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Introduction
April 6, 2015, c. Leeham Co. The next 15 years may well be the last new airplane programs of major airliners that look like today’s tube-and-wing aircraft because demands for new efficiency will require go beyond what engines can do within a reasonable size, says Alan Epstein, VP of technology and environment at Pratt & Whitney.
Major changes to the airframe will have to provide added efficiency gains in combination with new and evolving technology from today’s engines.
The next new airplane, the so-called Middle of the Market (MOM) aircraft, will look like today’s airplanes. The next plane after that, the replacements for the Airbus A320 and Boeing 737 families, will probably be the last iterations of the planes of today. After that, new designs are likely to emerge, Epstein says.
Summary
Discussion
Getting more efficiency from engines means the use of more advance materials, evolving and new technology but larger fans have traditionally been a key to gains. The 81 inch fan on PW’s Geared Turbo Fan on the A320neo is pushing the engine size on the single-aisle airplane in traditional configuration, Epstein says.
“It looks like you can get one more iteration at…taxi weight limits and longer landing gear. You could go for four engines,” Epstein says—an idea that is counter-intuitive to trends since the introduction of the Boeing 757 for high-performance, 3,500nm-4,000nm aircraft, intended to replace the three-engine, mid-range Boeing 727-200A.
(Lest Airbus and its supporters weigh in on the introduction of the A300 in 1974, we’re talking about single-aisle airplanes at this point.)
The idea of a four-engine single-aisle aircraft raises immediate questions about fuel burn and maintenance costs of four vs two. While our own analysis, with respect to the Airbus A380, concludes the four-engine maintenance cost perception is overblown, Epstein points out that if an airplane needs 80,000 lbs of thrust (for example), this may be achieved with two 40k or four 20k engines. Maintenance costs for four engines can be achieved for the price of two, he says.
Different fuselage shapes can provide dramatic gains in efficiency, Epstein says. A NASA concept of a “D” with the flat side on top, with engines mounted on the flat side, cuts 6%-10% in fuel usage from the fuselage alone because it “cancels the wake” generated by today’s aircraft.
Airbus has been quite public showing futuristic designs, Boeing less so. While Boeing liked to position the 787 as revolutionary when the design was first revealed, it was in fact more evolutionary—a major evolution, to be sure, but still an evolution. The concepts on the drawing boards will be the first revolutionary advance since the jump from pistons to jets and the creation of the Boeing 747. If Epstein is right, we could see the launch of the first of these within this generation.
If the wake comes from the shape of the nose, I suppose it makes sense to try to direct all oncoming air over or under the aircraft and not to the sides. Basically the energy used to displace the air needs to be recaptured for lift, going sideways is a waste.
“if an airplane needs 80,000 lbs of thrust (for example), this may be achieved with two 40k or four 20k engines”
I thought it was if an airplane needs 80K of thrust on take-off then it needed two 80K engines or four 27K engines, to total 80K if one goes out. 160K total for two, vs. 107 total for four.
Two engine airliners need 1.5 the total thrust of four engine airliners. Theoretically this should save engine weight on four engine airliners.
Its been done with the BAE-146.
Can a suitably qualified engineer please answer a question that I have been mulling over for a while now – in a quad, would there be any benefit to say, feathering the outboard engines and running the inboards at a higher thrust?
Let’s say that you use all four for takeoff and climb to altitude, assume that the four engines allows you to gain cruising altitude quickly so you can save fuel earlier. When cruising at altitude, you effectively only need around 40% of your available thrust, so if your reduce thrust (but do not switch them off) of #1 and #4, you can then use #2 and #3 to maintain speed.
Would this save any fuel or possibly maintenance?