The correct answer is the V-22 aircraft does not need anti torques devices. Please continue to read and I will explain it more and why.
This aircraft has two Rolls-Royce AE-1107C free turbine turboshaft engines, modular design, 14 stage axial compressor, annular combustor, 2 stage gas generator turbine, 2 stage power turbine, bottom mounted power section accessory gearbox, two single channel full authority digital electronic controls.
The engines are Type Certificate Data Sheet and the TCDS is NO. E00008CH by Rolls-Royce Indianapolis, Indiana. When the engines are installed they are considered public use, as is the aircraft. The AE 1107C model is intended for a US military application. Current US law does not require that public use or military aircraft/engines be operated or maintained in accordance with the FAA approved type design.
The AE 1107C model is intended for use only in a dual engine application 6,150 shp (4,586 kW) each.
Both engines rotate the same direction on the Bell V-22 cross-coupled transmissions allow either engine, separately or together, to power the rotors. The rotors turn different directions canceling out the adverse torque effect. This is why you do not need anti torque pedals or other devices.
On the instrument panel there is a torque meter that registers engine torque for each engine. A black box is install, which allows the engines to talk back and forth thru an electronic coax cable when engine torque changes and adds more fuel to balance the torque or RMP as required.
As a side note Rolls-Royce Oakland Engine Repair Station overhauls all the AE1107 engines when required.
Reference:
http://www.bellhelicopter.com/en/aircraft/military/bellV-22.cfm
http://www.boeing.com/rotorcraft/military/v22/docs/V-22_overview.pdf
http://www.faa.gov