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美国(2)
IPC部
F(2)
IPC大类
F28(2)
IPC小类
F28F(2)
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F28F013/18(2)
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2023(2)
申请年
2022(2)
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Material layer for, e.g. aero-engine applications, comprises porous synthesized carbon-containing composite materials, bonding layer, and hydraulically smooth surface interfacial layer comprising synthesized carbon-containing composite material(s).
STOWELL M, LANNING B
Creating thermal interface involves providing a template having multiple pores, depositing metal seed layer on one surface of template, and forming multiple nanowires within pores of template to height approximately even with surface of template opposite metal seed layer for forming nanowire array.
JING L, LI P, GONG W, SHEN S
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