Project Zero | |
---|---|
Role | Experimental tiltrotor VTOL aircraft |
National origin | Italy |
Manufacturer | AgustaWestland |
First flight | June 2011 |
Status | Under development / flight testing |
The AgustaWestland Project Zero is a hybrid tiltrotor/Lift fan aircraft. It has been developed by AgustaWestland as a technology demonstrator, and is used to investigate all-electric propulsion and other advanced technologies. It is the world's first electric tiltrotor aircraft. [1]
In December 2010, AgustaWestland's management approved the formation of a team under James Wang with the intention of producing a technology demonstrator incorporating as many new innovations as possible on a single airframe. [2] Speaking in 2013, Wang noted that electric technologies were rapidly advancing, and that the function of Project Zero was to achieve readiness with electric aircraft technologies: "Rather than waiting for the battery to become even better, then working on electric aircraft technology, the team has positioned itself to be ready for the next generation of batteries". [3]
At AgustaWestland and its partner companies, a total of two dozen full-time engineers worked on the project in a skunkworks-style of development at AgustaWestland's Cascina Costa facility in Italy. [4] According to Wang, those appointed to the team were handpicked, and were typically young and passionate; each member had a specific specialty in one area. [5] The team quickly decided that, instead of pursuing an electric-powered but otherwise conventional airplane or helicopter, a more radical approach would be adopted: A twin-rotor electric tiltrotor, lacking any transmission or swashplates. Wang summarised the team's philosophy as "Anything that is bordline impossible, we want to do". [6]
Noting that the AgustaWestland AW169's development had been completed in under four years, management decided to challenge the team to complete the project within a single year, including initial flight testing. The team worked almost continuously, 24 hours per day and seven days per week for the initial six-month period. [6] Team members did not wait on emails or voicemail, instead going directly to one another in person, being based in the same office, this also assisted in maintaining secrecy - direct teamwork in this fashion was heavily encouraged. [7] AgustaWestland's Advanced Concepts Group performed extensive model testing for the project; this involved the creation of multiple flight-capable 1/10th-scale models, which were flown to test the extremes of the flight envelope due to the aircraft's atypical shape. [2] The use of computer aided design (CAD) tools was also essential to meeting the extremely fast schedule of the program; computational fluid dynamics and finite element modeling were both used extensively. [3]
Various companies in Italy, the UK, the U.S. and Japan worked on the design and/or manufacturing of elements of Project Zero, including four different branches of Finmeccanica. Ansaldo Breda designed a custom-built electric motor inverter and accompanying motor control algorithm, Selex ES provided the High-Integrity Flight Control Computer and the Actuator Control Unit. [8] Lucchi R.Elettromeccanica custom-built the axial flux permanent magnetic motors; Rotor Systems Research LLC worked in conjunction with AgustaWestland on the aerodynamic design of the rotor blades. [6] Lola Composites produced the composite material from which most of the exterior surfaces are made of Carbon-fiber-reinforced polymer (CFRP), while UCHIDA manufactured the composite structure for the rotor blades, shrouds, and spokes. [6] Stile Bertone worked to develop the aesthetic and aerodynamic styling of the aircraft. [8]
The designation Project Zero was derived from an observation that this was a unique internal project with no comparable counterpart within the company's history. [2] The development of Project Zero was conducted within a short amount of time; the time between the start of the design phase and the first flight of the demonstrator itself was less than six months. [8] In order to ensure that tangible benefits from the project were made, it was decided that a full-scale aircraft must be produced and flown. [9] In June 2011, a full-scale demonstrator performed an initial tethered flight at Cascina Costa, Italy. [2] According to Wang, there was no need for any redesigning or corrective work "Everything worked - the whole design - first time". [9]
On 4 March 2013, the existence of the program was announced to the public at the Helicopter Association International (HAI) Heli-Expo. [10] In June 2013, the aircraft was publicly displayed at the Paris Air Show. [11] In early 2014, the Project Zero team was awarded AHS International's prestigious 2014 Grover E. Bell Award—named for Larry Bell's late brother—given to the individual or organization that has fostered and encouraged research and experimentation in helicopter development. [12]
Following the flight testing period, AgustaWestland set about learning from the project and studying means to transfer technologies produced into its existing rotorcraft product line. It has been emphasised that Project Zero itself is not a product, but an investment in technologies to benefit the wider company. [9] In 2016, it was noted that the active blade control system developed for Project Zero, which removes the need for a swash plate and a separate vibration-damping system, was to undergo flight testing on an AgustaWestland AW139; separately, the flight control laws used by Project Zero shall be used for a future tiltrotor project by AgustaWestland. [13]
