JUNE 2019 Electric Aircraft Working Group Report ACKNOWLEDGEMENTS
Department of Commerce Zunum Aero The Boeing Company Volta Enterprises Verdego Aero magniX Diamondstream Partners Stellar Aerospace Aerospace Futures Alliance Andrew Graham Aircraft Consulting Kenmore Air Center for Excellence in Aerospace and Advanced Manufacturing Federal Aviation Administration Seattle Tacoma International Airport Wenatchee Pangborn Memorial Airport Airline Pilots Association Kitsap Aerospace Defense Alliance Avista Utilities Puget Sound Energy ELECTRIC AIRCRAFT WORKING GROUP REPORT
EAWG REPORT EXECUTIVE SUMMARY
he Washington State Department of Washington State has unique geography that Transportation Aviation Division, at the makes traveling within the state challenging and T direction of the legislature, formed a often time consuming. Improvements in regional working group with the goal of exploring the air travel options could greatly expand a citizens’ electric aircraft industry and how electric aircraft ability to travel easily and efficiently throughout technology could be used to expand regional air the state and region. Electric and hybrid-electric transportation in the state of Washington. This aircraft are forecast to offer lower operational report is required in ESSB 6106, Section 212 (4). costs for air carriers. If air carriers are able to Members of the working group represent the operate more efficiently and at a lower cost, the electric aircraft industry, the aircraft manufacturing savings may allow them to offer commercial air industry, electric utilities, the battery industry, the service to underserved communities. The electric state Department of Commerce, the Department and hybrid-electric aircraft that are currently being of Transportation Aviation Division, the airline developed are anticipated to accommodate 9-15 pilots association, a primary airport representing passengers. Because of the aircraft’s smaller size an airport association, investment firms and the they will be able to operate from runways as short airline industry. The group selected work in areas as 3,000 feet in length. Over half of the airports that affect the industry. Each member provided in the state would be able to accommodate valuable information towards the introduction of the landing distance required for electric and these aircraft into commercial service. hybrid-electric aircraft. Short takeoff and landing The aircraft development and subsequent capabilities coupled with lower operational costs manufacturing process is challenging for any make these aircraft viable for the role of increasing new aircraft. Electric and hybrid-electric aircraft intrastate and interstate air travel. Industry and the manufacturers are innovating both in terms of markets will determine if initial use of these aircraft propulsion and battery technology. This innovation are on demand, scheduled charter service or for requires the cooperation and collaboration with business travel. the Federal Aviation Administration to develop Electric and hybrid-electric aircraft promise standards and regulations for these systems. to reduce consumption of fossil fuels and Battery technology for use in large aircraft greenhouse gas emissions. These aircraft are propulsion is in its infancy and is an important projected to operate at 85% to 90% efficiency, factor in bringing larger electric aircraft to market. 20% to 40% more efficient than piston and Currently batteries are heavy and lack the required turbine aircraft. Because the energy used for energy density for larger aircraft. Manufacturers propulsion is electricity, the emissions are tied to and designers have dealt with this by developing the electric grid and the source that is generating smaller aircraft. Some manufacturers plan to that electricity. Washington State benefits from develop the aircraft initially as a hybrid with the obtaining the majority of its electricity from potential of converting to fully electric once the renewable sources. A concern of electric aircraft battery technology is further developed. Many is the disposition process for the batteries that of the entrants in the electric aircraft market are are no longer viable for aircraft use. It is possible smaller startup companies who require sizable that these batteries are subsequently re-used investments from outside investors.
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in a secondary operation such as backup power Resource Recommendation: Resources are for server locations, to reduce the impact on the required for continued support of Washington’s environment. Electric Aircraft Working Group. A qualified Aviation work force is another concern. The aerospace consultant should further the efforts of aviation industry is currently facing a large the working group by examining opportunities for shortage of pilots and aircraft maintenance electric propulsion aircraft in Washington State. technicians. Demand for air travel is rising, and The study should include the following: with the advent of expanded regional air service i) Infrastructure requirements necessary to the shortage will only worsen, in the near term, facilitate electric aircraft operations at airports; as industry and aviation education centers ii) Potential economic and public benefits work together to meet the needs. Similarly, including but not limited to the direct manufacturers of electric aircraft are working and indirect impact on the number of to minimize the amount of required retraining manufacturing and service jobs and the wages for the pilots and technicians operating and from those jobs in Washington state; maintaining the aircraft. Manufacturers will iii) Potential incentives for industry in the also need to engage with aircraft maintenance manufacturing and operation of electric schools to ensure maintenance technicians have aircraft for regional air travel; the necessary skills to maintain and manufacture electric aircraft. iv) Educational/workforce requirements for manufacturing and maintaining electric Finally, similar to electric vehicles, electric aircraft aircraft; will require modifications and/or additions to airport infrastructure in order to accommodate v) Demand and forecast for electric aircraft use aircraft battery charging. Handling peak loads for to include expected timeline of the aircraft electricity demands requires planning. Some of the entering the market given FAA certification electrical demands could be offset by using solar requirements; power on airport property. vi) Identification of up to six airports in Washington State that may benefit from a pilot Recommendations moving forward: program once an electrically propelled aircraft The Electric Aircraft Working Group finds, for commercial use becomes available; that given the potential to expand aerospace vii) Recommendations to further the advancement manufacturing; open up new markets providing of the electrification of aircraft for regional both economic and public benefits; impact commercial use within the state; the development of the next generation of The study and accompanying recommendations aircraft resulting in a reduction of greenhouse should be provided to the transportation gas emissions and noise pollution; and provide committees of the legislature November 15, 2020. a regional transportation option that provides The department should also provide a progress relief to congested roadways; continuing to study report on implementation of the recommendations while working towards the integration of electric to the transportation committees by February 2022. propulsion of aircraft is in the best interest of the state.
