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Practical electric ultralight

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Electric powered flight is moving ahead, now practical ultralights are here. Electric UAV's are a real near future technology, and if advances in energy storage technology, fuel cells or something else can approach the energy density of hydrocarbon fuels, then practical electric flight will take off:

http://www.wired.com/autopia/2009/07/espyder/

Dream Flying On Electric Wings
By Jason Paur  July 31, 2009  |  2:07 pm  |  Categories: Air Travel, EVs and Hybrids


OSHKOSH, Wisconsin — It’s nice to read about something, but seeing it in person is altogether different. Such was the case watching Tom Peghiny roll down the grass and take to the skies in his electric ultralight.

You always hear the buzz of small engines — most of them noisy two-strokes — when you’re approaching the ultralight field here at AirVenture. But when the crowd watched Peghiny push the control lever of the eSpyder forward and take off almost silently into the sunset, it was eerie.

“It’s very nice to relax and see windmills on the far side of the lake. It all feels like the future is now,” Peghiny said of flying the eSpyder. “It’s more like dream flying because it’s so quiet.”

Peghiny has made several flights when the wind is calm in the evening, after long days talking to visitors at the largest airshow on earth.

“It’s been very fulfilling,” Peghiny told Wired.com of the reaction people have to his plane. “Many people are interested in this technology.”

We told you a little about the eSpyder when it made its first flight two weeks ago. The airplane is a joint project between Flightstar, Peghiny’s Connecticut company that builds the airframe, and Yuneec, the Shanghai company that makes the power system. (Yuneec brought its own e-plane to AirVenture; see our earlier post for the details.) His airplane is based on a Flightstar ultralight airframe he designed in the early 1980s. It is powered by a 20 kilowatt brushless motor and can fly 40 minutes on two lithium polymer batteries.

The tiny eSpyder isn’t by any means meant for serious transportation. It’s more Vespa LX than BMW GS. But it provides just about anyone a chance to take to the air with the stealth of a bird and survey the world from several hundred feet up. You need a little training, but not a license, to fly it.

You’ll also need around $24,000 and some skill with a wrench. That’s the expected price for the kit. Peghiny concedes the eSpyder isn’t as cheap as other ultralights. But to see (and hear) it fly, it’s obvious the eSpyder is a new paradigm. Peghiny thinks the same kind of early adopters buying electric cars will buy electric airplanes.

“Why do people drive a Tesla?” Peghiny asked. “They’re not doing it to save money. It’s an emerging technology and it’s really exciting to be part of it.”

After making a few passes overhead that kept everyone’s eyes on the sky, Peghiny quietly touched down and with a soft whir taxied to his tent. As he came to a stop, the crowd gathered around the future of flying.

Photos: Jason Paur / Wired.com. Video Catherina Centanni

Lots of very large pictures on link








 
OK, not so ultralight, but electric flight never the less:

http://nextbigfuture.com/2009/12/superconductors-could-enable-electric.html

Superconductors could Enable Electric Jet Planes

Next Generation More-Electric Aircraft: A Potential Application for HTS
Superconductors (14 pages, 2008] Fully superconducting machines have the
potential to be 3 times lighter.

Sustainability in the aviation industry calls for aircraft that are significantly quieter and more fuel efficient than today’s fleet. Achieving this will require revolutionary new concepts, in particular, electric propulsion. Superconducting machines offer the only viable path to achieve the power densities needed in airborne applications. This paper outlines the main issues involved in using superconductors for aeropropulsion. We review the work done under a 5-year program to investigate the feasibility of superconducting electric propulsion, and to integrate, for the first time, the multiple disciplines and areas of expertise needed to design electric aircraft. It is shown that superconductivity is clearly the enabling technology for the more efficient turbo-electric aircraft of the future.

