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.)
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,
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
Wir haben über zwei Themen vortragen:
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 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 TurbineThe 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+In modern gas turbines, the film cooling technology is essential for the protection of hot parts. Today, shaped holes are widely used, but besides others, the NEKOMIMI-shaped cooling holes have shown that there is still potential to increase the film cooling effectiveness by generation of Anti-Counter-Rotating Vortices (ACRV). As a result, the cooling air remains close to the wall and spreads in lateral direction along the surface. The ACRV result from the special shape of the expanding hole exits (NEKOMIMI-shape). Thus, the design parameters have a crucial impact to the film cooling effectiveness behind the hole. In this study the design parameters are varied and optimized within a multi-objective Pareto optimization in order to show the capabilities of the technology and the potential of HEEDS and Optimate+ for automated design space explorations.
IGTC Tokyo 2015
ASME Turbo Expo 2015, 15-19 Juni
VGB Fachtagung Gasturbinen und Gasturbinenbetrieb, Lübeck, 6/7 Mai
"Certificate of appreciation" von Kawasaki Heavy Industries, LTD.
Dr. Karsten Kusterer, CEO of B&B-AGEMA, wurde von Dr. Minoru Makumura, Senior Vice President of
Kawasaki Heavy Industries, LTD. ein "Certificate of appreciation" für seinen Beitrag zum Kawasaki Hydrogen Project überreicht.|
right: Dr. Minoru Makumura, 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.