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ELECTRIC AND HYBRID-ELECTRIC AIRCRAFT USE IN WASHINGTON STATE
I. Background • Public acceptance of the technology In the spring of 2018, Washington State • Cost comparison of fossil fuel and electric or Department of Transportation Aviation Division hybrid-electric aircraft engines (WSDOT) was tasked by the legislature with • Emission reduction potential forming a working group to explore the feasibility • Policy changes needed to facilitate electric of introducing electric or hybrid-electric aircraft or hybrid-electric powered aircraft use for for regional air transportation in the state. The regional commercial air travel in Washington group was comprised of subject matter experts state from a variety of different fields that are likely to WSDOT Aviation organized three working group be impacted by the introduction of electric aircraft. meetings to discuss how this technology will Members of the working group represent the impact Washington State and air travel in general. electric aircraft industry, the aircraft manufacturing The working group discussed the topics requested industry, electric utilities, the battery industry, the by legislators along with many other factors that state Department of Commerce, the Department relate to electric aviation. The first meeting was of Transportation aviation division, the airline pilots held at Zunum Aero’s Headquarters in Bothell and association, a primary airport representing an focused on the current state of the electric aircraft airport association, investment firms and the airline industry. The group also brainstormed ideas industry. for how the working group should proceed and The work group was to consider and make topics to research further. The second meeting, recommendations on the feasibility of electric or held at SeaTac International Airport, addressed hybrid-electric flight given: manufacturing and certification opportunities • Federal certification requirements and challenges. The final in-person meeting was • Current and anticipated advancements in held at the WSDOT Aviation office in Tumwater. battery technology The group discussed impacts on the environment, public perception, and the opportunities for the • Infrastructure requirements and capacity state of Washington. impacts at primary airports Following the first meeting, the working group was • Need for and feasibility of industry incentives broken into six functional area breakout groups • Potential for public private partnerships to discuss specifics of operating, manufacturing, • Impacts to revenues generated from aviation infrastructure requirements, and other impacts on fuel sales industry, the state, and the region. The members were subject matter experts in each functional • Educational requirements for maintaining area and were gathered to take a closer look at electric or hybrid-electric powered aircraft different aspects of their subject of focus. Section • Homeland security checkpoint requirements IV of this report will explore these topics in detail.
