레이돔 구조
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전자기적으로 투명하면서 기상 레이더를 보호하는 복합소재 기수 덮개.
Overview
The radome — a portmanteau of radar and dome — is the nose cone of the aircraft, a structure that must simultaneously satisfy two fundamentally conflicting engineering requirements. Structurally, it must be strong enough to protect the weather radar antenna and associated equipment from bird strikes, hail, and aerodynamic loads. Electrically, it must be essentially transparent to the microwave frequencies used by the weather radar (typically 9–10 GHz in the X-band), introducing minimal attenuation, reflection, or phase distortion that would degrade radar performance. Meeting both requirements at minimum weight and with long service life requires careful selection of materials, layup design, and manufacturing quality control.
How It Works
A well-designed radome achieves electromagnetic transparency by using materials with low dielectric constant and loss tangent at radar frequencies, and by controlling the wall thickness to create a half-wave wall — where the thickness is an integer multiple of half-wavelengths at the design frequency. At these thicknesses, reflections from the front and rear surfaces cancel, minimizing the reflected signal and maximizing transmission. The effect is frequency- and incidence-angle-dependent, so radome designers optimize for the typical scan angles used by the weather radar system.
The most common construction is a sandwich panel: two thin CFRP or fiberglass-reinforced epoxy face sheets bonded to a low-density honeycomb core of Nomex (aramid fiber) or fiberglass. The core provides structural stiffness with minimal weight and — critically — its air-filled cells contribute negligible dielectric effect. The face sheets are thin enough that their electrical contribution can be tuned by the wall-thickness optimization.
Key Components
- Outer face sheet: Thin woven fiberglass or quartz-fiber-reinforced epoxy layer providing aerodynamic surface and weather protection.
- Honeycomb core: Nomex or fiberglass hexagonal-cell core, typically 10–25 mm thick, providing structural depth and shear stiffness without electrical penalty.
- Inner face sheet: Matching face sheet completing the sandwich structure.
- Rain erosion coating: Polyurethane or neoprene coating on the nose tip and forward surfaces protecting against rain erosion at cruising speeds, where rain droplets at 500–600 mph impact have significant abrasive effect.
- Lightning diverter strips: Metallic or conductive-composite strips running fore-aft on the radome exterior, providing a path to ground for lightning strike energy while minimizing interference with radar.
- Attachment flanges and frames: Metal (typically aluminum) interface structure connecting the radome to the forward fuselage pressure bulkhead.
Aircraft Applications
All commercial jets use nose radomes housing weather radar. On narrowbodies like the Boeing 737 and Airbus A320, the radome diameter is approximately 0.6–0.9 m, limited by fuselage width. Widebody aircraft such as the Boeing 777 and 787 use radomes 1.0–1.3 m in diameter accommodating larger antenna arrays for longer-range weather detection. On the A380, the nose radome is one of the largest in commercial aviation. Military aircraft also use radomes — often with more sophisticated A-sandwich or B-sandwich constructions tailored to specific radar frequencies — but the underlying design methodology is shared with commercial practice.
Advantages and Limitations
Advantages: Modern sandwich radomes achieve 95%+ electromagnetic transmission efficiency while providing adequate bird-strike protection; light weight compared to metal nose cones; and can be removed quickly for radar maintenance (typically bolted or latched at the forward fuselage frame). Composite construction allows complex compound-curve nose shapes that minimize drag.
Limitations: Rain erosion is an ongoing challenge: the erosion-resistant coatings on the nose tip require periodic inspection and replacement, typically every 3,000–5,000 flight hours. Lightning strikes can delaminate or burn through the composite structure, requiring repair. The narrow-band nature of the half-wave wall optimization means radomes optimized for one radar frequency may not perform as well if the radar is changed. Moisture ingress into the honeycomb core can significantly degrade radar transmission and structural strength, requiring regular bond integrity checks.