Pipistrel Partners In ARTEM Project | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-08.08.22

Airborne-Uncrewed-08.09.22

Airborne-Unlimited-08.10.22

Airborne-Flight Training-08.11.22

Airborne-Unlimited-08.12.22

Sat, Apr 04, 2020

Pipistrel Partners In ARTEM Project

Aircraft Noise Reduction Technologies And Related Environmental iMpact Studies Aircraft Configurations

Pipistrel is a project partner in the ARTEM project (Aircraft noise Reduction Technologies and related Environmental iMpact) that aims at the maturing of promising novel concepts and methods which are directly coupled to new low noise and disruptive 2035 and 2050 aircraft configurations.

Last week, members of Pipistrel Vertical Solutions (PVS) research have just returned from a week long wind tunnel testing in INCAS, Bucharest. The team was performing tests on a composite design model wing with modular attachment points for different Distributed Electrical Propulsion (DEP) configurations, designed and built by PVS within the ARTEM European project.

ARTEM is a four-year European Union‘s Horizon 2020 research project devoted to the development of novel noise reduction technologies for low-noise 2035 and 2050 aircraft configurations.

PVS involvement in the ARTEM project is on the investigation of novel DEP aircraft configurations, whose global objective is the investigation and mitigation of noise emissions of DEP systems. Together with three ARTEM partners, VKI, ONERA and INCAS, PVS explored two different configurations of such integration. The mock-up is composed out of the main wing and three propellers positioned in front of the wing, resulting in the 'tractor configuration', or on top of the wing, resulting in the 'pusher configuration'.

PVS worked on the general definition of the DEP mock-up, defining all necessary functional requirements for the experiment. The conceptual and preliminary design phases followed with the selected concept having a modular design allowing for spanwise, chordwise and vertical positioning of the propellers in both configurations. An aerofoil profile, especially suited for DEP systems, was carefully designed. During the preliminary and detailed design phases a thorough numerical assessment of the DEP wing and subsystems was done using RANS/URANS CFD. In the detailed design phase, PVS finished the geometry and dimensioned the structure to withstand the loads imposed in the wind tunnel with minimal deflections. The wing shell and main spar were dimensioned to have less than 2 mm deflection on a 100-inch span in the nominal 30m/s loading condition at maximum AoA. The structure was also tested numerically with FEM, which predicts a factor of safety of 30 in the nominal design case.

Once the design was frozen, PVS finished the complete technical documentation for the moulds, integral wing parts and modules. The model wing was produced to the highest production standards using modern manufacturing technologies. Innovative production solutions were developed when facing very limited space within a 12-inch chord and merely 2-inch maximum thickness of the cross section. The mock-up seamlessly combines composite, aluminium and 3D printed parts in order to ensure quality and technical excellence while retaining a competitive price.

Finally, PVS operated the mock-up during the wind tunnel tests at INCAS to speeds up to 97 knots. Both configurations were successfully tested at INCAS wind tunnel in order to identify the noise sources and their relative weights between the wing and propeller regions, and between the tonal and broadband contributions. Experimental data will be at great help to the task partners to analyze parametric sensibilities of the noise in order to identify parameters of interest for acoustic reduction.

DEP type of propulsion became feasible with the introduction of state-of-the-art electric motors and offers numerous potential noise reduction configurations. It offers more degrees of freedom during the integration of a propulsion system on an aircraft. This is why PVS is heavily invested in facilitating research of such topics through implementing our broad spectre of knowledge and experience to bring ideas to life in a very fast cycle.

Most favorable configuration with respect to the acoustic and aerodynamic performance will be selected by PVS at the end of the project, and full recommendations for designing the state-of-the-art DEP system will be provided.

(Source: Pipistrel news release. Images provided)

FMI: www.pipistrel.com

Advertisement

More News

NASA Announces Astronaut Corps Ready For Artemis

Moon Project to Draw Upon Whole Corps of all Flight-Qualified Astronauts NASA has announced that the entire body of qualified astronauts in current service with the agency stand as>[...]

Aero-News: Quote of the Day (08.12.22)

“This announcement marks a new important phase in our relationship with Archer, and our commitment to eVTOL technology. We are witnessing an inflection point where consumers,>[...]

ANN's Daily Aero-Term (08.12.22): National Beacon Code Allocation Plan Airspace

National Beacon Code Allocation Plan Airspace (NBCAP) Airspace over United States territory located within the North American continent between Canada and Mexico, including adjacen>[...]

ANN's Daily Aero-Linx (08.12.22)

Aero Linx: The Lancair Owner & Builders Organization (LOBO) The Lancair Owner & Builders Organization (LOBO) is a collaborative group and type club for all people who own, >[...]

ANN's Daily Aero-Linx (08.13.22)

Aero Linx: The British Airline Pilots’ Association (BALPA) The British Airline Pilots’ Association (BALPA) is the professional association and registered trade union es>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2022 Web Development & Design by Pauli Systems, LC