Electromagnetic wave absorption material and electromagnetic wave absorber
US-2018370197-A1 · Dec 27, 2018 · US
US12474469B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12474469-B2 |
| Application number | US-202118010966-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 30, 2021 |
| Priority date | Jun 19, 2020 |
| Publication date | Nov 18, 2025 |
| Grant date | Nov 18, 2025 |
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A radar-absorbing structure is disclosed which includes a fiber, at least one binding agent disposed on the fiber and thus enabling the fiber to bind to another fiber.
Opening claim text (preview).
The invention claimed is: 1 . A radar absorbing structure ( 1 ) comprising: a plurality of fibers ( 2 ), each of the plurality of fibers ( 2 ) being a glass fiber reinforced fibers or a carbon fiber reinforced fiber, at least one binding agent ( 3 ) disposed on each of the plurality of fibers ( 2 ), enabling each of the plurality of fibers ( 2 ) to bind to another of the plurality of fibers ( 2 ), at least one barrier coating ( 4 ) disposed so as to cover the surface of each of the plurality of fibers ( 2 ), wherein at least one rod ( 5 ) which is graphene and/or graphene-based nanoribbons is disposed on the barrier coating ( 4 ) and at least one particle ( 6 ) is disposed on the binding agent ( 3 ), so that the at least one rod ( 5 ) is adhered to the associated fiber ( 2 ), and enabling the at least one rod ( 5 ) on each associated fiber ( 2 ) to absorb radar, at least one layer ( 7 ) composed of the plurality of fibers ( 2 ) and a binding agent ( 3 ), and at least one part ( 8 ) composed of the at least one layer ( 7 ), and wherein the at least one part ( 8 ) forms at least a part of an aircraft body ( 9 ). 2 . The radar absorbing structure ( 1 ) according to claim 1 , wherein the at least one rod ( 5 ) is disposed on the barrier coating ( 4 ) in a predetermined direction. 3 . The radar absorbing structure ( 1 ) according to claim 1 , wherein one of the as least one layer ( 7 ) is produced from glass fiber reinforced fibers ( 2 ). 4 . The radar absorbing structure ( 1 ) according to claim 1 , wherein one of the at least one layer ( 7 ) is produced from carbon fiber reinforced fibers. 5 . The radar absorbing structure ( 1 ) according to claim 1 , wherein the plurality of fibers ( 2 ) are disposed in the incident direction of radio waves (W) arriving at the least one part ( 8 ). 6 . The radar absorbing structure ( 1 ) as claimed in claim 1 , wherein the at least one layer ( 7 ) comprises at least two layers ( 7 ), wherein one of the at least two layers ( 7 ) is produced from glass fiber reinforced fibers ( 2 ) and another of the at least two layers ( 7 ) is produced from carbon fiber reinforced fibers ( 2 ), wherein the layer ( 7 ) produced from glass fiber reinforced fibers ( 2 ) being disposed closer to an outer surface of the aircraft body ( 9 ) than the layer ( 7 ) produced from carbon fiber reinforced fibers ( 2 ). 7 . The radar absorbing structure ( 1 ) according to claim 1 , wherein each of the plurality of rods ( 5 ) gradually increase in density and/or length from an outer surface of the aircraft body ( 9 ) towards an interior of the aircraft body ( 9 ). 8 . The radar absorbing structure ( 1 ) according to claim 1 , wherein each of the plurality of rods ( 5 ) is coated on the barrier coating ( 4 ) by chemical vapor deposition (CVD) and/or spray coating method. 9 . The radar absorbing structure ( 1 ) according to claim 1 , comprising transition metal particles ( 601 ) from transition metals. 10 . The radar absorbing structure ( 1 ) according to claim 9 , comprising iron-based particles ( 602 ) which are iron-based nanoparticles. 11 . A part ( 8 ) for use in air and/or space and/or marine vehicles formed from the radar absorbing structure ( 1 ) of claim 1 .
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