Priority Date: 18.11.13 (US 201314082755)

Gas turbine engine turbine blade tip active clearance control system and method

  • Application ID: EP14189292
  • Status: PATENT GRANTED

Applicant

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Specialization

This patent has the IPC combination F01 (MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES) and F02 (COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS) Patent Outsourcing Limited is specialized in the combination F01 and F02. We found, that Kuhnen & Wacker, Dehns Ltd, Beetz & Partner, Martin Reuther Patentanwalt, Bockermann Ksoll Griepenstroh Osterhoff and 36 others are specialized in all of these IPC classes as well. For a similar patent, they might be a good choice.

Timeline

  • 18.11.2013 - Priority Date (US 201314082755)
  • 20.05.2015 - Publication A1 (EP2873813)
  • 21.09.2016 - Publication B1 (EP2873813)

IPC Classification