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Rolls-Royce Dart

From Wikipedia, the free encyclopedia
1940s British turboprop aircraft engine

Dart
Rolls-Royce Dart RDa. 3 Mk506
TypeTurboprop
ManufacturerRolls-Royce Limited
First run1946
Major applications
Number builtmore than 7,100

TheRolls-Royce RB.53 Dart is aturboprop engine designed and manufactured byRolls-Royce Limited. First run in 1946, it powered theVickers Viscount on its maiden flight in 1948. A flight on July 29 of that year, which carried 14 paying passengers betweenNortholt andParis–Le Bourget Airport in a Dart-powered Viscount, was the first regularly scheduled airline flight by a turbine-powered aircraft.[1] The Viscount was the first turboprop-powered aircraft to enter airline service -British European Airways (BEA) in 1953.

The Dart was still in production forty years later when the lastFokker F27 Friendships andHawker Siddeley HS 748s were produced in 1987.

Following the company's convention for naming gas turbine engines after rivers, this turboprop engine design was named after theRiver Dart.

History

[edit]

Designed in 1946 by a team led by Lionel Haworth, the Dart engine was derived using experience gained from the earlier more powerfulRolls-Royce Clyde turboprop. A two-stage centrifugal compressor was specified to achieve the desired overall pressure ratio. A 3 stage, shared load, axial turbine was used to drive both the load (via a reduction gearbox) and the compression system. A photo showing a cutaway section of typical Dart engine is given below.

Unlike the Clyde, the engine lacked a free power turbine. Consequently, under normal operating conditions, the power delivered to the propeller could not be modulated at a fixed prop speed.[2]

The Dart was initially rated at 890 shp and first flew in October 1947 mounted to the nose of a convertedAvro Lancaster.

Improvements in the design boosted power output to 1,400 shp in the RDa.3, which went into production for the Viscount in 1952. The RDa.6 increased power to 1,600 shp and the RDa.7 to 1,800 shp by incorporating various improvements including a larger diameter second impeller.

Later Darts were rated up to 3,245 shp and remained in production until 1987, with approximately 7,100 produced, flying some 170 million hours.[3]

The Dart was also produced under licence in India byHindustan Aeronautics Limited.[4]

Haworth and his team later went on to design and develop the larger and more powerfulRolls-Royce Tyne.[5]

Variants

[edit]

As well as the RB.53 designation each mark of Dart engine was allocated aMinistry of Supply (MoS) "RDa.n" number as well as Mk.numbers.

RDa.1
Initial prototype engines – 1,250 shp (930 kW) plus 300 lbf (1.3 kN) residual thrust[6]
RDa.2
Initial production engines
RDa.3
1,480 hp (1,100 kW) estimated power – 1,345 hp (1,003 kW) shaft power + 350 lbf (1.6 kN) residual thrust at 14,500 rpm
RDa.6
1,670 hp (1,250 kW) estimated power – 1,535 hp (1,145 kW) shaft power + 350 lbf (1.6 kN) residual thrust at 14,500 rpm
RDa.7
1,815 hp (1,353 kW) estimated power – 1,630 hp (1,220 kW) shaft power + 480 lbf (2.1 kN) residual thrust at 15,000 rpm
RDa.7/1
1,910 hp (1,420 kW) estimated power – 1,730 hp (1,290 kW) shaft power + 470 lbf (2.1 kN) residual thrust at 15,000 rpm
RDa.7/2
2,020 hp (1,510 kW) estimated power – 1,835 hp (1,368 kW) shaft power + 485 lbf (2.16 kN) residual thrust at 15,000 rpm
RDa.7 Mk 21
2,099 hp (1,565 kW) estimated power - used forBréguet 1050 Alizé
RDa.7/2 Mk.529
2,100 hp (1,600 kW) estimated power – 1,910 hp (1,420 kW) shaft power + 495 lbf (2.20 kN) residual thrust at 15,000 rpm
RDa.10
2,555 hp (1,905 kW) estimated power – 2,305 hp (1,719 kW) shaft power + 670 lbf (3.0 kN) residual thrust at 15,000 rpm
RDa.10/1
3,030 hp (2,260 kW) estimated power – 2,750 hp (2,050 kW) shaft power + 750 lbf (3.3 kN) residual thrust at 15,000 rpm
RDa.10/1
3,245 hp (2,420 kW) estimated power at 15,000 rpm, with Water/Methanol injection for theHawker-Siddeley HS.748MF Andover C Mk.1.
RDa.11
Mk.506
(RDa.3)
Mk.510
(RDa.6)
Mk.511
(RDa.6)
Mk.512
(RDa.6)
Mk.514
(RDa.6)
Mk.520
(RDa.7)
Mk.525
(RDa.7/1)
Mk.526
(RDa.7/2)
Mk.527
(RDa.7/2)
Mk.528
(RDa.7/2)
Mk.529
(RDa.7/2)
Mk.530
(RDa.7/2)
Mk.531
(RDa.7/2)
Mk.551
(RDa.7)
Mk.552
(RDa-7)
Mk.540
(RDa.10)
Mk.541
(RDa.11)
Mk.542
(RDa.10/1)

