Goodrich Engine Components Pratt & Whitney Component Solutions Symposium 8/25/10 Bob Proctor Business Development Manager Chris Kuble Business Development Director A Global Leader in Aerospace and Defense One of the largest worldwide aerospace and defense suppliers Broadest portfolio of systems and products in industry 2009 Sales - $6.8 Billion Over 24,000 employees at more than 90 locations worldwide 10 major business divisions Aerospace Industrial Spray Processing Aerospace Engine Components Division Locomotive Industrial Gas Turbine (IGT) Oil Heat Aerospace History of Engine Components December 2006 – Divisional Consolidation Announced Three Goodrich groups combined to create Engine Components • Power Transmissions Systems – 1 facility (drive shafts and couplings) • Turbomachinery Products – 5 facilities (airfoils and rotating components) • Turbine Fuel Technologies – 6 facilities (Fuel nozzles and manifolds) – Delavan Inc. is the legacy name – Aerospace parts manufacturer for over 70 years Fuel Nozzle Customers & Markets OE Customers Markets Aerospace Aerospace Rolls-Royce plc General Electric Aircraft Engine Pratt & Whitney Canada Honeywell Hamilton-Sundstrand Industrial Turbine GE Power Systems Seimens-Westinghouse Rolls-Royce ABB Kawasaki Heavy Industries Large Commercial Turbofan Regional/Business Aviation Military Fighter/Transport/VTOL Auxiliary Power Units Product Support Industrial Turbine Frame Engines Standby Power Aero Derivatives Micro Turbo-Generators Product Support Description of the Fuel Nozzle Business Balance in markets served Aerospace Power Generation Oil Heating Systems Industrial Spray Processing Global leader in several markets Business Turboprops APU’s Military Business Jets Rotocraft Regional Jets Turbine-Powered UAV’s Regional Turboprops Nozzle Products Propulsion Fuel Nozzles Hydro-mechanical Valves APU Nozzles Lubrication system valves & nozzles Integrated Systems Spraybars Manifold Products Fuel Nozzle Product Support Global Presence Regional Offices Atlanta GA Austin TX West Des Moines IA Birmingham UK MRO Operations West Des Moines, Iowa Carroll, Iowa Widnes, England Singapore, SE Asia Aerospace Engine Product Summary PWC PT6A PT6C JT-15D PW118/120/121/ 123/124/127 PW206/207 PW305/306 PW307 PW530 PW535 PW545 PW615 PW901 Rolls-Royce Bristol RTM 322 GNOME (T58) Rolls-Royce Derby Trent 900 Industrial Trent WLE RB 211 ANTLE Hamilton Sundstrand APS500R APS1000 APS2000 APS2100 APS2300 APS3200 APS5000 Rolls-Royce Corporation (Indianapolis) AE 3007 A, C, H, A1, A1E, AX AE 2100 AE 1107/T-406 501/601 570/571 T56 AE 250 M1 Abrams Honeywell International TPE 331-10 131-9A/B TPE 331-14 Model 36 T53 331-350/400 T55 331-500/600 ALF502/LF507 331-200/250 F124 (ITEC 1042) G250 T800 JFS100 HTF 7000 JFS135 AGT1500 JSF190 ATF3 GTCP LT101 RE100 TF40/50 RE220 [GV/GX] RE220 [RJ] GEAE CT7 CF34-10 F404 J79 T58 TF34 T64 T700 Primary MRO facility, West Des Moines Repair/overhaul more than 8,000 fuel nozzles and manifolds per month Total service provider Overhaul and repair Modifications Engineering services Repair development AOG coverage Rotable exchanges Spares sales for many engine types Repair capability PW901 APU nozzle with sheath and tip replaced Fuel Nozzle Functions Functions of a Fuel Nozzle Inject Meter Distribute Insulate Aerate Atomize ~ DISPENSE FUEL Other Functions Allow Manufacture Permit Assembly to Engine Prevent Air and Fuel Leaks Permit Repair Meet Life Factors affecting fuel nozzle MTBR’s Maintenance intervals can be radically different among engine types Range • Several hundred to thousands of hours • Depending on engine and design Why?? Factors affecting fuel nozzle MTBR’s Factors affecting removal intervals: Nozzle type Operating environment of combustor Passage sizes Split between flow rates Manufacturing cost vs. maintenance cost as a design criteria Current designs generally have higher MTBR’s Simplex Pressure Atomizer Advantages Simplest form of atomization. Easier to manage thermal environment due to single circuit design. Spray angle consistent over operating range. Spray Angle typically 30° 70°. Lowest cost. Disadvantages Limited by turndown ratio of engine (max flow / min flow) Presents greater challenge to meet smoke and emissions requirements. Wider spray angles subject to instability. Difficult to product narrow angle with higher FN. Duplex Pressure Atomizer Advantages Global SMD droplet size larger when secondary circuit cuts in. Spray angles consistent over operating range. Provides the best ignition characteristics. Disadvantages Fuel system requires flow divider valve. Small internal fuel passages which increases the propensity of internal carbon. Presents greater challenge to manage thermal environment due to multiple fuel circuit design. Higher cost. Pure Air-blast Nozzle Advantages Only utilizes a single fuel circuit. Large internal fuel passages which reduces the propensity of internal carbon. Longer life than piloted airblast design. Low to moderate cost. Disadvantages Typical FN should be greater than 4.0. Larger SMD droplet sizes at ignition compared to piloted airblast. Tip requires additional heatshielding due to T3 air flowing through nozzle. Piloted Air-blast Nozzle Advantages Achieves the smallest global SMD droplet size compared to all other configurations. Provides the best ignition characteristics. Disadvantages Requires flow divider valve. Small internal fuel passages which increases the propensity of internal carbon. Presents greater challenge to manage thermal environment due to multiple fuel circuit design. Highest overall cost. Product Mix Aerospace Gas Turbine Fuel Injection Simplex Injectors - Pressure Atomizing; Spill Return; Flat Spray; Air Aspirating; Air Assisted Dual Orifice Injectors - Air Aspirating; Air Assisted Piloted Air-blast Injectors Air-blast Injectors - Simplex; Flat Spray; Discrete Jet; Pre-Filming, Passive Purge Vaporizers Summary Engine Components provides wide variety of products and services OEM and full service maintenance provider Provide technical solutions Global support