Various alternative propulsion arrangements for Project Zero have been envisioned by the Advanced Concepts Group, including hybrid diesel propulsion, the incorporation of fuel cells, and other unspecified technologies. [9] In its original configuration, ten minutes flight time is the current operational limit; speaking in 2016, Wang stated that he is hopeful that battery technology will advance within a decade to support a 100-minute operating time. [14]
Project Zero is an unconventional electric-propelled convertiplane of tiltrotor configuration. [6] It is an advanced demonstrator, intended to explore and showcase the capabilities of electric propulsion in aviation. The aircraft is powered by rechargeable batteries. [15] AgustaWestland has stated that, when furnished with a suitable powerplant, the aircraft would be capable of speeds equivalent of traditional tiltrotor designs and possess a typical cruising height double that of a conventional helicopter. [6] The technology demonstrator has not been optimised for production. [6] It can either be flown by a single pilot seated within the cockpit, or alternatively operated as an unmanned aerial vehicle. [14]
Key to Project Zero is the innovative propulsion system that it was developed to demonstrate and test. The two large rotors of the aircraft are driven by advanced electric motors, which are in turn powered by energy stored in batteries [8] [3] The all-electric design eliminates the need for a transmission, as used on conventional aircraft; it also operates with low acoustic and thermal signatures and without a dependency on oxygen. [3] On the ground, the batteries may be recharged by tilting the rotors into the wind to act as turbines. The demonstrator was designed to accommodate numerous different energy sources for the electric motors; an alternative hybrid propulsion option also exists, this uses a lightweight diesel engine to drive a generator to provide electricity for the motors, which was developed by ORAL Engineering. [8] During cruise flight, the majority of the lift is provided by the wings; the outer wings are detachable, which could be useful for shorter range missions mainly using the 'helicopter mode' of flight. [3]
In excess of 80 percent of the aircraft's composition is composite materials, including all of the skin, rotor blades, shroud, and spokes; the structure is almost entirely aluminium and carbon. Materials were selected on the basis of providing the greatest speed at reasonable weight and finance costs. [16] According to the company, the aircraft "employs no hydraulics, doesn't burn fossil fuel and generates zero emissions." [2] In place of hydraulics, electromechanical actuators have been used for functions such as the retraction of the undercarriage, tilting the nacelles, and actuating the aircraft's elevons; these actuators were purpose-developed by Microtecnica. [8]
Key technologies of Project Zero have been patented; a European Patent, EP2551190 (A1), was filed on 29 July 2011 and granted 30 January 2013, [17] while patents (listing James Wang as the inventor) were also granted in parallel in the United States, US2013026303 (A1); [18] Other patents were filed in Korea (KR20130014450 (A)), Japan (JP2013032147 (A)), and China (CN102897317 (A)). [6]
In June 2011, the unmanned demonstrator conducted its first tethered flight at AgustaWestland's Cascina Costa facility in Italy. [2] It was flown in secured areas multiple times in 2011 and 2012, including flights with and without the ducted shrouds around its tilting rotors; a further modification included an alternative and more advanced set of rotor blades with a non-linear twist and custom airfoils being installed. Flight testing allowed for the fine-tuning of the propulsion system, which resulted in a 30 per cent gain in effective power. [2]
Project Zero has made numerous public appearances since being revealed in March 2013. Flight testing has also continued, this has focused on 1/3rd-scale models rather than the full-scale demonstrator due to the limited flight endurance it possesses. In February 2016, it was announced that a hybrid drive system would be installed on the full-scale aircraft, this is aimed at extending the flight endurance from 10 minutes to 35–45 minutes. [13]
External videos | |
---|---|
News coverage of Project Zero at the Paris Air Show 2013 | |
News report in 2016 on Project Zero |
Related lists
A vertical take-off and landing (VTOL) aircraft is one that can take off and land vertically without relying on a runway. This classification can include a variety of types of aircraft including helicopters as well as thrust-vectoring fixed-wing aircraft and other hybrid aircraft with powered rotors such as cyclogyros/cyclocopters and gyrodynes.
A tiltrotor is an aircraft that generates lift and propulsion by way of one or more powered rotors mounted on rotating shafts or nacelles usually at the ends of a fixed wing. Almost all tiltrotors use a transverse rotor design, with a few exceptions that use other multirotor layouts.
AgustaWestland was an Anglo-Italian helicopter design and manufacturing company, which was a wholly owned subsidiary of Finmeccanica. It was formed in July 2000 as an Anglo-Italian multinational company, when Finmeccanica and GKN merged their respective helicopter subsidiaries to form AgustaWestland, with each holding a 50% share. Finmeccanica acquired GKN's stake in AgustaWestland in 2004.
Bell Textron Inc. is an American aerospace manufacturer headquartered in Fort Worth, Texas. A subsidiary of Textron, Bell manufactures military rotorcraft at facilities in Fort Worth, and Amarillo, Texas, USA as well as commercial helicopters in Mirabel, Quebec, Canada.
The Bell XV-15 is an American tiltrotor VTOL aircraft. It was the second successful experimental tiltrotor aircraft and the first to demonstrate the concept's high speed performance relative to conventional helicopters.