Applications

[edit]
A Rolls-Royce Dart mounted on aFokker F27 Friendship
Rolls-Royce Darts on aVickers Viscount

Largely associated with the very successfulVickers Viscount medium-rangeairliner, it powered a number of other European and Japanese designs of the 1950s and 60s and was also used to convert American-manufactured piston aircraft to turboprop power. The list includes:

Power output was around 1,500 hp (1,120 kW) in early versions, and close to twice that in later versions, such as those that powered theNAMC YS-11 airliner. Some versions of the engine were fitted with water methanol injection, which boosted power in hot and high altitude conditions.

Engines on display

[edit]
Rolls Royce Dart Engine on Display at the Pima Air and Space Museum in Tucson, Arizona

Specifications (Dart RDa.7)

[edit]
Rolls-Royce Dart Turboprop engine, cut-away display

Data fromJane's All The World's Aircraft 1965–66.[17]

General characteristics

  • Type: Turboprop
  • Length: 97.6 in (2,480 mm)
  • Diameter: 37.9 in (960 mm)
  • Dry weight: 1,207 lb (547 kg) (dry)

Components

  • Compressor: Two-stagecentrifugal compressor
  • Combustors: 7 straight-flow combustion chambers with ignitors in No 3 and 7 chambers
  • Turbine: 3-stage axial turbine
  • Fuel type: Kerosene
  • Oil system: Self contained, 25 pint (14 L) capacity oil tank

Performance

See also

[edit]

Comparable engines

Related lists

References

[edit]

Notes

[edit]
  1. ^Turner 1968, p. 9.
  2. ^"Fokker F27 Mk 500 Friendship, G-JEAH, 4 August 1995"(PDF). Archived fromthe original(PDF) on 4 February 2017.
  3. ^"World Encyclopedia of Aero Engines – 5th edition" byBill Gunston, Sutton Publishing, 2006, p.195
  4. ^Taylor 1982, p. 736.
  5. ^"World Encyclopedia of Aero Engines – 5th edition" byBill Gunston, Sutton Publishing, 2006, p.197
  6. ^"gear box | strut gear | oil tank | 1953 | 0371 | Flight Archive".www.flightglobal.com. Archived fromthe original on 19 May 2015.
  7. ^"Tails Through Time: The Turboprop B-17 Flying Fortress".www.tailsthroughtime.com. Archived fromthe original on 25 March 2016. Retrieved5 April 2016.
  8. ^Johnsen, Frederick."Airailimages.com". Kenneth G. Johnsen.
  9. ^Royal Air Force Museum Cosford – Rolls-Royce DartArchived 4 March 2016 at theWayback Machine www.rafmuseum.org.uk Retrieved: 31 July 2012
  10. ^"GATWICK AVIATION MUSEUM - AERO ENGINES".www.gatwick-aviation-museum.co.uk. Archived fromthe original on 14 February 2004.
  11. ^"Rolls-Royce Dart Mk. 520 Turboprop Engine, Cutaway | National Air and Space Museum".airandspace.si.edu. Archived fromthe original on 20 September 2015.
  12. ^"Rolls-Royce Dart 506".
  13. ^"Rolls Royce Dart". Archived fromthe original on 4 March 2016. Retrieved11 November 2015.
  14. ^"Aviation Heritage Museum | Bull Creek, Perth".
  15. ^"Engines List".City of Norwich Aviation Museum. Retrieved27 August 2023.
  16. ^"Engines List".City of Norwich Aviation Museum. Retrieved27 August 2023.
  17. ^Taylor 1965, pp. 485–6.

Bibliography

[edit]
  • Gunston, Bill.World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989.ISBN 1-85260-163-9
  • Taylor, John W. R.Jane's All The World's Aircraft 1965–66. London: Sampson Low, Marston & Company Ltd, 1965.
  • Taylor, John W. R.Jane's All The World's Aircraft 1982–83. London: Jane's Yearbooks, 1982.ISBN 0-7106-0748-2.
  • Turner, P. St. John.Handbook of the Vickers Viscount. London: Ian Allan, 1968.ISBN 978-0711000520.

External links

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