초록

The present invention provides a non-axisymmetric flow member disposed in a duct of a gas turbine engine. The flow member narrows the area aft of a vane to reduce the cross sectional area through which a wake from the vane traverses.

대표청구항 ▼

1. An apparatus for use in a gas turbine engine comprising: an inner wall member;an outer wall member spaced from the inner wall member to define a fluid flowpath;a compressor including a guide vane stage located upstream from the fluid flowpath, the guide vane stage including a plurality of vanes p

1. An apparatus for use in a gas turbine engine comprising: an inner wall member;an outer wall member spaced from the inner wall member to define a fluid flowpath;a compressor including a guide vane stage located upstream from the fluid flowpath, the guide vane stage including a plurality of vanes positioned around a portion of the fluid flowpath; anda plurality of elongated protrusions located downstream of the guide vane stage and extending into the fluid flowpath. 2. The apparatus of claim 1 wherein the fluid flowpath is either s-shaped or bifurcated. 3. The apparatus of claim 1, wherein the plurality of elongated protrusions extend into the fluid flowpath up to about 30% of the distance between the inner wall and the outer wall. 4. The apparatus of claim 1, wherein the inner wall member includes an inner wall diffusion, the outer wall includes an outer wall diffusion, and the plurality of elongated protrusions is formed in the wall having the higher diffusion. 5. The apparatus of claim 1, wherein at least one of the plurality of protrusions is located downstream of each of the plurality of vanes. 6. The apparatus of claim 1, wherein one of the plurality of protrusions is located on each of the inner wall and outer wall downstream of each of the plurality of vanes. 7. The apparatus of claim 1, wherein at least one of the plurality of elongated protrusions is operatively connected to an actuator. 8. The apparatus of claim 1, wherein at least one of the plurality of elongated protrusions is passive. 9. An apparatus comprising: a fluid flowpath;a compression stage located upstream from the fluid flow path;a plurality of guide vanes positioned circumferentially around a portion of the fluid flowpath; anda plurality of restrictors located in the fluid flowpath for preventing separated flow downstream of the guide vanes. 10. The apparatus of claim 9, wherein the compression stage is a compressor. 11. The apparatus of claim 9, wherein the compression stage is a fan. 12. The apparatus of claim 9, wherein the restrictors are disposed on a rotor. 13. The apparatus of claim 9, wherein the plurality of restrictors extend into the flowpath. 14. The apparatus of claim 9, wherein each of the plurality of restrictors is elongate in shape. 15. The apparatus of claim 14, wherein the elongate shape has a length to width ratio of 3:1. 16. A method comprising: rotating a rotatable stage of a compressor to increase the pressure of a working fluid;flowing the working fluid through an outlet guide vane stage into a fluid flow passageway;encountering a protrusion that includes a first circumferential lateral side, a second circumferential lateral side, and an intermediate portion higher than the first circumferential lateral side and the second circumferential lateral side; andcontrolling the diffusion in the fluid flow passageway as a result of said encountering. 17. The method of claim 16, wherein in the encountering includes a plurality of protrusions extending into the flowpath downstream of the outlet guide vane stage. 18. The method of claim 17, wherein the controlling includes actuating at least one of the plurality of protrusions. 19. The method of claim 16, wherein the controlling includes changing the diffusion of the fluid flow after the outlet guide vane from that of the core flow in the duct.