Open main menu
Home
Random
Recent changes
Special pages
Community portal
Preferences
About Wikipedia
Disclaimers
Incubator escapee wiki
Search
User menu
Talk
Dark mode
Contributions
Create account
Log in
Editing
Engine Alliance GP7000
Warning:
You are not logged in. Your IP address will be publicly visible if you make any edits. If you
log in
or
create an account
, your edits will be attributed to your username, along with other benefits.
Anti-spam check. Do
not
fill this in!
{{Short description|Turbofan engine manufactured by Engine Alliance}} {|{{Infobox aircraft begin |name= GP7000 |image= File:EA GP7200.jpg |caption= A GP7270 installed on an [[Airbus A380]], operated by [[Emirates (airline)|Emirates]]. }} {{Infobox aircraft engine |type = [[Turbofan]] |national origin = [[United States]] |manufacturer = [[Engine Alliance]] |first run = April 2004 |major applications = [[Airbus A380]] |number built = |developed from = [[General Electric GE90]] <br /> [[Pratt & Whitney PW4000]] |developed into = |variants with their own articles = }} |} 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]]. ==Design and development== [[File:Airbus Lagardère - GP7200 engine MSN108 (1).JPG|thumb|Engine Alliance GP7000 turbofan awaiting installation on an [[Airbus A380]]]] [[File:Air France Airbus A380-861 F-HPJA @ Paris CDG.jpg|thumb|GP7000 inspection]] Originally intended to power [[Boeing Commercial Airplanes]]' cancelled [[Boeing 747#747-500X, -600X, and -700X|747-500X/-600X]], the engine has since been pushed for [[Airbus]]' [[Airbus A380|A380-800]] superjumbo. It is built around an 0.72 scale of the [[General Electric GE90|GE90]]-110B/115B core <ref>{{cite news | url = http://www.flightglobal.com/news/articles/ge90-115-paves-way-for-39gen-x39-sonic-cruiser-139714/ | title = GE90-115 paves way for 'GEN X' Sonic Cruiser development | publisher = Flight Global | date = 2001-12-04 | access-date = 2016-02-14 }}</ref> and contains a [[Pratt & Whitney]] fan and low-pressure system design. The competing [[Rolls-Royce Trent 900]] was named as the lead engine for the then-named A3XX in 1996 and was initially selected by almost all A380 customers. However, the GE/PW engine increased its share of the A380 engine market to the point where, as of September 2007, it will power 47% of the super-jumbo fleet. This disparity in sales was resolved in a single transaction, with [[Emirates (airline)|Emirates]]' order of 55 GP7000-powered A380-800s, comprising over one quarter of A380 sales (as of September 2007). Emirates has traditionally been a Rolls-Royce customer. A380 aircraft powered by the GP7000s will have A380-86X model numbers as 6 is the code for [[Engine Alliance]] engines. The engine powers an estimated 60% of Airbus A380 in service as reported in 2017.<ref>{{cite news|last1=Freed|first1=Jamie|title=FAA orders A380 engine inspections after Air France incident|url=http://uk.reuters.com/article/us-air-france-canada-faa/faa-orders-a380-engine-inspections-after-air-france-incident-idUKKBN1CI0CI?il=0|archive-url=https://web.archive.org/web/20171013172624/http://uk.reuters.com/article/us-air-france-canada-faa/faa-orders-a380-engine-inspections-after-air-france-incident-idUKKBN1CI0CI?il=0|url-status=dead|archive-date=October 13, 2017|access-date=13 October 2017|work=Reuters|date=13 Oct 2017}}</ref> Ground testing of the engine began in April 2004 and was first flight tested as the number two engine on GE's 747 flying testbed over Victorville, CA in December 2004.<ref>{{cite press release| url = http://www.geaviation.com/press/gepw/gepw_20041207.html| title = GP7200 Takes to the Skies in First Flight Test| publisher = GE Aviation| date = 7 December 2004 |archive-url=https://web.archive.org/web/20160304050422/http://www.geaviation.com/press/gepw/gepw_20041207.html |archive-date=4 March 2016 |url-status=dead}}</ref> The American [[Federal Aviation Administration]] certified the engine for commercial operation on January 4, 2006.<ref>{{cite press release |url=http://www.enginealliance.com/en/media/press_archive.aspx?view=press20060104 |publisher=Engine Alliance |title=GP7200 Achieves FAA Certification |date=2006-01-04 |access-date=2012-06-24 }}{{dead link|date=December 2016 |bot=InternetArchiveBot |fix-attempted=yes }}</ref> The engine was ground run for the first time on an A380 on August 14, 2006, in Toulouse.