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MIT Designs Aircraft That Uses 70% Less Fuel Than Conventional Planes

greenrainbow writes "Today a team of researchers at MIT unveiled their design for an airplane that uses 70% less fuel than conventional aircraft. The MIT design comes thanks to a NASA-funded initiative to increase fuel efficiency, lower emissions, and allow planes to take off on shorter runways. The team accomplished all of NASA's set goals with their innovative D-series plane, lovingly referred to as the 'double bubble,' which has thinner, longer wings and a smaller tail, and engine placement at the rear of the plane instead of on the wings."

30 of 459 comments (clear)

  1. hmmm by meerling · · Score: 4, Interesting

    Looks like it's fuselage is also a lifting body.

    1. Re:hmmm by gyrogeerloose · · Score: 4, Interesting

      Looks like it's fuselage is also a lifting body.

      On the larger one, yeah, it does.

      Interestingly, TFA mentions that NASA was also soliciting new designs for a supersonic transport aircraft; given the reluctance of nations to allow those in their airspace and the resulting eventual demise of the Concorde (which, IIRC, never made a profit anyway), one has to wonder why.

      --
      This ain't rocket surgery.
    2. Re:hmmm by ircmaxell · · Score: 4, Interesting

      Well, it's possible to travel supersonic with a minimal or even no sonic boom (I remember someone came out with a design for a boom-less Learjet recently). IF they can do that reliably, perhaps the countries will open up their airspace to it... Or perhaps it's a losing battle. Either way, some good science should result from it (What NASA is ultimately, a science organization. It's not Airbus)...

      --
      If a man isn't willing to take some risk for his opinions, either his opinions are no good or he's no good
    3. Re:hmmm by vtcodger · · Score: 4, Interesting

      ***The faster you go, the less time you spend going.***

      Of course. My understanding is that's why drag related fuel losses only increase with the square of velocity rather than the cube of velocity. Still, given likely future trends in fuel costs, I expect that we're more likely to see zeppelins return than supersonic airliners return.

      --
      You can't see ANYTHING from a car, You've got to get out of the goddamned contraption and walk...Edward Abbey
    4. Re:hmmm by Grishnakh · · Score: 4, Interesting

      Who cares if there's a sonic boom? A large portion of long-distance air travel happens over the Atlantic and Pacific Oceans. As long as a SST plane slows to subsonic speed before crossing over land, which it'll probably need to do anyway because it's preparing to land, there shouldn't be a problem.

      Think about it, most really long flights are going to be trips like LA to Tokyo, LA to Beijing, LA to Sydney, NYC to London, NYC to Paris, etc. The vast majority of the distance is over international waters, and these airports are mostly very close to the water. Obviously, trips over Western Europe will have to be subsonic, but it's really not that far from the Ocean to any airport in Western Europe so the subsonic leg shouldn't be a big deal. Trips over North America can be supersonic, since it's doubtful the American government will care about sonic booms. If they do, I'm sure a few "campaign donations" will fix that....

      Even trips from LA to Western Europe shouldn't be a problem, since most of the journey is over the North Pole IIRC.

    5. Re:hmmm by shermo · · Score: 3, Interesting

      It's my understanding that drag increases as the square of velocity. This leads to fuel consumption per unit of distance increasing linearly.

      Go twice as fast, use twice as much fuel getting there. Your rate of fuel consumption is four times higher, but you spend half the time getting there.

      --
      Insanity: voting in the same two parties over and over again and expecting different results
    6. Re:hmmm by cmiller173 · · Score: 4, Interesting
    7. Re:hmmm by Wyatt+Earp · · Score: 4, Insightful

      The extra distance would also cost fuel, more fuel, more weight, fewer paying passengers, lower profits and now that route isn't viable, more time in the air, more maintenance and less total life on the airframe.

    8. Re:hmmm by Martin+Blank · · Score: 3, Informative

      The FAA has prohibited overland supersonic flight except for explicitly-approved military flights for decades now. Even the military has to get permission when outside of established supersonic corridors, most of which are controlled by the FAA. (Many people are often amazed at how much authority the FAA has over military flights within US borders.)

      NASA has conducted a great deal of research into quieting sonic booms, either by deflecting them upward or by canceling them out. I imagine those will be or have been factored into MIT's proposals.

      --
      You can never go home again... but I guess you can shop there.
    9. Re:hmmm by MechaStreisand · · Score: 3, Informative

      Not exponentially! No! Something that is rising exponentially is rising as 2^x, which is like hitting a brick wall compared to something rising quadratically, which, if your math is right, is how fuel costs would rise with increasing speed. And your math seems right.

      --
      Disclaimer: IANAL. This post is, however, legal advice, and creates an attorney-client relationship.
  2. Intrigued to know more by ICLKennyG · · Score: 3, Insightful

    I wonder how the seating configurations are for these planes. There is no scale provided so you wonder what they are calculating on, is it fuel per mile per passenger? Anything else would be irrelevant.

