公开(公告)号：US09211674B2

公开(公告)日：2015-12-15

申请号：US14119974

申请日：2012-05-25

Applicant: Michael Johannes Leonardus Van Tooren

Inventor： Michael Johannes Leonardus Van Tooren

IPC: B29C65/00 ,  B29C65/02 ,  B32B27/08 ,  B32B37/06 ,  B32B3/18 ,  B29C65/18 ,  B29C65/34 ,  B29C65/76

CPC classification number: B29C66/348 ,  B29C65/02 ,  B29C65/18 ,  B29C65/34 ,  B29C65/3408 ,  B29C65/3468 ,  B29C65/3476 ,  B29C65/3488 ,  B29C65/3492 ,  B29C65/76 ,  B29C66/003 ,  B29C66/0342 ,  B29C66/1122 ,  B29C66/474 ,  B29C66/71 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/723 ,  B29C66/72525 ,  B29C66/73116 ,  B29C66/73751 ,  B29C66/73753 ,  B29C66/73755 ,  B29C66/7392 ,  B29C66/7394 ,  B29C66/73941 ,  B29C66/87445 ,  B29C66/91411 ,  B29C66/919 ,  B29C66/91931 ,  B29C66/91935 ,  B29C66/91943 ,  B29C66/929 ,  B32B3/18 ,  B32B27/08 ,  B32B37/06 ,  Y10T428/31511 ,  Y10T428/31533 ,  Y10T428/31721 ,  B29K2081/04 ,  B29K2079/085 ,  B29K2063/00 ,  B29K2271/00 ,  B29K2307/04 ,  B29K2309/08 ,  B29K2067/00 ,  B29K2071/00

Abstract: The invention relates to a method for bonding a thermoplastic polymer to a thermosetting polymer component, the thermoplastic polymer having a melting temperature that exceeds the curing temperature of the thermosetting polymer. The method comprises the steps of providing a cured thermosetting polymer component comprising an implant of a thermoplastic polymer at least at the part of the thermosetting polymer component to be bonded, locating a thermoplastic polymer in contact with at least the part to be bonded, heating the assembly to the melting temperature of the thermoplastic polymer, whereby the thermoplastic polymer of the implant melts and fuses with the thermoplastic polymer, and cooling the assembly. The thermoplastic polymer has a melting temperature that exceeds the curing temperature of the thermosetting polymer, and the implant is designed such that heating above the maximum operating temperature of the thermosetting polymer at the interface of the implant with the thermosetting polymer component is avoided during the bonding step.

Abstract translation: 本发明涉及一种将热塑性聚合物粘合到热固性聚合物组分的方法，该热塑性聚合物的熔融温度超过热固性聚合物的固化温度。 该方法包括以下步骤：提供固化的热固性聚合物组分，其至少在待粘合的热固性聚合物组分的部分包含热塑性聚合物的植入物，将热塑性聚合物定位成与至少要结合的部分接触，加热 组装到热塑性聚合物的熔融温度，由此植入物的热塑性聚合物熔化并与热塑性聚合物熔合，并冷却组件。 热塑性聚合物具有超过热固性聚合物的固化温度的熔融温度，并且植入物被设计成使得在接合期间避免在植入物与热固性聚合物组分的界面处的热固性聚合物的最大操作温度以上的加热 步。

公开(公告)号：US09039858B2

公开(公告)日：2015-05-26

申请号：US13074430

申请日：2011-03-29

Applicant: Kenneth M. Dull ,  William H. Ingram

Inventor： Kenneth M. Dull ,  William H. Ingram

IPC: B29C65/00 ,  B29C70/54 ,  B29C70/34 ,  B29C70/44 ,  B32B17/04 ,  B32B19/04 ,  B32B37/00 ,  B32B37/02 ,  B32B37/12 ,  B29C39/00 ,  B29C37/02

CPC classification number: B29C70/54 ,  B29C37/02 ,  B29C39/00 ,  B29C65/02 ,  B29C65/48 ,  B29C65/5057 ,  B29C66/1122 ,  B29C66/522 ,  B29C66/5326 ,  B29C66/71 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/723 ,  B29C66/73751 ,  B29C66/73753 ,  B29C66/7394 ,  B29C66/73941 ,  B29C70/342 ,  B29C70/446 ,  B29L2031/3082 ,  B32B17/04 ,  B32B19/04 ,  B32B37/00 ,  B32B37/02 ,  B32B2037/1253 ,  B32B2305/076 ,  B32B2309/10 ,  Y10T156/10 ,  Y10T156/1093 ,  Y10T428/24752 ,  Y10T428/2476 ,  B29K2307/04 ,  B29K2067/00 ,  B29K2063/00 ,  B29K2027/18 ,  B29K2071/00 ,  B29K2081/06 ,  B29K2309/08 ,  B29K2307/02 ,  B29K2309/02 ,  B29K2277/10

Abstract: A composite strip and a method of manufacturing a pre-cured composite strip. A pre-cured composite strip having a thermoset resin may be placed on a surface of a portion of a composite component where a caul plate seam may be expected. Caul plates may be placed on the composite component after placing the pre-cured composite strip to form the caul plate seam. The composite component may be cured after placing the caul plates on the composite component.

