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词条 Rolls-Royce RB3011
释义

  1. Design and development

  2. See also

  3. References

  4. External links

{{Refimprove|date=July 2009}}{{Use dmy dates|date=August 2017}}{{Use British English|date=August 2017}}
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}}{{Infobox Aircraft Engine

type= Propfanmanufacturer= Rolls-Royce plcfirst run=major applications=number built =program cost =unit cost =developed from =developed into =variants with their own articles =
}}

The Rolls-Royce RB3011 (previously designated RB2011) is a prototype propfan engine in development by Rolls-Royce plc. The design is also known as an "open rotor" engine.

Design and development

The RB3011 is designed for the 180-300 passenger aircraft (e.g. Boeing 737 or Airbus A320). The RB3011 was renamed from RB2011, because Rolls-Royce employees kept confusing the 2011 with the expected service entry date.[1] Rolls-Royce bought the Allison Engine Company in 1995, and has studied the Pratt & Whitney/Allison 578-DX propfan engine built in the 1980s.

The engine has two contra-rotating rotors (fans) on the outside of the engine nacelle, either at the front of the assembly ("tractor") or at the rear ("pusher"). Both pusher and tractor open rotor designs form part of Rolls Royce's long-term "15-50" vision, which is examining various architectures to tackle the 150 seat-aircraft market. Within 15-50 group -named for specific fuel consumption reductions of 15-50% compared with current generation engines- there are various options based on technology availability and maturity.[2]

The open rotor design is known to have increased noise compared to normal turbofan engines, where noise is contained by the engine duct. The forward rotor is larger in diameter than the rear rotor, to avoid problems with eddies from the forward rotor tips. The rotors are powered by the engine shaft via an epicyclic gearbox. These{{Clarify|date=October 2009}} produce a large amount of heat.

The engine has been tested at the Aircraft Research Association in Bedford, Bedfordshire. Wind tunnel testing has taken place at DNW in Marknesse in the Netherlands.[3]

It is hoped to reduce the fuel consumption of an aircraft, compared to those with normal turbofan engines, by up to 30%. This is the main reason for choosing this design of engine. Certification is planned for 2017-2018, with market entry with airlines by 2020.

See also

{{Aircontent
|related=
|similar engines=
  • General Electric GE36
  • Progress D-27
  • Pratt & Whitney/Allison 578-DX

|lists=
  • List of aircraft engines

|see also=
}}

References

1. ^{{cite web |website=FlightGlobal/Blogs |title=Open season for game-changing name-changing |url=http://www.flightglobal.com/blogs/future-proof/2009/05/open-season-for-game-changing-name-changing.html |dead-url=yes |archive-date=June 6, 2009 |archive-url=https://web.archive.org/web/20090606000353/http://www.flightglobal.com/blogs/future-proof/2009/05/open-season-for-game-changing-name-changing.html |department=Future Proof |date=May 1, 2009 |given=Aimee |surname=Turner}}
2. ^Aviation Week & Space Technology/24 November 2008
3. ^Home » DNW Aero

External links

  • {{cite magazine |work=Flight International |url=http://www.flightglobal.com/articles/2009/10/05/333097/keeping-options-open.html |title=Keeping options open |date=May 10, 2009 |given=Andrew |surname=Doyle |dead-url=yes |archive-date=October 20, 2009 |archive-url=https://web.archive.org/web/20091020142412/http://www.flightglobal.com/articles/2009/10/05/333097/keeping-options-open.html |department=Aircraft}}
  • {{cite magazine |work=Aerospace America |url=http://www.aerospaceamerica.org/Documents/March%202010/Open%20rotor%20research%20revs%20up_MAR2010.pdf |dead-url=yes |archive-date=April 2, 2015 |archive-url=https://web.archive.org/web/20150402143222/http://www.aerospaceamerica.org/Documents/March%202010/Open%20rotor%20research%20revs%20up_MAR2010.pdf |pages=38–42 |publication-date=March 2010 |given=Philip |surname=Butterworth-Hayes |title=Open rotor research revs up}}
  • {{cite web |given=Mark |surname=Taylor |title=Open Rotor Engine Design and Validation |url=http://aerosociety.com/Assets/Docs/Greener%20by%20Design/%286%29%20Mark%20Taylor.pdf |place=Royal Aeronautical Society |dead-url=yes |archive-date=April 2, 2015 |archive-url=https://web.archive.org/web/20150402104200/http://aerosociety.com/Assets/Docs/Greener%20by%20Design/%286%29%20Mark%20Taylor.pdf}}
{{Rolls-Royce plc aeroengines}}

3 : Rolls-Royce aircraft gas turbine engines|Propfan engines|Proposed engines

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