公开(公告)号：US09432074B2

公开(公告)日：2016-08-30

申请号：US14865233

申请日：2015-09-25

Applicant: Incipio, LLC

Inventor： Andy Fathollahi

IPC: H04M1/00 ,  B29C45/14 ,  H04B1/3888 ,  B29K101/12 ,  B29K305/00 ,  B29K303/00 ,  B29L31/34

CPC classification number: B29C45/14065 ,  B29C45/14631 ,  B29C45/1671 ,  B29C45/1676 ,  B29D99/006 ,  B29K2101/12 ,  B29K2303/00 ,  B29K2305/00 ,  B29L2031/3481 ,  H04B1/3888 ,  H04M1/185

Abstract: A protective case for a mobile device having a co-molded multi-layered construction having a first layer that generally forms the external back face surface of the case. A second layer generally forms the perimeter bumper of the case. The first layer is comprised of material that has a hardness and/or rigidity that is greater than the second layer. The layers are configured to interact with one another so that they are capable of distributing impact forces to mitigate damage to the mobile device. One or more reinforcing support members in the form of a beam or rod are provided and extend internally and longitudinally near the sides of the case and preferably near the long sides of a rectangular shaped case. The reinforcing support members are formed of even harder or more rigid materials, such as metal alloy or cured fiber reinforced composite rods or beams, relative to the first and second layer and are capable of providing additional support and rigidity to the mobile device to stop or mitigate unintentional or undesired bending of the mobile device.

Abstract translation: 一种用于具有共模塑多层结构的移动设备的保护壳体，其具有通常形成壳体的外部背面表面的第一层。 第二层通常形成外壳的周边保险杠。 第一层由具有大于第二层的硬度和/或刚度的材料构成。 这些层被配置为相互交互，使得它们能够分配冲击力以减轻对移动设备的损坏。 提供了梁或杆形式的一个或多个加强支撑构件，并且在壳体的侧面的内部和纵向附近延伸，并且优选地在矩形形状的壳体的长边附近延伸。 加强支撑构件由相对于第一层和第二层的甚至更硬或更刚性的材料形成，例如金属合金或固化的纤维增强复合材料棒或梁，并且能够为移动装置提供额外的支撑和刚性以停止或 减轻移动设备的无意或不期望的弯曲。

公开(公告)号：US11008438B2

公开(公告)日：2021-05-18

申请号：US15830808

申请日：2017-12-04

Applicant: Stephen Gleason, Sr.

Inventor： Stephen Gleason, Sr.

IPC: C08K3/30 ,  C08J5/04 ,  C08J5/18 ,  C08J5/24 ,  C08K3/013 ,  C08L35/02 ,  B29C70/70 ,  B29C41/30 ,  B29C70/30 ,  B29C70/68 ,  B29C70/86 ,  B29C70/02 ,  B29C37/00 ,  B29C41/20 ,  B29C70/54 ,  B29C70/60 ,  B29C41/00 ,  B29C70/88 ,  B29C41/32 ,  B29C41/22 ,  B29K31/00 ,  B29K67/00 ,  B29K105/06 ,  B29K105/16 ,  B29K267/00 ,  B29K231/00 ,  B29K105/20 ,  B29K309/00 ,  B29K303/04 ,  B29K631/00 ,  B29K667/00 ,  B29K509/00 ,  B29K303/00 ,  G01N1/36 ,  G01N33/44 ,  G01N3/10

Abstract: A composite core material and methods for making same are disclosed herein. The composite core material comprises mineral filler discontinuous portions disposed in a continuous encapsulating resin. Further, the method for forming a composite core material comprises the steps of forming a mixture comprising mineral filler, an encapsulating prepolymer, and a polymerization catalyst; disposing the mixture onto a moving belt; and polymerizing said encapsulating prepolymer to form a composite core material comprising mineral filler discontinuous portions disposed in a continuous encapsulating resin.

公开(公告)号：US09914246B2

公开(公告)日：2018-03-13

申请号：US14333605

申请日：2014-07-17

Applicant: Airbus Operations GmbH

Inventor： Hauke Seegel ,  Claus Fastert ,  Lionel Winkelmann ,  Paulin Fideu Siagam

IPC: B29C43/56 ,  B29C70/44 ,  B29C43/36 ,  B29K303/00

CPC classification number: B29C43/56 ,  B29C43/3642 ,  B29C70/443 ,  B29C2043/561 ,  B29K2303/00 ,  B29K2911/00

Abstract: A system for liquid composite molding includes a first rigid tool part onto which a semi-finished fiber material is positioned, a first vacuum foil arrangeable on the first rigid tool part to provide a first gastight chamber therebetween having a first port, a second vacuum foil and the first vacuum foil providing a second gastight chamber, and granulated material arranged in the second gastight chamber. The semi-finished fiber material is infusible with a matrix material via the first port. A second port is provided at the second gastight chamber for applying a negative pressure thereto. Therein, the granulated material is adapted for forming a second rigid tool part when negative pressure is applied to the second port. I.e. the first vacuum foil, the second vacuum foil and the granulated material function similarly to a vacuum mattress and may be stiffened and collapsed.