Here is a propulsion system design that uses advanced superconducting, cryogenically cooled electric generators and motors to drive a multitude of low noise electric fans. The obvious break-through that must be achieved for this to happen is a marked increase in the power to weight ratio of electric generators and motors

Present-day high bypass turbofans

The bypass ratio (BPR), defined as the ratio of the mass flow rate of the stream passing outside the core divided by that of the stream flowing through the core, plays a key design parameter of the engine. A higher BPR, in general, yields lower exhaust speed, which serves to reduce fuel consumption and engine noise at the cost of an increase in weight and fan diameter

* Turbofans can be very compact with specific power in the range of 3-8 kW/kg.
* Recent engines such as the GE90 turbofan exhibit a BPR of 9:1.

The Case for Electric Propulsion

Torque and speed are coupled in turbofans, limiting any potential efficiency gain through speed control. Fig. 5.b illustrates a notional example of how HTS motor
technology can help relax this coupling. The electric propulsion scheme opens
up the aircraft design space to many new possibilities in which major leaps can be made towards achieving the performance goals. Decoupling torque and speed would lead to very valuable control flexibility to enable a more favorable trade between on-design and off-design performance. In addition, this architecture is intrinsically compatible with the emerging concept of “distributed propulsion” that produces thrust by means of multiple small propulsors or engines embedded on the wing or fuselage. This arrangement is anticipated to surpass other distributed propulsion concepts in many aspects. Such a system is feasible only if electrical motors can be of about the same size or better than aero turbines. Conventional motors exhibit a specific power up to 0.5 kW/kg. Superconductors can raise the specific power limits.

Cryocoolers

Off-the-shelf cryocoolers exhibit efficiencies of about 10- 15% of Carnot efficiency, which correspond to about 70W/W at 30 K. The lightest cryocoolers today weigh about 5 lb/HPinput (or 3 kg/kW-input). This is just for the cold head portion, the associated compressors and ancillaries represent an overhead of about 5 times that weight. The use of packaged turbocompressors may reduce this overhead significantly, and coupled with the development of much lighter cold heads, it may be possible to reach the target of 3 kg/kW-input as overall specific weight for cryocoolers (2030-2035)

Superconducting Generators

LEI is developing a 3MVA/15,000 RPM generator.

General Electric used a bulk piece of magnetic material at the rotor magnetized by a stationary superconducting coil. This configuration provides a very robust rotor able to spin at high RPM. The flux distribution is not optimal but the high rotation
speed brings the power density to an impressive 7 kW/kg.

Superconducting motor for a Cessna has been made:

Total length 160 mm
External diameter 220 mm
Number of poles 8
Rotation speed 2700 RPM
Power 160 kW
Total mass (including conduction cooling apparatus) 30 kg
Power density 5 kW/kg
Heat load of superconducting part < 10W
Operating temperature 30 K

The turbine engines in a typical small business jet are about 1.5 MW. The concept described above is modular, and more HTS coils/YBCO plates can be stacked axially to increase power. The power density of this system was estimated to be 6.6 kW/kg, comparable to that of state-of-the-art turbines.

A case study of an unmanned aircraft, fully electric, able to fly and loiter for up to 14 days without refueling or returning to base. For maximum efficiency, the superconducting motor for the propulsor needs to be both extremely light and compact, but also have very low losses. We chose a lead-less axial flux configuration (allowing for higher trapped flux for compactness). The design concept, described is projected to achieve an impressive power density of 7.4 kW/kg using conventional HTS materials available today.

Superconducting Jetplane Design

A study is now being conducted to design short-field regional subsonic transport aircraft having a full payload of nominally 100 passengers. These aircraft are for the N+2 time frame, and the study has been extended to include a design having a
superconducting electric propulsion system (for possible N+3 introduction).

Superconducting generator is designed using the methodology outlined in this paper, and the result is truly remarkable. The diameter of the generator at 10.24 inches is half that of the maximum engine diameter, and the light weight of the fully superconducting generator yields a power to weight ratio of 40 HP/lb (66 kW/kg). The generator rotates at engine rotational speed resulting in reduced torque and very light weight (335 lb each generator, with each turbine engine at 894 lb).

Five fans per wing are installed above the wing with the exhaust nozzle near the trailing edge.

The fully superconducting motor outside diameter at 7.24 inches is an excellent match with the hub diameter of the fan exit, and the light weight of the motors is based on a power to weight ratio of 24.6 HP/lb (40 kW/kg), a lower power density that the generators. Each motor weighs 110 lb, and with cables included, the total
turboelectric propulsion system weighs slightly more than 5100 lbs.

