Jump to content
Main menu
Main menu
move to sidebar
hide
Navigation
Main page
Recent changes
Random page
Help about MediaWiki
Special pages
Niidae Wiki
Search
Search
Appearance
Create account
Log in
Personal tools
Create account
Log in
Pages for logged out editors
learn more
Contributions
Talk
Editing
Bell Boeing V-22 Osprey
(section)
Page
Discussion
English
Read
Edit
View history
Tools
Tools
move to sidebar
hide
Actions
Read
Edit
View history
General
What links here
Related changes
Page information
Appearance
move to sidebar
hide
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!
===Propulsion=== [[File:V-22-166480-FAR01.jpg|thumb|Closeup of rotor and engine of a MV-22B |alt=A closeup of an MV-22B's rotor and engine tilted slightly upward.]] The V-22's two [[Rolls-Royce T406|Rolls-Royce AE 1107C]] engines are connected by [[drive shaft]]s to a common central [[Transmission (mechanics)|gearbox]] so that one engine can power both proprotors if an engine failure occurs.<ref name=Norton_p98-9>Norton 2004, pp. 98β99.</ref> Either engine can power both proprotors through the wing driveshaft.<ref name=v22fly/> However, the V-22 is generally not capable of hovering on one engine.<ref>Whittle, Richard. "[http://breakingdefense.com/2015/07/fatal-crash-prompts-marines-to-change-osprey-flight-rules/ Fatal Crash Prompts Marines To Change Osprey Flight Rules] {{Webarchive|url=https://web.archive.org/web/20150719000019/http://breakingdefense.com/2015/07/fatal-crash-prompts-marines-to-change-osprey-flight-rules/ |date=2015-07-19}}". ''Breaking Defense'', 16 July 2015.</ref> If a proprotor gearbox fails, that proprotor cannot be [[Propeller (aircraft)#Feathering|feathered]], and both engines must be stopped before an [[emergency landing]]. The autorotation characteristics are poor because of the rotors' low [[inertia]].<ref name=v22fly/> The AE 1107C engine has a two-shaft axial design with a 14-stage compressor, an effusion-cooled annular combustor, a two-stage gas generator turbine, and two-stage power turbine.<ref>{{cite web |last=Welt |first=Flying |date=14 May 2023 |title=Bell Boeing V 22 Osprey, the World's First Production Military Tiltrotor Aircraft |url=https://www.flyingwelt.com/2023/05/bell-boeing-v-22-osprey-the-worlds-first-production-military-tiltrotor-aircraft/ |access-date=24 November 2023 |website=Flying Welt |language=en-US |archive-date=24 November 2023 |archive-url=https://web.archive.org/web/20231124051636/https://www.flyingwelt.com/2023/05/bell-boeing-v-22-osprey-the-worlds-first-production-military-tiltrotor-aircraft/ |url-status=live}}</ref> [[File:V22-Osprey.jpg|thumb|left|V-22 with rotors tilted, condensation trailing from propeller tips]] In September 2013, Rolls-Royce announced that it had increased the AE-1107C engine's power by 17% via the adoption of a new Block 3 turbine, increased fuel valve flow capacity, and software updates; it should also improve reliability in high-altitude, high-heat conditions and boost maximum payload limitations from {{convert|6000|to|8000|ft|m|abbr=on}}. A Block 4 upgrade is reportedly being examined, which may increase power by up to 26%, producing close to {{convert|10000|shp|kW|abbr=on}}, and improve fuel consumption.<ref>[https://archive.today/20130920190720/http://www.defensenews.com/article/20130916/DEFREG02/309160009/Rolls-Royce-Boosts-Power-V-22-Engines "Rolls-Royce Boosts Power for V-22 Engines"]. Defense News, 16 September 2013.</ref> In August 2014, the U.S. military issued a [[request for information]] for a potential drop-in replacement for the AE-1107C engines. Submissions must have a power rating of no less than {{convert|6100|shp|kW|abbr=on}} at 15,000 rpm, operate at up to {{convert|25000|ft|m|abbr=on}} at up to {{convert|130|F|C|abbr=off}}, and fit into the existing wing nacelles with minimal structural or external modifications.<ref>[http://www.flightglobal.com/news/articles/us-military-seeking-replacement-v-22-engines-403177/ US military seeking replacement V-22 engines] {{Webarchive|url=https://web.archive.org/web/20140907171441/http://www.flightglobal.com/news/articles/us-military-seeking-replacement-v-22-engines-403177/ |date=7 September 2014}} β Flightglobal.com, 29 August 2014</ref> In September 2014, the U.S. Navy, who already purchase engines separately to airframes, was reportedly considering an alternative engine supplier to reduce costs.<ref>Wall, Robert, "US mulls engine options for its Osprey aircraft", ''The Wall Street Journal'', 2 September 2014, p.B3</ref> The [[General Electric GE38]] is one option, giving commonality with the [[Sikorsky CH-53K King Stallion]].