Turboprop
A turboprop is a
A turboprop consists of an
Technological aspects
Exhaust thrust in a turboprop is sacrificed in favor of shaft power, which is obtained by extracting additional power (beyond that necessary to drive the compressor) from turbine expansion. Owing to the additional expansion in the turbine system, the residual energy in the exhaust jet is low.[4][5][6] Consequently, the exhaust jet produces about 10% of the total thrust.[7] A higher proportion of the thrust comes from the propeller at low speeds and less at higher speeds.[8]
Turboprops have bypass ratios of 50–100,[9][10] although the propulsion airflow is less clearly defined for propellers than for fans.[11][12]
The propeller is coupled to the turbine through a
The propeller itself is normally a
The constant-speed propeller is distinguished from the reciprocating engine constant-speed propeller by the control system. The turboprop system consists of 3
To make the engine more compact, reverse airflow can be used. On a reverse-flow turboprop engine, the compressor intake is at the aft of the engine, and the exhaust is situated forward, reducing the distance between the turbine and the propeller.[15]
Unlike the small-diameter fans used in
Propellers work well until the flight speed of the aircraft is high enough that the airflow past the blade tips reaches the speed of sound. Beyond that speed, the proportion of the power that drives the propeller that is converted to propeller thrust falls dramatically. For this reason turboprop engines are not commonly used on aircraft
While the power turbine may be integral with the gas generator section, many turboprops today feature a free power turbine on a separate coaxial shaft. This enables the propeller to rotate freely, independent of compressor speed.[21]
History
Alan Arnold Griffith had published a paper on compressor design in 1926. Subsequent work at the Royal Aircraft Establishment investigated axial compressor-based designs that would drive a propeller. From 1929, Frank Whittle began work on centrifugal compressor-based designs that would use all the gas power produced by the engine for jet thrust.[22]
The world's first turboprop was designed by the Hungarian mechanical engineer György Jendrassik.[23] Jendrassik published a turboprop idea in 1928, and on 12 March 1929 he patented his invention. In 1938, he built a small-scale (100 Hp; 74.6 kW) experimental gas turbine.[24] The larger Jendrassik Cs-1, with a predicted output of 1,000 bhp, was produced and tested at the Ganz Works in Budapest between 1937 and 1941. It was of axial-flow design with 15 compressor and 7 turbine stages, annular combustion chamber. First run in 1940, combustion problems limited its output to 400 bhp. Two Jendrassik Cs-1s were the engines for the world's first turboprop aircraft – the Varga RMI-1 X/H. This was a Hungarian fighter-bomber of WWII which had one model completed, but before its first flight it was destroyed in a bombing raid.[25][26] In 1941, the engine was abandoned due to war, and the factory converted to conventional engine production.
The first mention of turboprop engines in the general public press was in the February 1944 issue of the British aviation publication
The Soviet Union built on German World War II turboprop preliminary design work by Junkers Motorenwerke, while BMW,
The first American turboprop engine was the
The first turbine-powered, shaft-driven helicopter was the
December 1963 saw the first delivery of
1964 saw the first deliveries of the
Usage
In contrast to turbofans, turboprops are most efficient at flight speeds below 725 km/h (450 mph; 390 knots) because the jet velocity of the propeller (and exhaust) is relatively low.[citation needed] Modern turboprop airliners operate at nearly the same speed as small regional jet airliners but burn two-thirds of the fuel per passenger.[38]
Compared to piston engines, their greater
Turboprop engines are generally used on small subsonic aircraft, but the
In 2017, the most widespread turboprop
Turboprop
Reliability