The gross weight of the electric powered aircraft is approximately 5% lower than the turbofan powered aircraft primarily due to a reduction in the propulsion system weight.

A development roadmap includes:
• Develop and demonstrate fully superconducting rotating machines in the range of 25-40 kW/kg for motors, and 40-80 kW/kg for high rotation speed generators (up to 15,000 RPM)
• Develop low AC loss HTS conductors (<10 W/Am @ 500Hz, equivalent to 10 μm filament) for fully superconducting machines
• Develop cryocoolers capable of 30% of carnot efficiency and weighing less than 3 kg/kW-input (or alternative lightweight refrigeration schemes)
• Refine the physics-based models for superconducting machines and ancillaries to continue exploration of aircraft design space and alternative concepts

FURTHER READING
Compact superconducting power systems for airborne applications (3 pages)

A major issue with superconducting wire has been overcome with the recent introduction of the YBCO coated conductor. The latest 2G power cables can conduct up to 10 times the amount of power comparable copper cables manage.
* MEGAWATT AIRBORNE GENERATOR
* GYROTRON MAGNET
* COMPACT POWER CABLES
by using a high-temperature superconductor system (HTS) instead of copper wire, transmission power densities could be increased three- to ten-fold, and the system heat loss and weight could be reduced by 10-15 kW and 1500-3000 lbs., respectively.
 
And in between electric ultralights and 747's, a battery powered small plane:

http://nextbigfuture.com/2010/01/analytical-mechanical-associates-making.html

Analytical Mechanical Associates and NASA Mark Moore Pushing Electric Aircraft - Niche Applications

Analytical Mechanical Associates (AMA) has been in the business of aerospace engineering for more than forty years.

Jan 20, 2010 (today) at American Helicopter Society meeting Mark Moore, an aerospace engineer at NASA's Langley Research Center and his colleagues will officially unveil the Puffin design

Scientific American has details

In principle, the Puffin can cruise at 240 kilometers per hour and dash at more than 480 kph. It has no flight ceiling—it is not air-breathing like gas engines are, and thus is not limited by thin air—so it could go up to about 9,150 meters before its energy runs low enough to drive it to descend. With current state-of-the-art batteries, it has a range of just 80 kilometers if cruising, "but many researchers are proposing a tripling of current battery energy densities in the next five to seven years, so we could see a range of 240 to 320 kilometers by 2017," says researcher Mark Moore.

* At up to 95 percent efficiency, electric motors are far more efficient than internal combustion engines, which only rate some 18 to 23 percent.

* Electric aircraft are much quieter than regular planes—at some 150 meters, it is as loud as 50 decibels, or roughly the volume of a conversation, making it roughly 10 times quieter than current low-noise helicopters.

The UK Register has coverage and perspective and history of the work of Mark Moore.

Wikipedia has a survey of Electric aircraft Several electric aircraft are in low volume commercial production.

The Lange Antares 20E is a self-launching motor glider with a 42-kW electric motor and SAFT VL 41M lithium-ion batteries. The motor actuates 2-blade fixed pitch propeller. It can climb up to 3,000 meters with fully charged cells. After launch it can function as a conventional, though heavy, glider (sailplane). Over 50 had been built as at January 2010.


 
Power beaming for aircraft. Next step, power beaming to ships and ground vehicles?

http://nextbigfuture.com/2010/05/laser-powerbeaming-to-uavs.html

Laser Powerbeaming to UAVs

LaserMotive White Paper – Power Beaming for UAVs (9 page pdf)

Laser Motive will be competing in the 2010 Powerbeaming (Space Elevator Games) competition. The last date given for the competition is May 10, 2010. However, this would seem likely to slip as their should be word of the teams being onsite and the course being setup by now for a competition in one week.

The UAV powerbeaming is at technology readiness 5 or 6.

