오픈 로터 엔진 (Open Rotor Engine) (None: Open Rotor Engine)
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Definition
제트 속도에서 터보프롭 수준의 효율을 내기 위해 덕트 없는 반전 회전 팬 블레이드를 사용하는 차세대 추진 개념.
What Is an Open Rotor Engine?
An open rotor engine — also called an unducted fan (UDF) or propfan — is a propulsion system that drives large, highly swept, counter-rotating blades exposed directly to the airstream without a surrounding nacelle duct. By eliminating the duct's weight and drag while retaining the aerodynamic benefits of counter-rotation, open rotor designs promise fuel efficiency approaching that of turboprops while achieving cruise speeds close to conventional turbofan-powered aircraft.
How It Works
An open rotor typically features two contra-rotating blade rows driven by a turbine core. The forward rotor accelerates a large mass of air; the rear rotor, spinning in the opposite direction, recovers the swirl energy left by the forward rotor and provides additional thrust. This energy-recovery mechanism allows extremely high propulsive efficiency — theoretically 20–30% better than equivalent high-bypass turbofans — because the effective bypass ratio is essentially unlimited by any duct diameter constraint.
The blades are highly swept and twisted, resembling scimitar-shaped propeller blades, to manage compressibility effects at cruise Mach numbers of 0.75–0.82. Advanced composite materials allow complex three-dimensional blade geometries that would be impractical in metal.
Performance Specifications
- Projected fuel savings: 20–30% vs. CFM56-class turbofans
- Target cruise speed: Mach 0.75–0.82
- Equivalent bypass ratio: effectively 30:1 or higher
- Noise challenge: interaction tone noise between fore and aft rotors remains a key certification hurdle
Aircraft Examples
- CFM RISE (Revolutionary Innovation for Sustainable Engines) — CFM International's open fan demonstrator, targeting 20% fuel burn reduction, ground testing began 2024 with flight tests planned for late 2020s
- GE36 UDF — demonstrator tested on Boeing 727 in 1986–1988, reached Mach 0.84 with 26–30% fuel savings vs. CF6
- Airbus CFM Open Fan — planned for narrowbody replacement aircraft in the 2030s
Despite promising 1980s demonstrations, open rotor engines stalled over noise and FOD (foreign object damage) concerns. Rising fuel prices and decarbonization pressure have revived serious industry investment, with CFM's RISE program representing the most credible path to entry into service around 2035.
Related Terms
연료 효율
승객 1인당 킬로미터당 소비되는 연료량으로, 항공기 운항 경제성과 환경 영향의 핵심 척도.
프롭팬 (Propfan)
후퇴각이 크고 고부하의 프로펠러 블레이드를 사용해 터보프롭의 연료 효율과 터보팬 수준의 속도를 결합한 하이브리드 추진 설계.
터보팬 엔진 (Turbofan Engine)
대형 팬을 사용하여 대부분의 추력을 생성하는, 상용 항공에서 가장 일반적인 제트 엔진 유형.
터보프롭 엔진 (Turboprop Engine)
감속 기어박스를 통해 프로펠러를 구동하는 제트 엔진으로, 저고도 및 단거리 노선에서 높은 효율을 제공한다.