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Aircraft must consume fuel to supply the energy needed to move the vehicles and their passengers. Fuel economy is a measure of how much fuel an aircraft needs to operate, and can be expressed in several ways, for example by the liters of fuel consumed per passenger per kilometer. Aerodynamic drag, which exerts a force on the aircraft in the opposite direction from the velocity, is a principal determinant of energy consumption in aircraft because they operate at such high speeds.
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Factors in aircraft fuel economy
Each model of aircraft has a maximum range speed for a given total load (fuel plus payload), which is the speed at which it is most fuel efficient. Flying slower or faster than this optimum speed increases fuel consumption per mile flown. There is an optimum speed for efficiency because the component of drag resulting from airframe skin friction against the air increases at a square function of air speed, but the drag resulting from generating lift decreases with air speed. (These are technically called parasitic drag and induced drag, respectively.) The desirability of a low maximum range speed to reduce environmental and climate impacts is at odds in aircraft design with the benefit from the revenue generated by making the design speed higher thereby increasing the passenger miles flown per day.
Aircraft weight is also a factor in fuel economy, because more lift-generating drag (induced drag) results as weight increases. If the airframe weight is reduced, engines that are smaller and lighter can be used, and for a given range the fuel capacity can be reduced. Thus some weight savings can be compounded for an increase in fuel efficiency. A rule-of-thumb being that a 1% weight reduction corresponds to around a 0.75% reduction in fuel consumption.
Flight altitude affects engine efficiency. Jet-engine efficiency increases with altitude up to the tropopause, the temperature minimum of the atmosphere; at lower temperatures, the engine efficiency is higher.[1] Jet engine efficiency is also increased at high speeds, but above about Mach 0.85 the aerodynamic drag on the airframe overwhelms this effect.
Above that speed, shockwaves begin to form that greatly increase drag. For supersonic flight (Mach 1.0 or higher), fuel consumption is increased tremendously.
Changes in commercial aircraft fuel economy since the 1950s
Modern jet aircraft have twice the fuel efficiency of the earliest jet airliners. Late 1950s piston airliners like the Lockheed L-1049 Super Constellation and DC-7 were 1% to 28% more energy intensive than 1990s jet airliners which cruise 40 to 80% faster. The early jet airliners were designed at a time when air crew labor costs were higher relative to fuel costs than today. Despite the high fuel consumption, because fuel was inexpensive in that era the higher speed resulted in favorable economical returns since crew costs and amortization of capital investment in the aircraft could be spread over more seat miles flown per day.
Today's turboprop airliners have better fuel efficiency than current jet airliners, in part because of their lower cruising speed and propellers that are more efficient than those of the 1950s-era piston-powered airlines. Among major airlines, those with turboprop equipped regional carrier subsidiaries typically rank high in overall fleet fuel efficiency. For example, although Alaska Airlines scored at the top of a 2011-2012 fuel efficiency ranking, if its regional carrier—turbo-prop equipped Horizon Air—were dropped from the consideration, the airline's ranking would be lower.
Jet aircraft efficiency
Jet aircraft efficiency is improving: Between 1960 and 2000 there was a 55% overall fuel efficiency gain (if one were to consider the Boeing 707 as the base case). Most of the improvements in efficiency were gained in the first decade when jet craft first came into widespread commercial use. Between 1971 and 1998 the fleet-average annual improvement per available seat-kilometre was estimated at 2.4%. Nonetheless, from the 1960s to the present total fleet emissions of the greenhouse gas carbon dioxide have outpaced efficiency gains, due to growth in the air travel market.
Concorde the supersonic transport managed about 17 passenger-miles to the Imperial gallon, which is 16.7 L/100 km per passenger; similar to a business jet, but much worse than a subsonic turbofan aircraft. Airbus states a fuel rate consumption of their A380 at less than 3 L/100 km per passenger (78 passenger-miles per US gallon), however this is for an unspecified number and configuration of seats. The maximum configuration is 850 economy passengers, but with a typical 525-seat multi-class configuration the fuel consumption is "comparable to that of a B747-400 ER and even about 15% worse than a B777-300ER on a passenger-mile basis."
Weight effect
The 84t maximum payload of a modern Airbus A380 represents 14.6% of its 575t maximum take-off weight. There remains considerable room for future improvements in fuel efficiency. The weight of an aircraft can be reduced by using light-weight materials such as titanium, carbon fiber and other composite plastics. Expensive materials may be used, if the reduction of mass justifies the price of materials through improved fuel efficiency. The improvements achieved in fuel efficiency by mass reduction, reduce the amount of fuel an aircraft must carry. This further reduces the mass of the aircraft, and therefore provides further gains in fuel efficiency. For example, the Airbus A380 design includes multiple light-weight materials. The Boeing 787 Dreamliner was the first major commercial airplane to have a composite fuselage, composite wings, and use composites in most other airframe components.
Very long non-stop flights suffer from the weight penalty of the large quantity of fuel required, limiting the number of available seats to compensate. For such flights, the critical fiscal factor is the quantity of fuel burnt per seat-nautical mile. For these reasons the world's longest commercial flights were cancelled circa 2013. An example is Singapore Air's former New York to Singapore flight, which could carry only 100 passengers (all business class) on the 10,300 mile flight. According to an industry analyst, "It [was] pretty much a fuel tanker in the air."
