Permanent Magnet thrusters

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Permanent Magnet thrusters Why PM thrusters Gunnar Johnsen, Head of Electrical System R&T 2015 Rolls-Royce plc and/or its subsidiaries The information in this document is the property of Rolls-Royce plc and/or its subsidiaries and may not be copied or communicated to a third party, or used for any purpose other than that for which it is supplied without the express written consent of Rolls-Royce plc and/or its subsidiaries. This information is given in good faith based upon the latest information available to Rolls-Royce plc and/or its subsidiaries, no warranty or representation is given concerning such information, which must not be taken as establishing any contractual or other commitment binding upon Rolls-Royce plc and/or its subsidiaries. Trusted to deliver excellence

Permanent Magnet Thruster development timeline Technology Demonstrator returned to Ulsteinvik Assembly of 1 st commercial PMTT1600, 800kW 1998-2004 2007-2009 2010 2011 2005-2007 2008-2010 2010-2011 Evaluation of technology and development of preliminary design/sketches 50 kw prototype design, build and start-up 50 kw thruster testing (functional and water tank test) Full-scale (800kW) technology demonstrator development Installation on Olympic Octopus Product testing and design qualification Design approval modified design (Central Shaft bearing design) Decision to do quay side testing October 2011

PMazimuth units installed on R/V Gunnerus Commissioning of test rig and test start March 2012 PMTT finished October 2012 Commissioning on Olympic Octopus Jan 2013 2012-2013 2014 2015 R/V Gunnerus PMazimuth Design and review of PMazimuth Pmazimuth FAT tests and delvery PMTT deliveries Pmazimuth Seatrial PMTT sales release at SMM Hamburg September 2012

Why PM Technology for Thrusters. Efficiency Compactness Robustness (Simplicity) Asynchronous induction motor Integrated synchronous permanent magnet machine + Oil filled, geared thruster unit

Why PM Technology for Thrusters? Efficiency Compactness Robustness (Simplicity) Multiple moving parts -Nozzle got 1 moving part (propeller) -Steering gear with improved classic design Pitch system + Mechanical transmission line

Why PM Technology for Thrusters Efficiency Compactness Robustness (Simplicity) >4,6m 3,1m

Why PM Technology for Thrusters Efficiency Compactness Robustness (Simplicity) >4,6m Inside: 1,3M Hull and Nozzle: 3,6m All in 1 room

Noise measurements Olympic Octopus Airborne noise Structure borne noise 4-8 db 6-12 db Noise emitted to sea 5-6 db Measurements conducted by DNV, April 2013

Rolls-Royce proprietary information

PMazimuth, main propulsion demonstrator installed on R/V Gunnerus. Vessel is owned by Norwegian University of Science and Technology Project funding by Rolls-Royce and Norwegian Research Council Propulsion system : 2x500kW, 440V 60Hz Classic diesel electric Length: 31,25m Breath: 9,6m Remove: Rudder with steering gear incl.nozzle with propeller Shaftline Gear Electrical motor Frequency converter Bridge control system Install: Pmazm steering gear Lubrication systems Helicon- control system Frequency Converter HEMOS

Design and inhouse testing 500 kw azimuth thruster driven by a PM motor placed inside the nozzle. Mechanical strength is 1000kW. Nozzle have space for a 1000kW PM motor. Reuse elements from PMTunnel thruster. Helicon-X control system, RR PES Frequency converters. HEMOS data acquisition system, Design and production: 2012 to Nov 2014 FAT. Delivered Seatrail: Nov-Dec- 2014 Dec-14 March-April-15

Control system and frequency converters Helicon-X control system and Rolls-Royce frequency converters, well proven products Rolls-Royce proprietary information

Installation Delivered in transportation and installation frame. Hoisted in place using crane and tackle blocks Rolls-Royce proprietary information

R/V Gunnerus with PMAZM Two PMAZM1900 prototypes installed at R/V Gunnerus Propeller diameter: 1,9 m Speed trials March 27th, 2015

Power vs. speed before / after PMAZM retrofit Comparison of power consumption. The results, when corrected for increased displacement, indicate significant power savings: 8.8 kn ; 10.5 kn ; 11.5 kn ; 13 % Saving 11 % Saving 7 % Saving

PMazm summary Even though the units only have been in operation for some weeks, some of the operational benefits are already clear: l l l l Improved efficiency Low vibration and noise Quick response, (azimuth and rpm) Good manoeuvrability