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Rolls-Royce Trent 500

Trent 500
A Trent 500 turbofan mounted on an Airbus A340-600 of Lufthansa.
Type Turbofan
National origin United Kingdom
Manufacturer Rolls-Royce
First run May 1999
Major applications A340-500/600
Produced 2001–2012
Developed from Trent 700 fan, Trent 800 core
Developed into Trent 900

The Rolls-Royce Trent 500 is a high-bypass turbofan produced by Rolls-Royce to power the larger A340-500/600 variants. It was selected in June 1997,[1] first ran in May 1999,[2] first flew in June 2000, and achieved certification on 15 December 2000.[3] It entered service in July 2002 and 524 engines were delivered on-wing until the A340 production ended in 2012.

Keeping the three spool architecture of the Trent family, it has the Trent 700's 2.47 m (97.5 in) fan and a Trent 800 core scaled down.[4] It produces up to 275 kN (62,000 lbf) of thrust at take-off and has a bypass ratio up to 8.5:1 in cruise.[5]

Development

In 1995, Airbus began considering an engine for two new long-range derivatives of its four-engined A340, the A340-500/600. The existing A340-200/300 was powered by CFM International CFM56 engines. However, the CFM56 was at the limit of its development capability, and would be unable to power the new A340-500/-600. In April 1996, Airbus signed an agreement with GE Aviation to develop a suitable engine, but decided not to proceed when GE demanded an exclusivity deal on the A340.[6][1]

Certification was applied for on 9 February 1998,[5] and first ran in May 1999.[2] By July 1999, Rolls-Royce had secured $5 billion worth of Trent 500 orders.[7] Flight testing began in late June 2000 on a modified A340 testbed. By July 2000, the test program had amassed 1,750h and 2,00 cycles, and aimed for 15,000h and 4,000-5,000 cycles before introduction.[4] It achieved certification on 15 December 2000.[5]

The Trent 500 entered service on the A340-600 with Virgin Atlantic in July 2002 and on the ultra-long range A340-500 with Emirates in December 2003. Air Canada had been expected to be the launch customer for the A340-500 in May 2003, but just before this on 1 April 2003 the airline filed for bankruptcy protection which resulted in delivery of its two A340-500s being delayed. This allowed Emirates to be the first airline to operate the type.[citation needed] After production of the Airbus A340 ended in 2011, a total of 131 A340-500/-600 have been delivered with 524 Trent 500 engines altogether; Lufthansa is the largest operator, with 24 delivered A340-600.[8]

Design

The Trent 500 is a high bypass turbofan with three spools: the fan is powered by a 5 stage Low Pressure turbine (nominal speed: 3,900 RPM), the Intermediate pressure spool has an 8-stage axial compressor (9,100 RPM) and the High Pressure spool has an 6-stage axial compressor (13,300 RPM), both driven by a single turbine stage. It has an annular combustor and is equipped with an Electronic Engine Control System.[5]

It is flat rated at ISA + 15°C for 248.1–275.3 kN (55,800–61,900 lbf) net thrust at take-off and has an 8.5:1 bypass ratio in cruise.[5]

The Trent 500 is essentially a scaled Trent 800, with a 2.47 m (97 in) fan with 26 unswept blades like the Trent 700. The IP and HP compressors and scaled-down by 20% from the Trent 892, while the turbines are scaled-down by 90% and are made of single crystal CMSX-4 alloy with thermal barrier coatings. Fuel burn is 1% lower because of 3D aerodynamics. It was tested up to 68,000 lbf (300 kN) to establish limits.[4]

The Trent 500 powers the A340-500/600.[9] It was certificated at 60,000 lbf (270 kN) thrust, but derated to 53,000 lbf (240 kN) as the Trent 553 to power the A340-500, and to 56,000 lbf (250 kN) as the Trent 556 for the A340-600 and A340-500HGW. However, a 60,000 lbf (270 kN) version is installed in the A340-600HGW (High Gross Weight), a higher-performance version of the A340-600. The Trent 500 has the same wide chord fan as the Trent 700, together with a core scaled from the Trent 800.

Applications

Specifications

Trent 500 engines on the left wing of an Iberia A340-600

Data from EASA[5]

General characteristics

  • Type: Three-shaft high bypass turbofan
  • Length: 468.9 cm (184.6 in)
  • Diameter: 247 cm (97 in)[10]
  • Dry weight: 4,990 kg (11,000 lb)

Components

  • Compressor: Single-stage fan, eight-stage intermediate pressure compressor, six-stage high pressure compressor
  • Combustors: Tiled annular with 20 fuel injectors
  • Turbine: Single-stage high pressure turbine, single-stage intermediate pressure turbine, five-stage low pressure turbine

Performance

See also

Related development

Comparable engines

Related lists

References

  1. ^ a b "Airbus A340-600". Flug Revue (in English and German). 21 March 2000. Archived from the original on 3 September 2009.
  2. ^ a b G E Kirk (19 August 2003). "The Design of The Rolls-Royce Trent 500 Aero Engine". International Conference on Engineering Design. Archived from the original on 3 November 2019. Retrieved 8 January 2025.
  3. ^ Cite error: The named reference TCDS/ was invoked but never defined (see the help page).
  4. ^ a b c "Trent 500 Shapes Up". Flight International. 25 July 2000. Archived from the original on 6 March 2016. Retrieved 11 December 2013.
  5. ^ a b c d e f g "Type-Certificate Data Sheet E.060 for RB211 Trent 500 Series Engines" (PDF). EASA. 21 February 2019.
  6. ^ "Airbus Shoots for 25". Aviation Week & Space Technology. 21 July 1997. Archived from the original on 6 January 2016. Retrieved 8 January 2025.
  7. ^ Michael Harrison (8 July 1999). "Blow to Rolls as Boeing picks US rival". The Independent. Archived from the original on 30 October 2019. Retrieved 8 January 2025.
  8. ^ "Airbus Orders & deliveries". Airbus. Archived from the original (Excel) on 14 July 2014. Retrieved 12 July 2014.
  9. ^ "Civil Aerospace" (PDF) (Press release). Rolls-Royce. February 2002. Archived from the original (PDF) on 23 October 2007. Retrieved 5 December 2008.
  10. ^ a b c "Trent 500" (PDF). Rolls-Royce plc. 2009. Archived from the original (PDF) on 31 May 2012.
  11. ^ "Trent 500 infographic". Rolls-Royce plc. 2014. Archived from the original on 5 February 2016.
  12. ^ "Gas Turbine Engines" (PDF). Aviation Week & Space Technology. 28 January 2008. pp. 137–138. Archived from the original (PDF) on 6 November 2018.
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