Gas turbine mixer apparatus
AssigneeThe Boeing Company
InventorPeter K. C. Rudolph
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AssigneeThe Boeing Company
InventorPeter K. C. Rudolph
Estimating the term…
Fluid mixing apparatus for mixing the coaxially flowing streams of fan air and primary exhaust within a turbofan engine are disclosed. Each of the disclosed arrangements include a generally tubular mixer section that extends axially rearward from the engine turbine flange. The mixing apparatus includes axially extending regions in which contiguous portions of the fan stream are induced to flow radially inward to penetrate the primary flowstream and includes axially extending regions in which contiguous portions of the primary flowstream are induced to flow radially outward to penetrate the fan stream. The regions inducing the outwardly directed flow of the primary flowstream and the regions inducing the inwardly directed flow of the fan stream are circumferentially interspersed with one another to establish a flow pattern which causes mixing to occur along the axial length of the mixing apparatus and causes mixing to continue within a common exhaust duct located aft of the mixing apparatus. In some of the disclosed arrangements, a series of deflection vanes are positioned across each of the regions that divert the fan flowstream and each of the regions that divert the primary flowstream. In other arrangements, only the regions for diverting fan flow or the regions for diverting primary flow include such deflection vanes. In each arrangement an annular free mixing boundary is formed along the forward portion of the mixing apparatus to minimize the effect of the mixer geometry on the engine cycle of the gas turbine engine in which the apparatus is employed.
Mixing apparatus for mixing first and second fluid streams with one another wherein said first fluid stream flows through an inner duct and said second fluid stream flows through an annular passageway formed between said inner duct and an outer duct that coaxially surrounds said inner duct, the direction of fluid flow of said first and second fluid streams substantially being in the same axial direction relative to said coaxially arranged inner and outer ducts, said outer duct extending axially in the direction of fluid flow beyond the terminus of said inner duct to define a common duct for the mixing of said first and second fluid streams, said mixing apparatus comprising:
Mixer apparatus for use in combination with a gas turbine engine of the turbofan variety, said turbofan engine including a first fluid duct mounted coaxially within a second fluid duct, said second fluid duct extending rearwardly beyond the aft terminus of said first fluid duct to form a common exhaust duct wherein the primary fluid stream of said turbofan engine passes rearwardly through said first fluid duct and the secondary fluid stream of said turbofan engine passes into said common exhaust duct through the annular passage formed between said first and second fluid ducts, said primary and secondary fluid streams passing rearwardly through said common exhaust duct for discharge into the atmosphere, said mixer apparatus comprising:
Dependencies are inferred from the claim text.