(19)
(11)EP 2 725 192 A3

(12)EUROPEAN PATENT APPLICATION

(88)Date of publication A3:
05.11.2014 Bulletin 2014/45

(43)Date of publication A2:
30.04.2014 Bulletin 2014/18

(21)Application number: 13179919.9

(22)Date of filing:  09.08.2013
(51)International Patent Classification (IPC): 
F01D 5/14(2006.01)
F01D 5/28(2006.01)
(84)Designated Contracting States:
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
Designated Extension States:
BA ME

(30)Priority: 25.10.2012 US 201213660989

(71)Applicant: General Electric Company
Schenectady, New York 12345 (US)

(72)Inventor:
  • Garcia-Crespo, Andres Jose
    Greenville, SC South Carolina 29615 (US)

(74)Representative: Cleary, Fidelma 
GPO Europe GE International Inc. The Ark 201 Talgarth Road Hammersmith
London W6 8BJ
London W6 8BJ (GB)

  


(54)Turbomachine blade reinforcement


(57) Embodiments of the present invention include a system having a turbomachine blade segment including a blade (22) and a mounting segment (50) coupled to the blade (22), wherein the mounting segment (50) has a plurality of reinforcement pins (60) laterally extending at least partially through a neck (62) of the mounting segment (52).







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