초록 ▼

Flow restrictors (4), (14) are widely utilized with regard to providing flow control in such situations as with respect to sealing and pressurization of bearing chambers in gas turbine engines. The restrictor (4), (14) restricts a flow (5), (15) but with prior arrangements may be susceptible to depo

Flow restrictors (4), (14) are widely utilized with regard to providing flow control in such situations as with respect to sealing and pressurization of bearing chambers in gas turbine engines. The restrictor (4), (14) restricts a flow (5), (15) but with prior arrangements may be susceptible to deposition upon flank surfaces of the restrictor (4). These depositions may fragment and block an aperture (7), (17) of the restrictor (4), (14) reducing operational effectiveness. By provision of a deflector (18) having a deflector surface (19) flows (15) can be presented such that a greater proportion of the flow including droplets or other matter which may result in surface deposition or erosion will pass directly through an aperture (7, 17) rather than impinge upon the flank surfaces of the restrictor (14). Furthermore, the deflector (18) is dimensioned such that surfaces which may be susceptible to deposition have dimensions smaller than the aperture (17).

대표청구항 ▼

1. A flow control arrangement comprising: a flow path,a flow restrictor in the flow path of reduced area relative to the flow path,a deflector provided upstream of the flow restrictor in the flow path at a displaced position and orientated towards the restrictor, anda sealing arrangement upstream of

1. A flow control arrangement comprising: a flow path,a flow restrictor in the flow path of reduced area relative to the flow path,a deflector provided upstream of the flow restrictor in the flow path at a displaced position and orientated towards the restrictor, anda sealing arrangement upstream of the deflector and configured to provide a fluid flow comprising solid or fluid particles entrained in a gas, whereinthe deflector comprises at least one deposition surface having a width less than a width of the reduced area of the flow restrictor,the deflector is displaced upstream of the restrictor between four and six times the width of the reduced area of the flow restrictor,the deflection surface includes a sacrificial deposition area for deposits taken from the flow, andthe deposition area is arranged to limit deposition particle sizes upon fragmentation from the deposition area. 2. An arrangement as claimed in claim 1 wherein the deflector has a deflector surface at a deflection angle towards a position upstream of the restrictor. 3. An arrangement as claimed in claim 2 wherein the position is along a vent axis central to the flow path and/or the restrictor. 4. An arrangement as claimed in claim 2 wherein the deflection angle is dependent upon an expected flow rate for the flow in use. 5. An arrangement as claimed in claim 2 wherein the deflection angle can be adjusted. 6. An arrangement as claimed in claim 1 wherein the deflection surface has a width sufficient to deflect the flow in use. 7. An arrangement as claimed in claim 1 wherein the deflection surface is smooth. 8. An arrangement as claimed in claim 1 wherein the deflection surface is undulated or grooved. 9. An arrangement as claimed in claim 1 wherein the deposition area has a width less than the restrictor size. 10. An arrangement as claimed in claim 1 wherein the deflection surface includes a coating to inhibit deposition. 11. An arrangement as claimed in claim 1 wherein the deflector is variably deployable into the flow path. 12. An arrangement as claimed in claim 1 wherein the flow in use is air with entrained oil droplets. 13. An arrangement as claimed in claim 1 wherein the flow in use is air with entrained particulate matter, where deposition and build is possible. 14. An arrangement as claimed in claim 1 wherein the flow deflection feature is hardened or otherwise treated to sacrificially resist erosion. 15. An arrangement as claimed in claim 1 wherein the restrictor is an orifice. 16. A gas turbine engine incorporating a flow control arrangement as claimed in claim 1.