| 1. |
- Grönstedt, Tomas, 1970, et al.
(författare)
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Catalytic Burner Device
- 2007
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Annan publikation (övrigt vetenskapligt/konstnärligt)abstract
- The invention relates to gas turbine engine comprising a first flow passage, and main combustion means in the first flow passage. The engine further comprises a second flow passage, and first catalytic combustion means in the second flow passage, wherein the second flow passage can communicate with the first flow passage at at least one upstream passage junction upstream of the main combustion means and upstream of the first catalytic combustion means, and the second flow passage can communicate with the first flow passage at at least one downstream passage junction downstream of the main combustion means and downstream of the first catalytic combustion means.
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| 2. |
- Grönstedt, Tomas, 1970
(författare)
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Effektivare motorer, flyget och miljön
- 2018
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Annan publikation (övrigt vetenskapligt/konstnärligt)abstract
- Flyget står inför stora mijöutmaningar. I presentationen ges fyra punkter där stora miljövinster kan åstadkommas och detta backas med teknik och åtgärder som kan stödja framstegen.
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| 3. |
- Grönstedt, Tomas, 1970
(författare)
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In response to the public consultation on Clean Aviation Partnership: A short comment on ultra-efficient gas turbines and sustainable aviation fuels
- 2020
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Annan publikation (övrigt vetenskapligt/konstnärligt)abstract
- This two-page comment on the Clean Aviation SRIA, contains output from two Horizon 2020 projects, ULTIMATE (ultra-efficient engines) and ENABLEH2 (hydrogen aircraft). The report has also been updated by a coordinated effort on collecting strategic inputs from Chalmers University of Technology. Some output from efforts on road-mapping conducted together with leading aero engine manufacturers is also supporting this comment. The comment concentrates on giving input on the two key thrusts “3. Ultra-efficient Aircraft and Gas Turbines” and “4. Sustainable Aviation Fuels enabled Aircraft”. However, for all four thrust areas, it is noted that as aircraft design complexity increases the need for dynamic modelling, energy management and optimal control increases.
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| 4. |
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