This application claims the priority benefit of Taiwan application serial no. 108137535, filed on Oct. 17, 2019. The entirety of the above-mentioned patent application is hereby incorporated by reference herein and made a part of this specification.
The invention relates to stealth technology, and more particularly to a capacitive stealth composite structure.
The so-called stealth technology mainly uses two methods to reduce the radar cross section (RCS) reflected from the target to the radar. The first common method is to reflect an electromagnetic wave emitted by a radar to a direction in which signals may not be intercepted by a radar receiving station by changing the geometric shape. In the other method, a material having the property of absorbing electromagnetic waves is added to the outer casing of a fighter or a warship to achieve stealth by changing geometric shape.
However, the former requires changing the shape of the aircraft, which changes the aerodynamics and affects the speed of the aircraft; the latter produces conical edge scattering at the edge of the material and the intersection between the materials and reduces the absorption effect.
Due to the inherent impedance of the material itself having the property of absorbing electromagnetic waves not matching the inherent impedance of the air, the electromagnetic waves emitted by the radar are often reflected before entering the material for absorption, thus affecting stealth.
The invention provides a capacitive stealth composite structure having the properties of light weight, small thickness, and improved electromagnetic wave absorption pattern.
A capacitive stealth composite structure of the invention includes a plurality of structural layers stacked in a thickness direction, and the number of layers of the structural layers is 3 or more, wherein each of the structural layers consists of a plurality of electromagnetic wave absorbing patterns and a plurality of insulation patterns alternately arranged in a horizontal direction. The electromagnetic wave absorbing patterns in each of the structural layers are aligned with the insulation patterns of an adjacent structural layer, and the insulation patterns in each of the structural layers are aligned with the electromagnetic wave absorbing patterns of an adjacent structural layer.
In an embodiment of the invention, a material of the electromagnetic wave absorbing patterns is selected from at least one of carbon nanotubes, carbon black, ferrite, iron nitride, carbonyl iron, polycrystalline iron, magnetic powder with iron cobalt nickel, carbon fiber, silicon carbide, and activated carbon.
In an embodiment of the invention, the material of the electromagnetic wave absorbing patterns may further include a resin.
In an embodiment of the invention, a material of the insulation patterns includes a thermosetting resin such as an epoxy resin, a phenol resin, a melamine resin, a urea resin, a polyester resin, a urethane resin, or an acrylic resin; or a thermoplastic resin such as polyethylene, polypropylene, an ethylene-vinyl acetate copolymer, polyvinyl chloride, polyvinylidene chloride, polystyrene, acrylic, polyvinyl alcohol, or polyethylene terephthalate.
In an embodiment of the invention, a spacing between the electromagnetic wave absorbing patterns in the horizontal direction is between 3 cm and 10 cm.
In an embodiment of the invention, a thickness of each of the structural layers may be 3 mm or less.
In an embodiment of the invention, the capacitive stealth composite structure may further include a reinforcing material disposed in the electromagnetic wave absorbing patterns and the insulation patterns in each of the structural layers.
In an embodiment of the invention, the reinforcing material is made of, for example, glass fiber, carbon fiber, aromatic polyamide fiber, or the like, or adopts a natural material such as paper, wood, asbestos, or basalt fiber as fiber.
In an embodiment of the invention, a shielding band of the capacitive stealth composite structure is, for example, 8 GHz to 12 GHz.
In an embodiment of the invention, a shielding band of the capacitive stealth composite structure is variable with a spacing of the electromagnetic wave absorbing patterns.
Based on the above, in the invention, via electromagnetic wave absorbing patterns and insulation patterns alternately arranged in the thickness direction and the horizontal direction, the effect of improved the electromagnetic wave absorptivity is achieved.
In order to make the aforementioned features and advantages of the disclosure more comprehensible, embodiments accompanied with figures are described in detail below.
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification. The drawings illustrate embodiments of the invention and, together with the description, serve to explain the principles of the invention.
Some embodiments are provided hereinafter and described in detail with reference to figures. However, the embodiments provided are not intended to limit the scope of the invention. Moreover, the figures are only descriptive and are not drawn to scale. For ease of explanation, the same devices below are provided with the same reference numerals.
Referring to
In
A manufacturing method of a capacitive stealth composite structure is provided below, but the invention is not limited thereto.
