Empuxo (Thrust)
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Definition
A força para frente produzida pelos motores de uma aeronave, medida em libras-força (lbf) ou quilonewtons (kN).
O que é empuxo?
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.
Como funciona
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.
Especificações de desempenho
- 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.
Exemplos de aeronaves
- 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
Consumo específico de combustível
Uma medida da eficiência do motor: a massa de combustível consumida por unidade de empuxo por hora.
Controle digital de motor com autoridade total (FADEC)
Um sistema computadorizado com autoridade completa sobre todos os parâmetros do motor, sem backups mecânicos.
Motor turboélice
Um motor a jato que aciona uma hélice via caixa de redução, oferecendo alta eficiência em baixas altitudes.
Motor turbofan
O tipo de motor a jato mais comum na aviação comercial, utilizando um grande fan para gerar a maior parte do empuxo.
Pós-combustão
Um sistema de combustão suplementar a jusante da turbina que injeta combustível extra para um aumento massivo e de curto prazo do empuxo, usado principalmente em aeronaves militares.
Reversor de empuxo
Um dispositivo mecânico que redireciona temporariamente o escapamento do motor para frente, fornecendo força de frenagem após o pouso.
Velocidade Mínima de Controle
A velocidade aerodinâmica mínima na qual uma aeronave multimotora pode manter o controle direcional após a falha de um motor crítico com empuxo assimétrico máximo.