Rolls-Royce Trent 800

Last updated

Trent 800
Rolls Royce Triebwerk.jpg
Boeing 777 nacelle
Type Turbofan
National origin United Kingdom
Manufacturer Rolls-Royce plc
First runSeptember 1993 [1]
Major applications Boeing 777
Produced1993–2010
Developed from Trent 700
Developed into Trent 500
Trent 900
MT30

The Rolls-Royce Trent 800 is a high-bypass turbofan produced by Rolls-Royce plc, one of the engine options for the first-generation Boeing 777 variants, also known as 777 Classics. Launched in September 1991, [2] it first ran in September 1993, [1] was granted EASA certification on 27 January 1995, [3] and entered service in 1996. [4] It reached a 40% market share, [5] ahead of the competing PW4000 and GE90, and the last Trent 800-powered 777 was delivered in 2010. [6] The Trent 800 has the Trent family three shaft architecture, with a 280 cm (110 in) fan. [7] With a 6.4:1 bypass ratio and an overall pressure ratio reaching 40.7:1, it generates up to 413.4 kN (92,900 lbf) of thrust. [3]

Contents

Development

Rear view of a 777 nacelle with separate core and bypass flows 9V-SQI - c-n 28530 - 777-212ER - Singapore Airlines - Singapore - Changi (8392103750) (cropped).jpg
Rear view of a 777 nacelle with separate core and bypass flows

By 1990, as Boeing was studying the enlarged 767-X, Rolls-Royce was proposing its Trent engine with a larger 110 in (280 cm) fan driven by a new, bigger LP turbine, a modified IP compressor and no exhaust mixer. [7] It would attain 75,000 to 85,000 lbf (330 to 380 kN), to be certified in early 1995 for a mid-1995 introduction, with growth potential to 90,000–95,000 lbf (400–420 kN) with a new HP core. [7]

Certification was applied for on 2 April 1992. [3] By September 1992, its fan was to be tested in December and a full test was planned for September 1993. [1] Certification was granted by the EASA on 27 January 1995. [3] The first Boeing 777 with Trent 800 engines flew on 26 May 1995 and ETOPS approval was granted by the FAA on 10 October 1996. [8] The Trent 800 entered service on the Boeing 777 in 1996, [4] with Thai Airways on 31 March. By June 1998, the 33 aircraft fleet had a Trent 800 dispatch reliability over 99.96%. [9]

After being rebuffed by British Airways who selected the GE90 for their initial batch of Boeing 777s, Rolls-Royce launched the Trent 800 in September 1991 with a £250 million ($432.5 million) order from Thai Airways for their 15 Boeing 777s, with first deliveries for January 1996. [2] In 1995, the Trent 800 won a large order from Singapore Airlines, a traditional Pratt & Whitney customer. The Singapore order was followed by large orders from American Airlines and Delta Air Lines. British Airways announced in September 1998 that it was returning to Rolls-Royce for its second batch of 777s, and did so again in April 2007. [10] Other major operators of Trent 800-powered 777s include Air New Zealand and Kenya Airways. In 1996, Rolls-Royce had a 32% market share, above GE but behind PW. [10] By July 1999, Rolls had won 45% of all engine orders for the 777. [11] The Trent 800 later reached a 40% share of the engine market on the 777 variants for which it is available. [5] The last Trent 800-powered 777 was delivered in 2010. [6]

Rolls-Royce had unsuccessfully offered the Trent 8104 for the second-generation 777 (originally 777-X, eventually produced as the -300ER, -200LR, 777-200LRF or 777F). However Boeing selected GE Aviation as the exclusive engine supplier for the second-generation 777 with high-output derivatives of the General Electric GE90, and again for the third-generation Boeing 777X (-8, -9) which will be equipped by the General Electric GE9X. [9]

As of 2014, Rolls-Royce is offering an upgraded version of the engine, known as the Trent 800EP. It incorporates technology from Trent 1000 and Trent XWB engines including elliptical leading edges on intermediate- and high-pressure compressor blades. Rolls-Royce claims that it provides a 0.7% fuel-burn benefit. [12]

Design

The 280 cm (110 in) fan has 26 wide chord titanium fan blades. Rolls Royce Trent 892 (777-200ER) (6098401787).jpg
The 280 cm (110 in) fan has 26 wide chord titanium fan blades.

