초록 ▼

A sealing apparatus in a gas turbine. The sealing apparatus includes a seal housing apparatus coupled to a disc/rotor assembly so as to be rotatable therewith during operation of the gas turbine. The seal housing apparatus comprises a base member, a first leg portion, a second leg portion, and spann

A sealing apparatus in a gas turbine. The sealing apparatus includes a seal housing apparatus coupled to a disc/rotor assembly so as to be rotatable therewith during operation of the gas turbine. The seal housing apparatus comprises a base member, a first leg portion, a second leg portion, and spanning structure. The base member extends generally axially between forward and aft rows of rotatable blades and is positioned adjacent to a row of stationary vanes. The first leg portion extends radially inwardly from the base member and is coupled to the disc/rotor assembly. The second leg portion is axially spaced from the first leg portion, extends radially inwardly from the base member, and is coupled to the disc/rotor assembly. The spanning structure extends between and is rigidly coupled to each of the base member, the first leg portion, and the second leg portion.

대표청구항 ▼

1. Sealing apparatus in a gas turbine comprising forward and aft rows of rotatable blades coupled to a disc/rotor assembly and a row of stationary vanes positioned between the forward and aft rows of rotatable blades, the sealing apparatus comprising: seal housing apparatus coupled to the disc/rotor

1. Sealing apparatus in a gas turbine comprising forward and aft rows of rotatable blades coupled to a disc/rotor assembly and a row of stationary vanes positioned between the forward and aft rows of rotatable blades, the sealing apparatus comprising: seal housing apparatus coupled to the disc/rotor assembly so as to be rotatable with the disc/rotor assembly during operation of the gas turbine, said seal housing apparatus comprising: a base member extending generally axially between the forward and aft rows of rotatable blades and positioned adjacent to the row of stationary vanes;a first leg portion extending radially inwardly from said base member, said first leg portion coupled to the disc/rotor assembly;a second leg portion axially spaced from said first leg portion, said second leg portion extending radially inwardly from said base member and being coupled to said disc/rotor assembly; andspanning structure extending between and rigidly coupled to each of said base member, said first leg portion, and said second leg portion, said spanning structure comprising first, second, and third truss members, each of said truss members including: a first end portion rigidly coupled to a respective one of said base member, said first leg portion, and said second leg portion; anda second end portion, said second end portion of each of said truss members rigidly coupled together. 2. The sealing apparatus as set out in claim 1, wherein: said first truss member extends generally radially inwardly from said base member towards the disc/rotor assembly;said second truss member extends axially from said first leg portion toward said second leg portion and joins said first truss member at a knee junction; andsaid third truss member extends axially from said second leg portion toward said first leg portion and is joined to said first and second truss members at said knee junction. 3. The sealing apparatus as set out in claim 2, wherein said second and third truss members extend radially outwardly from the respective first and second leg portions to said knee junction. 4. The sealing apparatus as set out in claim 1, further comprising: a first seal retainer plate structure associated with the forward row of rotatable blades and having first axially extending seal structure;a first seal member associated with said first axially extending seal structure and said seal housing apparatus so as to seal a gap between said first seal retainer plate structure and said seal housing apparatus;a second seal retainer plate structure associated with the aft row of rotatable blades and having second axially extending seal structure; anda second seal member associated with said second axially extending seal structure and said seal housing apparatus so as to substantially prevent leakage through a gap between said second seal retainer plate structure and said seal housing apparatus. 5. The sealing apparatus as set out in claim 1, further comprising a first sealing structure coupled to one of the row of stationary vanes and said base member, said first sealing structure substantially preventing leakage through a gap between the row of stationary vanes and said base member. 6. The sealing apparatus as set out in claim 5, further comprising a second sealing structure coupled to the other of the row of stationary vanes and said base member, said second sealing structure cooperating with said first sealing structure to substantial prevent leakage through said gap between the row of stationary vanes and said base member. 7. The sealing apparatus as set out in claim 6, wherein said first sealing structure comprises one of an abradable layer and a honeycomb layer and said second sealing structure comprises labyrinth teeth. 8. The sealing apparatus as set out in claim 1, wherein said seal housing apparatus comprises a plurality of separate and circumferentially adjacent seal housing members and further comprising a seal structure between adjacent seal housing members. 9. The sealing apparatus as set out in claim 1, wherein said leg portions of said seal housing apparatus each includes a foot member, and wherein said foot member of each of said leg portion is: radially inserted through a respective radially facing slot formed in the disc/rotor assembly; andcircumferentially displaced so as to not be circumferentially aligned with said respective radially facing slot formed in the disc/rotor assembly. 