Between 2012 and 2016, the ATSB observed 417 events with turboprop aircraft, 83 per year, over 1.4 million flight hours: 2.2 per 10,000 hours. Three were "high risk" involving engine malfunction and unplanned landing in single‑engine Cessna 208 Caravans, four "medium risk" and 96% "low risk". Two occurrences resulted in minor injuries due to engine malfunction and terrain collision in
Current engines
Manufacturer | Country | Designation | Dry weight (kg) | Takeoff rating (kW) | Application |
---|---|---|---|---|---|
DEMC | China | WJ5E |
720 | 2130 | Harbin SH-5, Xi'an Y-7 |
Europrop International | Multinational | TP400-D6 | 1800 | 8203 | Airbus A400M
|
General Electric | United States | CT7-5A | 365 | 1294 | |
General Electric | United States | CT7-9 | 365 | 1447 | CASA/IPTN CN-235, Let L-610, Saab 340, Sukhoi Su-80 |
General Electric | United States / Czech Republic | H80 Series[43]
|
200 | 550–625 | Nextant G90XT
|
General Electric | United States | T64-P4D | 538 | 2535 | Aeritalia G.222, de Havilland Canada DHC-5 Buffalo, Kawasaki P-2J |
Honeywell | United States | TPE331 Series |
150–275 | 478–1650 | |
Honeywell | United States | LTP 101-700 | 147 | 522 | Air Tractor AT-302, Piaggio P.166
|
KKBM | Russia | NK-12MV | 1900 | 11033 | Antonov An-22, Tupolev Tu-95, Tupolev Tu-114 |
Progress | Ukraine | TV3-117VMA-SB2 | 560 | 1864 | Antonov An-140 |
Klimov | Russia | TV7-117S | 530 | 2100 | Ilyushin Il-112, Ilyushin Il-114 |
Ivchenko-Progress | Ukraine | AI20M | 1040 | 2940 | Antonov An-12, Antonov An-32, Ilyushin Il-18 |
Ivchenko-Progress | Ukraine | AI24T | 600 | 1880 | Antonov An-24, Antonov An-26, Antonov An-30 |
LHTEC | United States | LHTEC T800 | 517 | 2013 | Ayres LM200 Loadmaster (not built) |
OMKB | Russia | TVD-20 | 240 | 1081 | Antonov An-3, Antonov An-38 |
Pratt & Whitney Canada | Canada | PT-6 Series |
149–260 | 430–1500 | |
Pratt & Whitney Canada | Canada | PW120 | 418 | 1491 | ATR 42-300/320 |
Pratt & Whitney Canada | Canada | PW121 | 425 | 1603 | Bombardier Dash 8 Q100
|
Pratt & Whitney Canada | Canada | PW123 C/D | 450 | 1603 | Bombardier Dash 8 Q300
|
Pratt & Whitney Canada | Canada | PW126 C/D | 450 | 1950 | BAe ATP
|
Pratt & Whitney Canada | Canada | PW127 | 481 | 2051 | ATR 72 |
Pratt & Whitney Canada | Canada | PW150A | 717 | 3781 | Bombardier Dash 8 Q400
|
PZL | Poland | TWD-10B | 230 | 754 | PZL M28
|
RKBM |
Russia | TVD-1500S | 240 | 1044 | Sukhoi Su-80 |
Rolls-Royce Limited | United Kingdom | Dart Mk 536 | 569 | 1700 | Fokker F27, Vickers Viscount
|
Rolls-Royce Limited | United Kingdom | Tyne 21 | 1085 | 4500 | Breguet Atlantic, Transall C-160
|
Rolls-Royce plc |
United Kingdom | 250-B17 | 88.4 | 313 | Cessna 210, Soloy Cessna 206, Propjet Bonanza
|
Rolls-Royce plc | United Kingdom | Allison T56 | 828–880 | 3424–3910 | C-130 Hercules
|
Rolls-Royce plc | United Kingdom | AE2100A | 715.8 | 3095 | Saab 2000 |
Rolls-Royce plc | United Kingdom | AE2100J | 710 | 3424 | ShinMaywa US-2 |
Rolls-Royce plc | United Kingdom | AE2100D2, D3 | 702 | 3424 | Alenia C-27J Spartan, Lockheed Martin C-130J Super Hercules |
Rybinsk |
Russia | TVD-1500V | 220 | 1156 | |
Saturn |
Russia | TAL-34-1 | 178 | 809 | |
Turbomeca |
France | Arrius 1D | 111 | 313 | Socata TB 31 Omega |
Turbomeca | France | Arrius 2F | 103 | 376 | |
Walter | Czech Republic | M601 Series[44] | 200 | 560 | |
Walter | Czech Republic | M602A | 570 | 1360 | Let L-610 |
Walter | Czech Republic | M602B | 480 | 1500 |
See also
References
- ISBN 978-1-60239-780-4.
- ^ "Aviation Glossary – Turboprop". dictionary.dauntless-soft.com. Retrieved 7 July 2019.
- ^ Rathore, Mahesh. Thermal Engineering. Tata McGraw-Hill Education. p. 968.
- ^ a b Hall, Nancy (2021). "Turboprop Engine". Glenn Research Center. NASA. Retrieved 14 March 2023.
- ^ a b Hall, Nancy (2021). "Turboprop Thrust". Glenn Research Center. NASA. Retrieved 14 March 2023.
- ^ a b "Variations of Jet Engines". smu.edu. Retrieved 31 August 2016.
- ^ a b ""The turbofan engine Archived 18 April 2015 at the Wayback Machine", page 7. SRM Institute of Science and Technology, Department of aerospace engineering.
- ISBN 0080538649.
