時(shí)間：2011-10-07 12:02來源：藍(lán)天飛行翻譯 作者：航空 點(diǎn)擊：次
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Advanced Flight Controls The advanced flight controls of the G650 ensure consistent handling qualities for a more comfortable ride as well as flight envelope protection for improved safety. With a three-axis, fly-by-wire system for outstanding safety, redundancy and maintainability as well as a builtin backup flight control system, the G650 will be one of the most advanced and safest business aircraft flying. ENGINES Two Rolls-Royce BR725 engines, each with up to 16,100 pounds (71.6 kN) of thrust, power the G650. Utilizing the latest, swept fan technology with a high bypass ratio, these advanced engines will offer better fuel efficiency than ever before. The BR725 will also be more environmentally friendly with lower emissions and quieter noise levels – better than the latest State 4 noise limits. Another advantage is the 10,000-hour time between overhaul (TBO) with no mid-life inspection required. This will ultimately help to lower operating costs and improve the availability of your aircraft. Plane Connect ™ This smart technology automatically transmits information from your aircraft to maintenance operations on the ground – including Gulfstream’s Technical Operations center, if desired. By providing information while the G650 is still in flight, PlaneConnect enables speedy resolution of any maintenance issues that may arise. Performance faster and farther The G650 will fly faster and farther than any other purpose-built business jet flying today. The world’s most remote destinations lie well within its nonstop range, and worldwide city pairs are never more than a single refueling stop away. With a maximum operating speed of Mach 0.925, it will be the fastest civil aircraft in the world, providing greater time savings over any other business jet flying today. *NBAA IFR theoretical range. Actual range will be affected by ATC routing, operating speed, weather, outfitting options and other factors. **Stated weights are based on theoretical standard outfitting configurations. Actual weights will be affected by outfitting options and other factors. ***Theoretical mission analysis departing at maximum takeoff weight with 18 passengers, Mach 0.85 cruise speed, ISA day conditions, 85% annual winds and landing with a minimum of NBAA IFR fuel reserves. Actual performance will be affected by ATC routing, operating speed, weather, outfitting options and other factors. |
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