Referring to
Next, in step 310, the above steps are repeated N times to obtain N+1 structural layers, wherein N is a positive integer.
Then, in step 320, the N+1 structural layers are stacked, and the electromagnetic wave absorbing patterns in each structural layer need to be aligned with the insulation patterns of an adjacent structural layer, and the insulation patterns in each structural layer also need to be aligned with the electromagnetic wave absorbing patterns of an adjacent structural layer.
Thereafter, in step 330, hot pressing is performed. The temperature range and time of the hot pressing may be adjusted according to the type of material contained in the structural layers, the thickness of the structural layers, or the area size of the structural layers.
In addition, if the structural layers do not contain a reinforcing material, other manufacture means may be adopted, such as coating the surface of a metal substrate (such as an aircraft casing) layer by layer to manufacture the capacitive stealth composite structure 100 as shown in
To verify the effects of the invention, experiments are provided below, but the invention is not limited to the experiments below.
<Electromagnetic Wave Absorption Analysis>
The analysis was performed using the Arch Method of the United States Naval Research Laboratory (NRL), as shown in
In
A capacitive stealth composite structure was manufactured according to the steps of
First, the electromagnetic wave absorbing material was stirred by a triaxial roller for 1 hour and vacuum pumped, and the mixed electromagnetic wave absorbing material and the insulating material were alternately coated on the glass fiber cloth in a horizontal direction by pouring, wherein the width of the electromagnetic wave absorbing patterns was about 3 cm to 10 cm and the spacing of the electromagnetic wave absorbing patterns was about 3 cm to 10 cm, and the width of the electromagnetic wave absorbing patterns was substantially equal to the spacing between the electromagnetic wave absorbing patterns.
The above steps were repeated to prepare three structural layers, and the three structural layers were alternately stacked and hot-pressed at 120° C. for 3 hours to obtain the capacitive stealth composite structure of Experimental example 1. Then, electromagnetic wave absorption analysis was performed, and the results are shown in
Similar to the preparation method of Experimental example 1, but the entire surface of the electromagnetic wave absorbing material was directly coated on the glass fiber cloth without an insulation pattern. Then, electromagnetic wave absorption analysis was performed, and the results are shown in
Similar to the preparation method of Comparative example 1, but structural layers were added to form a composite structure obtained by stacking and hot pressing four structural layers. Then, electromagnetic wave absorption analysis was performed, and the results are shown in
It may be seen from
Similar to the preparation method of Experimental example 1, but the spacing between the electromagnetic wave absorbing patterns was changed to 10 cm. Then, electromagnetic wave absorption analysis was performed, and the results are shown in
Similar to the preparation method of Experimental example 1, but the spacing between the electromagnetic wave absorbing patterns was changed to 3 cm. Then, electromagnetic wave absorption analysis was performed, and the results are shown in
As may be seen from
For example, if based on a reflection loss of −10 dB, the shielding band of Experimental example 1 was 8.49 GHz to 12.38 GHz, which is applicable to the electromagnetic wave shielding of radars, satellite communication, and speed guns. The shielding band of Experimental example 2 was 13.4 GHz to 15.3 GHz, which is applicable to the electromagnetic wave shielding of satellite communication and speed cameras. The shielding band of Experimental example 3 was 5.2 GHz to 9.25 GHz, which is applicable to the electromagnetic wave shielding of, for example, electronic toll collection (ETC), Wi-Fi, satellite communication, and the like.
Based on the above, the capacitive stealth composite structure of the invention is configured by interleaving electromagnetic absorbing patterns and insulation patterns of similar capacitance in both the thickness direction and the horizontal direction to reduce impedance mismatch, enhance destructive interference, control the position of maximum reflection loss, and increase the capacity of dissipation of electromagnetic waves in the electromagnetic wave absorbing material, so that the capacitive stealth composite structure may be applied to electromagnetic wave shielding at various frequencies, such as the X band range commonly used in the military. Moreover, by the addition of the reinforcing material, a composite structure having mechanical strength may be directly formed without the issue of peeling off.
Although the invention has been described with reference to the above embodiments, it will be apparent to one of ordinary skill in the art that modifications to the described embodiments may be made without departing from the spirit of the invention. Accordingly, the scope of the invention is defined by the attached claims not by the above detailed descriptions.
Number | Date | Country | Kind |
---|---|---|---|
108137535 | Oct 2019 | TW | national |