Rolls-Royce Dart Explained
The Rolls-Royce RB.53 Dart is a turboprop engine designed and manufactured by Rolls-Royce Limited. First run in 1946, it powered the Vickers Viscount on its maiden flight in 1948. A flight on July 29 of that year, which carried 14 paying passengers between Northolt and Paris–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 last Fokker F27 Friendships and Hawker 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 the River Dart.
History
Designed in 1946 by a team led by Lionel Haworth, the Dart engine was derived using experience gained from the earlier more powerful Rolls-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 converted Avro 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 by Hindustan Aeronautics Limited.[4]
Haworth and his team later went on to design and develop the larger and more powerful Rolls-Royce Tyne.[5]
Variants
As well as the RB.53 designation each mark of Dart engine was allocated a Ministry of Supply (MoS) "RDa.n" number as well as Mk.numbers.
- RDa.1: Initial prototype engines – 1,250 shp plus 300lb residual thrust[6]
RDa.2: Initial production engines
RDa.3: 1480abbr=onNaNabbr=on estimated power – 1345abbr=onNaNabbr=on shaft power + 350abbr=onNaNabbr=on residual thrust at 14,500 rpm
RDa.6: 1670abbr=onNaNabbr=on estimated power – 1535abbr=onNaNabbr=on shaft power + 350abbr=onNaNabbr=on residual thrust at 14,500 rpm
RDa.7: 1815abbr=onNaNabbr=on estimated power – 1630abbr=onNaNabbr=on shaft power + 480abbr=onNaNabbr=on residual thrust at 15,000 rpm
RDa.7/1: 1910abbr=onNaNabbr=on estimated power – 1730abbr=onNaNabbr=on shaft power + 470abbr=onNaNabbr=on residual thrust at 15,000 rpm
RDa.7/2: 2020abbr=onNaNabbr=on estimated power – 1835abbr=onNaNabbr=on shaft power + 485abbr=onNaNabbr=on residual thrust at 15,000 rpm
RDa.7 Mk 21: 2099abbr=onNaNabbr=on estimated power - used for Bréguet 1050 Alizé
RDa.7/2 Mk.529: 2100abbr=onNaNabbr=on estimated power – 1910abbr=onNaNabbr=on shaft power + 495abbr=onNaNabbr=on residual thrust at 15,000 rpm
RDa.10: 2555abbr=onNaNabbr=on estimated power – 2305abbr=onNaNabbr=on shaft power + 670abbr=onNaNabbr=on residual thrust at 15,000 rpm
RDa.10/1: 3030abbr=onNaNabbr=on estimated power – 2750abbr=onNaNabbr=on shaft power + 750.4abbr=onNaNabbr=on residual thrust at 15,000 rpm
RDa.10/1: 3245abbr=onNaNabbr=on estimated power at 15,000 rpm, with Water/Methanol injection for the Hawker-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
Largely associated with the very successful Vickers Viscount medium-range airliner, 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 the NAMC 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
References
Bibliography
- Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989.
- 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. .
- Turner, P. St. John. Handbook of the Vickers Viscount. London: Ian Allan, 1968. .
External links
Notes and References
- Turner 1968, p. 9.
- https://assets.publishing.service.gov.uk/media/5422ef5f40f0b6134200023b/dft_avsafety_pdf_500083.pdf
- "World Encyclopedia of Aero Engines – 5th edition" by Bill Gunston, Sutton Publishing, 2006, p.195
- Taylor 1982, p. 736.
- "World Encyclopedia of Aero Engines – 5th edition" by Bill Gunston, Sutton Publishing, 2006, p.197
- Web site: gear box strut gear oil tank 1953 0371 Flight Archive . www.flightglobal.com . dead . https://web.archive.org/web/20150519040405/http://www.flightglobal.com/pdfarchive/view/1953/1953%20-%200371.html . 2015-05-19.
- Web site: Tails Through Time: The Turboprop B-17 Flying Fortress. www.tailsthroughtime.com. 2016-04-05. 25 March 2016. https://web.archive.org/web/20160325214629/http://www.tailsthroughtime.com/2010/06/in-late-1950s-many-of-surplus-boeing-b.html. dead.
- Web site: Airailimages.com. Johnsen. Frederick. Kenneth G. Johnsen.
- http://www.rafmuseum.org.uk/research/collections/222/engine--rollsroyce-dart-rda-3-mk506 Royal Air Force Museum Cosford – Rolls-Royce Dart
- Web site: GATWICK AVIATION MUSEUM - AERO ENGINES . www.gatwick-aviation-museum.co.uk . dead . https://web.archive.org/web/20040214073816/http://www.gatwick-aviation-museum.co.uk/engines/engines.html . 2004-02-14.
- Web site: Rolls-Royce Dart Mk. 520 Turboprop Engine, Cutaway National Air and Space Museum . airandspace.si.edu . dead . https://web.archive.org/web/20150920203237/http://airandspace.si.edu/collections/artifact.cfm?object=nasm_A19820071000 . 2015-09-20.
- Web site: Rolls-Royce Dart 506.
- Web site: Rolls Royce Dart. 11 November 2015. 4 March 2016. https://web.archive.org/web/20160304065122/http://www.aarg.com.au/rolls-royce-dart.html. dead.
- Web site: Aviation Heritage Museum | Bull Creek, Perth.
- Web site: Engines List . City of Norwich Aviation Museum . 27 August 2023.