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| === Open rotor === | | === Open rotor === |
| [[File:Open rotor.png|left|thumb|250x250px]]
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| Safran's commitment to research and development is exemplified by its groundbreaking work on the Open Rotor, an innovative aircraft engine design. The Open Rotor project, featuring two counter-rotating propellers and no thrust reversers, represents a transformative approach to enhance fuel efficiency and reduce carbon emissions in the aviation sector. By pushing the boundaries of technology and collaborating with industry partners, Safran has demonstrated the feasibility of the Open Rotor concept through successful testing and research, positioning itself at the forefront of sustainable aviation solutions.<ref>https://www.safran-group.com/fr/actualite/quel-avenir-lopen-rotor-2019-03-28</ref>
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| Safran's dedication to the Open Rotor project underscores its vision for the future of aviation, striving to meet the industry's environmental challenges head-on. As the company continues to explore and develop this revolutionary engine architecture, Safran's R&D efforts highlight its commitment to driving innovation and shaping a greener, more sustainable aviation landscape for generations to come.
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| === Hydrogen engine === | | === Hydrogen engine === |