A tiltwing aircraft features a wing that is horizontal for conventional forward flight and rotates up for vertical takeoff and landing. It is similar to the tiltrotor design where only the propeller and engine rotate. Tiltwing aircraft are typically fully capable of VTOL operations.
The AgustaWestlandAW609, formerly the Bell/Agusta BA609, is a twin-engined tiltrotor VTOL aircraft with a configuration similar to that of the Bell Boeing V-22 Osprey. It is capable of landing vertically like a helicopter while having a range and speed in excess of conventional rotorcraft. The AW609 is aimed at the civil aviation market, in particular VIP customers and offshore oil and gas operators.
A gyrodyne is a type of VTOL aircraft with a helicopter rotor-like system that is driven by its engine for takeoff and landing only, and includes one or more conventional propeller or jet engines to provide forward thrust during cruising flight. During forward flight the rotor is unpowered and free-spinning, like an autogyro, and lift is provided by a combination of the rotor and conventional wings. The gyrodyne is one of a number of similar concepts which attempt to combine helicopter-like low-speed performance with conventional fixed-wing high-speeds, including tiltrotors and tiltwings.
The Bell XV-3 is an American tiltrotor aircraft developed by Bell Helicopter for a joint research program between the United States Air Force and the United States Army in order to explore convertiplane technologies. The XV-3 featured an engine mounted in the fuselage with driveshafts transferring power to two-bladed rotor assemblies mounted on the wingtips. The wingtip rotor assemblies were mounted to tilt 90 degrees from vertical to horizontal, designed to allow the XV-3 to take off and land like a helicopter but fly at faster airspeeds, similar to a conventional fixed-wing aircraft.
A convertiplane is defined by the Fédération Aéronautique Internationale as an aircraft which uses rotor power for vertical takeoff and landing (VTOL) and converts to fixed-wing lift in normal flight. In the US it is further classified as a sub-type of powered lift. In popular usage it sometimes includes any aircraft that converts in flight to change its method of obtaining lift.
Bell Agusta Aerospace Company (BAAC) was a joint venture formed in 1998 by Bell Helicopter and Agusta, who collaborated on a variety of products dating back to 1952. The joint venture was dissolved in 2011, when AgustaWestland took full ownership of the project, renaming it as the AgustaWestland Tilt-Rotor Company (AWTRC).
A powered lift aircraft takes off and lands vertically under engine power but uses a fixed wing for horizontal flight. Like helicopters, these aircraft do not need a long runway to take off and land, but they have a speed and performance similar to standard fixed-wing aircraft in combat or other situations.
A proprotor is a spinning airfoil that function as both an airplane-style propeller and a helicopter-style rotor. Several proprotor-equipped convertiplanes, such as the Bell Boeing V-22 Osprey tiltrotor, are capable of switching back and forth between flying akin to both helicopters and fixed-wing aircraft. Accordingly this type of airfoil has been predominantly applied to vertical takeoff and landing (VTOL) aircraft.
The Baldwin Mono Tiltrotor project is a research effort into a tiltrotor aircraft that uses only one rotor. Like other tiltrotor configurations, the mono tiltrotor combines the vertical lift capability and structural efficiency of a helicopter with the speed and range of a fixed-wing aircraft.
The Clean Sky Joint Undertaking (CSJU) is a public-private partnership between the European Commission and the European aeronautics industry that coordinates and funds research activities to deliver significantly quieter and more environmentally friendly aircraft. The CSJU manages the Clean Sky Programme (CS) and the Clean Sky 2 Programme (CS2), making it Europe's foremost aeronautical research body.
The Bell V-280 Valor is a tiltrotor aircraft being developed by Bell Helicopter for the United States Army's Future Vertical Lift (FVL) program. The aircraft was officially unveiled at the 2013 Army Aviation Association of America's (AAAA) Annual Professional Forum and Exposition in Fort Worth, Texas. The V-280 made its first flight on 18 December 2017 in Amarillo, Texas.
The Vertical Take-Off and Landing Experimental Aircraft program is an American research project sponsored by the Defense Advanced Research Projects Agency (DARPA). The goal of the program is to demonstrate a VTOL aircraft design that can take off vertically and efficiently hover, while flying faster than conventional rotorcraft. There have been many previous attempts, most of them unsuccessful.
The Leonardo Next-Generation Civil Tiltrotor is a tiltrotor aircraft demonstrator designed and developed by the Italian aerospace company Leonardo S.p.A. Studies for a two times larger tiltrotor than the AgustaWestland AW609 started in 2000. Since 2014, its development is sponsored by the European Union's Clean Sky 2 program. By May 2021, major components were under production By 2023, the maiden flight had been pushed back to 2024, from a 2020 initial plan.
European Future Advanced Rotorcraft (EuroFAR) was a proposed tiltrotor aircraft that was pursued during the 1980s and 1990s. It was a collaborative programme undertaken by the EuroFAR consortium, which comprised Aerospatiale, Agusta, Aeritalia, Messerschmitt-Bölkow-Blohm, Westland, and Construcciones Aeronáuticas SA (CASA).