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II. History of Electric and 2001. These aircraft set a number of altitude records for solar-powered, propeller driven aircraft. Hybrid-Electric Aircraft Another unmanned solar aircraft, called the While electric aircraft are perceived to be QinetiQ Zephyr set an endurance record of over futuristic, the first electrically powered flying 336 hours in July of 2010. Dunbar (2015) Possibly machine first flew in 1886, seventeen years before the most noteworthy feats of a solar powered the Wright Brothers flight at Kitty Hawk. Gaston aircraft was the manned circumnavigation of the Tissandier, chemist and early aviation pioneer, Earth by the Solar Impulse II. The Solar Impulse II attached a Seimens electric motor and propeller to departed Abu Dhabi, United Arab Emirates (UAE) a dirigible type airship and flew the craft making it on March 9, 2015 and returned to Abu Dhabi 16 the first electric aircraft. In the year that followed, months later on July 26, 2016. The 26,000 mile airship designers, Charles Renard and Arthur flight was the first circumnavigation of a manned Krebs, attached larger, more powerful electric fixed-wing aircraft on solar power alone. Around motors to another airship. However, even with the world to promote clean technologies. (2016). the more powerful motors, the airship suffered Electric aircraft traditionally have been light from a lack of performance due to the heavy aircraft until only recently. This is primarily due to accumulators used to store the electricity. Roland battery technology as the limiting factor. Heavy Berger (2017) batteries have been prohibitive for large payloads. The first-heavier-than air electrically powered Many experimental and research designs have aircraft took flight nearly ninety years after the been flown resulting in the development of light Tissandier electric airship in 1973. Motor-glider recreational and pilot training aircraft. Some legacy designer and manufacture, Heino Brditschka piston powered aircraft like the Cessna 172 have flew a modified version of his HB-3 motor-glider been retrofitted with an electrical propulsion with an electric powerplant. Brditschka’s electric system. The light aircraft market segment is an motor-glider was powered by four 24-hour charged excellent starting point to test systems and prove nickel-cadmium (NiCad) batteries that all together the viability of electric aviation. Because of this, generated 100 volts giving the aircraft roughly Siemens and Airbus have also tested light fully eight minutes of powered flight time. The motor electric aircraft to help further the technology. was taken from a forklift and modified for use on an aircraft. His first flight took place on October III. Overview of Electric 21, 1973 and flew roughly 300 meters above the Aircraft Technology ground for around nine to fourteen minutes. At the Electric motor technology has been around time of Brdischka’s first electric flight, the world was for nearly 200 years and excels at converting experiencing the first major oil crisis, thus the flight electricity into rotational power. Most of the attracted considerable public interest. Wolf (n.d.) potential energy available in the fuels used in In the 1970’s, solar technology and NiCad battery piston and turbine engines is lost to heat. Electric technology were being developed in earnest. In motors only lose a small portion of their potential 1979, the first solar-powered manned aircraft was energy from electric resistance. Conversely, an first introduced and flown. Numerous unmanned electric drivetrain can operate at higher than research aircraft have been developed to explore 90% potential energy to the shaft. A turboprop this technology. NASA’s Pathfinder, Pathfinder is capable of 20-25% potential energy for short Plus, and Helios were developed between 1985
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low altitude flights increasing to 35% efficiency at Hybrid-Electric Aircraft high altitudes. Turbofan engines are quite efficient Hybrid-electric aircraft, much like hybrid cars but not at the level of an electric motor. Electric and trucks, are powered with a combination motors are digitally controlled allowing them to of electricity from batteries and an internal be more reactive to pilot input. These motors are combustion engine. There are two types of hybrid- able to go from idle to full power much quicker electric aircraft configurations, series hybrid and than a piston or turbine engine. Another benefit parallel hybrid. Series hybrid aircraft use electric of electric motors is their ability to be scalable and motors for propulsion and the internal combustion still maintain the same efficiency notwithstanding motor drives a generator to produce supplemental the size of the motor. electricity for the electric motors. Parallel hybrid Turbine and piston engines rely on burning fuel and aircraft use both the internal combustion engine require contact between mechanical components and the electric motor for propulsion of the within the engine. This generates both heat and aircraft. wear, limiting the engine’s life. Electric motors have Turbo-Electric Aircraft relatively few moving parts, which means there is Turbo-electric aircraft take kinetic energy from far less wear and tear, as well as less maintenance a turboshaft to drive an electric generator. The compared to traditional aircraft engines. Aircraft generator is then used to power electric motors to used by regional airlines would benefit from the generate propulsion. Turbo-electric propulsion gives reliability and the long service life of electric designers added flexibility to place propulsion fans propulsion motors. All of these factors add up in locations to create a very efficient aircraft. This to the potential for reduction in maintenance particular design utilizes electric propulsion but is compared to conventional aircraft engines, as well still reliant on fossil fuels or other fuel sources. as reduced unexpected repairs. Electrification of aircraft currently exists More Electric Aircraft in two segments in the aviation industry, Throughout the development and evolution Electrical Propulsion and More Electric Aircraft of aircraft, systems such as control actuation, (electrification of certain aircraft systems). de-icing, and cabin climate control, have been powered with mechanical, pneumatic or hydraulic Types of Electric Propulsion: power. These systems have been powered by the aircraft’s engines that are also being used to Pure Electric Aircraft propel the aircraft. Because the aircraft’s primary Pure electric aircraft are aircraft powered only powerplant is powering all of these systems, there with electrical propulsion. The power is derived is a reduction in power and reduced efficiency. from a battery or another source of electric power. As electrical systems and electricity generating Electric motors lend themselves well to aircraft capabilities have evolved, older systems that propulsion because they are able to operate on a rely on the aircraft engines for mechanical or wide spectrum of revolutions-per-minute and are pneumatic power can now be provided with highly reliable. Because they are easily adaptable, the use of electric motors. Flight controls, cabin electric motors may be able to replace turboprops climate control, thrust reversers, wheel brakes, de- and turbofan engines as battery technology icing and other aircraft systems are being powered improves. by electric motors and actuators. Because of this technology advancement, the powerplant
