N61-0952-000-000:Layout 1.qxd
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N61-0952-000-000:Layout 1.qxd
N61-0952-000-000:Layout 1 02/02/2010 3:33 PM Page 1 HTS900 Turboshaft Engine A Next Generation High Performance Engine for the Bell 407 Honeywell Aerospace 1944 East Sky Harbor Circle Phoenix, AZ 85034 800-601-3099 International: 602-365-3099 www.honeywell.com N61-0952-000-000 January 2010 © 2010 Honeywell International Inc. N61-0952-000-000:Layout 1 02/02/2010 3:33 PM Page 3 Honeywell HTS900 Engine Enhanced engine performance, reliability, and efficiency provides increased payload and High / Hot capabilities for the Bell 407 HTS900 SHP/SFC Performance Ratings More Payload Capabilities More Power More Efficient The HTS900 engine is the latest engine Utilizing state of the art technology, The next generation technology developed Rating Sea Level ISA 4K / 95°F to join the Honeywell family of helicopter the HTS900 features a dual centrifugal by Honeywell results in increased engine Takeoff 1,021 / 0.526 766 / 0.545 engines dating back to 1950. The HTS900 compressor, cooled turbine blades and power while reducing specific fuel incorporates numerous next generation nozzles and a dual channel FADEC all of consumption. Lower fuel consumption technologies developed by Honeywell. which results in an output of 1,021 shaft increases both operational savings and The HTS900’s increased shaft horsepower horsepower; a 22% improvement in power the earning potential of the helicopter. output improves the payload capability output at high/hot conditions over the of the helicopter by 40% at 12,000 feet; incumbent engine while burning less fuel Max. Cont. 907 / 0.525 668 / 0.554 (Uninstalled, minimum engine, 6,317 rpm output speed – information, not guaranteed) resulting in increased helicopter capabilities Feature HTS900-2 Reduces Takeoff Specific Fuel Consumption and occupying less cubic space. Max Cont Power 12,000 Feet 35% Increase 8,000 Feet 16% Increase 4,000 Feet 1000 HTS900 Incumbent Engine* 0.55 Range Capability 0.50 HTS900 Power to Weight Ratio Takeoff Sea Level, ISA 22% Average Power Increase Takeoff 4K / 95°F Annual Fuel Cost Engine Size HTS900-2 Reduces MCP Specific Fuel Consumption 0.65 700 10% Reduction Transmission Limit (675 SHP) 600 500 HTS900 0.45 Takeoff Sea Level, ISA Takeoff 4K / 95°F Takeoff 6K / 95°F (*Based on public website data) MCP Sea Level, ISA Increased Value Decreased Value Incumbent Engine* 0.55 0.50 Payload Capability Mission Capability 0.60 Minimum Engine 6,317 rpm Output 400 Useful Load Carrying Comparison (Based on HOGE Hover at ISA+20C) SFC Incumbent Engine* 800 11% Increase 2,000 Feet 0.60 0.45 900 SFC lbs/hr/SHP Production 407 Shaft Horsepower (Minimum Engine, 6,317 rpm Output) 1100 SFC lbs/hr/SHP 8% Reduction HTS900 Engine Performance Comparision 40% Increase Takeoff Power 0.65 over a wider operating spectrum. Eagle 407HP with HTS900 Engine Value HTS900 Incumbent MCP 4K / 95ºF (*Based on public website data) HTS900 Benefits • Increased: – High/Hot capability – Payload capability – Mission capability – Safety – Mission range • Reduced fuel consumption