Template:Short description Template:Use dmy dates Template:Use American English
Template:Infobox aircraft engineThe Rolls-Royce T406 (company designation AE 1107) is a turboshaft engine developed by Allison Engine Company (now part of Rolls-Royce) that powers the Bell Boeing V-22 Osprey tiltrotor. The engine delivers 6,000 shp (4,470 kW).
DevelopmentEdit
In 1982, Detroit Diesel Allison (DDA) prepared a new engine design to enter the United States Army's Modern Technology Demonstrator Engine (MTDE) competition, which was expected to be developed into the powerplant for the United States Navy's JVX experimental tiltrotor aircraft program (which would eventually become the Bell Boeing V-22 Osprey).<ref name="LeyesFleming579580"/> After this engine, which DDA called the Model 580,<ref name="InsideIndy19830114"/> lost the competition to Pratt & Whitney and General Electric in 1983, Allison was separated from Detroit Diesel as a separate division within General Motors, and Allison's new management decided to pursue the V-22 engine contract anyway.<ref name="LeyesFleming579580"/>
On 24 December 1985, the U.S. Navy selected Allison's engine for full-scale engine development and production on the U.S. Marine Corps's V-22 Osprey.<ref name="UPI19851224"/> Before the engine was given its United States military aircraft engine designation of T406, it was known as the Model 501-M80C.<ref name="AWST19860317"/> The Navy and Allison signed a formal contract on 2 May 1986, and the first engine to test ran six months after.<ref name="Brussels1990"/>
The T406 is based on the Allison T56 turboprop from the P-3 and the C-130, with the free power turbine of the Allison T701 turboshaft from the defunct Heavy Lift Helicopter program. It was selected over the Pratt & Whitney PW3000 and General Electric GE27 competing for the US Army's Modern Technology Demonstrator Engine program.<ref name="Flight29jul1989"/> The T406 began flight testing on 19 March 1989.<ref name="Chambers1991"/>
The T406/AE 1107C Liberty shares a common core with the AE 3007 turbofan and AE 2100 turboprop series of engines, both of which have sold in the thousands of copies.<ref name="RR20170302"/><ref name="2300engines"/> 44-46 percent of parts are common between the T406 and the AE 3007, while about 76 percent of parts are common between the T406 and the AE 2100.<ref name="Weaknesses"/> In addition, Allison attempted to develop other types of engines based on the T406. In 1988, the company signed a memorandum of understanding (MoU) with Messerschmitt-Bölkow-Blohm (MBB) of West Germany and the China National Aero-Technology Import & Export Corporation (CATIC) to work on a version of the MPC 75 regional aircraft to be powered by a T406-derived propfan.<ref name="FI19880521"/> In 1990, Allison studied a Template:Cvt propfan powerplant driving Template:Cvt contra-rotating propellers to power Euroflag's proposed military airlift aircraft.<ref name="T406Derivatives"/> Also, the MT7 gas turbines that will be used to power the Ship-to-Shore Connector are a derived design of the T406.<ref name="MM20121101"/>
Production continued by Rolls-Royce after it acquired Allison in 1995 to establish a North American subsidiary. In 2009, the Government Accountability Office (GAO) found that the engines failed after less than 400 hours of service, as compared to the estimated life of 500–600 hours.<ref name="MCT20130813"/> Multiple updates to the engine platform in 2012-2013 have increased the lifespan significantly.
In April 2012, the United States Department of Defense (DoD) ordered 70 AE 1107C engines for the Osprey, with options for up to 268 engines.<ref name="rrann"/>
Rolls-Royce introduced a Block 3 turbine upgrade, which replaced the old turbine design with sturdier and more efficient components. The upgrade increased engine power by at least 17 percent, and the engine achieved a power output of over Template:Cvt during ground testing.<ref name="FI20140918"/> The Block 3 turbine became standard in July 2012 for new production models. By September 2012, all older engines that were undergoing regular maintenance were systematically upgraded to the Block 3 turbine.
Engines with a future planned block 4 upgrade would be expected to deliver nearly Template:Convert.<ref name="BoostsPower20130916"/>
An ongoing problem with the engines was their propensity for surging or stalling with 68 incidents reported between 2003 and October 2016 though this rate had reduced after the introduction of the Block 3 engine version. The US Naval Air Systems Command intends to award Rolls-Royce two contracts to examine the effectiveness of proposed reliability improvements, the first is a software tweak to the engine management software for the compressor guide vanes that internal testing showed could improve surge margin by 0.8% at sea level and 3% at altitude. The second is the discovery that a temperature sensor at the inlet of the compressor sends incorrect readings leading to 2.5% out of 4% steady power shortfall at the compressors correct rotational speed again correctable with a software fix. In addition, Bell Boeing is developing an inlet barrier system to reduce the power loss from the engine ingesting dust and sand particles to supplement the engines existing centrifugal based particle separators as they can only do so much to improve the quality of air they receive.<ref name="StallFixes"/>
In October 2021, Bell and Rolls-Royce jointly announced that the Bell V-280 Valor powerplant would switch from the General Electric T64 turboshaft used on the prototype to a derivative of the 1107C used on the Osprey which would be named the 1107F. At the same time as increasing power from 5,000 to 7,000 horsepower, the 1107C is a known element in tiltrotor aircraft with its two decades of prior use which lowers sustainment costs and de-risks the project.<ref>Bell Picks Rolls-Royce Engine for V-280 Valor in Army Black Hawk Replacement Contest</ref>
DesignEdit
The V-22's T406 powerplants are housed in wing-tip tilting nacelles, allowing the distinctive flight characteristics of the V-22. For take off and landing the nacelles are directed vertically (90° to fuselage), while for forward flight they are rotated parallel to fuselage. The engine has been considered as a cost-effective upgrade for existing heavylift helicopters such as the CH-47 Chinook and the CH-53.<ref name="RR-Liberty"/>
ApplicationsEdit
- Aurora XV-24 LightningStrike (1107C)<ref name="Engineer20170407">Template:Cite news</ref>
- Bell Boeing V-22 Osprey (1107C Liberty)
- Bell V-280 Valor (1107F)
- US Navy Ship-to-Shore Connector Landing Craft (MT7)
Specifications (T406)Edit
See alsoEdit
Template:Portal Template:Aircontent
ReferencesEdit
Further readingEdit
External linksEdit
- AE 1107C-Liberty at Rolls-Royce site
- AE 1107C-Liberty Fact Sheet
- Template:Cite report
- Template:Cite magazine
Template:Allison aeroengines Template:Rolls-Royce plc aeroengines Template:USAF gas turbine engines