之后，还可以加入气凝胶或相变材料以提供额外的热管理优点。

10. 发明申请

US20110171442A1 THERMAL INSULATION ASSEMBLIES AND METHODS FOR FABRICATING THE SAME 有权
标题翻译：热绝缘组件及其制造方法
公开(公告)号：US20110171442A1
公开(公告)日：2011-07-14
申请号：US12983918
申请日：2011-01-04
申请人： Vann HENG , Robert A. DiChiara, JR. , Elizabeth CHU , Dave ZORGER
发明人： Vann HENG , Robert A. DiChiara, JR. , Elizabeth CHU , Dave ZORGER
IPC分类号： B32B7/02 , B32B9/00 , B32B3/26 , B32B13/04 , B23P17/04
CPC分类号： B32B18/00 , C04B35/117 , C04B35/185 , C04B35/803 , C04B41/009 , C04B41/5031 , C04B41/87 , C04B2111/00982 , C04B2235/3217 , C04B2235/3463 , C04B2235/3826 , Y10T29/49826 , Y10T428/166 , Y10T428/24033 , Y10T428/24942 , Y10T428/24999 , C04B41/4539 , C04B41/5037 , C04B35/00 , C04B35/80
摘要： Thermal insulation assemblies, methods for fabricating thermal insulation assemblies, and thermally insulated structures are provided. In an exemplary embodiment, a thermally insulated structure is disclosed that includes a thermal insulation assembly comprises a ceramic tile having a surface coated with an alumina-mullite slurry. A ceramic matrix composite is disposed on the coated surface. The ceramic matrix composite comprises a first ply of a ceramic fiber impregnated with a ceramic matrix.
摘要翻译：提供隔热组件，制造隔热组件的方法和绝热结构。在示例性实施例中，公开了一种绝热结构，其包括绝热组件，其包括具有涂覆有氧化铝 - 莫来石浆料的表面的陶瓷砖。陶瓷基复合材料设置在涂层表面上。陶瓷基复合材料包括浸渍有陶瓷基体的陶瓷纤维的第一层。

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