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PUMAc-Fx: Aggregate Made in Aachen - Fuel X
Entwicklung einer ultraleichten Wasserstoffgasturbine mit maximaler Kraftstoffflexibilität (von 100% H2 bis Diesel/Kerosin)
Nun erhielten wir vom Bundesministerium für Bildung und Forschung (BMBF) grünes Licht für die erste Projektphase ab September 2020. (BMBF-Pressemitteilung)Wahl von Prof. Bohn in den Vorstand der ASUE
Webinar zum Thema Brennkammer Design mit Siemens PLM
Neuer Artikel im International Journal of Gas Turbine
B&B-AGEMA feiert ihr 25-jähriges Firmen-Jubiläum

International Gas Turbine Congress (IGTC), 17.-22. November 2019, Tokyo, Japan
- Comparison between RANS and Large Eddy Simulations for Nekomimi and 777-Shaped Film Cooling Holes
- Numerical Simulations of the Micromix DLN Hydrogen Combustion Technology
with LES and Comparison to Results of RANS and Experimental Data - Development of an Air Cooled Borescope for Infrared Thermal Load Monitoring
in Industrial Gas Turbine Combustors and Operational Experience
“Application of Low NOx Micro-Mix Hydrogen Combustion to 2MW Class Industrial Gas Turbine Combustor” (Horikawa, A., et al.)
Mitgliedschaft ASUE
Simcenter Conference - Europe, 3.-5. Dezember 2018, Prague, Tschechische Republik
VDI Wissensforum, 29.-30. November 2018
Simcenter Conference - Americas, 15.-17. Oktober 2018, Detroit, USA
International Gas Turbine Conference (IGTC), 10.-11. Oktober 2018, Brüssel, Belgien
International Symposium on Pump and Fan Technology, 26.-28. September 2018,
Shenyang, China
ETC 2017, Stockholm, Sweden, April 2017:
SGT5-4000F User Conference, Helsinki, 11-13 October 2016
VDI Spezialtag: „Schäden an Gasturbinen“, Nürnberg, 15. November 2016
ASME 2016, Seoul, South Korea, June 2016
Conjugate Heat Transfer Analysis of a Blade Leading Edge Cooling Configuration Using Double Swirl Chambers
Design Space Exploration of Advancded-Shaped Film Cooling Holes using the Sherpa Algorithm
B&B-AGEMA ist Mitglied der "Gas Turbine Society of Japan"
Contributing Organizations to GTSJ
ISROMAC 2016, Honolulu, 16. April 2016
Conjugate Heat Transfer Simulations for a Film Cooled Nozzle Guide Vane of a High-efficiency, Industrial Gas Turbine
The conjugate heat transfer (CHT) calculation technique is used for the three-dimensional thermal load prediction of an extensively cooled 1st nozzle test vane installed in a highest-efficient industrial gas turbine. The utilized numerical model contains all geometrical features (e.g. pin-fins, ribs, impingement sheets etc.) of the real test vane without simplifications. The comparison with thermal index paint measurements inside the test engine shows that a qualitatively and quantitatively good agreement between the CHT and the measurements results can be found. A consideration of advanced-shaped film cooling holes at the vane platforms also offers high potential to further reduce the material temperatures and decrease thermal stresses by lowering of platform temperatures and homogenization of the temperature distribution.STAR Global Conference, 07-09 March 2016, Prague
Design Space Exploration of Gas Turbine Film Cooling Holes with HEEDS & Optimate+

"Certificate of appreciation" von Kawasaki Heavy Industries, LTD.
Dr. Karsten Kusterer, CEO of B&B-AGEMA, wurde von Dr. Minoru Makimura, Senior Vice President of
Kawasaki Heavy Industries, LTD. ein "Certificate of appreciation" für seinen Beitrag zum Kawasaki Hydrogen Project überreicht.![]() right: Dr. Minoru Makimura, Senior Vice President, Kawasaki Heavy Industries, LTD. middle: Dr. Karsten Kusterer, Geschäftsführer B&B-AGEMA GmbH left: Dr. Koji Kadota, General Manager Corporate Technology Division, Kawasaki Heavy Industries LTD. |