Abstract translation: 复合带材和预固化复合带材的制造方法。 具有热固性树脂的预固化复合带可以放置在复合部件的可能预期产生刮板接缝的部分的表面上。 在放置预固化的复合带材以形成挡板接缝之后，可以将复合板材放置在复合部件上。 复合组件可以在将刮板放置在复合部件上之后固化。

公开(公告)号：US20140318693A1

公开(公告)日：2014-10-30

申请号：US14269157

申请日：2014-05-04

Applicant: The Boeing Company

Inventor： Karl M. Nelson ,  Joseph L. Hafenrichter ,  Kurtis S. Willden

IPC: B29C70/34 ,  B32B37/18

CPC classification number: B29C70/34 ,  B29C35/0266 ,  B29C35/0288 ,  B29C65/18 ,  B29C65/4835 ,  B29C65/5042 ,  B29C65/785 ,  B29C66/112 ,  B29C66/1122 ,  B29C66/1142 ,  B29C66/1162 ,  B29C66/118 ,  B29C66/131 ,  B29C66/14 ,  B29C66/232 ,  B29C66/301 ,  B29C66/432 ,  B29C66/4326 ,  B29C66/474 ,  B29C66/5221 ,  B29C66/524 ,  B29C66/532 ,  B29C66/61 ,  B29C66/721 ,  B29C66/73117 ,  B29C66/73751 ,  B29C66/73752 ,  B29C66/73753 ,  B29C66/73754 ,  B29C66/73941 ,  B29C66/81431 ,  B29C66/8244 ,  B29C66/83221 ,  B29C66/843 ,  B29C66/8432 ,  B29D99/0014 ,  B29K2105/243 ,  B29L2031/003 ,  B29L2031/008 ,  B29L2031/3082 ,  B29L2031/3085 ,  B32B37/18 ,  Y10T156/1002 ,  Y10T428/31504

Abstract: A composite structure is fabricated by staging at least a portion of an uncured, first composite component. The first composite component is assembled with a second composite component, and the staged portion of the first composite component is cocured with the second composite component.

Abstract translation: 通过分级未固化的第一复合组分的至少一部分来制造复合结构。 第一复合部件与第二复合部件组装，第一复合部件的分段部分与第二复合部件共固化。

公开(公告)号：US08834668B2

公开(公告)日：2014-09-16

申请号：US12274092

申请日：2008-11-19

Applicant: Karl M Nelson ,  Joseph L. Hafenrichter ,  Kurtis S Willden

Inventor： Karl M Nelson ,  Joseph L. Hafenrichter ,  Kurtis S Willden

IPC: B29C65/00 ,  B29D99/00 ,  B29C65/18 ,  B29C65/78 ,  B29C35/02 ,  B29C70/34 ,  B29C65/50 ,  B29L31/30 ,  B29K105/24 ,  B29L31/00

CPC classification number: B29C70/34 ,  B29C35/0266 ,  B29C35/0288 ,  B29C65/18 ,  B29C65/4835 ,  B29C65/5042 ,  B29C65/785 ,  B29C66/112 ,  B29C66/1122 ,  B29C66/1142 ,  B29C66/1162 ,  B29C66/118 ,  B29C66/131 ,  B29C66/14 ,  B29C66/232 ,  B29C66/301 ,  B29C66/432 ,  B29C66/4326 ,  B29C66/474 ,  B29C66/5221 ,  B29C66/524 ,  B29C66/532 ,  B29C66/61 ,  B29C66/721 ,  B29C66/73117 ,  B29C66/73751 ,  B29C66/73752 ,  B29C66/73753 ,  B29C66/73754 ,  B29C66/73941 ,  B29C66/81431 ,  B29C66/8244 ,  B29C66/83221 ,  B29C66/843 ,  B29C66/8432 ,  B29D99/0014 ,  B29K2105/243 ,  B29L2031/003 ,  B29L2031/008 ,  B29L2031/3082 ,  B29L2031/3085 ,  B32B37/18 ,  Y10T156/1002 ,  Y10T428/31504

Abstract: A composite structure is fabricated by staging at least a portion of an uncured, first composite component. The first composite component is assembled with a second composite component, and the staged portion of the first composite component is cocured with the second composite component.

