Under-root spacer for gas turbine engine fan blade
A gas turbine engine rotor includes a hub having a slot. A blade includes a root received in the slot. An under-root area is provided between the root and the fan hub in the slot. A spacer includes first and second portions that cooperate with one another to provide an adjustment feature with discrete height settings. The adjustment feature provides different radial heights of the spacer. The spacer is arranged in the under-root area beneath the root.
1. A rotor for a gas turbine engine comprising:
a hub having a slot;
a blade including a root received in the slot, and a under-root area provided between the root and the fan hub in the slot; and
a spacer including first and second portions that cooperate with one another to provide an adjustment feature with discrete height settings providing different radial heights of the spacer, the spacer arranged in the under-root area beneath the root, wherein the second portion includes opposing first and second ends, the first end pivotally secured to the first portion by a pin.
2. The rotor according to claim 1 , wherein the first and second portions are discrete from one another.
3. A rotor for a gas turbine engine comprising:
a hub having a slot;
a blade including a root received in the slot, and a under-root area provided between the root and the fan hub in the slot; and
a spacer including first and second portions that cooperate with one another to provide an adjustment feature with the discrete height settings providing different radial heights of the space, the space arranged in the under-root area beneath the root, wherein the adjustment feature is provided by an end cooperating with a feature on the first portion, wherein the adjustment feature on the first portion is provided by multiple tabs spaced apart from one another.
4. The rotor according to claim 1 , wherein the spacer is constructed from a polymer material.
5. The rotor according to claim 1 , wherein the second portion is spaced from the first portion a desired distance to provide a desired height setting.
6. The rotor according to claim 5 , wherein the root has an end surface, and the spacer engages the rotor and the end surface and applies a desired load on the root.
7. The rotor according to claim 1 , wherein the first and second portions are integral with one another.
8. The rotor according to claim 1 , comprising a fan section, wherein the hub is a fan hub, and the blade is a fan blade.
9. A spacer for a gas turbine engine rotor under-root area comprising:
first and second portions that cooperate with one another to provide an adjustment feature with discrete height settings providing different radial heights of the spacer, the adjustment feature on the first portion is provided by multiple tabs spaced apart from one another, and the second portion includes a free end, the second portion configured to be deflected to position the free end with respect to a desired one of the multiple tabs which corresponds to one of the different radial heights.
10. The spacer according to claim 9 , wherein the first and second portions are discrete from one another.
11. The spacer according to claim 10 , where the second portion includes opposing first and second ends, the first end pivotally secured to the first portion by a pin, and the second end corresponds to the free end.
12. The spacer according to claim 9 , wherein the first and second portions are integral with one another.
13. The spacer according to claim 9 , wherein the spacer is constructed from a polymer material.
14. The spacer according to claim 9 , wherein the second portion is spaced from the first portion a desired distance to provide a desired height setting for the spacer.
15. The spacer according to claim 9 , wherein the first portion is curved in a lateral direction relative to longitudinal direction in which the first and second portions extend.