JT9D
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Technical Specifications
- Thrust
- 244,0 kN (54 750 lbf)
- Bypass Ratio
- 5,0:1
- Fan Diameter
- 2,426 m
- Pressure Ratio
- 25,0:1
- SFC
- 0,3450 lb/lbf·h
- Dry Weight
- 4 030 kg
- Length
- 3,592 m
- First Run
- 1966
- In Service
- 1970
Descripción general
The Pratt & Whitney JT9D tiene la distinción de ser el primer motor turbofán de alto bypass del mundo en impulsar una aeronave comercial de fuselaje ancho. Desarrollado específicamente para el Boeing 747 a finales de los años 1960, hizo posible la era del Jumbo Jet al ofrecer la combinación de empuje y eficiencia de combustible necesaria para hacer comercialmente viable una aeronave de 400 pasajeros en rutas internacionales de largo recorrido. The JT9D's bypass ratio of 5:1 era radicalmente mayor que los turborreactores y los primeros turbofanes de bajo bypass que lo precedieron, produciendo niveles de consumo de combustible y ruido drásticamente menores.
The JT9D fue un programa técnicamente ambicioso y comercialmente arriesgado. Pratt & Whitney and Boeing efectivamente desarrollaron el 747 y el JT9D en paralelo, con cada programa dependiendo del éxito del otro. Los motores de producción inicial sufrieron graves problemas de fiabilidad — apagados de motor, sobretensiones por pérdida y consumo excesivo de combustible — que causaron interrupciones significativas to Pan Am y otros operadores iniciales del 747. Estos problemas se resolvieron metódicamente a lo largo de principios de los años 1970, and the JT9D acumuló un extenso historial de servicio en múltiples tipos de aeronaves.
Especificaciones técnicas
| Especificación | Valor |
|---|---|
| Empuje (máx.) | 244 kN / 54,750 lbf |
| Relación de derivación | 5.0:1 |
| Diámetro del fan | 2.426 m (95.5 in) |
| Relación de presión total | 25:1 |
| Peso en seco | 4,030 kg |
| Longitud | 3.592 m |
| SFC (crucero) | 0.3450 lb/(lbf·h) |
| Primera prueba | 1966 |
| En servicio | 1970 |
Variantes
- JT9D-3A: Launch variant for the Boeing 747-100 at 43,500 lbf. Suffered early reliability problems that were resolved through hardware and software modifications.
- JT9D-7: Improved variant with better reliability and fuel efficiency, rated at 45,500 lbf.
- JT9D-7R4: Significantly advanced variant introduced in the late 1970s, incorporating improved turbine cooling and new materials for higher thrust and better durability. Used on the 747SP, 747-200, and 747-300, as well as the Douglas DC-10 and Airbus A300.
- JT9D-59A/70A: Higher-thrust variants rated at 53,000–54,750 lbf for demanding high-temperature and high-altitude operations.
Aplicaciones en aeronaves
- Boeing 747-100 — aplicación de lanzamiento
- McDonnell Douglas DC-10
- Airbus A300-600R
Historia del desarrollo
The JT9D programme began in 1965 after Pan American World Airways and Boeing agreed to develop an aircraft of unprecedented size. Pratt & Whitney won the engine competition and committed to a programme that required engineering breakthroughs in nearly every engine discipline: fan aerodynamics, compressor design, turbine materials, and combustor technology. The first engine ran in 1966, and the 747 entered service with Pan Am on 22 January 1970 — the date commonly considered the birth of the widebody Jet Age. Early service was plagued by reliability problems serious enough that Boeing briefly worried about programme cancellation. By the mid-1970s these problems were resolved, and the JT9D became one of the most reliable engines of its generation. It was ultimately superseded by its direct descendant, the Pratt & Whitney PW4000, which entered service in 1987 with substantially improved efficiency and maintenance characteristics.