Composites, titanium and advanced aluminium-alloys are applied extensively throughout the A350 XWB’s fuselage, with their use tailored to the best characteristics of these materials. (1) The 53 per cent of composites utilised in the fuselage and wing reduces the need for fatigue-related inspections required on more traditional aluminium jetliners. (2) The composites and titanium also diminish the requirement for corrosion-related maintenance checks on the A350 XWB.
These two factors reduce the new aircraft’s overall fatigue and corrosion maintenance tasks by 60 per cent.
INNOVATIVE FUSELAGE DESIGN
Construction of the A350 XWB’s fuselage sections is made by assembling four-skin panel sections – two lateral side panels, one at the crown, and another for the belly – onto carbon fibre frames. In contrast to other composite aircraft, this construction technique allows for a tailoring of composite layup thickness to each panel, based on calculations of local fuselage stresses and loads.
SIMPLE PROVEN SYSTEMS
The A350 XWB’s onboard systems are designed for maximum reliability, operability and simplicity. They are optimised for two primary criteria: (1) Robustness for ensured reliability and operability; (2) Simplicity for reduced maintenance time and cost.
INFLUENCE OF THE AIRBUS FLAGSHIP -THE A380
Many of these systems are derived from Airbus’ A380, providing the advantages of operational experience with this 21st century flagship aircraft and ensuring a high level of maturity at the A350’s XWB entry into service.
(1) Solid-state power control technology on the A350 XWB eliminates the need for individual circuit breakers in the cockpit, cabin and electronics bay – providing a modern method of power control management throughout the aircraft.
(2) The application of variable frequency generators, which were first introduced with the A380, provides more power with less weight and lower maintenance costs, along with increased reliability and time-between-removals.
(3) Another A380-proven concept is the use of two hydraulic circuits (instead of three on other jetliners), with redundancy provided by a dual-channel electro-hydraulic backup system. In addition, A350 XWB’s hydraulics will be operated at the higher pressure level of 5,000 psi., which also is used on the A380. This increased operating pressure reduces the size of pipes, actuators and other system components while also facilitating the overall access – leading to improved reliability and maintainability, as well as reducing weight and increasing cost savings.
The A350 XWB will be a faster, more efficient and quieter aircraft as the result of its advanced wing design – which combines aerodynamic enhancements already validated on the A380 with further improvements developed by Airbus engineers.
(1) Built primarily from carbon composite materials, the wing is optimised through extensive use of computational fluid dynamics and wind tunnel testing for a fast cruise speed of Mach 0.85. This reduces trip times, improves overall efficiency, and extends the aircraft’s range.
(2) Both scaling & tailoring are permitted: a) Scaling. All three A350 XWB family members share the same wing planform – with a 64.7-metre wingspan, a total area of 442 sq. metres, and high swept leading edge. b)Tailored: In addition the internal wing structure will be scaled to meet the specific requirements of each aircraft variant.
(3) Innovative concepts applied to the A350 XWB wing’s high-lift devices will reduce noise and drag while also improving the aircraft’s low-speed performance. NB. One of these innovations is the stream-wise deployment of trailing-edge flaps. On a traditional swept-wing jetliner, the outboard flaps extend at an angle to the airflow. For the A350 XWB, flap deployment is along the direction of flight – resulting in better lift efficiency and improved low-speed performance, while reducing aerodynamic-generated noise.
(4) Other A350 XWB wing enhancements include;
-4a. the adoption of a drop-hinge mechanism to improve the flap’s deployment kinetics, along with
-4b. the introduction of a downwards movement for the upper wing spoilers to fill the gaps that occur when flaps are extended.
-4c. In addition, the A350 XWB’s flight computer will perform in-flight trimming of the inboard and outboard flaps, creating a variable camber wing that adapts to different flight conditions.
The first striking feature is the sheer scale of the machine - the diameter of the set of fan blades at the front of the engine is 118 inches (299cm), the largest ever made by the British company and roomy enough to accommodate the fuselage of a Concorde.
The blades themselves, made of titanium, are hollow and strengthened inside by a microscopically small grid construction. GE has opted for fan blades made of composite materials.
The size of the fan enables the engine to suck in enough air to fill a squash court every second, and then squeeze it to the size of a fridge-freezer - what's known as a "compression ratio" of 50 to 1, the highest pressure Rolls-Royce has yet attained.
The larger the flow of air into the engine, and the greater the potential compression, the better the efficiency of the whole process.
When the mix of fuel and air is ignited, the resulting gas reaches an extraordinary temperature of 2,200C - a higher level than has been achieved before - which is meant to maximise the output of each drop of fuel.
The searing heat of 2,200C is in fact 700C hotter than the melting point of the components in the combustion chamber - including the turbine blades that are driven by this fast-expanding gas.
So each blade is drilled with a network of 300 tiny holes about the size of a human hair. This allows cooling air to flow in a thin film over the turbines' surface and act as a form of insulation.
To withstand this exceptional heat - and the massive pressures involved - the 68 turbine blades are made of a nickel-based alloy and are grown in a single crystal to avoid the risk of any internal fissures becoming sources of weakness.
The result is that each blade, driven by the expanding gases, generates as much power as a Formula One car, spinning an internal shaft that drives the massive fan blades at the engine's front.
THE GOOD NEWS & THE BAD
THE GOOD
On average, aircraft engines have become about 1% more fuel-efficient every year for the past two decades.
The claims by Rolls Royce will inevitably be followed by similar assertions by GE when its next engines are unveiled.
Airlines facing rising fuel prices are desperate to reduce costs, and the aviation industry as a whole is also under pressure to minimize its carbon emissions.
THE BAD
But as the latest generations of engines become more efficient, any reductions in greenhouse gases are outweighed by the global growth in air traffic, especially in Asia.
Dr Peter Hollingsworth, lecturer in aerospace engineering at Manchester University, said that basic physics meant that there were likely to be limits to how much more efficiency could be extracted from existing designs.
"It's a real challenge. With aviation growing at the rate it's growing, there's not a whole lot you can do. You can do the 1-2% average so over a number of years you get 20% but even that's a real challenge.
"Now that engines are a lot more efficient, a 20% improvement isn't worth as much as it was, so you're always working with diminishing returns and, at the same time, aviation is growing."
SUS. DEV - THE FUTURE
The aviation industry has set itself a target of a 50% reduction in carbon emissions by 2050 compared with 2005 levels - and there's a recognition that that will only be achievable with a revolutionary shift in designs.
Among the ideas being considered are engines that are embedded within the wings and contra-rotating propellers.
Alan Newby, chief engineer for advanced projects at Rolls-Royce, said: "Ultimately, if we're going to make these radical changes then the aircraft will have to starting looking different.
The Trent XWB will be created by using advanced manufacturing techniques to develop a lighter, more capable and efficient engine to meet tomorrow’s operational needs.