公开(公告)号：US12221522B2

公开(公告)日：2025-02-11

申请号：US18466572

申请日：2023-09-13

Applicant: Composite Technologies International, LLC

Inventor： Stephen Gleason, Sr.

IPC: C08K3/30 ,  B29C37/00 ,  B29C41/00 ,  B29C41/20 ,  B29C41/22 ,  B29C41/30 ,  B29C41/32 ,  B29C70/02 ,  B29C70/30 ,  B29C70/54 ,  B29C70/60 ,  B29C70/68 ,  B29C70/70 ,  B29C70/86 ,  B29C70/88 ,  B29K31/00 ,  B29K67/00 ,  B29K105/06 ,  B29K105/16 ,  B29K105/20 ,  B29K231/00 ,  B29K267/00 ,  B29K303/00 ,  B29K303/04 ,  B29K309/00 ,  B29K509/00 ,  B29K631/00 ,  B29K667/00 ,  C08J5/04 ,  C08J5/18 ,  C08J5/24 ,  C08K3/013 ,  C08L35/02 ,  G01N1/36 ,  G01N3/10 ,  G01N33/44

Abstract: A composite core material and methods for making same are disclosed herein. The composite core material comprises mineral filler discontinuous portions disposed in a continuous encapsulating resin. Further, the method for forming a composite core material comprises the steps of forming a mixture comprising mineral filler, an encapsulating prepolymer, and a polymerization catalyst; disposing the mixture onto a moving belt; and polymerizing said encapsulating prepolymer to form a composite core material comprising mineral filler discontinuous portions disposed in a continuous encapsulating resin.

公开(公告)号：US11760862B2

公开(公告)日：2023-09-19

申请号：US17322372

申请日：2021-05-17

Applicant: Composite Technologies International, LLC

Inventor： Stephen Gleason, Sr.

IPC: C08K3/30 ,  G01N1/36 ,  C08J5/24 ,  C08J5/04 ,  C08J5/18 ,  G01N33/44 ,  C08K3/013 ,  C08L35/02 ,  B29C70/70 ,  B29C41/30 ,  B29C70/30 ,  B29C70/68 ,  B29C70/86 ,  B29C70/02 ,  B29C37/00 ,  B29C41/20 ,  B29C70/54 ,  B29C70/60 ,  B29C41/00 ,  B29C70/88 ,  B29C41/32 ,  B29C41/22 ,  B29K31/00 ,  B29K67/00 ,  B29K105/06 ,  B29K105/16 ,  B29K267/00 ,  B29K231/00 ,  B29K105/20 ,  B29K309/00 ,  B29K303/04 ,  B29K631/00 ,  B29K667/00 ,  B29K509/00 ,  B29K303/00 ,  G01N3/10

CPC classification number: C08K3/30 ,  C08J5/043 ,  C08J5/18 ,  C08J5/244 ,  C08J5/249 ,  G01N1/36 ,  G01N33/442 ,  B29C37/0025 ,  B29C41/00 ,  B29C41/003 ,  B29C41/20 ,  B29C41/22 ,  B29C41/30 ,  B29C41/32 ,  B29C70/02 ,  B29C70/30 ,  B29C70/305 ,  B29C70/545 ,  B29C70/60 ,  B29C70/68 ,  B29C70/682 ,  B29C70/70 ,  B29C70/86 ,  B29C70/865 ,  B29C70/88 ,  B29K2031/00 ,  B29K2067/00 ,  B29K2067/06 ,  B29K2105/06 ,  B29K2105/16 ,  B29K2105/20 ,  B29K2231/00 ,  B29K2267/00 ,  B29K2267/06 ,  B29K2303/00 ,  B29K2303/04 ,  B29K2309/00 ,  B29K2509/00 ,  B29K2631/00 ,  B29K2667/00 ,  B29K2667/06 ,  C08J2300/12 ,  C08J2335/02 ,  C08J2367/00 ,  C08K3/013 ,  C08K2003/3045 ,  C08L35/02 ,  G01N3/10 ,  G01N2001/364 ,  C08K3/30 ,  C08L35/02

Abstract: A composite core material and methods for making same are disclosed herein. The composite core material comprises mineral filler discontinuous portions disposed in a continuous encapsulating resin. Further, the method for forming a composite core material comprises the steps of forming a mixture comprising mineral filler, an encapsulating prepolymer, and a polymerization catalyst; disposing the mixture onto a moving belt; and polymerizing said encapsulating prepolymer to form a composite core material comprising mineral filler discontinuous portions disposed in a continuous encapsulating resin.