公开(公告)号：US11603142B2

公开(公告)日：2023-03-14

申请号：US15319571

申请日：2015-06-15

Applicant: SABIC Global Technologies B.V.

Inventor： Craig Lawrence Milne ,  Gregory E. Tremblay ,  Dhanendra Kumar Nagwanshi ,  Somasekhar Bobba Venkat ,  Arunachala Parameshwara ,  Matthew D. Marks

IPC: B62D29/04 ,  B29C45/14 ,  B29C70/46 ,  B29C70/50 ,  B60R21/04 ,  B32B3/04 ,  B32B3/12 ,  B32B3/28 ,  B32B5/02 ,  B32B27/08 ,  B32B37/06 ,  B32B37/10 ,  B32B38/18 ,  B62D63/04

Abstract: In an embodiment, an energy-absorbing device can comprise: a polymer reinforcement structure, wherein the polymer reinforcement structure comprises a polymer matrix and chopped fibers; and a shell comprising 2 walls extending from a back and forming a shell channel, wherein the shell comprises continuous fibers and a resin matrix; wherein the polymer reinforcement structure is located in the shell channel.

公开(公告)号：US10995204B2

公开(公告)日：2021-05-04

申请号：US16318048

申请日：2017-07-18

Applicant: SABIC Global Technologies B.V.

Inventor： Michael M. Laurin ,  Craig Lawrence Milne ,  Rein Mollerus Faber ,  Manish Nandi ,  Christianus Johannes Jacobus Maas ,  Hochul Jung ,  Mohammad Moniruzzaman

IPC: C08L23/12 ,  B29C70/12 ,  C08J5/04 ,  C08K7/14

Abstract: A fiber-reinforced thermoplastic composition includes a polypropylene polymer component including a low flow grade polypropylene and a high flow grade polypropylene, and a fiber reinforcement component. The fiber-reinforced thermoplastic composition is capable of being vacuum formed. In another aspect a thermoplastic composition includes a homopolymer component including polypropylene, a co-polymer component, an impact modifier, and one or more of a flame retardant component and a fiber reinforcement component. The thermoplastic composition is capable of being vacuum formed. The fiber-reinforced thermoplastic composition may be formed into an article such as an enclosure for an electrical component, and it may be chemically resistant to a medical grade cleaner.

公开(公告)号：US20200207004A1

公开(公告)日：2020-07-02

申请号：US16317931

申请日：2017-07-18

Applicant: SABIC Global Technologies B.V.

Inventor： Michael M. Laurin ,  Craig Lawrence Milne ,  Rein Mollerus Faber ,  Manish Nandi ,  Christianus Johannes Jacobus Maas

IPC: B29C51/00 ,  B29C51/10 ,  B29C51/42

Abstract: A method of making an article includes: heating a plaque formed from a thermoplastic composition; and vacuum forming the heated plaque to form the article. The thermoplastic composition includes a polypropylene polymer component and a fiber reinforcement component. The heating is implemented using one or more heaters having a maximum temperature output of between 1500-3000° C. and maximum intensity between 0.80 μm and 2 μm. The article may include a surgical tray having a bottom surface having side walls disposed around a periphery thereof and extending from the bottom surface.

公开(公告)号：US10427329B2

公开(公告)日：2019-10-01

申请号：US15306112

申请日：2015-06-26

Applicant: SABIC Global Technologies B.V.

Inventor： Craig Lawrence Milne

IPC: B29C33/06 ,  B29C45/73 ,  B29C35/08 ,  B29K69/00 ,  B29K105/16

Abstract: A mold apparatus comprising: a core portion comprising a core surface, a first induction coil, and an inner core, and wherein the core portion has a core portion mass; a cavity portion comprising a second induction coil and a cavity surface, and wherein the cavity portion has a cavity portion mass; wherein the inner core comprises a non-magnetic material, the core surface comprises a magnetic material, and a density of the non-magnetic material is less than a density of the magnetic material; and wherein the core portion mass and the cavity portion mass differ by less than or equal to than 5%.

公开(公告)号：US20190292334A1

公开(公告)日：2019-09-26

申请号：US16318016

申请日：2017-07-18

Applicant: SABIC Global Technologies B.V.