    LaserMotive envisions three general applications for laser-powered UAVs feasible with current technology:
    1. A stationary observing platform for long-­‐duration ISR (Intelligence, Surveillance, and Reconnaissance). The UAV can be a quadricopter, airplane, or aerostat.
    2. Extended or multi-­‐mission operations. An electric UAV is launched and flies to a target beyond laser range where it can loiter for some time. Once the on-­‐board energy storage goes below a predetermined level, the UAV flies to a location within line of sight of a recharging laser and recharges in the air.
    3. Unlimited patrol. Missions that can be conducted within line-­‐of-­‐sight (~10 miles for an altitude of 1 mile) of a laser station (which may itself be moving) can be continuously powered, enabling a UAV to patrol or shadow a target indefinitely.

    The following suggestions illustrate interesting systems which LaserMotive believes could be demonstrated in prototype form in ~18–24 months, using existing technology:
    • Small-­‐or Micro-­‐UAV recharging with multiple UAVs, maintaining one or more vehicles “on station” while others are in transit or recharging
    • High-­‐altitude (near-­‐vertical) loitering: power > 10 kWe, at a range of > 5 km (10,000 ft).
    • Long-­‐range, low-­‐angle beaming: > 10 kWe, horizontal range > 5 km, vertical range > 1.5 km.

Point to Point Powerbeaming
LaserMotive’s Point-to-Point (P2P) Power Link is a ground-based version of our long-range laser power link technology, providing power to remote devices without the need for wires.

    Perimeter sensors for military bases or field units can benefit from the P2P Power Link, by eliminating the need to run expensive copper wires over long distances or to send personnel out into dangerous areas to swap batteries.

    Field units or temporary bases can receive electrical power via the P2P Power Link, eliminating the need to truck fuel through dangerous locations.

    Communication relay towers can be deployed on remote mountaintops and powered by the P2P Power Link without needing a logistically difficult power supply line.

Further Reading
Xconomy has a feature on LaserMotive.
 
http://solarship.com/

A Canadian company is working on a hybrid airship which promises to have STOL performance and use limited amounts of energy to fly. The hybrid airship uses helium to offset the weight of the airframe, but still uses aerodynamic lift to fly. The developers believe that this combination can be powered by solar cells on the upper surface (the amount of engine power to fly would be less than a regular aircraft of this size), I would be interested to discover what sort of solar cell performance is really possible.
 
Another not ultralight idea, but this time a 737 sized aircraft using electric power to fly, and apparently feasable with current technology. The promised savings in fuel are interesting, and the size and shape of the proposed aircraft are quite interesting for many of our needs:

http://www.aviationweek.com/Blogs.aspx?plckBlogId=Blog:a68cb417-3364-4fbf-a9dd-4feda680ec9c&plckPostId=Blog%3Aa68cb417-3364-4fbf-a9dd-4feda680ec9cPost%3Acbc39e6b-d381-4909-bf5d-981f6b1839fa

Turboelectric Propulsion - Superconducting or Not?

Posted by Graham Warwick 1:27 AM on Mar 24, 2012
When NASA talks about turboelectric distributed propulsion, it talks in terms of superconducting generators and motors in a hybrid wing-body concept aircraft it calls the N3-X. But there are other ways of approaching all-electric propulsion.

Empirical Systems Aerospace (ESAero), a small advanced-design house based in Pismo Beach, California, assumed superconducting technology when it produced a concept (below) for a 2030-35 timeframe turboelectric-powered 150-seat airliner, the ECO-150.


Graphics: ESAero, via NASA

Designed to meet NASA's N+3-generation goals, which include a 60% reduction in energy consumption relative to the CFM56-powered 737-800, the ECO-150 features electrically driven fans embedded in the inboard wing sections, powered by mid-span turbogenerators supported by bracing struts attached to the tails. There are eight fan propulsors per side.

High-efficiency superconducting generators and motors require cryogenic cooling to work, and ESAero president Andy Gibson says the company did not have enough information on cryocoolers so it used liquid hydrogen to cool the electrical systems. Hydrogen is contained in tanks along the top of the fuselage and, after cooling the superconducting systems, is burned in the turbogenerators.

