Hydraulic seal arrangement
A hydraulic seal arrangement 5 between two shafts 1, 2 rotating relatively to each other, particularly in the same sense of rotation, of especially a gas turbine engine, where the radially outer shaft 2 has an annulus 5 a extending radially outwards on its circumference into which the radially inner shaft 1 projects with a fin 5 b that extends radially outwards on its circumference, said annulus 5 a can be filled siphon-fashion through an inlet area 5 d under centrifugal effect with a hydraulic fluid in the area of the free end of the fin 5 b as the shaft(s) 1, 2 rotate(s), with an opening 7 branching off from an annulus area 5 e for the discharge of hydraulic fluid, the annulus 5 a being formed by a first outer shell part 8 and a second outer shell part 9 situated on the shaft 2.
1. A hydraulic seal arrangement between two shafts rotating relatively to each other, comprising:
an annulus connected to a radially outer of the two shafts extending radially outwards on its circumference;
a fin connected to a radially inner of the two shafts that extends radially outwards on its circumference and projects into the annulus;
an inlet area through which the annulus can be filled siphon-fashion under centrifugal effect with a hydraulic fluid at least in an area of a free end of the fin as at least one of the shafts rotate; and
at least one first opening branching off from the annulus for discharging a partial quantity of the hydraulic fluid from the annulus;
wherein the annulus is formed by a first outer shell part and a second outer shell part which are connected to the radially outer shaft and the first outer shell part and the second outer shell part are arranged in a telescopic manner to form the annulus.
2. A hydraulic seal arrangement in accordance with claim 1 , wherein the annulus is formed between radially extending portions of the first outer shell part and the second outer shell part.
3. A hydraulic seal arrangement in accordance with claim 2 , and further comprising an annulus area formed between overlapping axially extending portions of the first outer shell part and the second outer shell part, the at least one first opening being connected to the annulus area to allow hydraulic fluid to flow from the annulus to the annulus area.
4. A hydraulic seal arrangement in accordance with claim 3 , wherein at least one of the first outer shell part and the second outer shell part includes at least one second opening for the discharge of hydraulic fluid from the annulus area to a bearing supporting the radially outer shaft.
5. A hydraulic seal arrangement in accordance with claim 4 , wherein the annulus is positioned directly radially inwardly from the bearing supporting the radially outer shaft.
6. A hydraulic seal arrangement in accordance with claim 5 , wherein at least one of the first outer shell part and the second outer shell part is secured in an axial direction with at least one retaining ring connected to the radially outer shaft.
7. A hydraulic seal arrangement in accordance with claim 6 , wherein the first outer shell part and the second outer shell part are secured against rotation relative to each other.
8. A hydraulic seal arrangement in accordance with claim 7 , and further comprising a seal positioned between the first outer shell part and the radially inner shaft to seal between the first outer shell part and the radially inner shaft.
9. A hydraulic seal arrangement in accordance with claim 8 , and further comprising the two shafts, which are shafts of a gas turbine engine.
10. A hydraulic seal arrangement in accordance with claim 1 , wherein the annulus is formed between radially extending portions of the first outer shell part and the second outer shell part.
11. A hydraulic seal arrangement in accordance with claim 1 , and further comprising an annulus area formed between overlapping axially extending portions of the first outer shell part and the second outer shell part, the at least one first opening being connected to the annulus area to allow hydraulic fluid to flow from the annulus to the annulus area.
12. A hydraulic seal arrangement in accordance with claim 11 , wherein at least one of the first outer shell part and the second outer shell part includes at least one second opening for the discharge of hydraulic fluid from the annulus area to a bearing supporting the radially outer shaft.
13. A hydraulic seal arrangement in accordance with claim 12 , wherein the annulus is positioned directly radially inwardly from the bearing supporting the radially outer shaft.
14. A hydraulic seal arrangement in accordance with claim 1 , wherein at least one of the first outer shell part and the second outer shell part is secured in an axial direction with at least one retaining ring connected to the radially outer shaft.