Inventor： Michael M. Laurin ,  Craig Lawrence Milne ,  Rein Mollerus Faber ,  Manish Nandi ,  Christianus Johannes Jacobus Maas

IPC: C08J5/04 ,  A61B50/33

Abstract: A surgical article formed from a fiber-reinforced thermoplastic composition includes a polypropylene polymer component and a fiber reinforcement component. The surgical article is formed using a vacuum forming process. The surgical article may include a surgical tray including a bottom surface having side walls disposed around a periphery thereof and extending from the bottom surface. The vacuum forming may include a heater profile configured to heat a surface area at a perimeter of a plaque such that a plaque thinning at the bottom surface is minimized and radius stretch through the side walls is minimized, thereby retaining maximum wall thickness.

公开(公告)号：US20170203551A1

公开(公告)日：2017-07-20

申请号：US15324436

申请日：2015-07-09

Applicant: SABIC Global Technologies B.V.

Inventor： Scott Michael Davis ,  Daniel Sowle ,  Craig Lawrence Milne ,  Christopher Wall ,  Emile Homsi

IPC: B32B27/12 ,  G06F1/16 ,  B32B7/02 ,  B29C45/14 ,  B32B1/02 ,  B32B5/02

CPC classification number: B32B27/12 ,  B29C45/14508 ,  B29K2069/00 ,  B29K2309/08 ,  B29K2713/00 ,  B29L2031/3481 ,  B32B1/02 ,  B32B5/024 ,  B32B7/02 ,  B32B27/08 ,  B32B27/20 ,  B32B27/281 ,  B32B27/286 ,  B32B27/288 ,  B32B27/32 ,  B32B27/34 ,  B32B27/36 ,  B32B27/365 ,  B32B2250/03 ,  B32B2250/24 ,  B32B2250/40 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/101 ,  B32B2262/106 ,  B32B2262/14 ,  B32B2307/302 ,  B32B2307/72 ,  B32B2307/732 ,  B32B2457/00 ,  G06F1/1633

Abstract: In an embodiment, an A-B-A structure, can comprise: a core layer comprising a first thermoplastic material having a first density (Y), wherein the core layer has a core thickness and wherein the core layer comprise at least one of (i) a through plane thermal conductivity of greater than equal to 0.1 W/m K, and (ii) a core layer density (X) that is X≧0.8Y; a first outer layer comprising a second thermoplastic material located on a first side of the core layer; and a second outer layer comprising the second thermoplastic material located on a second side of the core layer opposite the first side; wherein the core thickness is 30% to 75% of a total thickness of the A-B-A structure.

公开(公告)号：US20170095944A1

公开(公告)日：2017-04-06

申请号：US15306112

申请日：2015-06-26

Applicant: SABIC Global Technologies B.V.

Inventor： Craig Lawrence Milne

IPC: B29C33/06 ,  B29C45/73

CPC classification number: B29C33/06 ,  B29C45/73 ,  B29C2035/0811 ,  B29C2045/7368 ,  B29C2045/7393 ,  B29K2069/00 ,  B29K2105/16 ,  B29K2905/00 ,  B29K2909/02

Abstract: A mold apparatus comprising: a core portion comprising a core surface, a first induction coil, and an inner core, and wherein the core portion has a core portion mass; a cavity portion comprising a second induction coil and a cavity surface, and wherein the cavity portion has a cavity portion mass; wherein the inner core comprises a non-magnetic material, the core surface comprises a magnetic material, and a density of the non-magnetic material is less than a density of the magnetic material; and wherein the core portion mass and the cavity portion mass differ by less than or equal to than 5%.

公开(公告)号：US20160221298A1

公开(公告)日：2016-08-04

申请号：US14614043

申请日：2015-02-04

Applicant: SABIC Global Technologies B.V.