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generating the aircraft’s propulsion can operate respond in a cost-effective manner through at peak efficiency because it is driving just a performance-based airworthiness safety rules and generator and is no longer being used to power the consensus standards for compliance.” other aircraft systems. Part 25 certification standards are for transport category aircraft defined as; Jets with 10 or more IV. Electric Aircraft seats or a maximum takeoff weight (MTOW) Functional Areas greater than 12,500 pounds; or propeller-driven airplanes with greater than 19 seats or a MTOW a. Manufacturing/Certification of greater than 19,000 pounds. Part 25 has more Electric/Hybrid-Electric Aircraft stringent requirements to which manufacturers must adhere to and undergo scrutiny lengthier The certification of any aircraft is a complicated certification process over aircraft certified under process. Aircraft certification requires the Part 23. manufacturer to demonstrate that the aircraft they are developing meets the safety standards A challenge to the manufacturing and certification set forth in the standards for small aircraft and of electric and hybrid-electric aircraft is industry transport aircraft. Electric and hybrid-electric experience, and experience of the regulatory aircraft certification will provide challenges authorities (e.g., FAA). Most of the parties seeking to manufactures and the Federal Aviation certification and planning to produce electric/ Administration (FAA) alike. Developing technology hybrid-electric aircraft are new entrants in the field of any sort poses issues for a rigid and exhaustive of aviation with limited experience in certification certification process. Because challenges exist and manufacturing. Fortunately, many have ties for a rapidly changing technology area and for to established aviation industry that will provide novel configurations, it is unclear which existing guidance. For regulators, the challenge will be to regulations, or new regulations would be required establish new standards for new and novel designs for certification. that establish the level of safety consistent with existing standards for the category of aircraft, and The two main categories that the electric aircraft to do so in a timely manner. There currently exists under development would be certified under a lack of relevant standards for high performance are 14 CFR Part 23 and 14 CFR Part 25. Part 23 batteries and electrical components in propulsion certification standards are for small aircraft with a systems (electric and hybrid) in the aircraft maximum takeoff weight (MTOW) less than 19,000 environment. pounds and carry less than 19 passengers. This certification standard was recently rewritten to The FAA bases their certification procedures on a allow for a streamlined process to introduce new five-year certification program for transport aircraft technology and speed up the certification process following application and a three-year program for which could potentially reduce the cost of aircraft other aircraft, but even the well-established, most certification. The General Aviation Manufacturers experienced applicants typically exceed the five- Association (GAMA) called the new rule “a true year timeframe. One applicant, and other potential breakthrough for the light end of the general applicants, have proposed designs that are typically aviation sector. Rather than having to comply entirely new aircraft with novel systems (i.e., electric with overly prescriptive design requirements, propulsion, fly-by-wire flight controls, tilt rotors, manufacturers will now be able to more nimbly etc.). Due to this, the certification timeframe would
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likely be longer than a typical aircraft of today. that have been used with great success for Manufacturers are mitigating these challenges by decades. Manufacturers such as Zunum Aero working closely with the FAA. are creating designs with a relatively simple Applicants for type certification and production airframe to minimize the complications rather certification benefit the most from well-developed, than going with a complex design. However, detailed plans coordinated with the FAA. Regular manufacturing of hybrid and all electric airplanes updates to the plans and meetings between the may have significant differences from traditional applicants and the FAA are essential. Engagement airplanes. Integration of batteries and cooling with the FAA should occur in the early stages systems on the aircraft for optimization will of design and development so that the FAA can present new challenges. Distributed batteries, develop the appropriate airworthiness standards distributed motors, higher voltages, aerodynamic for the aircraft, and the applicant can adjust their considerations, wiring, among other challenges design to comply with established or expected may require unique manufacturing techniques. regulations with as little impact to their program These things can only be discovered within the schedules as possible. Also, more engagement by context of a full-scale development program. the applicants in ASTM International (formerly One of the keys to making electric and known as American Society for Testing and hybrid-electric aircraft a reality is the ongoing Materials) consensus standards would quicken the development to increase energy density of battery development of these standards which are used technology. Jet fuel has an energy density that is 6 for compliance with the regulations. to 8 times higher than a 500 Wh/kg battery. High The airframe manufacturing of electric and battery storage capacity and light weight batteries hybrid-electric aircraft is not markedly different are critical to fully electric and hybrid-electric than conventional aircraft. Designers have a aircraft. In order to accommodate a commercially number of very reliable construction methods viable payload and range, batteries will need such as composites and traditional aluminum energy density of 500 Watts per Kilogram
Roadmap for Lithium-Ion Battery Technology [Wh/kg] Projected automotive roadmaps indicate batteries will only reach the 500 Wh/kg level required for aerospace after 2025.
Potential for non-automotive applications Li/02 (Li air) technology