초록 ▼

A gas turbine engine augmentor includes an inter-liner cavity including an axially extending annular gap separating augmentor and tailpipe liners. A purge flow cavity is in fluid communication with a fan bypass duct and with the cavity. An ejector in fluid communication with the bypass duct includes

A gas turbine engine augmentor includes an inter-liner cavity including an axially extending annular gap separating augmentor and tailpipe liners. A purge flow cavity is in fluid communication with a fan bypass duct and with the cavity. An ejector in fluid communication with the bypass duct includes an ejector nozzle positioned and aimed to direct an ejector nozzle flow from inside the ejector nozzle across the cavity. The purge flow cavity may be bifurcated into forward and aft purge flow cavities which are in fluid communication with the ejector and inter-liner cavity respectively. An annular dividing wall having ejector metering apertures may be disposed between the forward purge flow cavity and an ejector plenum of the ejector. An annular trapped vortex cavity pilot may be located upstream of the annular gap. The aft purge flow cavity may be outwardly bounded by a seal having purge metering apertures disposed therethrough.

대표청구항 ▼

1. A gas turbine engine augmentor comprising: an inter-liner cavity including an axially extending annular gap separating augmentor and tailpipe liners,a purge flow cavity radially outwardly open to and in fluid communication with a fan bypass duct and radially inwardly open to and in fluid communic

1. A gas turbine engine augmentor comprising: an inter-liner cavity including an axially extending annular gap separating augmentor and tailpipe liners,a purge flow cavity radially outwardly open to and in fluid communication with a fan bypass duct and radially inwardly open to and in fluid communication with the inter-liner cavity,an ejector having an ejector nozzle positioned and aimed to direct an ejector nozzle flow from inside the ejector nozzle across the inter-liner cavity,the ejector nozzle having a nozzle flowpath therein and extending and converging aftwardly between an ejector nozzle inlet to an ejector nozzle outlet,the ejector nozzle inlet open to and in fluid communication with an ejector plenum,the purge flow cavity bifurcated into forward and aft purge flow cavities open to and in fluid communication with the fan bypass duct,the ejector plenum located radially inwardly of and in fluid communication with the forward purge flow cavity,the aft purge flow cavity located radially outwardly of and in fluid communication with the inter-liner cavity,a U-shaped wall formed at an aft or downstream end of a bifurcating duct wall bifurcating the annular bypass duct into annular radially outer and inner fan ducts, the U-shaped wall bifurcating the purge flow cavity into the forward and aft purge flow cavities, andthe forward and aft purge flow cavities open to and in fluid communication with the outer fan duct of the fan bypass duct. 2. An augmentor according to claim 1 further comprising an annular dividing wall having ejector metering apertures between the forward purge flow cavity and the ejector plenum. 3. An augmentor according to claim 2 further comprising a forward facing step at an upstream end of the tailpipe liner bordering the annular gap and the ejector nozzle outlet positioned and aimed to further direct the ejector nozzle flow at the forward facing step. 4. An augmentor according to claim 2 further comprising an ejector valve including a conical ejector ring having ejector holes rotatably alignable with the ejector metering apertures. 5. An augmentor according to claim 1 further comprising a forward facing step at an upstream end of the tailpipe liner bordering the annular gap and the ejector nozzle outlet positioned and aimed to further direct the ejector nozzle flow at the forward facing step. 6. An augmentor according to claim 1 further comprising an annular trapped vortex cavity pilot located upstream of the annular gap and operable for initiating and propagating a flame around in a combustion zone in an exhaust flowpath within the augmentor liner. 7. An augmentor according to claim 6 further comprising a forward facing step at an upstream end of the tailpipe liner bordering the annular gap and the ejector nozzle outlet positioned and aimed to further direct the ejector nozzle flow at the forward facing step. 8. An augmentor according to claim 6 further comprising an annular dividing wall having ejector metering apertures between the forward purge flow cavity and the ejector plenum. 9. An augmentor according to claim 8 further comprising a forward facing step at an upstream end of the tailpipe liner bordering the annular gap and the ejector nozzle outlet positioned and aimed to further direct the ejector nozzle flow at the forward facing step. 10. An augmentor according to claim 9 further comprising an ejector valve including a conical ejector ring having ejector holes rotatably alignable with the ejector metering apertures. 11. An augmentor according to claim 10 further comprising an ejector valve including a conical ejector ring having ejector holes rotatably alignable with the ejector metering apertures,the aft purge flow cavity radially outwardly bounded by an annular radially outer aft purge flow cavity seal having an annular array of purge metering apertures disposed therethrough, anda purge valve including a conical purge ring having purge holes rotatably alignable with the purge metering apertures. 12. An augmentor according to claim 1 further comprising the aft purge flow cavity radially outwardly bounded by an annular radially outer aft purge flow cavity seal having an annular array of purge metering apertures disposed therethrough. 13. An augmentor according to claim 12 further comprising a forward facing step at an upstream end of the tailpipe liner bordering the annular gap and the ejector nozzle outlet positioned and aimed to further direct the ejector nozzle flow at the forward facing step. 14. An augmentor according to claim 12 further comprising an annular trapped vortex cavity pilot located upstream of the annular gap and operable for initiating and propagating a flame around in a combustion zone in an exhaust flowpath within the augmentor liner. 15. An augmentor according to claim 12 further comprising an annular dividing wall having ejector metering apertures between the forward purge flow cavity and the ejector plenum, andan ejector valve including a conical ejector ring having ejector holes rotatably alignable with the ejector metering apertures and a purge valve including a conical purge ring having purge holes rotatably alignable with the purge metering apertures. 16. An augmentor according to claim 12 further comprising an annular dividing wall having ejector metering apertures between the forward purge flow cavity and the ejector plenum. 17. An augmentor according to claim 16 further comprising a forward facing step at an upstream end of the tailpipe liner bordering the annular gap and the ejector nozzle outlet positioned and aimed to further direct the ejector nozzle flow at the forward facing step.