The required superconducting technology does not exist today but ESAero, continuing internal studies into hybrid propulsion systems, became convinced that conventional, non-superconducting electrical systems could be made to work in a large aircraft. It was funded by NASA Ames to take the ECO-150 concept and rework it around ambient-temperature generator and motor technology available to meet NASA's 2020-25 timeframe N+2 goals.

To the evident surprise of both ESAero and NASA, the N+2 ECO-150 (above) design closed - met its requirements - despite having a significantly heavier turboelectric distributed-propulsion system using technology available today in industries outside aerospace. "Our main interest was could we even get the aircraft to close, and the answer is yes," says Gibson.

"This is our first shot at getting the aircraft to close, and performance is about equal to a CFM56-powered 737-700," he says. Without the benefit of high-efficiency superconducting motors and generators, the propulsors are significantly larger (below, superconducting on the right and non-superconducting on the left). Gibson says ESAero might redo the N+2 ECO-150 design and increase fan diameter, which would allow the motors to be shorter.

Ben Schiltgen, Gibson's business partner and architect of the propulsion system, says past studies of hybrid turboelectric power concluded it would take electric-motor power densities of 10hp/lb to make a design work. Current technology is around 4-5hp/lb. "Technology is not even close to 10hp/lb, but it appears we do not need that kind of power to close an aircraft," he says. The N+2 ECO-150 has generators and motors in the 2.4-4.5lb/hp range.

The result of all this work is growing military interest in turboelectric propulsion - superconducting and non-superconducting - and a Large Electric Aircraft Propulsion Technology (LEAPTECH) workshop was held in Dayton, Ohio, in January, where NASA and the US Air Force, Navy and Army shared their ideas in an effort to identify opportunities for collaboration - including the potential for a dual-use demonstrator.

Under its N+2 study contract from NASA, ESAero has also produced a dual-use commercial-airliner/military-transport concept. The two variants of this design have essentially the same fuselage - housing 130 seats as an airliner and 52,000lb of payload as an airlifter. The wing is scaled up 20%-plus for the military version (below).

Although ESAero believes the technology for such an aircraft is available, it is outside aerospace and needs to be scaled up. "The motors are about an order of magnitude larger than exist today," says Schiltgen. Even using today's non-superconducting technology, the time needed to scale up the motors, make sure they work at altitude and find ways to dissipate the heat they generate, would put a turboelectric-powered aircraft out into the 2025 timeframe, he believes.

While NASA believes ambient-temperature turboelectric propulsion could be used in a demonstrator aircraft, it continues to pursue cyrogenic superconducting technology to get the power density and energy efficiency it is seeking. To that end, it has awarded contracts to Rolls-Royce Liberty Works to design a 50MW-class propulsive electric grid; Advanced Magnet Lab for a fully superconducting motor/generator; Creare for a flight-weight cryocooler; and MTECH Laboratories for a cryogenic inverter/rectifier.

NOTE: Post corrected to identify NASA Ames as the sponsor of ESAero's N+2 and dual-use concept work.
 
Ionic thrusters are years away from flight, but the idea of a silent ultralight UAV which is almost invisible in the Infared band is pretty attractive. How well it could scale to an ulta light aircraft (I think they are talkig about light general aviation aircraft like a Cessna) remains to be seen; the idea of sitting inside an ultra high voltage transformer is a bit alarming:

http://web.mit.edu/newsoffice/2013/ionic-thrusters-0403.html

A mighty wind
Thrusters powered by ionic wind may be an efficient alternative to conventional atmospheric propulsion technologies.
Jennifer Chu, MIT News Office

April 3, 2013

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When a current passes between two electrodes — one thinner than the other — it creates a wind in the air between. If enough voltage is applied, the resulting wind can produce a thrust without the help of motors or fuel.

This phenomenon, called electrohydrodynamic thrust — or, more colloquially, “ionic wind” — was first identified in the 1960s. Since then, ionic wind has largely been limited to science-fair projects and basement experiments; hobbyists have posted hundreds of how-to videos on building “ionocrafts” — lightweight vehicles made of balsa wood, aluminum foil and wire — that lift off and hover with increased voltage.