- ^ Ilan Kroo and Juan Alonso. "Aircraft Design: Synthesis and Analysis, Propulsion Systems: Basic Concepts Archived 18 April 2015 at the Wayback Machine" Stanford University School of Engineering, Department of Aeronautics and Astronautics Main page Archived 23 February 2001 at the Wayback Machine
- MIT turbines, 2002. Thermodynamics and Propulsion
- ^ Hall, Nancy (2021). "Propeller Thrust". Glenn Research Center. NASA. Retrieved 14 March 2023.
- ISBN 9781405151030.
- ^ Airscrews For Turbines, Fairhurst, Flight magazine, 10 November 1949, p.609
- ^ ISBN 0884873382.
- ^ Martin, Swayne (16 May 2019). "How A Turboprop Engine Works". Boldmethod. Archived from the original on 6 November 2021. Retrieved 6 November 2021.
- ^ Paul Bevilaqua. The shaft driven Lift Fan propulsion system for the Joint Strike Fighter Archived 5 June 2011 at the Wayback Machine page 3. Presented 1 May 1997. DTIC.MIL Word document, 5.5 MB. Retrieved 25 February 2012.
- ^ Bensen, Igor B. "How They Fly". Archived from the original on 20 April 2001. Retrieved 31 May 2023.
{{cite web}}
: CS1 maint: unfit URL (link) - ISBN 978-0-486-68230-3.
- ISBN 978-0-486-64647-3.
- ^ "Operating Propellers during Landing & Emergencies". experimentalaircraft.info. Retrieved 8 July 2019.
- ^ "An Engine Ahead of Its Time". PT6 Nation. Pratt & Whitney Canada.
- ^ Gunston Jet, p. 120
- ^ Gunston World, p.111
- ^ "Magyar feltalálók és találmányok – JENDRASSIK GYÖRGY (1898–1954)". SZTNH. Retrieved 31 May 2012.
- ^ "The Jendrassik CS-1: The World's First Turboprop Engine". www.tailsthroughtime.com. Retrieved 4 September 2023.
- ^ "RMI / Repülő Muszaki Intézet Varga RMI-1/ X / H". Retrieved 4 September 2023.
- ^ "Our Contribution – How Flight Introduced and Made Familiar With Gas Turbines and Jet Propulsion" Flight, 11 May 1951, p. 569.
- ^ James p. 251-2
- ^ Green p.18-9
- ^ "rolls-royce trent – armstrong siddeley – 1950–2035 – Flight Archive". Flightglobal. Retrieved 31 August 2016.
- ^ Green p.82
- ^ Green p.81
- ISBN 978 1 86126 912 6, various pages
- ^ Green p.57
- ^ "Smithsonian National Air and Space Museum – Collections – Kaman K-225 (Long Description)". National Air and Space Museum. Archived from the original on 4 March 2016. Retrieved 4 April 2013.
- ^ "PT6 60 YEARS - Pratt & Whitney". www.pwc.ca. Retrieved 27 June 2023.
- ^ "Evolution of the Honeywell TPE331". aerospace.honeywell.com. Retrieved 27 June 2023.
- ^ "More turboprops coming to the market – maybe". CAPA – Centre for Aviation. 9 July 2010.
- ^ "Beechcraft King Air 350i rolls out improved situational awareness, navigation" (Press release). Textron Aviation. 30 May 2018.
- ^ "787 stars in annual airliner census". Flightglobal. 14 August 2017.
- ^ "Business Aviation Market Update Report" (PDF). AMSTAT, Inc. April 2017.
- ^ Gordon Gilbert (25 June 2018). "ATSB Study Finds Turboprop Engines Safe, Reliable".
- ^ "The H-Series Engine | Engines | B&GA | GE Aviation". www.geaviation.com. Retrieved 1 June 2016.
- ^ [1], PragueBest s.r.o. "History | GE Aviation". www.geaviation.cz. Archived from the original on 29 October 2017. Retrieved 1 June 2016.
{{cite web}}
: External link in
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Bibliography
- Green, W. and Cross, R.The Jet Aircraft of the World (1955). London: MacDonald
- Gunston, Bill (2006). The Development of Jet and Turbine Aero Engines, 4th Edition. Sparkford, Somerset, England, UK: Patrick Stephens, Haynes Publishing. ISBN 0-7509-4477-3.
- Gunston, Bill (2006). World Encyclopedia of Aero Engines, 5th Edition. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited. ISBN 0-7509-4479-X.
- James, D.N. Gloster Aircraft since 1917 (1971). London: Putnam & Co. ISBN 0-370-00084-6
Further reading
- ISBN 978-0-07-069633-4.
External links
- Jet Turbine Planes by LtCol Silsbee USAAF, Popular Science, December 1945, first article on turboprops printed
- Wikibooks: Jet propulsion
- "Development of the Turboprop" – a 1950 Flight article on UK and US turboprop engines