Inventor： Erich Otto Teutsch ,  Craig Lawrence Milne ,  Peter James Zuber

IPC: B32B5/08 ,  B32B5/10 ,  B32B5/12 ,  B29C51/08 ,  B29C35/02 ,  B29C35/16 ,  B29C43/20 ,  C08J5/04 ,  B32B5/26

CPC classification number: B32B5/08 ,  B29C35/02 ,  B29C35/16 ,  B29C43/203 ,  B29C48/21 ,  B29C48/2886 ,  B29C51/082 ,  B29C51/12 ,  B29C70/08 ,  B29K2105/08 ,  B29L2009/00 ,  B29L2031/3055 ,  B29L2031/3064 ,  B29L2031/3067 ,  B29L2031/3076 ,  B32B5/10 ,  B32B5/12 ,  B32B5/26 ,  B32B2250/02 ,  B32B2250/20 ,  B32B2262/02 ,  B32B2262/101 ,  B32B2305/026 ,  B32B2305/08 ,  B32B2605/003 ,  B32B2605/10 ,  B32B2605/12 ,  B32B2605/18 ,  C08J5/043 ,  D04H1/4209 ,  D04H1/4334 ,  D04H1/541 ,  D04H1/558 ,  D04H1/732 ,  D04H5/06

Abstract: A composition for the manufacture of a porous, compressible article, the composition comprising a combination of: a plurality of reinforcing fibers; a plurality of thermoplastic fibers; optionally a plurality of polymeric binder fibers; and continuous spaced carrier fibers; wherein the polymeric binder fibers have a melting point lower than the thermoplastic fibers; methods for forming the porous, compressible article; and articles containing the porous, compressible article. An article comprising a thermoformed composite is also disclosed, wherein the composite is not supported by a scrim layer and the composite exhibits improved conformation to fine mold details to which the scrim layer could not accurately conform.

Abstract translation: 一种用于制造多孔，可压缩制品的组合物，所述组合物包含以下组合：多个增强纤维; 多种热塑性纤维; 任选地多个聚合物粘合纤维; 和连续间隔的载体纤维; 其中所述聚合物粘合纤维的熔点低于所述热塑性纤维; 形成多孔，可压缩制品的方法; 和含有多孔，可压缩制品的制品。 还公开了一种包含热成型复合材料的制品，其中所述复合材料不被稀松布层支撑，并且所述复合材料显示出改进的构造，以使所述稀松布层不能精确地符合的细模具细节。

公开(公告)号：US20200247983A1

公开(公告)日：2020-08-06

申请号：US16318048

申请日：2017-07-18

Applicant: SABIC Global Technologies B.V.

Inventor： Michael M. Laurin ,  Craig Lawrence Milne ,  Rein Mollerus Faber ,  Manish Nandi ,  Christianus Johannes Jacobus Maas ,  Hochul Jung ,  Mohammad Moniruzzaman

IPC: C08L23/12 ,  C08J5/04 ,  B29C70/12

Abstract: A fiber-reinforced thermoplastic composition includes a polypropylene polymer component including a low flow grade polypropylene and a high flow grade polypropylene, and a fiber reinforcement component. The fiber-reinforced thermoplastic composition is capable of being vacuum formed. In another aspect a thermoplastic composition includes a homopolymer component including polypropylene, a co-polymer component, an impact modifier, and one or more of a flame retardant component and a fiber reinforcement component. The thermoplastic composition is capable of being vacuum formed. The fiber-reinforced thermoplastic composition may be formed into an article such as an enclosure for an electrical component, and it may be chemically resistant to a medical grade cleaner.

公开(公告)号：US10549512B2

公开(公告)日：2020-02-04

申请号：US15324436

申请日：2015-07-09

Applicant: SABIC Global Technologies B.V.

Inventor： Scott Michael Davis ,  Daniel Sowle ,  Craig Lawrence Milne ,  Christopher Wall ,  Emile Homsi

IPC: B32B27/12 ,  B29C45/14 ,  B32B1/02 ,  B32B5/02 ,  B32B7/02 ,  G06F1/16 ,  B29K69/00 ,  B29K309/08 ,  B29L31/34

Abstract: In an embodiment, an A-B-A structure, can comprise: a core layer comprising a first thermoplastic material having a first density (Y), wherein the core layer has a core thickness and wherein the core layer comprise at least one of (i) a through plane thermal conductivity of greater than equal to 0.1 W/m K, and (ii) a core layer density (X) that is X≥0.8Y; a first outer layer comprising a second thermoplastic material located on a first side of the core layer; and a second outer layer comprising the second thermoplastic material located on a second side of the core layer opposite the first side; wherein the core thickness is 30% to 75% of a total thickness of the A-B-A structure.