    1. Re:Intrigued to know more by AnonymousClown · · Score: 5, Insightful
      Seating is usually dictated by the individual airline that buys the planes. Rest assured that all of the US based carriers will cram as many seats in as possible so even a little guy like me - 5' 7" 155lbs - will feel cramped.

      Of course, when the airlines get these, there will be a "green" fee, a "designed by MIT" fee and an "environmental feel good" fee added onto your ticket price along with all the junk fees.

      --
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      July 4, 1776 - September 11, 2001

    2. Re:Intrigued to know more by Chris+Burke · · Score: 4, Informative

      There is no scale provided so you wonder what they are calculating on, is it fuel per mile per passenger? Anything else would be irrelevant.

      The two designs carry the exact same number of passengers as the planes they are hypothetically replacing, the 180-passenger 737 and 350-passenger 777, so there's no difference in this case between miles per gallon and passenger-miles per gallon. :)

      --

      The enemies of Democracy are
  3. Slower than current aircraft by sunderland56 · · Score: 5, Interesting

    One way they save fuel: flying slower than current aircraft. First, will customers accept that? And second, why not just fly current 737s a bit slower right now, to save on fuel?

    1. Re:Slower than current aircraft by sznupi · · Score: 5, Informative

      While I'm sure you can devise a design which, as part of greater fuel economy, flies slower (turboprops might be just that...) - it won't really work for existing aircraft, like mentioned by you 737s. Airlines take care to fly them at optimal speed, not the greatest speed; optimal for fuel economy.

      For example Rynair (which cares greatly about lowering costs...), some time ago, changed the guidalines for cruising speed by...2 or 3 km/h. Accidentally in this case it was lowering it, but might have been just as well an increase; what works best for given airplane / engines / routes / weight combo (didn't stop local journalists from proclaiming "Ryanair will fly slower to save fuel", which was technically correct, but....)

      --
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    2. Re:Slower than current aircraft by h4rr4r · · Score: 5, Interesting

      They sure will. If you can give me a 30% reduction in ticket price but a 10 hour flight instead of an 8 hour one across the atlantic that would be fine by me.

      Provided it is a nice European carrier like Lufthansa, who actually has free beer and back of the seat entertainment systems. Unlike American carriers who charge for beer and have 70s entertainment systems in the aircraft.

    3. Re:Slower than current aircraft by schon · · Score: 4, Informative

      One way they save fuel: flying slower than current aircraft.

      No. While they do fly slightly (10%) slower than existing aircraft, they do that to mitigate engine stress.

      will customers accept that?

      Well, they seem to "accept" waiting 2-3 hours in security lines, so I'm guesing yes.

      why not just fly current 737s a bit slower right now, to save on fuel?

      You honestly believe that flying a 737 10% slower will reduce fuel consumption by 50%? I can tell you that if an airline reduce their costs anywhere close to that much, they'd do it in a heartbeat.

    4. Re:Slower than current aircraft by LWATCDR · · Score: 4, Interesting

      Actually it is a lot more complex than that.
      The higher you fly the less fuel you burn but the higher the stall speed as well as the speed that offers you the best lift to drag.
      Also engines have an optimum power setting as well.
      Also the higher you fly the more fuel you burn in climb so there is a function of distance, altitude, and airspeed where the plane gets the best efficiency.
      The concept D looks like it is using the classic trick of increasing the aspect ratio of the wing. That increases climb rate and improves the lift to drag at a given speed.
      My guess by looking at the pictures they are using engines that have a much lower disk loading than current turbofans and a wing that is optimized for cruise at a lowers speed.

      The problem will be the increase in weight. When you increase the aspect ratio you increase the weight of the wing. If you decrease the disk loading of a turbo fan the weight goes up. It will be interesting to see if all the lines cross where they think they will.

      --
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  4. Answered my own question by Bruiser80 · · Score: 3, Interesting

    NASA's link says the 777 design flies 10% slower. A pretty good return!

    --
    Arguing with an engineer is like wrestling a pig in the mud. After a while, you realize the engineer enjoys it.
  5. Wing length is a Really Big Deal by PPalmgren · · Score: 4, Interesting

    I remember watching a documentary on the new Airbus plane. There are regulations on wing length, and that plane *has* to use the perpendicular tips at the end of its wings to help with lift, or its wings would be too long. If you require longer wings per pound, you will fit less passengers per plane to fit in regulation. They will have to find a way to collapse the wings without adding significant weight or complications to make this practical for larger planes. That is a very big hurdle, maybe they should focus on that next.

    I can't remember why, but I remember them stating that the wing length regulations had very good reasons behind them (logistics of current airports being a major one if I recall). I don't think changing the regulations would be practical if that was the case.

    1. Re:Wing length is a Really Big Deal by pavon · · Score: 4, Informative

      According to the article the proposed 737 replacement has standard wing length and is suitable for existing airports.

  6. Re:So Lets See, by MBGMorden · · Score: 3, Informative

    Having a viable prototype design that's gone through simulations and the like is a lot more than artists renderings. What the hell do you think they do to make an airplane? Take some steel, rivets, and aluminum out to the hangar and just see where things end up?

