F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
F - Mech Eng,Light,Heat,Weapons
01
D
F01D 9/02 (2006.01) F23R 3/02 (2006.01)
Patent
CA 2570631
A turbine engine nozzle assembly (50) includes an outer band (54) including a leading edge (70), a trailing edge (74), and a body (78) extending therebetween; an inner band (56) including a leading edge (72), a trailing edge (76), and a body (78) extending therebetween; and at least one vane (52) extending between the outer and inner bands including a first sidewall (60) and a second sidewall (62) connected together at a leading edge (64) and a trailing edge (66), the at least one vane leading edge (64) being positioned downstream from the inner and outer band leading edges. The turbine engine nozzle assembly (50) further includes a retention system to couple the nozzle to an engine combustor that includes a first annular ring (290) coupled between the outer band and the combustor, and a second annular ring (291) coupled between the inner band and the combustor.
Fortuna Douglas Marti
Guentert Joseph M.
Iles Mitchell E.
Lee Ching-Pang
Lu Wenfeng
Company General Electric
Craig Wilson And Company
LandOfFree
Methods and apparatus for assembling turbine engines does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Methods and apparatus for assembling turbine engines, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Methods and apparatus for assembling turbine engines will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-1349407