Glossary Engine Technology

세라믹 기지 복합소재 (Ceramic Matrix Composite) (CMC: Ceramic Matrix Composite)

Definition

터빈 엔진의 고온부에 사용되는 고내열성 첨단 소재로, 높은 작동 온도와 경량화를 가능하게 한다.

What Is a Ceramic Matrix Composite?

A ceramic matrix composite (CMC) is an advanced engineering material consisting of ceramic fibers embedded within a ceramic matrix, most commonly silicon carbide fibers in a silicon carbide matrix (SiC/SiC). CMCs combine the heat resistance of ceramics with substantially improved toughness and damage tolerance, making them transformative for jet engine hot-section components that must withstand extreme temperatures while minimizing cooling air demands and structural weight.

How It Works

Conventional nickel superalloy turbine components require active cooling — bleed air from the compressor diverted through internal channels to keep metal temperatures below their melting point near 1,315°C (2,400°F). CMC components can withstand operating temperatures of 1,315–1,480°C (2,400–2,700°F) without equivalent cooling, meaning less compressor bleed air is wasted, more air enters the combustor for thrust, and overall engine efficiency rises.

CMC parts are also approximately one-third the density of nickel superalloys (2.7 g/cm³ vs. 8.2 g/cm³), directly reducing component weight and the centrifugal loads transmitted to surrounding structures. This weight reduction cascades through the engine design.

Performance Specifications

  • Operating temperature: up to 1,480°C (2,700°F) without thermal barrier coatings
  • Density: approximately 2.7 g/cm³ (vs. 8.2 g/cm³ for nickel superalloys)
  • Weight reduction: up to 33% vs. metallic equivalent parts
  • Cooling air reduction: GE9X uses CMC in 5 component types, reducing cooling air needs by approximately 20%
  • Fuel burn improvement contribution: approximately 5% of GE9X's overall 10% gain over GE90

Aircraft Examples

  • GE9X on the Boeing 777X — first production engine with CMC combustor liners, stage-1 high-pressure turbine shrouds, and nozzles, introduced 2020s
  • LEAP-1A/1B/1C on Airbus A320neo, Boeing 737 MAX, and COMAC C919 — CMC high-pressure turbine shrouds reduce cooling requirements
  • GE Passport on the Bombardier Global 7500 — CMC combustor

GE Aviation pioneered production CMC use in commercial engines, investing over 20 years and establishing dedicated manufacturing facilities in Asheville, North Carolina. CMC adoption is expected to expand to rotating turbine blades as manufacturing processes mature through the late 2020s.

Frequently Asked Questions

What is 세라믹 기지 복합소재 (Ceramic Matrix Composite) (CMC)?
터빈 엔진의 고온부에 사용되는 고내열성 첨단 소재로, 높은 작동 온도와 경량화를 가능하게 한다.
What does CMC stand for?
CMC stands for 세라믹 기지 복합소재 (Ceramic Matrix Composite) (CMC). 터빈 엔진의 고온부에 사용되는 고내열성 첨단 소재로, 높은 작동 온도와 경량화를 가능하게 한다.
Why is 세라믹 기지 복합소재 (Ceramic Matrix Composite) (CMC) important in aviation?
What Is a Ceramic Matrix Composite? A ceramic matrix composite (CMC) is an advanced engineering material consisting of ceramic fibers embedded within a ceramic matrix, most commonly silicon carbide fibers in a silicon carbide matrix (SiC/SiC).
What are examples of 세라믹 기지 복합소재 (Ceramic Matrix Composite) (CMC)?
Common examples of 세라믹 기지 복합소재 (Ceramic Matrix Composite) (CMC) include: GE9X combustor liners and HP turbine shrouds on Boeing 777X, CFM LEAP-1A HP turbine shrouds on Airbus A320neo, GE Passport combustor on Bombardier Global 7500.
How does 세라믹 기지 복합소재 (Ceramic Matrix Composite) (CMC) relate to other aviation concepts?
세라믹 기지 복합소재 (Ceramic Matrix Composite) (CMC) is closely related to 복합 재료 and 단결정 터빈 블레이드 (Single-Crystal Turbine Blade), among other key aviation concepts.

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