The Trent 800 is an axial flow, high bypass turbofan with three coaxial shafts. The fan is driven by a 5-stage axial LP turbine (3300 rpm), the 8-stage IP compressor (7000 rpm) and the 6-stage HP compressor (10611 rpm) are each powered by a single stage turbine. It has an annular combustor with 24 fuel nozzles and is controlled by an EEC. The engine has a 6.4:1 bypass ratio in cruise and an overall pressure ratio of 33.9 to 40.7:1 at sea level, for a 340.6–413.4 kN (76,600–92,900 lbf) take-off thrust. [3] The 280 cm (110 in) fan has 26 diffusion bonded, wide chord titanium fan blades. [10]

The Trent 800 is the lightest Boeing 777 engine, with a 8,000 lb (3.6 t) weight saving over the GE90 and 5,400–6,500 lb (2.4–2.9 t) over the PW4000. [5] The Trent 800 weighs 6.078 t (13,400 lb) dry, [3] while the GE90 is 17,400 lb (7.89 t), [13] and the PW4000 is 16,260 lb (7.38 t). [14]

Japanese KHI and Marubeni Corporation are risk and revenue sharing partners on the Trent 800. [4]

Incidents

On 17 January 2008, a British Airways Boeing 777-236ER, operating as BA038 from Beijing to London, crash-landed at Heathrow after both Trent 800 engines lost power during the aircraft's final approach. The subsequent investigation found that ice released from the fuel system had accumulated on the fuel-oil heat exchanger, leading to a restriction of fuel flow to the engines. [15] On 26 November 2008, Delta Air Lines Flight 18 from Shanghai to Atlanta, a Trent 895-powered Boeing 777, experienced an "uncommanded rollback" of one engine while in cruise at 39,000 ft (12,000 m). The National Transportation Safety Board (NTSB) concluded the cause of both incidents was the same - ice clogging the inlet side of the fuel-oil heat exchanger (FOHE) of the affected engines. [16]

These incidents, along with a similar incident in May 2009 involving an Airbus A330 with Rolls Royce Trent-700 engines, resulted in Airworthiness Directives mandating the replacement of the fuel-oil heat exchangers in similar Rolls Royce Trent series engines. [17] Rolls-Royce developed a modification to prevent the problem recurring that involved replacing a face plate that had many small protruding tubes with one that is flat. [18] [19]

Engines on display

Rolls-Royce Trent 800 at Imperial War Museum Duxford Trent 800 duxford.JPG
Rolls-Royce Trent 800 at Imperial War Museum Duxford

A Trent 800 is on display at the Rolls-Royce Heritage Trust Collection, Derby.

A Trent 800 is on display at the Imperial War Museum Duxford, in the first hall.

Variants

Specifications (Trent 800)

Data from EASA [3]

General characteristics

Components

Performance

See also

Related development

Comparable engines

Related lists

Related Research Articles

<span class="mw-page-title-main">Boeing 777</span> Wide-body, long-range, twin-engine jet airliner family

The Boeing 777, commonly referred to as the Triple Seven, is an American long-range wide-body airliner developed and manufactured by Boeing Commercial Airplanes. The 777 is the world's largest twinjet and the most-built wide-body airliner. The jetliner was designed to bridge the gap between Boeing's other wide body airplanes, the twin-engined 767 and quad-engined 747, and to replace aging DC-10 and L-1011 trijets. Developed in consultation with eight major airlines, the 777 program was launched in October 1990, with an order from United Airlines. The prototype aircraft rolled out in April 1994, and first flew in June of that year. The 777 entered service with the launch operator United Airlines in June 1995. Longer-range variants were launched in 2000, and first delivered in 2004.

<span class="mw-page-title-main">Turbofan</span> Airbreathing jet engine designed to provide thrust by driving a fan

A turbofan or fanjet is a type of airbreathing jet engine that is widely used in aircraft propulsion. The word "turbofan" is a combination of references to the preceding generation engine technology of the turbojet and the additional fan stage. It consists of a gas turbine engine which achieves mechanical energy from combustion, and a ducted fan that uses the mechanical energy from the gas turbine to force air rearwards. Thus, whereas all the air taken in by a turbojet passes through the combustion chamber and turbines, in a turbofan some of that air bypasses these components. A turbofan thus can be thought of as a turbojet being used to drive a ducted fan, with both of these contributing to the thrust.

<span class="mw-page-title-main">Rolls-Royce RB211</span> 1960s British turbofan aircraft engine

The Rolls-Royce RB211 is a British family of high-bypass turbofan engines made by Rolls-Royce. The engines are capable of generating 41,030 to 59,450 lbf of thrust. The RB211 engine was the first production three-spool engine and turned Rolls-Royce from a significant player in the aero-engine industry into a global leader.

<span class="mw-page-title-main">Pratt & Whitney JT9D</span> Turbofan aircraft engine first flown in 1968

The Pratt & Whitney JT9D engine was the first high bypass ratio jet engine to power a wide-body airliner. Its initial application was the Boeing 747-100, the original "Jumbo Jet". It was Pratt & Whitney's first high-bypass-ratio turbofan.

