Gas turbine engine fuel injector
US-2019292987-A1 · Sep 26, 2019 · US
US11486580B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11486580-B2 |
| Application number | US-202016752182-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 24, 2020 |
| Priority date | Jan 24, 2020 |
| Publication date | Nov 1, 2022 |
| Grant date | Nov 1, 2022 |
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A spacer for a fluid nozzle can include a body configured to fit within a sheath of the fluid nozzle such that a fluid tube positioned within the sheath is held bent over its longitudinal dimension by the body thereby altering a natural frequency of the fuel tube compared to if the fuel tube were not held bent.
Opening claim text (preview).
What is claimed is: 1. A spacer for a fluid nozzle, comprising: a body configured to fit within a sheath of the fluid nozzle such that a fluid tube positioned within the sheath is held bent over its longitudinal dimension by the body thereby altering a natural frequency of the fuel tube compared to if the fuel tube were not held bent; and an off-center hole defined through the body at least in an orthogonal direction to a plane that is coplanar with the body, wherein the off-center hole is configured to receive a fluid tube within the sheath of the fluid nozzle to bend the fluid tube within the sheath, wherein the off-center hole is closer to a center of the body than a radially outer diameter of the body. 2. The spacer of claim 1 , wherein the body is a disk, wherein the off-center hole is symmetrically shaped. 3. The spacer of claim 2 , wherein the off-center hole is not aligned with a center of the disk such that an axis defining a center of the off-center hole and an axis defining the center of the disk are separated from each other in a radial direction. 4. The spacer of claim 3 , further comprising one or more weight reduction features configured to reduce a weight of the disk. 5. The spacer of claim 4 , wherein the body is made of a nickel alloy or stainless steel. 6. A fluid nozzle, comprising: a sheath; a nozzle base; a nozzle tip; a fluid tube configured to be contained within the sheath and supported at the nozzle base and the nozzle tip; and at least one spacer disposed within the sheath such the fluid tube is held bent over its longitudinal dimension thereby altering a natural frequency of the fuel tube compared to if the fuel tube were not held bent, the spacer further comprising: a body configured to fit within the sheath of the fluid nozzle; and an off-center hole defined through the body at least in an orthogonal direction to a plane that is coplanar with the body, wherein the off-center hole is configured to receive the fluid tube within the sheath of the fluid nozzle to bend the fluid tube within the sheath, wherein the off-center hole is closer to a center of the body than a radially outer diameter of the body. 7. The nozzle of claim 6 , wherein the spacer contacts an inner wall of the sheath and the fluid tube passes through the spacer, wherein the spacer is configured to bend the fluid tube within the sheath to modify a vibrational characteristic of the fluid tube, wherein the fluid tube is mounted centrally within the sheath at the nozzle base and the nozzle tip. 8. The nozzle of claim 6 , wherein the body is a disk. 9. The nozzle of claim 8 , wherein the off-center hole is symmetrically shaped. 10. The nozzle of claim 9 , wherein the off-center hole is not aligned with a center of the disk such that an axis defining a center of the off-center hole and an axis defining the center of the disk are separated from each other in a radial direction. 11. The nozzle of claim 10 , further comprising one or more weight reduction features configured to reduce a weight of the disk. 12. The nozzle of claim 11 , wherein the body is made of a nickel alloy or stainless steel. 13. The nozzle of claim 6 , wherein an outer shape of the spacer is the same shape as the inner wall of the sheath. 14. The nozzle of claim 6 , wherein the sheath has a cylindrical tube shape. 15. The nozzle of claim 6 , wherein the at least one spacer is disposed near a longitudinal center of the fluid tube. 16. The nozzle of claim 15 , further comprising one or more centered spacers having a centered hole, each centered spacer disposed apart from the at least one spacer along a length of the fluid tube within the sheath. 17. The spacer of claim 4 , wherein the one or more weight reduction holes are positioned radially outward of the off-center hole.
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