Despite this wealth of hobbyist information, there have been few rigorous studies of ionic wind as a viable propulsion system. Some researchers have theorized that ionic thrusters, if used as jet propulsion, would be extremely inefficient, requiring massive amounts of electricity to produce enough thrust to propel a vehicle.

Now researchers at MIT have run their own experiments and found that ionic thrusters may be a far more efficient source of propulsion than conventional jet engines. In their experiments, they found that ionic wind produces 110 newtons of thrust per kilowatt, compared with a jet engine’s 2 newtons per kilowatt. The team has published its results in the Proceedings of the Royal Society.

Steven Barrett, an assistant professor of aeronautics and astronautics at MIT, envisions that ionic wind may be used as a propulsion system for small, lightweight aircraft. In addition to their relatively high efficiency, ionic thrusters are silent, and invisible in infrared, as they give off no heat — ideal traits, he says, for a surveillance vehicle.

“You could imagine all sorts of military or security benefits to having a silent propulsion system with no infrared signature,” says Barrett, who co-authored the paper with graduate student Kento Masuyama.

Shooting the gap

A basic ionic thruster consists of three parts: a very thin copper electrode, called an emitter; a thicker tube of aluminum, known as a collector; and the air gap in between. A lightweight frame typically supports the wires, which connect to an electrical power source. As voltage is applied, the field gradient strips away electrons from nearby air molecules. These newly ionized molecules are strongly repelled by the corona wire, and strongly attracted to the collector. As this cloud of ions moves toward the collector, it collides with surrounding neutral air molecules, pushing them along and creating a wind, or thrust.

To measure an ion thruster’s efficiency, Barrett and Masuyama built a similarly simple setup, and hung the contraption under a suspended digital scale. They applied tens of thousands of volts, creating enough current draw to power an incandescent light bulb. They altered the distance between the electrodes, and recorded the thrust as the device lifted off the ground. Barrett says that the device was most efficient at producing lower thrust — a desirable, albeit counterintuitive, result.

“It’s kind of surprising, but if you have a high-velocity jet, you leave in your wake a load of wasted kinetic energy,” Barrett explains. “So you want as low-velocity a jet as you can, while still producing enough thrust.” He adds that an ionic wind is a good way to produce a low-velocity jet over a large area.

Getting to liftoff

Barrett acknowledges that there is one big obstacle to ionic wind propulsion: thrust density, or the amount of thrust produced per given area. Ionic thrusters depend on the wind produced between electrodes; the larger the space between electrodes, the stronger the thrust produced. That means lifting a small aircraft and its electrical power supply would require a very large air gap. Barrett envisions that electrodynamic thrusters for aircraft — if they worked — would encompass the entire vehicle.

Another drawback is the voltage needed to get a vehicle off the ground: Small, lightweight balsa models require several kilovolts. Barrett estimates a small craft, with onboard instrumentation and a power supply, would need hundreds or thousands of kilovolts.

“The voltages could get enormous,” Barrett says. “But I think that’s a challenge that’s probably solvable.” For example, he says power might be supplied by lightweight solar panels or fuel cells. Barrett says ionic thrusters might also prove useful in quieter cooling systems for laptops.

Ned Allen, chief scientist and senior fellow at Lockheed Martin Corp., says that while ionic thrusters face serious drawbacks — particularly for aerospace applications — the technology “offers nearly miraculous potential.”

“[Electrohydrodynamic thrust] is capable of a much higher efficiency than any combustion reaction device, such as a rocket or jet thrust-production device,” Allen says. Partly for this reason, Allen says Lockheed Martin is looking into the technology as a potential means of propulsion.

“Efficiency is probably the number one thing overall that drives aircraft design,” Barrett says. “[Ionic thrusters] are viable insofar as they are efficient. There are still unanswered questions, but because they seem so efficient, it’s definitely worth investigating further."
 
Seems like the idea of hybrid electric aircraft has taken hold in the industry. How practical this actually is remains to be seen; the extra weight of the electric motors, separate fans, batteries, turbogenerators, control electronics and (possibly) cyro coolers might more than offset any potential savings from using smaller turbine engines:

http://www.technologyreview.com/news/516576/once-a-joke-battery-powered-airplanes-are-nearing-reality/

Once a Joke, Battery-Powered Airplanes Are Nearing Reality
Aerospace companies are working on hybrid electric airplanes, and the earliest versions will likely arrive before the end of the decade.

