Patent classifications
C01B2202/24
Carbon nanotube-based thermal interface materials and methods of making and using thereof
Multilayered or multitiered structures formed by stacking of vertically aligned carbon nanotube (CNT) arrays and methods of making and using thereof are described herein. Such multilayered or multitiered structures can be used as thermal interface materials (TIMs).
CARBON NANOTUBE-BASED THERMAL INTERFACE MATERIALS AND METHODS OF MAKING AND USING THEREOF
Single-layer CNT composites and multilayered or multitiered structures formed therefrom, by stacking of vertically aligned carbon nanotube (CNT) arrays, and methods of making and using thereof are described herein. Such multilayered or multitiered structures can be used as thermal interface materials (TIMs) for a variety of applications, such as burn-in testing.
Carbon nanotube compositions
Metal-carbon nanotube composites having nanotubes which are uniformly dispersed within the metal matrix of the composite, and which are unbundled or substantially unbundled, have high lengths, and which can be controllably aligned are disclosed herein. Such metal-carbon nanotube composites can show improved electrical, thermal, and mechanical properties, as compared to a pristine metal or metal alloy which does not contain nanotubes dispersed therein. Facile and scalable methods of fabricating such metal-nanocarbon composites are also disclosed.
Arrangement of carbon nanotubes and a method for manufacturing the arrangement
An arrangement of carbon nanotubes (CNTs) is disclosed. The arrangement includes: a substrate (100); a first CNT block (110) rising up from the substrate (100); a second CNT block (120) rising up from the substrate (100), the first CNT block (110) and the second CNT block (120) being spaced apart from each other; and a CNT link (130) connecting the first CNT block (110) to the second CNT block (120). The CNTs of the CNT link (130) are aligned in a same direction as the CNTs of the first CNT block (110) and the second CNT block (120), and the CNT link (130) is configured as a CNT bridge.
Electrically and thermally conductive polymer concrete
An electrically and thermally conductive polymer concrete (made of a polymer and aggregate particles without cement) comprising non-functionalized nanoparticles (e.g. non-functionalized multi-walled carbon nanotubes (NF-MWCNTs), non-functionalized carbon nanofibers, non-functionalized nanoalumina) dispersed therein and methods of making same.
Manufacturing method of carbon nanotube composite for heat dissipation and LED light therewith
The present invention relates to a method for preparing a carbon nanotube-based heat-dissipating material and an LED lighting device. The LED lighting device comprises second LED substrates and a heat-dissipating frame. The heat-dissipating frame comprises: a frame body formed in a polygonal column shape being open at its upper and lower ends, in which substrate contact surfaces, with which the second LED substrates respectively come into contact, are formed on outer sides of the frame body; and auxiliary heat sinks made of a carbon nanotube-based heat-dissipating material and attachably and detachably provided on inner sides corresponding to the substrate contact surfaces of the frame body.
Polymeric blend composite and a process for preparing the same
The present disclosure relates to a polymeric blend composite comprising Poly Ether Ketone/Poly-(2,5-Benzimidazole) containing pre-treated multi walled carbon nanotubes (MWCNTs) between 0.5 to 5 wt % were melt processed on a twin-screw extruder and granules so obtained were injection molded to determine heat deflection temperature (HDT) of these composites and storage modulus using DMA. It was found that HDT and storage Modulus for so produced reinforced blends were unexpectedly extremely high as compared to PEK/ABPBI blends without MWCNTs.
Carbon nanotube (CNT) or carbon allotrobe based induction heating for aircraft ice protection
A system for inductive heating of an aircraft surface includes a conductive outer layer configured to be located on an outer portion of the aircraft surface. The system further includes a carbon nanotube (CNT) yarn configured to receive and conduct electrical current. The system further includes an insulator located between the conductive outer layer and the CNT yarn such that the electrical current flowing through the CNT yarn generates induction heating on the conductive outer layer.
Carbon nanotube-based thermal interface materials and methods of making and using thereof
Single-layer CNT composites and multilayered or multitiered structures formed therefrom, by stacking of vertically aligned carbon nanotube (CNT) arrays, and methods of making and using thereof are described herein. Such multilayered or multitiered structures can be used as thermal interface materials (TIMs) for a variety of applications, such as burn-in testing.
Method for making carbon nanotube array
A method for making carbon nanotube array includes depositing a catalyst layer on a substrate surface of a growth substrate, to form a composite structure. The composite structure is placed in a chamber. The carbon source gas and protective gas are supplied to the chamber, and the composite structure is heated to a first temperature, to grow a carbon nanotube array on the substrate surface. Then the carbon nanotube is oxidized.