Abstract translation: 通过分级未固化的第一复合组分的至少一部分来制造复合结构。 第一复合部件与第二复合部件组装，第一复合部件的分段部分与第二复合部件共固化。

公开(公告)号：US20140220356A1

公开(公告)日：2014-08-07

申请号：US14119974

申请日：2012-05-25

Applicant: Michael Johannes Leonardus Van Tooren

Inventor： Michael Johannes Leonardus Van Tooren

IPC: B32B37/06 ,  B32B27/08

CPC classification number: B29C66/348 ,  B29C65/02 ,  B29C65/18 ,  B29C65/34 ,  B29C65/3408 ,  B29C65/3468 ,  B29C65/3476 ,  B29C65/3488 ,  B29C65/3492 ,  B29C65/76 ,  B29C66/003 ,  B29C66/0342 ,  B29C66/1122 ,  B29C66/474 ,  B29C66/71 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/723 ,  B29C66/72525 ,  B29C66/73116 ,  B29C66/73751 ,  B29C66/73753 ,  B29C66/73755 ,  B29C66/7392 ,  B29C66/7394 ,  B29C66/73941 ,  B29C66/87445 ,  B29C66/91411 ,  B29C66/919 ,  B29C66/91931 ,  B29C66/91935 ,  B29C66/91943 ,  B29C66/929 ,  B32B3/18 ,  B32B27/08 ,  B32B37/06 ,  Y10T428/31511 ,  Y10T428/31533 ,  Y10T428/31721 ,  B29K2081/04 ,  B29K2079/085 ,  B29K2063/00 ,  B29K2271/00 ,  B29K2307/04 ,  B29K2309/08 ,  B29K2067/00 ,  B29K2071/00

Abstract: The invention relates to a method for bonding a thermoplastic polymer to a thermosetting polymer component, the thermoplastic polymer having a melting temperature that exceeds the curing temperature of the thermosetting polymer. The method comprises the steps of providing a cured thermosetting polymer component comprising an implant of a thermoplastic polymer at least at the part of the thermosetting polymer component to be bonded, locating a thermoplastic polymer in contact with at least the part to be bonded, heating the assembly to the melting temperature of the thermoplastic polymer, whereby the thermoplastic polymer of the implant melts and fuses with the thermoplastic polymer, and cooling the assembly. The thermoplastic polymer has a melting temperature that exceeds the curing temperature of the thermosetting polymer, and the implant is designed such that heating above the maximum operating temperature of the thermosetting polymer at the interface of the implant with the thermosetting polymer component is avoided during the bonding step.

Abstract translation: 本发明涉及一种将热塑性聚合物粘合到热固性聚合物组分的方法，该热塑性聚合物的熔融温度超过热固性聚合物的固化温度。 该方法包括以下步骤：提供固化的热固性聚合物组分，其至少在待粘合的热固性聚合物组分的部分包含热塑性聚合物的植入物，将热塑性聚合物定位成与至少要结合的部分接触，加热 组装到热塑性聚合物的熔融温度，由此植入物的热塑性聚合物熔化并与热塑性聚合物熔合，并冷却组件。 热塑性聚合物具有超过热固性聚合物的固化温度的熔融温度，并且植入物被设计成使得在接合期间避免在植入物与热固性聚合物组分的界面处的热固性聚合物的最大操作温度以上的加热 步。

公开(公告)号：US20110308722A1

公开(公告)日：2011-12-22

申请号：US13186027

申请日：2011-07-19

Applicant: Peter Sander ,  Hans Marquardt ,  Hauke Lengsfeld

Inventor： Peter Sander ,  Hans Marquardt ,  Hauke Lengsfeld

IPC: B32B37/10 ,  B32B37/14

CPC classification number: B29C66/721 ,  B29C65/02 ,  B29C66/1122 ,  B29C66/474 ,  B29C66/532 ,  B29C66/61 ,  B29C66/73751 ,  B29C66/73753 ,  B29C66/7394 ,  B29C66/81455 ,  B29D99/0014 ,  B29K2105/06 ,  B29K2105/24 ,  B29L2031/3076 ,  B29L2031/766 ,  Y10T156/1089

Abstract: The invention relates to a method for joining precured stringers to at least one structural component of an aircraft or spacecraft, including depositing covering vacuum films in advance at least on a predetermined region of each of the stringers to be joined, placing the stringers onto the at least one structural component, depositing and pressing respective vacuum film strips such that each strip is attached to a pair of stringers and present between the pair of stringers with the use of vacuum sealing in such a manner that a continuous vacuum arrangement, including the covering vacuum films and the vacuum film strips, is formed, and pressurized joining of the stringers to the at least one structural component by the continuous vacuum arrangement formed.