By Kevin Bullis on July 8, 2013

Last month Siemens and EADS demonstrated a new gas-electric vehicle capable of carrying two people and their luggage 900 kilometers—roughly the distance from New York to Detroit—between refuels and recharges. The prototype was not a car, but a small two-seater airplane.

The hybrid plane is similar to the Chevrolet Volt in that it relies on an electric motor and uses a gas engine as backup. The airplane matches the performance of some private airplanes already on the market, but it has two distinct advantages: it’s remarkably quiet, and uses about 25 percent less fuel.

The achievement presages what is likely to be a big shift toward hybrid propulsion in airplanes. Several major corporations envision a future in which airplanes rely at least in part on electric propulsion. Although the technology will be applied to small planes at first, eventually it could help reduce noise and emissions from airliners.

“Within this decade, we will certainly see hybrid electric aircraft entering the market,” says Frank Anton, who heads the hybrid aircraft efforts at Siemens. Four-seat hybrid aircraft are likely within that time frame, he says, but even 19 seaters are possible before the decade is out. Anton predicts that eventually we will see 100-passenger hybrid aircraft that use half as much fuel as today’s airplanes.

Boeing is taking this a step further with a concept for hybrid airplanes the size of 737s, which can seat more than 150 passengers, although it’s unlikely these will come into service before 2030. EADS, the parent company of Airbus, has also developed a conceptual design for passenger airplanes that fly exclusively on electricity, although the range of these aircraft would be limited.


Motor head: The new plane is the first to have a hybrid drivetrain.

“A few years ago, the idea of flying an airplane on batteries was a joke,” says Marty Bradley, a principle investigator for advanced aircraft concepts at Boeing Research and Technology. While batteries and electric motors are efficient and quiet, batteries tend to be big and heavy, storing far less energy than liquid fuels.

Two things have changed. The amount of energy that batteries can store is steadily improving, and this looks likely to continue as they’re developed for use in portable electronics and electric vehicles, Bradley says. Meanwhile, the technologies needed to integrate batteries and electric motors with conventional engines are getting smaller, lighter, and more efficient. Siemens demonstrated an earlier version of its hybrid airplane in 2011, but it was too heavy to be practical. For the new plane, Siemens decreased the weight of the electric motor, power electronics, and gears by 100 kilograms to bring its cargo and passenger capacity up to the level of similarly sized small planes.

In airplanes, a hybrid electric design improves efficiency mainly by making it possible to use a relatively small gas-powered engine designed to run at its most efficient at cruising speeds. The battery and electric motor provide the extra power needed for takeoff and ascent. The batteries also make it possible to recover energy during descent much the way hybrid cars capture energy during braking (propellers spin a generator). And, as batteries improve, they will provide more and more of the energy on board.

Electric motors confer other advantages. They can be mounted in unusual places on an airplane, which can be used to improve aerodynamics. They can also be steered: angled upward, for example, during takeoff to get a plane off the ground faster. In flight, the motor could be pointed left or right to steer the plane, eliminating the need for a rudder. These design changes, together with the efficiency of the hybrid propulsion, could help decrease fuel consumption by half, he says (see “‘Hybrid Wing’ Uses Half the Fuel of a Standard Airplane”).

How fast electric propulsion is adopted depends mostly on the development of the batteries. EADS’s electric airplane plans call for a battery that can store 1,000 watt hours per kilogram, which is about five times more energy than a typical lithium-ion battery. New battery chemistries like lithium-air and lithium-sulfur could provide more capacity, but some big challenges remain (see “Nanostructures Boost Battery Life Fivefold” and “Beyond Lithium Ion: ARPA-E Places Bets on Novel Energy Storage”). Bradley expects that all-electric aircraft will be limited to 1,600 kilometers until after 2050.

For larger aircraft, electric propulsion might be used to help spin the large turbofans on the front of a jet engine. The first application of electric propulsion for large planes will be for taxiing, allowing planes to save fuel on the ground, he says.