<ref>{{cite news | url = http://www.flightglobal.com/news/articles/picture-airbus-begins-engine-runs-on-engine-alliance-gp7200-powered-a380-in-toulouse-208485/ | title = Picture: Airbus begins engine runs on Engine Alliance GP7200-powered A380 in Toulouse | publisher = Flight Global | date = 2006-08-15 | access-date = 2012-06-24 }}</ref> On August 25, 2006, the same aircraft, A380-861 test aircraft (MSN 009), made the first flight of an Engine Alliance powered A380. The flight began and ended at [[Toulouse]] and lasted about four hours. Tests were performed on the engines' flight envelope, cruise speed, and handling. A day earlier, the same aircraft performed [[rejected takeoff]] tests on the engines. The [[Engine Alliance]] offered the GP7200 for the Airbus A380 passenger and freighter configurations. The GP7270 is rated at {{convert|74735|lbf|kN|abbr=on}} of thrust whilst the GP7277 is rated at {{convert|80290|lbf|kN|abbr=on}}. The engine is offered with two ratings appropriate for the various A380 configurations and take-off weights: GP7270 for the 560-tonne variant, and GP7277 for the 590 tonne A380-800 freighter (which was subsequently cancelled by Airbus). In mid-2011 an upgrade was announced which will lead to a cut in weight for each engine by {{convert|23|kg|abbr=on}}. The new components come from [[Volvo Aero]].<ref>{{cite news | url = http://www.flightglobal.com/articles/2011/06/22/358619/paris-engine-alliance-cuts-another-50-pounds-from-gp7200.html | title = PARIS: Engine Alliance cuts another 50 pounds from GP7200 | author = John Croft | publisher = Flight Global | date = 2011-06-22 | access-date = 2012-06-24 }}</ref> [[MTU Aero Engines]] is a major partner of the programme, with 22.5% share. The German company produces the high-pressure turbine, the low-pressure turbine and the turbine center frame. [[Safran]] with 17.5% designs and produces the low-pressure compressor.<ref> [http://www.mtu.de/fileadmin/EN/7_News_Media/2_Media/Brochures/Engines/GP7000.pdf GP7000 turbofan engine] MTU Aero Engines {{webarchive|date=23 June 2017|url=https://web.archive.org/web/20170623192850/http://www.mtu.de/fileadmin/EN/7_News_Media/2_Media/Brochures/Engines/GP7000.pdf}}</ref> MDS Aero Support Corporation, a Canadian company, is working hand in hand with MTU to develop next-generation test beds. MDS in joint cooperation is building the facility to test the next version of this engine in France.<ref>{{Cite web|url=http://www.afiklmem.com/AFIKLMEM/en/g_page_standard/MediaRelation/BlueLink_10_October2012/BlueLink_10_EngineTestBench.html|title = Air France Industries KLM Engineering & Maintenance}}</ref> ==Variants== *'''GP7270''' with {{convert|332.44|kN|abbr=on}} of thrust. In use by A380-861 of [[Air France]], [[Etihad Airways]], [[Korean Air]], and [[Qatar Airways]], as well as 90 of the 123 A380s ordered by [[Emirates (airline)|Emirates]].<ref>{{cite news|url=https://www.bbc.com/news/business-32347783|title=Record £6bn order for Rolls-Royce|work=BBC News|date=17 April 2015|access-date=20 April 2018}}</ref><ref>{{cite web|url=http://www.aircraft.airbus.com/market/orders-deliveries/|title=Orders and deliveries|website=Airbus|access-date=20 April 2018|archive-date=4 December 2017|archive-url=https://web.archive.org/web/20171204134056/http://www.aircraft.airbus.com/market/orders-deliveries/|url-status=dead}}</ref> *'''GP7277''' with {{convert|357.1|kN|abbr=on}} of thrust. Originally for use on the now-cancelled [[Airbus A380#A380F|A380F]] freighter. ==Applications== * [[Airbus A380]] ==Notable incidents== On 30 September 2017, [[Air France Flight 66]], an Airbus A380 with registration F-HPJE, suffered an [[Turbine engine failure#Contained and uncontained failures|uncontained engine failure]] during flight where the entire fan module (blades and disc) and nose cowl on its [[aircraft engine position number|number-four]] GP7270 engine separated from the engine. The aircraft was flying from [[Paris Charles de Gaulle Airport]] to [[Los Angeles International Airport]].<ref>{{cite web|url= http://avherald.com/h?article=4af15205&opt=0 |title=Incident: France A388 over Greenland on Sep 30th 2017, uncontained engine failure, fan and engine inlet separated|website=avherald.com|access-date=20 April 2018}}</ref> The aircraft was safely diverted to [[CFB Goose Bay]], Canada.<ref>{{cite news|url= https://www.reuters.com/article/us-air-france-canada/air-france-flight-with-engine-damage-makes-emergency-landing-in-canada-idUSKCN1C50PV |title=Air France flight with engine damage makes emergency landing in Canada|website=reuters.com|date=30 September 2017|access-date=20 April 2018}}</ref> To repatriate the stranded jet, the damaged engine would be replaced and sent back to GE's workshop at Cardiff; a replacement engine had to be placed in the same position to balance the weight for takeoff but not operable.