    --
    "People who think they know everything are very annoying to those of us who do."-Mark Twain
  7. Re:So Lets See, by fuzzyfuzzyfungus · · Score: 4, Funny

    Well, that and a bottle of jack daniel's, yeah...

  8. Re:How to pressurize it? by ThreeGigs · · Score: 3, Interesting

    It's actually two cylindical (or semi-cylindrical) cabins joined together lengthwise, with a stressed interior partition framework. Kinda like a number 8 laying on its side. Pressurization isn't difficult in that case, and the interior stressed partition can be a latticework. It's not a new idea, although it's never been done for reasons of practicality, just a lot simpler to make the body a long tapered tube and be done.

  9. Both of TFA's linked sadly lacking in details by Larson2042 · · Score: 5, Interesting

    I'm disappointed in both of the linked articles. Some real substance about the design would have been nice, but as it is, I'm left with a lot of questions:
    -70% less fuel? How much of that is aerodynamic savings and how much of that is engine efficiency savings?
    -Did they do any wind tunnel testing of their model? How close were their CFD and tunnel test results?
    -Are they using engines based closely off existing ones, or are they projecting fuel savings 25 years into the future (the 2035 time frame from the article)?
    -What sort of structural weight-saving advances are they assuming, or projecting from?
    -So they made the tail smaller, what makes up for the reduction in control authority there?
    -Plus other more detailed questions based on the answers to those questions. Would it have been so hard for MIT to link a design document pdf or something? I guess not being a public university, they don't have to if they don't want to. Too bad.

  10. Re:So Lets See, by EdZ · · Score: 3, Funny

    It's not impossible. I used to bullseye flow dynamic calculations on my Ti-15 back home, they're not much bigger than two OOM.

  11. Type D ment to work with existing airports by buback · · Score: 4, Informative

    The type D is specifically designed to work with existing airports without drastically changing the terminals.

    The type H, however, would require changes to current airports. The article says that these designs are planed for a 2035 deployment, though, so plenty of time to make the requisite changes, if the airlines so chose.

  12. Re:Great... insurance by dltaylor · · Score: 4, Interesting

    It took FOREVER to get a composite commercial aircraft into production because the insurance companies had no data on hull integrity to do the underwriting. As a result, the proposed premiums were based on utter disaster.

    It may have been the Beech Starship http://www.wingsoverkansas.com/legacy/article.asp?id=775 that provided some useful data. Although a turboprop, it is pressurized, and the more-frequent pressure cycling of a corporate hauler may have given them some idea that composites aren't highly more likely than conventional aluminum hulls to become convertibles (Aloha 737) in flight.

    If the US gov't really wanted to help advance the aircraft industry, they'd create an insurance agency for new designs and materials.

  13. Hmmm... slower than a 737 by DieByWire · · Score: 3, Funny

    the design mitigates some of the drawbacks of the BLI technique by traveling about 10 percent slower than a 737.

    I wonder if they accounted for the added weight of beefing up the trailing edge of the wing to withstand bird strikes.

    --
    Never shake hands with a man you meet in a fertility clinic.
  14. Move along... by Evtim · · Score: 3, Interesting

    You know, people, it is perhaps shameful to admit in front of this audience but despite working at the cutting edge of technology I only shrug at news like this one. Instead of all the exiting engineering/scientific thoughts that most of you exhibited and made the discussion interesting the only thing that crossed my mind was something like:

    "So, we are going to save 70% of the fuel. What would happen in such "vacuum" Well, we will just build 70% more plains, fly even more people around, cheaper perhaps so the "gain" in efficiency will be quickly drowned by the increased volume of planes and passengers. Move along, nothing to see here..."

    I don't want to rain on anybody's parade but every time when some new technological development frees us time, it is immediately filled with more work, not more recreation or hobbies or family life. When it comes to food and water it is even worst. Just consider the "green revolution" from the 70's. Population pressure due to the baby boom after the war. Solution - industrial agriculture which completely kills the taste of food (especially fruits and vegetables) but its efficient and easier to transport and preserve. When it was all over , did we wipe out the noble sweat and sat down to enjoy the fruits of our ingenuity (pun intended)?

    No, because the population pressure was already pushing us again. We will never catch up with this. And as every scientist will tell you , every next step will require more energy and more effort to squeeze maximum yield from minimum volume. Asymptotic approach to use the proper term. Like trying to accelerate a mass to the speed of light. As long as we do not stop the geometrical progression of our multiplication we will never be able (most of us) to enjoy what the progress is all about - giving MORE time for ourselves and our personal development and personal life. Giving MORE and higher quality goods and services per person (population flat, but efficiency increases).

    Globally as humans we experience what we people in the west experience with the constant inflation - you have to run ever harder just to stand still. Miss one year's promotion or a raise and your buying power goes down. The effect of missing one year only is accumulative like compound interest. I am sick to the teeth that I have to run like a mouse on an endless tread just to stand still. Just to exists. And being told all the time how good I have it.