15. A hydraulic seal arrangement in accordance with claim 1 , wherein the first outer shell part and the second outer shell part are secured against rotation relative to each other.
16. A hydraulic seal arrangement in accordance with claim 1 , and further comprising a seal positioned between the first outer shell part and the radially inner shaft to seal between the first outer shell part and the radially inner shaft.
17. A hydraulic seal arrangement in accordance with claim 1 , and further comprising the two shafts, which are shafts of a gas turbine engine.
18. A hydraulic seal arrangement in accordance with claim 1 , wherein the annulus is positioned directly radially inwardly from a bearing supporting the radially outer shaft.
19. A hydraulic seal arrangement between two shafts rotating relatively to each other, comprising:
an annulus connected to a radially outer of the two shafts extending radially outwards on its circumference;
a fin connected to a radially inner of the two shafts that extends radially outwards on its circumference and projects into the annulus;
an inlet area through which the annulus can be filled siphon-fashion under centrifugal effect with a hydraulic fluid at least in an area of a free end of the fin as at least one of the shafts rotate; and
at least one first opening branching off from the annulus for discharging a partial quantity of the hydraulic fluid from the annulus;
wherein the annulus is formed by a first outer shell part and a second outer shell part which are connected to the radially outer shaft and the annulus is positioned directly radially inwardly from a bearing supporting the radially outer shaft.
20. A hydraulic seal arrangement in accordance with claim 19 , wherein the annulus is formed between radially extending portions of the first outer shell part and the second outer shell part.
21. A hydraulic seal arrangement in accordance with claim 20 , and further comprising an annulus area formed between overlapping axially extending portions of the first outer shell part and the second outer shell part, the at least one first opening being connected to the annulus area to allow hydraulic fluid to flow from the annulus to the annulus area.
22. A hydraulic seal arrangement in accordance with claim 21 , wherein at least one of the first outer shell part and the second outer shell part includes at least one second opening for the discharge of hydraulic fluid from the annulus area to a bearing supporting the radially outer shaft.
23. A hydraulic seal arrangement in accordance with claim 22 , wherein at least one of the first outer shell part and the second outer shell part is secured in an axial direction with at least one retaining ring connected to the radially outer shaft.
24. A hydraulic seal arrangement in accordance with claim 23 , wherein the first outer shell part and the second outer shell part are secured against rotation relative to each other.
25. A hydraulic seal arrangement in accordance with claim 24 , and further comprising a seal positioned between the first outer shell part and the radially inner shaft to seal between the first outer shell part and the radially inner shaft.
26. A hydraulic seal arrangement in accordance with claim 25 , and further comprising the two shafts, which are shafts of a gas turbine engine.
27. A hydraulic seal arrangement in accordance with claim 19 , and further comprising an annulus area formed between overlapping axially extending portions of the first outer shell part and the second outer shell part, the at least one first opening being connected to the annulus area to allow hydraulic fluid to flow from the annulus to the annulus area.
28. A hydraulic seal arrangement in accordance with claim 27 , wherein at least one of the first outer shell part and the second outer shell part includes at least one second opening for the discharge of hydraulic fluid from the annulus area to a bearing supporting the radially outer shaft.
29. A hydraulic seal arrangement in accordance with claim 19 , wherein at least one of the first outer shell part and the second outer shell part is secured in an axial direction with at least one retaining ring connected to the radially outer shaft.
30. A hydraulic seal arrangement in accordance with claim 19 , wherein the first outer shell part and the second outer shell part are secured against rotation relative to each other.
31. A hydraulic seal arrangement in accordance with claim 19 , and further comprising a seal positioned between the first outer shell part and the radially inner shaft to seal between the first outer shell part and the radially inner shaft.
32. A hydraulic seal arrangement in accordance with claim 19 , and further comprising the two shafts, which are shafts of a gas turbine engine.