Abstract translation: 本发明涉及一种用于将预固化桁条连接到飞行器或航天器的至少一个结构部件的方法，包括至少在要连接的每个桁条的预定区域上预先沉积覆盖真空膜，将桁条放置在 至少一个结构部件，沉积和压制相应的真空薄膜条，使得每个条带连接到一对桁条，并且以这样的方式使用真空密封件存在于一对桁条之间，使得连续的真空装置包括覆盖真空 形成薄膜和真空薄膜条，并且通过形成的连续真空装置将桁条加压连接到至少一个结构部件。

公开(公告)号：US20100124659A1

公开(公告)日：2010-05-20

申请号：US12274092

申请日：2008-11-19

Applicant: Karl M. Nelson ,  Joseph L. Hafenrichter ,  Kurtis S Willden

Inventor： Karl M. Nelson ,  Joseph L. Hafenrichter ,  Kurtis S Willden

IPC: B32B27/00 ,  B32B37/02 ,  B29D7/00

CPC classification number: B29C70/34 ,  B29C35/0266 ,  B29C35/0288 ,  B29C65/18 ,  B29C65/4835 ,  B29C65/5042 ,  B29C65/785 ,  B29C66/112 ,  B29C66/1122 ,  B29C66/1142 ,  B29C66/1162 ,  B29C66/118 ,  B29C66/131 ,  B29C66/14 ,  B29C66/232 ,  B29C66/301 ,  B29C66/432 ,  B29C66/4326 ,  B29C66/474 ,  B29C66/5221 ,  B29C66/524 ,  B29C66/532 ,  B29C66/61 ,  B29C66/721 ,  B29C66/73117 ,  B29C66/73751 ,  B29C66/73752 ,  B29C66/73753 ,  B29C66/73754 ,  B29C66/73941 ,  B29C66/81431 ,  B29C66/8244 ,  B29C66/83221 ,  B29C66/843 ,  B29C66/8432 ,  B29D99/0014 ,  B29K2105/243 ,  B29L2031/003 ,  B29L2031/008 ,  B29L2031/3082 ,  B29L2031/3085 ,  B32B37/18 ,  Y10T156/1002 ,  Y10T428/31504

Abstract: A composite structure is fabricated by staging at least a portion of an uncured, first composite component. The first composite component is assembled with a second composite component, and the staged portion of the first composite component is cocured with the second composite component.

Abstract translation: 通过分级未固化的第一复合组分的至少一部分来制造复合结构。 第一复合部件与第二复合部件组装，第一复合部件的分段部分与第二复合部件共固化。

公开(公告)号：US20100061858A1

公开(公告)日：2010-03-11

申请号：US12205966

申请日：2008-09-08

Applicant: William F. Jones

Inventor： William F. Jones

IPC: F04D29/34 ,  B21D53/78

CPC classification number: F04D29/023 ,  B29C43/3642 ,  B29C66/02245 ,  B29C66/1222 ,  B29C66/1226 ,  B29C66/12822 ,  B29C66/12841 ,  B29C66/30322 ,  B29C66/5324 ,  B29C66/612 ,  B29C66/634 ,  B29C66/71 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/73161 ,  B29C66/73753 ,  B29C66/7394 ,  B29C66/742 ,  B29C66/81455 ,  B29D99/0025 ,  B29L2031/08 ,  F01D5/147 ,  F01D5/282 ,  F01D5/284 ,  F01D5/30 ,  F04D29/34 ,  F04D29/388 ,  F05D2230/23 ,  F05D2300/6033 ,  Y10T29/49316 ,  Y10T29/49336 ,  Y10T29/49337 ,  B29K2309/08 ,  B29K2063/00

Abstract: A method of making a composite blade that is attachable to a rotating shaft using a conventional metal blade attachment. A blade is formed from a composite material with a blade root at one end thereof. A metallic member having an external shape conforming to a conventional metal blade root is shaped with an interior cavity having an opening for receipt of the blade root. Before the composite material is fully cured, a bladder is formed into or is inserted into an end of the blade root and inflated, thereby forcing the composite material into intimate contact with the interior cavity of the metallic member, thereby ensuring a fret-free interface upon final curing of the composite material. The interior cavity of the metallic member may be shaped or surfaced to improve the load carrying capability there between.