Aerodynamics
Airbus has showcased wingtip devices (sharklets or winglets) that can achieve 3.5 percent reduction in fuel consumption. There are wingtip devices on the Airbus A380. Further developed Minix winglets have been said to offer 6 percent reduction in fuel consumption. Winglets at the tip of an aircraft wing, can be retrofitted to any airplane, and smooths out the wing-tip vortex, reducing the aircraft's wing drag.
NASA and Boeing are conducting tests on a 500 lb (230 kg) "blended wing" aircraft. This design provides greater fuel efficiency, since the whole craft produces lift, not just the wings. The blended wing body (BWB) concept offers advantages in structural, aerodynamic and operating efficiencies over today's more conventional fuselage-and-wing designs. These features translate into greater range, fuel economy, reliability and life cycle savings, as well as lower manufacturing costs. NASA has created a cruise efficient STOL (CESTOL) concept.
Fraunhofer Institute for Manufacturing Engineering and Applied Materials Research (IFAM) have researched a shark skin imitating paint that would reduce drag through a riblet effect. Aircraft is a major potential application for new technologies such as aluminium metal foam and nanotechnology such as the shark skin imitating paint.
Multiple concepts are projected to reduce fuel consumption:
Fuel consumption factors
To save fuel, Simon Weselby presented the following measures while flying, in his example of an A330 flying 2,500 nautical miles (4,600 km) like Bangkok-Tokyo:
Also operational procedures can save fuel:
Maintenance saves fuel as well:
Propellers versus jets
Propfans are a more fuel efficient technology than jets or turboprops, but turboprops have an optimum speed below about 450 mph (700 km/h). This speed is less than used with jets by major airlines today. However, the decrease in speed reduces drag. With the current high price for jet fuel and the emphasis on engine/airframe efficiency to reduce emissions, there is renewed interest in the propfan concept for jetliners that might come into service beyond the Boeing 787 and Airbus A350XWB. For instance, Airbus has patented aircraft designs with twin rear-mounted counter-rotating propfans. NASA has conducted an Advanced Turboprop Project (ATP), where they researched a variable pitch propfan that produced less noise and achieved high speeds.
For private aircraft in general aviation, the current record is 37 km/kg fuel or 3.7 L/100 km in a Monnett Sonerai.
Related to fuel efficiency is the impact of aviation emissions on climate.
Range
For very long haul flights, the airplane is heavier to transport additional fuel, leading to a higher fuel consumption. Above a certain distance, it becomes more fuel efficient to make a halfway stop to refuel even if it leads to an additional less efficient descent and climb. For example, for a Boeing 777-300 the tipping point is at 3,000 nautical miles (5,600 km) : it is more fuel efficient to make a non-stop flight below this distance and to make a stop above.
Airline fuel efficiency
Fuel economy in air transport comes from aircraft fuel efficiency combined with airlines efficiency : seating configuration, passenger load factor and air cargo. For instance, over the transatlantic route, the most active intercontinental market, in 2014 the average fuel consumption was 32 pax-km per L - 3.13 litres per 100 kilometres (75 mpg‑US) per passenger. The most fuel efficient airline was Norwegian Air Shuttle with 40 pax-km/L - 2.5 litres per 100 kilometres (94 mpg‑US) per passenger, thanks to its fuel efficient Boeing 787-8, a high 86% passenger load factor and a high density of 1.18 seat/m² due to a low 11% premium seating. On the other side, the least efficient was British Airways at 27 pax-km/L - 3.7 litres per 100 kilometres (64 mpg‑US) per passenger, using fuel inefficient Boeing 747-400s with a low density of 0.79 seat/m² due to a high 24% premium seating, in spite of a high 83% load factor.
Research projects such as Boeing's ecoDemonstrator program have sought to identify ways of improving the fuel economy of commercial aircraft operations. The U.S. government has encouraged such research through grant programs, including the FAA's Continuous Lower Energy, Emissions and Noise (CLEEN) program, and NASA's Environmentally Responsible Aviation (ERA) Project.
2,160–3,000 nautical miles (4,000–5,560 km)
3,000 nautical miles (5,600 km) is typically transatlantic, e.g. New York JFK - London-Heathrow
5,000–7,600 nautical miles (9,300–14,100 km)
6,000 nautical miles (11,000 km) is typically transpacific, e.g. Hong kong international - San Francisco Intl
For comparison, a Volvo Buses 9700 averages 0.41 litres per 100 kilometres (570 mpg‑US) per seat for 63 seats. In highway travel an average auto has the potential for 1.61 litres per 100 kilometres (146 mpg‑US) per seat (assuming 4 seats) and for a 5-seat 2014 Toyota Prius, 0.98 litres per 100 kilometres (240 mpg‑US). While this shows the capabilities of the vehicles, the load factors (percentage of seats occupied) may differ between personal use (commonly just the driver in the car) and societal averages for long-distance auto use, and among those of particular airlines.