<span class="mw-page-title-main">Pratt & Whitney PW4000</span> High-bypass turbofan aircraft engine

The Pratt & Whitney PW4000 is a family of dual-spool, axial-flow, high-bypass turbofan aircraft engines produced by Pratt & Whitney as the successor to the JT9D. It was first run in April 1984, was FAA certified in July 1986, and was introduced in June 1987. With thrust ranging from 50,000 to 99,040 lbf, it is used on many wide-body aircraft.

<span class="mw-page-title-main">General Electric GE90</span> High-bypass turbofan aircraft engine

The General Electric GE90 is a family of high-bypass turbofan aircraft engines built by GE Aerospace for the Boeing 777, with thrust ratings from 81,000 to 115,000 pounds-force. It entered service with British Airways in November 1995. It is one of three engines for the 777-200 and -200ER, and the exclusive engine of the -200LR, -300ER, and 777F. It was the largest jet engine, until being surpassed in January 2020 by its successor, the 110,000 lbf (490 kN) GE9X, which has a larger fan diameter by 6 inches (15 cm). However, the GE90-115B, the most recent variant of the GE90, is rated for a higher thrust than the GE9X.

<span class="mw-page-title-main">Rolls-Royce Trent</span> Family of turbofan aircraft engines

The Rolls-Royce Trent is a family of high-bypass turbofans produced by Rolls-Royce. It continues the three spool architecture of the RB211 with a maximum thrust ranging from 61,900 to 97,000 lbf. Launched as the RB-211-524L in June 1988, the prototype first ran in August 1990. Its first variant is the Trent 700 introduced on the Airbus A330 in March 1995, then the Trent 800 for the Boeing 777 (1996), the Trent 500 for the A340 (2002), the Trent 900 for the A380 (2007), the Trent 1000 for the Boeing 787 (2011), the Trent XWB for the A350 (2015), and the Trent 7000 for the A330neo (2018). It also has marine and industrial variants such as the RR MT30.

<span class="mw-page-title-main">Pratt & Whitney PW2000</span> Series of high-bypass turbofan aero engines

The Pratt & Whitney PW2000, also known by the military designation F117 and initially referred to as the JT10D, is a series of high-bypass turbofan aircraft engines with a thrust range from 37,000 to 43,000 lbf. Built by Pratt & Whitney, they were designed for the Boeing 757. As a 757 powerplant, these engines compete with the Rolls-Royce RB211.

<span class="mw-page-title-main">Engine Alliance GP7000</span> Turbofan engine manufactured by Engine Alliance

The Engine Alliance GP7000 is a turbofan jet engine manufactured by Engine Alliance, a joint venture between General Electric and Pratt & Whitney. It is one of the powerplant options available for the Airbus A380, along with the Rolls-Royce Trent 900.

<span class="mw-page-title-main">Rolls-Royce BR700</span> Turbofan aircraft engine

The Rolls-Royce BR700 is a family of turbofan engines for regional jets and corporate jets. It is manufactured in Dahlewitz, Germany, by Rolls-Royce Deutschland: this was initially a joint venture of BMW and Rolls-Royce plc established in 1990 to develop this engine. The BR710 first ran in 1995. The United States military designation for the BR725 variant is F130.

<span class="mw-page-title-main">General Electric GEnx</span> Turbofan jet engine

The General Electric GEnx is an advanced dual rotor, axial flow, high-bypass turbofan jet engine in production by GE Aerospace for the Boeing 747-8 and 787. The GEnx succeeded the CF6 in GE's product line.

<span class="mw-page-title-main">General Electric CF6</span> Turbofan aircraft engine family

The General Electric CF6, US military designations F103 and F138, is a family of high-bypass turbofan engines produced by GE Aviation. Based on the TF39, the first high-power high-bypass jet engine, the CF6 powers a wide variety of civilian airliners. The basic engine core also powers the LM2500 and LM6000 marine and power generation turboshafts. It is gradually being replaced by the newer GEnx family.

<span class="mw-page-title-main">Rolls-Royce Trent 500</span> 1990s British turbofan aircraft engine

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, first ran in May 1999, first flew in June 2000, and achieved certification on 15 December 2000. It entered service in July 2002 and 524 engines were delivered on-wing until the A340 production ended in 2012.

<span class="mw-page-title-main">Rolls-Royce Trent 700</span> 1990s British turbofan aircraft engine

The Rolls-Royce Trent 700 is a high-bypass turbofan aircraft engine produced by Rolls-Royce plc to power the Airbus A330. Rolls-Royce was studying a RB211 development for the A330 at its launch in June 1987. It was first selected by Cathay Pacific in April 1989, first ran in summer 1992, was certified in January 1994 and was put into service on 24 March 1995. Keeping the characteristic three-shaft architecture of the RB211, it is the first variant of the Trent family. With its 97.4 in (247 cm) fan for a 5:1 bypass ratio, it produces 300.3–316.3 kN (67,500–71,100 lbf) of thrust and reaches an overall pressure ratio of 36:1. It competes with the General Electric CF6-80E1 and the PW4000 to power the A330.