<ref>[http://www.flightglobal.com/news/articles/us-navy-developing-early-plans-for-v-22-mid-life-upgrade-411212/ "US Navy developing early plans for V-22 mid-life upgrade"] {{Webarchive|url=https://web.archive.org/web/20150416231330/http://www.flightglobal.com/news/articles/us-navy-developing-early-plans-for-v-22-mid-life-upgrade-411212/ |date=16 April 2015}} β Flightglobal.com, 15 April 2015.</ref> The V-22 has a maximum rotor [[downwash]] speed of over {{convert|80|kn|mph kph}}, more than the {{convert|64|kn|mph kph|adj=on}} lower limit of a [[hurricane]].<ref name=randwash>John Gordon IV et al. [https://www.rand.org/pubs/documented_briefings/2005/RAND_DB472.pdf Assessment of Navy Heavy-Lift Aircraft Options] p39. ''[[RAND Corporation]]'', 2005. Retrieved 18 March 2012. {{ISBN|0-8330-3791-9}}. [https://web.archive.org/web/20110927172859/https://www.rand.org/pubs/documented_briefings/2005/RAND_DB472.pdf Archived] in 2011.</ref><ref name=NOAA>[https://web.archive.org/web/20080226215213/http://www.srh.noaa.gov/fwd/wcm/hurric.pdf "Hurricanes... Unleashing Nature's Fury: A Preparedness Guide"]. [[National Oceanic and Atmospheric Administration]], [[National Weather Service]], September 2006.</ref> The rotorwash usually prevents the starboard door's usage in hover; the rear ramp is used for rappelling and hoisting instead.<ref name="v22fly">McKinney, Mike. [http://www.verticalmag.com/features/features_article/20112-flying-the-v-22.html "Flying the V-22"] ''[[Vertical (magazine)|Vertical]]'', 28 March 2012. [https://web.archive.org/web/20140430000553/http://www.verticalmag.com/features/features_article/20112-flying-the-v-22.html Archived] on 30 April 2014.</ref><ref name=fastrope>Waters, USMC Cpl. Lana D. [https://web.archive.org/web/20041120010423/http://www.navy.mil/view_single.asp?id=18900 V-22 Osprey Fast rope 1] ''[[United States Marine Corps|USMC]]'', 6 November 2004. [https://web.archive.org/web/20050321095806/http://www.navy.mil/view_single.asp?id=18900 Archived] on 21 March 2005.</ref> The V-22 loses 10% of its vertical lift over a [[tiltwing]] design when operating in helicopter mode because of the wings' airflow resistance, while the tiltrotor design has better short takeoff and landing performance.<ref>Trimble, Stephen. [http://www.flightglobal.com/blogs/the-dewline/2009/06/boeing-looks-ahead-to-a-v-23-o.html "Boeing looks ahead to a 'V-23' Osprey"]. {{Webarchive|url=https://web.archive.org/web/20090625022409/http://www.flightglobal.com/blogs/the-dewline/2009/06/boeing-looks-ahead-to-a-v-23-o.html |date=25 June 2009}} ''Flight Global'', 22 June 2009. [https://web.archive.org/web/20150112022437/http://www.flightglobal.com/blogs/the-dewline/2009/06/boeing-looks-ahead-to-a-v-23-o/ Archived] on 12 January 2015.</ref> V-22s must keep at least {{convert|25|ft|m|abbr=on}} of vertical separation between each other to avoid each other's rotor wake, which causes turbulence and potentially control loss.<ref name=whittle2015-05-15/> The extreme rotor downwash of the V-22 has caused incidents when rappelling or fast roping from the aircraft, including a soldier being blown 3 meters away from his intended dismount point by the force of the downwash.<ref>{{Cite web |last=|date=1996-03-13 |title=Concerns about V-22 downwash crop |url=https://www.flightglobal.com/concerns-about-v-22-downwash-crop/10171.article |access-date=2024-11-03 |website=Flight Global |language=en}}</ref> The downwash is strong enough to destroy unstrengthened helipads and can create flying debris in the landing zone that can injure bystanders or potentially damage the aircraft; an incident involving a Marine Corps Osprey in 2010 resulted in 10 bystanders suffering downwash-related injuries.<ref>{{Cite web |last=Trevithick |first=Joseph |date=2021-04-22 |title=Watch This CV-22 Osprey's Rotor Downwash Absolutely Demolish A Hospital's Helipad |url=https://www.twz.com/40289/watch-this-cv-22-ospreys-rotor-downwash-absolutely-demolish-a-hospitals-helipad |access-date=2024-11-03 |website=The War Zone |language=en-US}}</ref><ref>"Marine aircraft blows tree branches, injures 10 on ground during NYC landing for Fleet Week" May 31, 2010 Fox News https://www.foxnews.com/us/marine-aircraft-blows-tree-branches-injures-10-on-ground-during-nyc-landing-for-fleet-week</ref>
Summary:
Please note that all contributions to Niidae Wiki may be edited, altered, or removed by other contributors. If you do not want your writing to be edited mercilessly, then do not submit it here.
You are also promising us that you wrote this yourself, or copied it from a public domain or similar free resource (see
Encyclopedia:Copyrights
for details).
Do not submit copyrighted work without permission!
Cancel
Editing help
(opens in new window)
Search
Search
Editing
Bell Boeing V-22 Osprey
(section)
Add topic