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Method of assembly of bi-cast turbine vane
One aspect of the present disclosure includes a turbine vane assembly comprising a vane made from ceramic matrix composite material having an outer wall extending between a leading edge and a trailing edge and between a first end and an opposing second end; an endwall made at least partially from a ceramic matrix composite material configured to engage the first end of the vane; and a retaining region including corresponding bi-cast grooves formed adjacent the first end of the vane and a receiving aperture formed in the endwall; wherein a bond is formed in the retaining region to join the vane and endwall together.
Method of assembly of bi-cast turbine vane
One aspect of the present disclosure includes a turbine vane assembly comprising a vane made from ceramic matrix composite material having an outer wall extending between a leading edge and a trailing edge and between a first end and an opposing second end; an endwall made at least partially from a ceramic matrix composite material configured to engage the first end of the vane; and a retaining region including corresponding bi-cast grooves formed adjacent the first end of the vane and a receiving aperture formed in the endwall; wherein a bond is formed in the retaining region to join the vane and endwall together.
Method of assembly of bi-cast turbine vane
FREEMAN TED J (author) / PROCTOR ROBERT F (author) / LANDWEHR SEAN E (author) / CHAMBERLAIN ADAM L (author)
2020-04-07
Patent
Electronic Resource
English
IPC:
F01D
Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen
,
NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
/
B23P
Sonstige Metallbearbeitung
,
OTHER WORKING OF METAL
/
B29C
Formen oder Verbinden von Kunststoffen
,
SHAPING OR JOINING OF PLASTICS
/
C04B
Kalk
,
LIME
AIRFOIL ASSEMBLY FOR A GAS TURBINE ENGINE, CORRESPONDING VANE AND METHOD OF ASSEMBLING A VANE
European Patent Office | 2025
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