Abstract translation: 使用传统的金属刀片附件制造可附接到旋转轴的复合刀片的方法。 叶片由其一端具有叶根的复合材料形成。 具有符合常规金属叶片根部的外部形状的金属构件成型为具有用于接收叶片根部的开口的内部空腔。 在复合材料完全固化之前，将囊状物形成或插入叶片根部的端部并膨胀，从而迫使复合材料与金属构件的内部空腔紧密接触，从而确保无纺布界面 最终固化复合材料。 金属构件的内部空腔可以成形或表面以改善其间的承载能力。

公开(公告)号：US06552095B1

公开(公告)日：2003-04-22

申请号：US09856925

申请日：2001-05-30

Applicant: Takahiro Tochioka ,  Kazuhisa Toh ,  Mitsuharu Kaneko

Inventor： Takahiro Tochioka ,  Kazuhisa Toh ,  Mitsuharu Kaneko

IPC: C08J922

CPC classification number: B32B27/065 ,  B05D1/18 ,  B29C41/18 ,  B29C44/1228 ,  B29C44/3484 ,  B29C63/0073 ,  B29C65/02 ,  B29C65/10 ,  B29C65/1412 ,  B29C65/1422 ,  B29C65/522 ,  B29C66/1122 ,  B29C66/45 ,  B29C66/545 ,  B29C66/71 ,  B29C66/723 ,  B29C66/73161 ,  B29C66/73753 ,  B29C66/73755 ,  B29C66/73921 ,  B29C66/8221 ,  B29C66/8324 ,  B29K2995/0072 ,  B32B5/18 ,  B32B2266/025 ,  C08J9/141 ,  C08J9/32 ,  C08J2203/22 ,  C08J2207/02 ,  C08J2325/10 ,  C09J5/08 ,  C09J125/10 ,  Y10T428/24996 ,  B29K2075/00 ,  B29K2071/12 ,  B29K2055/02 ,  B29K2027/06 ,  B29K2023/12 ,  B29K2023/00

Abstract: A laminate comprising a pair of thermoplastic resin members having fluctuation of clearance between the adhesion surfaces thereof, and a thermoplastic material foam layer which adheres the pair of the thermoplastic resin members. This laminate is formed from thermoplastic resin as a whole and can absorb the fluctuation of clearance between the members, and the thermoplastic resin members are firmly adhered with the thermoplastic material foam layer.

Abstract translation: 一种层压体，包括一对在其粘合表面之间具有间隙的波动的热塑性树脂构件和粘附一对热塑性树脂构件的热塑性材料泡沫层。 该层叠体由热塑性树脂整体形成，能够吸收构件之间的间隙的波动，并且热塑性树脂构件与热塑性材料泡沫层牢固地粘合。

公开(公告)号：US5582949A

公开(公告)日：1996-12-10

申请号：US634376

申请日：1990-12-27

Applicant: Richard W. Bigelow ,  Jeffrey W. Drawe ,  Richard L. Schank

Inventor： Richard W. Bigelow ,  Jeffrey W. Drawe ,  Richard L. Schank

IPC: B29C65/00 ,  G03G5/00 ,  G03G5/02 ,  G03G5/10 ,  G03G5/147

CPC classification number: B29C66/038 ,  B29C65/08 ,  B29C66/0382 ,  B29C66/1122 ,  B29C66/4322 ,  B29C66/4324 ,  B29C66/73921 ,  B29C66/7394 ,  G03G5/005 ,  G03G5/0202 ,  G03G5/0205 ,  G03G5/10 ,  G03G5/147 ,  B29C66/71 ,  B29C66/73753 ,  Y10T428/19 ,  Y10T428/197

Abstract: A process for coating flexible belt seams including providing a flexible belt having an outwardly facing surface and a welded seam, forming a smooth liquid coating on the welded seam, the liquid coating comprising a film forming polymer and a fugitive liquid carrier in which the belt surface is substantially insoluble, and removing the fugitive liquid carrier to form a smooth solid coating on the seam.

Abstract translation: 一种用于涂覆柔性带缝的方法，包括提供具有向外表面和焊接缝的柔性带，在焊缝上形成光滑的液体涂层，该液体涂层包括成膜聚合物和缓冲液体载体，其中带表面 基本上不溶，并且除去短暂的液体载体以在接缝上形成光滑的固体涂层。