10. Sealing apparatus in a gas turbine comprising forward and aft rows of rotatable blades coupled to a disc/rotor assembly and a row of stationary vanes positioned between the forward and aft rows of rotatable blades, the sealing apparatus comprising: seal housing apparatus coupled to the disc/rotor assembly so as to be rotatable with the disc/rotor assembly during operation of the gas turbine, said seal housing apparatus comprising: a base member extending generally axially between the forward and aft rows of rotatable blades and positioned adjacent to the row of stationary vanes;a first leg portion extending radially inwardly from said base member, said first leg portion coupled to the disc/rotor assembly;a second leg portion axially spaced from said first leg portion, said second leg portion extending radially inwardly from said base member and being coupled to said disc/rotor assembly;spanning structure extending between and rigidly coupled to each of said base member, said first leg portion, and said second leg portion;a first seal retainer plate structure associated with the forward row of rotatable blades and having first axially extending seal structure; anda first seal member associated with said first axially extending seal structure and said seal housing apparatus so as to seal a gap between said first seal retainer plate structure and said seal housing apparatus. 11. The sealing apparatus as set out in claim 10, further comprising: a second seal retainer plate structure associated with the aft row of rotatable blades and having second axially extending seal structure; anda second seal member associated with said second axially extending seal structure and said seal housing apparatus so as to substantially prevent leakage through a gap between said second seal retainer plate structure and said seal housing apparatus. 12. The sealing apparatus as set out in claim 10, further comprising a first sealing structure coupled to one of the row of stationary vanes and said base member and a second sealing structure coupled to the other of the row of stationary vanes and said base member, said first and second sealing structures cooperating to substantial prevent leakage through a gap between the row of stationary vanes and said base member. 13. The sealing apparatus as set out in claim 10, wherein said spanning structure comprises first, second, and third truss members, each of said truss members including: a first end portion rigidly coupled to a respective one of said base member, said first leg portion, and said second leg portion; anda second end portion, said second end portion of each of said truss members rigidly coupled together. 14. The sealing apparatus as set out in claim 10, wherein said seal housing apparatus comprises a plurality of separate and circumferentially adjacent seal housing members and further comprising a seal structure between adjacent seal housing members. 15. Sealing apparatus in a gas turbine comprising forward and aft rows of rotatable blades coupled to a disc/rotor assembly and a row of stationary vanes positioned between the forward and aft rows of rotatable blades, the sealing apparatus comprising: seal housing apparatus coupled to the disc/rotor assembly so as to be rotatable with the disc/rotor assembly during operation of the gas turbine, said seal housing apparatus comprising: a base member extending generally axially between the forward and aft rows of rotatable blades and positioned adjacent to the row of stationary vanes;a first leg portion extending radially inwardly from said base member, said first leg portion coupled to the disc/rotor assembly;a second leg portion axially spaced from said first leg portion, said second leg portion extending radially inwardly from said base member and being coupled to said disc/rotor assembly; andspanning structure extending between and rigidly coupled to each of said base member, said first leg portion, and said second leg portion;wherein said leg portions of said seal housing apparatus each includes a foot member, and wherein said foot member of each of said leg portion is: radially inserted through a respective radially facing slot formed in the disc/rotor assembly; andcircumferentially displaced so as to not be circumferentially aligned with said respective radially facing slot formed in the disc/rotor assembly. 16. The sealing apparatus as set out in claim 15, wherein said foot member of said first leg portion extends axially toward said second leg portion, and said foot member of said second leg portion extends axially toward said first leg portion. 17. The sealing apparatus as set out in claim 15, wherein each said foot member is tapered in a radial direction for engagement with an angled surface of the disc/rotor assembly. 18. The sealing apparatus as set out in claim 15, wherein said sealing apparatus further comprises: first seal retainer plate structure associated with the forward row of rotatable blades and having first axially extending seal structure;second seal retainer plate structure associated with the aft row of rotatable blades and having second axially extending seal structure;a first seal member associated with said first axially extending seal structure and said seal housing apparatus so as to seal a gap between said first seal retainer plate structure and said seal housing apparatus; anda second seal member associated with said second axially extending seal structure and said seal housing apparatus so as to seal a gap between said second seal retainer plate structure and said seal housing apparatus. 19. The sealing apparatus as set out in claim 15, further comprising a first sealing structure coupled to one of the row of stationary vanes and said base member and a second sealing structure coupled to the other of the row of stationary vanes and said base member, said first and second sealing structures cooperating to substantial prevent leakage through a gap between the row of stationary vanes and said base member. 20. The sealing apparatus as set out in claim 15, wherein said seal housing apparatus comprises a plurality of separate and circumferentially adjacent seal housing members and further comprising a seal structure between adjacent seal housing members.