<span class="mw-page-title-main">Rolls-Royce Trent 900</span> 2000s British turbofan aircraft engine

The Rolls-Royce Trent 900 is a high-bypass turbofan produced by Rolls-Royce plc to power the Airbus A380, competing with the Engine Alliance GP7000. Initially proposed for the Boeing 747-500/600X in July 1996, this first application was later abandoned but it was offered for the A3XX, launched as the A380 in December 2000. It first ran on 18 March 2003, made its maiden flight on 17 May 2004 on an A340 testbed, and was certified by the EASA on 29 October 2004. Producing up to 374 kN (84,000 lbf) of thrust, the Trent 900 has the three shaft architecture of the Rolls-Royce Trent family with a 2.95 m (116 in) fan. It has a 8.5–8.7:1 bypass ratio and a 37–39:1 overall pressure ratio.

<span class="mw-page-title-main">Rolls-Royce Trent 1000</span> British turbofan engine, developed from earlier Trent series engines

The Rolls-Royce Trent 1000 is a high-bypass turbofan engine produced by Rolls-Royce, one of the two engine options for the Boeing 787 Dreamliner, competing with the General Electric GEnx. It first ran on 14 February 2006 and first flew on 18 June 2007 before a joint EASA/FAA certification on 7 August 2007 and entered service on 26 October 2011. Corrosion-related fatigue cracking of intermediate pressure (IP) turbine blades was discovered in early 2016, grounding up to 44 aircraft and costing Rolls-Royce at least £1.3 billion.

<span class="mw-page-title-main">Progress D-18T</span> Soviet high-bypass turbofan

The Progress D-18T is a 51,500 lbf (229 kN) high-bypass turbofan that powers the Antonov An-124 Ruslan and An-225 large freighters.

<span class="mw-page-title-main">General Electric Passport</span> High bypass turbofan aircraft engine

The General Electric Passport is a turbofan developed by GE Aerospace for large business jets. It was selected in 2010 to power the Bombardier Global 7500 and 8000, first run on June 24, 2013, and first flown in 2015. It was certified in April 2016 and powered the Global 7500 first flight on November 4, 2016, before its 2018 introduction. It produces 14,000 to 20,000 lbf of thrust, a range previously covered by the General Electric CF34. A smaller scaled CFM LEAP, it is a twin-spool axial engine with a 5.6:1 bypass ratio and a 45:1 overall pressure ratio and is noted for its large one-piece 52 in (130 cm) fan 18-blade titanium blisk.

<span class="mw-page-title-main">Rolls-Royce Trent 7000</span> Jet engine

The Rolls-Royce Trent 7000 is a high-bypass turbofan engine produced by Rolls-Royce, an iteration of the Trent family powering exclusively the Airbus A330neo. Announced on 14 July 2014, it first ran on 27 November 2015. It made its first flight on 19 October 2017 aboard on the A330neo. It received its EASA type certification on 20 July 2018 as a Trent 1000 variant. It was first delivered on 26 November, and was cleared for ETOPS 330 by 20 December. Compared to the A330's Trent 700, the 68,000–72,000 lbf (300–320 kN) engine doubles the bypass ratio to 10:1 and halves emitted noise. Pressure ratio is increased to 50:1, and it has a 112 in (280 cm) fan and a bleed air system. Fuel consumption is improved by 11%.

<span class="mw-page-title-main">General Electric GE9X</span> High-thrust turbofan jet engine

The General Electric GE9X is a high-bypass turbofan developed by GE Aerospace exclusively for the Boeing 777X. It first ran on the ground in April 2016 and first flew on March 13, 2018; it powered the 777-9's maiden flight in early 2020. It received its Federal Aviation Administration (FAA) type certificate on September 25, 2020. Derived from the General Electric GE90 with a larger fan, advanced materials like ceramic matrix composites (CMCs), and higher bypass and compression ratios, it was designed to improve fuel efficiency by 10% compared to the GE90. It is rated at 110,000 lbf (490 kN) of thrust, which is 5,000 lbf less than the GE90 highest thrust variant, the GE90-115, rated at 115,000 lbf (510 kN).

References

Notes

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  6. 1 2 Broderick, Sean (29 September 2017). "Trent 800 Aftermarket To Waver Slightly Through 2021". MRO network.
  7. 1 2 3 "Rolls-Royce to Enlarge Trent Engine Fan For 767-X But Retain Much Commonality". Aviation Week. 16 April 1990. pp. 21–22.
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  9. 1 2 Norris, Guy (3 June 1998). "Rolls-Royce completes Trent 8104 design and waits for 777-X". Flightglobal. Archived from the original on 30 October 2019. Retrieved 30 October 2019.
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