US2022339830A1PendingUtilityA1

Method for the preparation of composite material in sandwich form

Assignee: SAINT GOBAIN PERFORMANCE PLASTICS FRANCEPriority: Dec 18, 2018Filed: Jul 5, 2022Published: Oct 27, 2022
Est. expiryDec 18, 2038(~12.4 yrs left)· nominal 20-yr term from priority
B32B 2260/046B32B 2250/40B29C 70/086B29K 2309/08B32B 9/046B29C 70/541B32B 2260/021B32B 2307/732B32B 5/26B29K 2277/00B32B 17/066B29C 2045/1454B32B 2250/03B32B 5/026B32B 37/146B32B 7/12B32B 2262/12B32B 2262/0269B32B 5/18B29C 35/02B29C 45/0005B29D 24/005B29K 2069/00B32B 2262/062B29C 2043/182B29D 99/0021B32B 2262/101B32B 19/02B29C 45/0001B29C 35/16B32B 19/04B32B 2605/08B32B 5/245B32B 9/007B29C 45/14786B32B 2266/0214B32B 2262/0253B29C 2045/1477B29C 70/70B29K 2105/0872B32B 2262/103B29K 2307/04B32B 19/06B32B 2307/72B32B 2262/10B29K 2101/10B32B 3/12B32B 2605/18B29K 2071/00B29K 2079/085B29C 2045/1825B29K 2063/00B29C 70/681B32B 2307/714B32B 37/10B29C 70/48B32B 2266/0271B32B 37/16B29C 45/7207B29K 2101/12B29D 24/002B29K 2023/12B32B 2262/106B32B 2305/076B32B 37/02B29C 45/14508B29C 70/34B29C 70/68B32B 17/04B29K 2083/00B32B 2305/182B32B 5/12B32B 2305/024B29C 70/467B29C 70/18B32B 38/10B32B 2309/105B29L 2023/007B29L 2023/005
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Claims

Abstract

The object of the invention can be a method of manufacturing a product in the form of a sandwich comprising a core and outer layers. The outer layers may be composed of composite material comprising a fiber-reinforced polymeric matrix. The method uses an insert of heat-resistant material, for example silicone. The object of this invention can be to provide a method of manufacturing a sandwich that dissociates the choice of material of the core of the sandwich from the choice of the material of the outer layers.

Claims

exact text as granted — not AI-modified
What is claimed is: 
     
         1 . A method of manufacturing a sandwich-shaped composite material product wherein the sandwich-shaped composite material product comprises two outer layers and a core, the outer layers having a matrix of fiber-reinforced polymeric material, the polymeric material having a melting point below the melting point of the material constituting the fibers;
 wherein the method being is characterized in that it uses an insert consisting of material having a melting point higher than the melting point of the polymeric material, on which the outer layers are consolidated; and   wherein this insert is subsequently replaced by the core of the sandwich-shaped composite material product to form an assembly, the assembly then undergoing a consolidation treatment for bonding the outer layers to the core,   wherein the method is further characterized in that it comprises the following steps:   juxtaposition, in a mold, of a fabric or knit made of reinforcing material, the insert, and a second fabric or knit made of reinforcing material;   injection of a resin of polymeric material under pressure and temperature;   removal of the insert and insertion of the core of the sandwich;   consolidation curing to adhere the outer layers to the core of the sandwich;   cooling of the product thus obtained.   
     
     
         2 . The method according to  claim 1 , characterized in that the insert is made of silicone. 
     
     
         3 . The method according to  claim 1 , characterized in that the reinforcing material is chosen from glass, carbon and aramid fibers. 
     
     
         4 . The method according to  claim 1 , characterized in that the polymeric material is of the thermoplastic type chosen from polycarbonate (PC), polyetherimide (PEI), polypropylene (PP), poly(ethylene terephthalate) (PET), and polyether ether ketone (PEEK). 
     
     
         5 . The method according to  claim 1 , characterized in that the polymeric material is of the thermosetting type, chosen from epoxy, cyanate ester, phenolic resins and polyester. 
     
     
         6 . The method according to  claim 1 , characterized in that the core of the sandwich-shaped composite material product consists of cellular honeycomb material. 
     
     
         7 . The method according to  claim 1 , characterized in that the thickness of the core is at least about 2 mm and not greater than about 50 mm. 
     
     
         8 . The method according to  claim 1 , characterized in that the thickness of each of the outer layers is at least about 0.2 mm and not greater than about 5 mm.

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