推力 (Thrust)
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Definition
飞机发动机产生的前进力,以磅力(lbf)或千牛顿(kN)为单位测量,使飞行和爬升成为可能。
什么是推力?
Thrust is the reaction force generated by an aircraft engine that propels the aircraft forward. It is produced in accordance with Newton's Third Law: by accelerating a mass of air rearward, the engine creates an equal and opposite forward force on the aircraft. Thrust must overcome aerodynamic drag to maintain level flight, and exceed drag plus the component of weight along the flight path to climb.
工作原理
Different engine types generate thrust through different mechanisms:
- Turbofan: The fan accelerates a large bypass airstream rearward while the core expels hot exhaust. Combined reaction produces thrust. See Turbofan Engine.
- Turboprop: A propeller accelerates a very large mass of air at lower velocity — highly efficient at low airspeeds. See Turboprop Engine.
- Piston/propeller: Similar to turboprop but with a reciprocating piston engine.
- Rocket: Carries its own oxidizer — produces thrust in vacuum but used only for spacecraft.
Thrust is measured in pounds-force (lbf) in the United States and kilonewtons (kN) in most other countries. One lbf equals approximately 4.448 N.
性能参数
- Static vs. in-flight: Thrust decreases with airspeed as net momentum difference reduces; also falls with altitude as air density decreases.
- Thrust-to-weight ratio (TWR): Must exceed 1.0 for vertical takeoff. Commercial airliners typically achieve 0.25–0.35 TWR.
- Takeoff thrust (full rated): Boeing 737 MAX: ~56,000 lbf total (2 × 28,000); Boeing 777X: ~210,000 lbf total (2 × 105,000)
- Derated thrust: Airlines frequently use reduced thrust takeoffs (flex thrust) to extend engine life on cool, light, or short-runway days.
- Flat rated temperature: Most engines maintain full rated thrust up to ~30–35 °C (ISA+15); above this, thrust decreases with temperature.
飞机案例
- Airbus A380: 4 × GP7270 engines, 311,000 lbf total thrust at takeoff
- Boeing 777X: 2 × GE9X-105B1A, 210,000 lbf — most powerful twin-engine airliner
- Concorde (retired): 4 × Olympus 593, 152,200 lbf total with afterburner
- Embraer E175: 2 × CF34-8E5, 28,900 lbf total
After landing, Thrust Reversers redirect engine output forward to assist braking.
Related Terms
全权限数字发动机控制(FADEC)
对所有发动机参数拥有完全控制权的计算机系统,无机械备份,可优化性能并防止发动机损坏。
加力燃烧室
主要用于军用飞机的辅助燃烧系统,在涡轮下游喷入额外燃料以短时大幅提升推力。
反推装置
着陆后将发动机排气暂时转向前方以提供制动力的机械装置。
最小操纵速度
多发飞机在临界发动机失效、处于最大非对称推力状态下仍能保持方向操纵的最低空速。
涡扇发动机
使用大型风扇产生大部分推力的商用航空中最常见的喷气发动机类型。
涡桨发动机
通过减速齿轮箱驱动螺旋桨的喷气发动机,在低空和短途航线上效率很高。
耗油率(SFC)
发动机燃油效率的衡量标准:每小时每单位推力消耗的燃油质量,以lb/(lbf·h)或kg/(kN·h)表示。