So for the next several years hybrid technology will be limited to small planes. One near-term benefit of the technology is that small airports (which are often located near residential areas) will be quieter, says Jean Koster, a professor of aerospace engineering sciences at the University of Colorado at Boulder who has founded a company to commercialize a more compact gearbox for combining gas and electric power. Hybrid designs could also put an end to one of the last holdouts of fuel that contains lead: small airplanes with high compression engines still require lead additives. In fact, the battery boost could make it possible to use the same gas-powered engines used in hybrid cars.

Note: Diesel engines, especially highly turbocharged ones could probably do the job today, and diesel has a higher energy density and is safer in case of an accident to boot.

This second article isn't about electric aircraft per se, but highlights the technology that might be used to build ultralight and ultrastrong aircraft:

http://www.technologyreview.com/news/509916/hybrid-wing-uses-half-the-fuel-of-a-standard-airplane/

“Hybrid Wing” Uses Half the Fuel of a Standard Airplane
NASA has demonstrated a manufacturing breakthrough that will allow hybrid wing aircraft to be scaled up.

By Kevin Bullis on January 24, 2013

Aerospace engineers have long known that ditching a conventional tubular fuselage in favor of a manta-ray-like “hybrid wing” shape could dramatically reduce fuel consumption. A team at NASA has now demonstrated a manufacturing method that promises to make the design practical.

Combined with an extremely efficient type of engine, called an ultra-high bypass ratio engine, the hybrid wing design could use half as much fuel as conventional aircraft. Although it may take 20 years for the technology to come to market, the manufacturing method developed at NASA could help improve conventional commercial aircraft within the next eight to 10 years, estimates Fay Collier, a NASA program manager.

The manufacturing technique lowers the weight of structural components of an aircraft by 25 percent, which could significantly reduce fuel consumption. The advances are the culmination of a three-year, $300 million effort by NASA and partners including Pratt & Whitney and Boeing.

There are two key challenges with the flying wing design. One is how to control such a plane at low speeds. NASA previously addressed this by building a six-meter-wide remote-controlled test aircraft (the X-48B) to demonstrate ways to control hybrid wings. Based on those tests and wind tunnel tests, NASA built a larger remote-controlled aircraft that started test flights last year.

The second challenge is building a full-scale version of the aircraft with pressurized cabins that is structurally sound. One reason tubular airplanes have persisted is that it’s relatively easy to build a tube that can withstand the forces acting on it from the outside during flight while maintaining cabin pressure. The hybrid wing design involves a flatter, box-like fuselage that blends with the wings. The flatter structure, which includes some near-right angles, is much more difficult to build in a way that’s strong enough and light enough to be practical.

NASA’s manufacturing process starts with preformed carbon composite rods. The rods are covered with carbon fiber fabric and stitched into place. Fabric is then stitched over foam strips to create cross members. The fabric is impregnated with an epoxy to create a rigid composite structure.

Sections of a fuselage built with the technique were tested and shown to withstand up to the forces that would be applied to a finished aircraft. Tests also showed that when enough pressure was applied to cause the parts to fail, the stitching used to make the structure stopped cracks from spreading—a key to avoiding catastrophic failure in flight.

The researchers are now building a 30-foot-wide, two-level pressurized structure that will be used in an attempt to validate the manufacturing approach. That structure is scheduled to be finished by 2015.

To achieve a 50 percent reduction in fuel consumption, the hybrid wing design will need to incorporate an advanced engine design. Collier says ultra-high bypass engines are a good match. In an ultra-high bypass design, the front fan on the engine is far larger than the core of the engine, where air is compressed and combustion takes place. Such large fans can be difficult to mount under the wing, as engines are mounted in most conventional airliners. The hybrid wing design involves mounting the engines on top of the plane, rather than under the wings. (The top-mount design also cuts noise levels.)

NASA has helped Pratt & Whitney develop prototype ultra-high bypass engines, which are slated to go into commercial use for the first time next year, starting on Bombardier’s C-Series aircraft. NASA is further optimizing the engines to take advantage of the top-mount design in the hybrid wing airplane.
 
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