Rolls-Royce Trent 500
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Rolls-Royce Trent 500

Trent 500
Trent 500.JPG
A Trent 500 turbofan mounted on an Airbus A340-600 of Lufthansa.
Type Turbofan
United Kingdom
Manufacturer Rolls-Royce plc
First run May 1999
Airbus A340-500/-600
Produced 2001-2012
Trent 800
Trent 900

The Rolls-Royce Trent 500 is a high-bypass turbofan aircraft engine, developed from the Rolls-Royce RB211 and is a member of the Trent family of engines.

Design and development

In 1995, Airbus began considering an engine for two new long-range derivatives of its four-engined A340 aircraft, designated A340-500/-600. The existing -200 and -300 models were 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 General Electric to develop a suitable engine, but decided not to proceed when General Electric demanded an exclusivity deal on the A340. After a contest with Pratt & Whitney, Airbus announced on 15 June 1997 at the Paris Air Show that it had selected the Trent 500 to power the A340-500 and -600.[1]

The Trent 500 first ran in May 1999 and achieved certification in December 2000. It entered service on the A340-600 with Virgin Atlantic Airways in July 2002 and on the ultra-long range A340-500 with Emirates in December 2003.[a] 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.[2]

The Trent 500 powers the Airbus A340-500 and A340-600.[3] 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 556)

Trent 500 engines on the left wing of an Iberia A340-600
Four Trent 500 engines on a Virgin Atlantic A340-600

Data from [4][5][6]

General characteristics

  • Type: Three-shaft high bypass ratio turbofan engine
  • Length: 155 in (3.9 m)
  • Diameter: 97.4 in (2.47 m)
  • Dry weight: 10,660 lb (4,840 kg)

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

Notes
  1. ^ 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.[]
Citations
  1. ^ "Airbus A340-600". Flug Revue (in English and German). 21 March 2000. Archived from the original on 3 September 2009. Retrieved 2017. Concrete studies began in April 1996, when Airbus and General Electric signed an exclusive agreement to study engine requirements for a stretched A340. GE pulled out in February 1997, but Rolls-Royce came in with an offer for the Trent 500, and this engine was confirmed on a non-exclusive basis in June 1997.
  2. ^ "Airbus Orders & deliveries". Airbus. Archived from the original (Excel) on 14 July 2014. Retrieved 2014.
  3. ^ "Press Packs" (PDF). [Rolls-Royce]. February 2002. Archived from the original (PDF) on 23 October 2007. Retrieved 2008.
  4. ^ Gas Turbine Engines. Aviation Week & Space Technology 2009 Source Book. pg. 122.
  5. ^ "Trent 500" (PDF). Rolls-Royce plc. 2009. Archived from the original (PDF) on 31 May 2012. Retrieved 2017.
  6. ^ "Trent 500 infographic". Rolls-Royce plc. 2 October 2014. Archived from the original on 15 April 2016. Retrieved 2017.

External links


  This article uses material from the Wikipedia page available here. It is released under the Creative Commons Attribution-Share-Alike License 3.0.

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