Heatshield with damper member
A gas turbine engine includes a shaft and a heatshield that circumscribes the shaft. The heatshield defines a cylindrical body that has radially inner and outer sides and extends between first and second axial ends. The heatshield is exclusively supported on the shaft at the first and second axial ends. The heatshield includes at least one seal member on the radially outer side. A damper member is disposed at the radially inner side of the heatshield for attenuating vibration of the heatshield.
1. A gas turbine engine comprising:
a shaft;
a heatshield circumscribing the shaft,
the heatshield defining a cylindrical body having radially inner and outer sides and extending between first and second axial ends,
the heatshield being exclusively supported on the shaft at the first and second axial ends,
the heatshield including at least one seal member on the radially outer side, the heatshield having an axial length from the first axial end to the second axial end that is from 2.5 centimeters to 13 centimeters, and the at least one seal member is located in a range of 25% to 75% of the axial length; and
a damper member disposed at the radially inner side of the heatshield for attenuating vibration of the heatshield.
2. The gas turbine engine as recited in claim 1 , wherein the shaft comprises a first shaft segment and a second shaft segment coupled in a joint to the first shaft segment, the heatshield circumscribing the joint.
3. The gas turbine engine as recited in claim 1 , wherein the inner side of the heatshield defines a groove, and the damper member is seated in the groove.
4. The gas turbine engine as recited in claim 3 , wherein the heatshield has a diameter, the diameter and the axial length falling within a vibration excitation range, and wherein the damper member is configured to be moveable within the groove with respect to the vibration excitation range.
5. The gas turbine engine as recited in claim 3 , wherein the heatshield further comprises first and second projecting lips flanking the groove.
6. The gas turbine engine as recited in claim 3 , wherein the groove is adjacent the at least one seal member.
7. The gas turbine engine as recited in claim 6 , wherein the at least one seal member includes first and second seal members, and the groove is between the first and second seal members.
8. The gas turbine engine as recited in claim 1 , wherein there is an annular dead space between the heatshield and the shaft and there is no cooling air flow into or out of the annular dead space.
9. The gas turbine engine as recited in claim 1 , wherein the damper member is a split ring.
10. The gas turbine engine as recited in claim 1 , wherein the cylindrical body extends from the first axial end to the second axial end.
11. The gas turbine engine as recited in claim 10 , wherein the shaft comprises a first shaft segment and a second shaft segment coupled in a joint to the first shaft segment, the heatshield circumscribing the joint.
12. The gas turbine engine as recited in claim 1 , wherein the at least one seal member includes a knife edge seal.
13. A heatshield assembly for a gas turbine engine, comprising:
a heatshield defining a cylindrical body having radially inner and outer sides and extending between first and second axial ends, the heatshield including at least one seal member on the radially outer side, the heatshield having an axial length from the first axial end to the second axial end that is from 2.5 centimeters to 13 centimeters, and the at least one seal member is located in a range of 25% to 75% of the axial length; and
a split ring damper member disposed at the radially inner side of the heatshield for attenuating vibration of the heatshield.
14. The heatshield assembly as recited in claim 13 , wherein the inner side of the heatshield defines a groove, and the damper member is seated in the groove.
15. The heatshield assembly as recited in claim 14 , wherein the groove is adjacent the at least one seal member.
16. The heatshield assembly as recited in claim 15 , wherein the at least one seal member includes first and second seal members, and the groove is between the first and second seal members.
17. The heatshield assembly as recited in claim 16 , wherein the heatshield further comprises first and second projecting lips flanking the groove.
18. A gas turbine engine comprising:
a shaft;
a heatshield circumscribing the shaft,
the heatshield defining a cylindrical body having radially inner and outer sides and extending between first and second axial ends,
an annular space radially bound by the radially inner side of the cylindrical body and the shaft,
the heatshield being exclusively supported on the shaft at the first and second axial ends,
the heatshield including at least one seal member on the radially outer side; and
a damper member disposed in the annular space at the radially inner side of the cylindrical body for attenuating vibration of the heatshield.