<ref name="Reuters101017">{{cite news|last1=Hepher|first1=Tim |title=Damaged A380 to be flown to France to investigate engine blast|url= https://www.reuters.com/article/uk-air-france-canada-idAFKBN1CF2R6 |access-date=19 July 2022|work=Reuters|date=10 Oct 2017}}</ref> The French accident investigation agency BEA, which is conducting the investigation into the incident, released photos of the first engine fan, fan hub and cowling parts being recovered in [[Greenland]].<ref>{{Cite news|url= https://news.aviation-safety.net/2017/10/06/first-parts-af66-engine-cowling-recovered-greenland/ |title=First parts of AF66 engine and cowling recovered from Greenland. - ASN News|date=2017-10-06|work=ASN News|access-date=2017-10-13 |language=en-US}}</ref><ref name="Reuters101017"/><ref>{{Citation|title=AIRBUS A380 F-HPJ Greenland Fan Hub Recovery by GEUS / BEA (June 2019)| date=3 July 2019 |url= https://www.youtube.com/watch?v=zPcSU0A1G9w |language=en|access-date=2019-08-13}}</ref> ==Specifications (GP7270)== {{jetspecs |<!-- If you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] --> <!-- Please include units where appropriate (main comes first, alt in parentheses). If data are missing, leave the parameter blank (do not delete it). For additional lines, end your alt units with )</li> and start a new, fully-formatted line with <li> --> |type = two-spool high-bypass [[turbofan]] engine |length = {{convert|4.92|m|ft in|abbr=on}} spinner to flange<ref>[https://www.easa.europa.eu/system/files/dfu/20140404_TCDS_IM.E.026_issue04_0.pdf EASA Type certificate data sheet] European Aviation Safety Agency 4 April 2014 {{webarchive|date=23 December 2017 |url=https://web.archive.org/web/20171223075120/https://www.easa.europa.eu/system/files/dfu/20140404_TCDS_IM.E.026_issue04_0.pdf}}</ref> |diameter = {{convert|3.16|m|ft in|abbr=on}}, fan {{convert|2.96|m|ft in|abbr=on}} |weight = {{convert|6712|kg|lb|abbr=on}} |compressor = 24 swept [[Wide chord|wide-chord]] hollow titanium fan blades, 8.8:1 by-pass ratio; five-stage low-pressure [[axial compressor]]; nine-stage high-pressure axial compressor |combustion = low-emissions single annular combustor |turbine = two-stage high pressure turbine, boltless architecture, single crystal blades, split blade cooling and thermal barrier coatings, axial flow; six-stage low-pressure axial flow |fueltype = |oilsystem = |compression = 43.9 |aircon = 900 to 1,200 kg/s (2,000 to 2,600 lb/s) |fuelcon = |specfuelcon = |thrust= 36,980 kgf, 363 kN, 81,500 lbf |thrust/weight = 5.197 (assuming 13,400 lbf weight of engine and 70,000 lbf of thrust) }} ==See also== {{Aircontent |related= *{{annotated link|General Electric GE90}} *{{annotated link|Pratt & Whitney PW4000}} |similar engines= *{{annotated link|Rolls-Royce Trent 900}} |lists= *[[List of aircraft engines]] |see also= }} ==References== {{reflist}} * [http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/114398eac7af8d93862570fc00591557/$FILE/E00072EN.pdf FAA certificate data sheet] ==External links== {{Commons category}} * [http://www.enginealliance.com/ Official site], Engine Alliance * [https://web.archive.org/web/20070212080414/http://www.geaviation.com/engines/commercial/gp7000/ Official site], GE-Aviation * [http://www.pw.utc.com/GP7200_Engine Official site], Pratt & Whitney {{Joint development aeroengines}} [[Category:High-bypass turbofan engines]] [[Category:2000s turbofan engines]]
Edit summary
(Briefly describe your changes)
By publishing changes, you agree to the
Terms of Use
, and you irrevocably agree to release your contribution under the
CC BY-SA 4.0 License
and the
GFDL
. You agree that a hyperlink or URL is sufficient attribution under the Creative Commons license.
Cancel
Editing help
(opens in new window)
Pages transcluded onto the current version of this page
(
help
)
:
Template:Aircontent
(
edit
)
Template:Citation
(
edit
)
Template:Cite news
(
edit
)
Template:Cite press release
(
edit
)
Template:Cite web
(
edit
)
Template:Commons category
(
edit
)
Template:Convert
(
edit
)
Template:Dead link
(
edit
)
Template:Infobox aircraft begin
(
edit
)
Template:Infobox aircraft engine
(
edit
)
Template:Jetspecs
(
edit
)
Template:Joint development aeroengines
(
edit
)
Template:Reflist
(
edit
)
Template:Short description
(
edit
)
Template:Webarchive
(
edit
)