초록 ▼

A gas turbine engine thermal control apparatus includes at least one annular spray tube having spray holes oriented to impinge thermal control air onto a fillet between an outer casing and a forward thermal control ring and, in a more particular embodiment, into a center of the fillet. The apparatus

A gas turbine engine thermal control apparatus includes at least one annular spray tube having spray holes oriented to impinge thermal control air onto a fillet between an outer casing and a forward thermal control ring and, in a more particular embodiment, into a center of the fillet. The apparatus may include an annular segmented stator shroud attached to the outer casing and circumscribing radial outer blade tips of turbine blades of a turbine rotor. A thermal air distribution manifold encircling a portion of the outer casing includes an annular supply tube connected in fluid supply relationship to plenums of header assemblies. The annular spray tube is connected to at least one of the plenums and may be elongated radially inwardly and axially. Baffles attached to radially outwardly facing surfaces of the panels may be contoured to form exhaust passages having exhaust passage inlets and outlets between the baffles and the panels.

대표청구항 ▼

What is claimed is: 1. A thermal control apparatus comprising: at least one annular spray tube having spray holes oriented to impinge thermal control air onto a fillet between an outer casing and a forward thermal control ring, the annular spray tube being circumscribed about an axis and elongated

What is claimed is: 1. A thermal control apparatus comprising: at least one annular spray tube having spray holes oriented to impinge thermal control air onto a fillet between an outer casing and a forward thermal control ring, the annular spray tube being circumscribed about an axis and elongated radially inwardly, and the annular spray tube having a generally light bulb cross-sectional shape with a circular radially outer cross-sectional portion connected to a smaller circular radially inner cross-sectional portion by a transition section, the circular radially outer cross-sectional portion having a cross-sectional first diameter, the circular radially inner cross-sectional portion having a cross-sectional second diameter, the transition section having a radially outer maximum cross-sectional third diameter and a radially inner minimum cross-sectional fourth diameter, and the cross-sectional second diameter, the cross-sectional third diameter, and the cross-sectional fourth diameter all being substantially smaller than the cross-sectional first diameter. 2. A thermal control apparatus as claimed in claim 1 further comprising an annular segmented stator shroud mounted to the outer casing and the shroud circumscribing radial outer blade tips of turbine blades of a turbine rotor. 3. A thermal control apparatus as claimed in claim 1 further comprising: a thermal air distribution manifold encircling a portion of the outer casing, the manifold including an annular supply tube connected in fluid supply relationship to a plurality of plenums of a plurality of header assemblies, and the annular spray tube connected in fluid supply relationship to at least one of the plurality of plenums and having spray holes oriented to impinge thermal control air onto a fillet between the outer casing and a thermal control ring. 4. A thermal control apparatus as claimed in claim 3 further comprising an annular segmented stator shroud attached to the outer casing and the shroud circumscribing radial outer blade tips of turbine blades of a turbine rotor. 5. A thermal control apparatus as claimed in claim 3 further comprising the spray holes being oriented to impinge the thermal control air into a center of the fillet. 6. A thermal control apparatus as claimed in claim 5 further comprising an annular segmented stator shroud mounted to the outer casing and the shroud circumscribing radial outer blade tips of turbine blades of a turbine rotor. 7. A thermal control apparatus as claimed in claim 3 further comprising: the manifold further including a plurality of header assemblies circumferentially positioned around the outer casing, each one of the header assemblies including one or more of the plenums, and an annular segmented stator shroud attached to the outer casing and the shroud circumscribing radial outer blade tips of turbine blades of a turbine rotor. 8. A thermal control apparatus comprising: a thermal air distribution manifold encircling a portion of an outer casing, the manifold including an annular supply tube connected in fluid supply relationship to a plurality of plenums of a plurality of header assemblies, and a plurality of annular spray tubes connected in fluid supply relationship to at least one of the plurality of plenums and having only spray holes oriented to impinge thermal control air onto fillets between the outer casing and at least two thermal control rings, the header assemblies including base panels, headers connected to the supply tube and attached to radially outer sides of the base panels forming the plenums therebetween, first panel holes disposed through the base panels forming inlets for the thermal control air to flow from the plenums to the plurality of spray tubes, and baffles brazed or otherwise attached to radially outwardly facing surfaces of the base panels. 9. A thermal control apparatus comprising: a thermal air distribution manifold encircling a portion of an outer casing, the manifold including an annular supply tube connected in fluid supply relationship to a plurality of plenums of a plurality of header assemblies, and a plurality of annular spray tubes connected in fluid supply relationship to at least one of the plurality of plenums and having only spray holes oriented to impinge thermal control air onto fillets between the outer casing and at least two thermal control rings, the header assemblies including base panels, the header assemblies including headers attached to radially outer sides of the base panels forming the plenums therebetween, the headers being connected to the supply tube, first panel holes disposed through the base panels forming inlets for the thermal control air to flow from the plenums to the plurality of spray tubes, and baffles brazed or otherwise attached to radially outwardly facing surfaces of the base panels. 10. A thermal control apparatus as claimed in claim 9 further comprising a spent thermal air exhaust system including exhaust passages to exhaust the thermal control air from a generally annular region between the outer casing and the distribution manifold after the thermal control air has been sprayed on the thermal control rings and/or onto the outer casing by the spray tubes. 11. A thermal control apparatus as claimed in claim 10 further comprising the baffles being contoured to form the exhaust passages between the baffles and the base panel. 12. A thermal control apparatus as claimed in claim 11 further comprising the exhaust passages having exhaust passage inlets formed by generally radially facing exhaust holes through the baffles and generally circumferentially facing exhaust passage outlets formed between the baffles and the base panel. 13. A thermal control apparatus as claimed in claim 12 further comprising the spray holes in at least one of the spray tubes being oriented to impinge the thermal control air into a center of one of the fillets. 14. A thermal control apparatus as claimed in claim 12 further comprising at least one row of the spray holes all of the spray tubes being oriented to impinge the thermal control air into a center of one of the fillets. 15. A thermal control apparatus as claimed in claim 14 further comprising an annular segmented stator shroud attached to the outer casing and the shroud circumscribing radial outer blade tips of turbine blades of a turbine rotor. 16. A thermal control apparatus as claimed in claim 15 further comprising: the two thermal control rings being forward and aft ring respectively, the annular spray tubes being arcuate segments and closed and sealed at circumferential ends of the spray tubes, the annular spray tubes including at least first, second, and third spray tubes, the first spray tube located axially forward of the forward thermal control ring, the second spray tube located axially between the forward and aft thermal control rings, and the third spray tube located axially aft of the aft thermal control ring. 17. A thermal control apparatus as claimed in claim 16 further comprising: the annular segmented stator shroud including shroud segments mounted by forward and aft shroud hooks to an annular segmented shroud support, the annular segmented shroud support attached to the outer casing by forward and aft case hooks. 18. A thermal control apparatus comprising: an annular spray tube having a generally light bulb cross-sectional shape with a circular radially outer cross-sectional portion connected to a smaller circular radially inner cross-sectional portion by a transition section, the circular radially outer cross-sectional portion having a cross-sectional first diameter, the circular radially inner cross-sectional portion having a cross-sectional second diameter, the transition section having a radially outer maximum cross-sectional third diameter and a radially inner minimum cross-sectional fourth diameter, and the cross-sectional second diameter, the cross-sectional third diameter, and the cross-sectional fourth diameter all being substantially smaller than the cross-sectional first diameter. 19. A thermal control apparatus as claimed in claim 18 further comprising at least one circular row of the spray holes.