Methods and apparatus for assembling turbine engines

Details Methods and apparatus for assembling turbine engines Methods and apparatus for assembling turbine engines

2008-04-22

2008-04-22

Look, Edward K. (Department: 3745)

Rotary kinetic fluid motors or pumps

With diversely oriented inlet or additional inlet for...

C029S889220, C060S796000

Reexamination Certificate

active

11297672

ABSTRACT:
A method facilitates the assembly of a gas turbine engine. The method comprises providing a turbine nozzle including an inner band, an outer band, and at least one vane extending between the inner and outer bands, wherein the vane includes a first sidewall and a second sidewall connected together at a leading edge and a trailing edge and coupling the turbine nozzle to a combustor that includes a plurality of circumferentially-spaced cooling openings that are oriented with respect to the turbine nozzle such that cooling air discharged therefrom during engine operation is biased towards the vane leading edge.

REFERENCES:
patent: 3965066 (1976-06-01), Sterman et al.
patent: 4821522 (1989-04-01), Matthews et al.
patent: 5417545 (1995-05-01), Harrogate
patent: 5470198 (1995-11-01), Harrogate et al.
patent: 6227798 (2001-05-01), Demers et al.
patent: 6398488 (2002-06-01), Solda et al.
patent: 6612811 (2003-09-01), Morgan et al.
patent: 6684626 (2004-02-01), Orlando et al.
patent: 6893217 (2005-05-01), Brainch et al.
patent: 6921246 (2005-07-01), Brainch et al.
patent: 6935837 (2005-08-01), Moniz et al.
patent: 6969233 (2005-11-01), Powis et al.
patent: 6983608 (2006-01-01), Allen, Jr. et al.

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