2013[3] Part 23 certification anticipated for in 2022[4][5]
Status
In development
The gasoline-powered version of the Panthera is intended to cruise at 198 KTAS (366.7 km/h) at FL 080 for over 1,000 nmi (1,852 km) with a 14.8 gph (56 L/h) fuel burn. There are two other versions planned, one with a 145kW hybrid-electric power system, and the other with a 145kW pure electric system. These two latter variants will only seat two people to accommodate the electric systems.[3][6][7][8][9]
The company is offering the Panthera as an experimental aircraft, either factory-built or as a kit for amateur construction, with the type certified variant expected in 2022.[4]
Design and development
Pipistrel Panthera roll-out
In May 2011, Pipistrel was working on constructing the prototype, powered by the Lycoming engine, with all of the aircraft molds already completed. The first flight was planned for autumn of the same year, with the aircraft being tested the following summer with the electric technologies derived from the Green Flight Challenge electric Taurus project. It will be initially offered in kit form, and Pipistrel indicated that construction will take place in Italy.[10]
Features of the aircraft will include an airframe ballistic parachute designed for use at high speeds and low altitudes[11] and a glass cockpit.[3] The Pipistrel Panthera has an all-composite airframe, made from carbon fiber, glass fiber, and kevlar, and it sports trailing-link electrically retractible landing gear made of titanium and aluminum alloys,[12] which will be of benefit for operations from grass runways.[13] The composite materials used for the exterior of the aircraft were selected in part based on their ability to withstand lightning strikes,[14][15] which merit increased consideration when employing composite materials instead of a traditional aluminum airframe.[16]
In March 2014 it was announced that the intended four-cylinder Lycoming IO-390 powerplant will be replaced by a six-cylinder Lycoming IO-540. The change was made due to Lycoming Engines not planning to certify the IO-390 for automotive fuel as an option. The IO-540 will provide the same cruise performance and fuel economy, but weighs 41kg (90lb) more. However, it will allow the Panthera's gross weight to be increased by 95.25kg (210lb) to make up for the extra weight. The aircraft will use the existing cowling, which was originally designed to accommodate a six-cylinder engine anyway.[17]
Operational history
Pipistrel Panthera public presentation at AERO Friedrichshafen 2012
A test article was introduced at AERO Friedrichshafen 2012 in April 2012. On March 29, 2013, the Panthera had its first successful engine start, using a 210hp (157kW) Lycoming engine,[18] and subsequently began taxi tests[18][19] in preparation for the "complete flight test programme".[18] The Pipistrel Panthera made its 54-minute maiden flight less than one week later on April 4, starting the evaluations of performance, handling and systems in flight.[1][2] Less than one month later, the Panthera flew over the Alps to the Aero fair at the Friedrichshafen Airport.[20]
The EU funded the Hypstair program over three years till 2016: a Panthera mockup received a serial hybrid-electric powertrain, ground testing a 200-kW motor driven by batteries only, by a 100-kW generator-only and by both combined.
It is followed by Mahepa project from 2017, EU-funded over four years.
The Panthera drivetrain will be divided in modules: electric motor thrust generator and internal combustion power generator in the nose, human-machine interface and computing, fuel and batteries in the wing.
Ground testing is planned for 2019 before flight tests in 2020.[21] In October 2021, Pipistrel and the Mahepa consortium announced the hybrid-electric version of the Panthera has completed the first phase of its flight test program.[22]
Variants
Panthera (IO-360)
Initial experimental variant powered by a Lycoming IO-360, 210hp (160kW) engine.[4] 3 units built.
Panthera (IO-540)
Experimental variant powered by a Lycoming IO-540, 260hp (190kW) engine.[4]
Panthera Individual
Experimental homebuilt kit variant powered by a Lycoming IO-540 engine.[4]
Panthera EASA TC
EASA CS-23 type-certified variant, powered by a Lycoming IO-540 engine. Launch expected in 2022.[4]
Panthera Hybrid
Variant equipped with a hybrid-electric powertrain. In development.[4]
Panthera Electro
Battery-powered fully electric variant. In development.[4]
Powerplant: 1 × Lycoming IO-540-V4A5 six cylinder piston aircraft engine, 190kW (260hp) Variants will include a hybrid system and a pure electric option, each 150kW (201hp) continuous power.
Propellers: 3-bladed
Performance
Cruise speed: 359km/h (223mph, 194kn) at 75% power, FL080
Stall speed: 102km/h (63mph, 55kn) flaps extended
Never exceed speed: 410km/h (250mph, 220kn)
Range: 1,900km (1,200mi, 1,000nmi) at 155 KTAS, FL120, with 4 people aboard
Service ceiling: 7,600m (25,000ft)
Rate of climb: 6.6m/s (1,300ft/min) at MTOM and VY
Fuel consumption:14.8USgal (56l) per hour
Avionics
Garmin G3X GDU 460 dual 10-inch display PFD and MFD
Garmin GMC 307 2-axis GPS-slaved digital autopilot
Garmin GTN 750 Xi Com/Nav/IFR GPS
Garmin GTX 345R Transponder
See also
Aircraft of comparable role, configuration, and era
Другой контент может иметь иную лицензию. Перед использованием материалов сайта WikiSort.org внимательно изучите правила лицензирования конкретных элементов наполнения сайта.
2019-2025 WikiSort.org - проект по пересортировке и дополнению контента Википедии