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According to an embodiment of the present invention, a rotating nozzle assembly includes a rotatable shaft having a bore to transport a cryogenic fluid therethrough. The rotatable shaft has an upstream portion associated with a feed chamber and a downstream portion. The nozzle assembly further incl

According to an embodiment of the present invention, a rotating nozzle assembly includes a rotatable shaft having a bore to transport a cryogenic fluid therethrough. The rotatable shaft has an upstream portion associated with a feed chamber and a downstream portion. The nozzle assembly further includes a seal disposed within the feed chamber and surrounding at least a portion of the rotatable shaft, and a seal backup disk disposed proximate the seal. The seal backup disk includes an orifice surrounding an outside diameter of the rotatable shaft, the orifice having a diameter such that, when the cryogenic fluid is flowing through the bore of the rotatable shaft, the rotatable shaft can freely rotate while the seal prevents the cryogenic fluid from seeping past the seal.

대표청구항 ▼

What is claimed is: 1. A rotating nozzle assembly, comprising: a rotatable shaft having a bore to transport a cryogenic fluid therethrough, the rotatable shaft having an upstream portion associated with a feed chamber and a downstream portion; a seal disposed within the feed chamber and surrounding

What is claimed is: 1. A rotating nozzle assembly, comprising: a rotatable shaft having a bore to transport a cryogenic fluid therethrough, the rotatable shaft having an upstream portion associated with a feed chamber and a downstream portion; a seal disposed within the feed chamber and surrounding at least a portion of the rotatable shaft; a seal backup disk disposed proximate the seal, the seal backup disk including an orifice surrounding an outside diameter of the rotatable shaft, the orifice having a diameter such that, when the cryogenic fluid is flowing through the bore of the rotatable shaft, the rotatable shaft can freely rotate while the seal prevents the cryogenic fluid from seeping past the seal; and one or more bearings disposed within a bearing chamber and operable to allow the rotation of the rotatable shaft, wherein the one or more bearings are located downstream of the seal backup disk and comprise two angular contact bearings and one radial contact bearing. 2. The rotating nozzle assembly of claim 1, wherein the one or more bearings are lubricated with a cryogenically-rated aerospace grease. 3. The rotating nozzle assembly of claim 1, wherein the one or more bearings are bearings that require no lubrication. 4. The rotating nozzle assembly of claim 3, wherein the bearings are selected from the group consisting of sputter coated bearings and ceramic bearings. 5. The rotating nozzle assembly of claim 1, wherein the seal comprises a body formed from an ultra-high molecular weight polyethylene. 6. The rotating nozzle assembly of claim 1, wherein the orifice has a diameter between 0.191 inch and 0.193 inch. 7. The rotating nozzle assembly of claim 1, further comprising a universal head coupled to the downstream portion of the rotatable shaft. 8. A rotating nozzle assembly, comprising: a rotatable shaft having a bore to transport a cryogenic fluid therethrough, the rotatable shaft having an upstream portion associated with a feed chamber and a downstream portion; a seal disposed within the feed chamber and surrounding at least a portion of the rotatable shaft, the seal comprising a body formed from an ultra-high molecular weight polyethylene and a spring disposed within a groove formed in an upstream end of the body; a seal backup disk disposed proximate the seal, the seal backup disk including an orifice surrounding an outside diameter of the rotatable shaft, the orifice having a diameter between 0.191 inch and 0.193 inch; and two angular contact bearings and one radial contact bearing disposed within a bearing chamber and operable to allow the rotation of the rotatable shaft, the bearings located downstream of the seal backup disk. 9. The rotating nozzle assembly of claim 8, wherein the bearings are lubricated with a cryogenically-rated aerospace grease. 10. The rotating nozzle assembly of claim 8, wherein the bearings require no lubrication. 11. The rotating nozzle assembly of claim 10, wherein the bearings are sputter coated bearings. 12. The rotating nozzle assembly of claim 10, wherein the bearings are ceramic bearings. 13. A method, comprising: providing a feed chamber in fluid communication with a bore formed in an upstream portion of a rotatable shaft; providing a seal within the feed chamber, the seal surrounding at least a portion of the rotatable shaft; allowing rotation of the rotatable shaft by one or more bearings disposed within a bearing chamber; lubricating the one or more bearings with a cryogenically-rated aerospace grease; and preventing a cryogenic fluid flowing through the bore of the rotatable shaft from seeping past the seal by utilizing a seal backup disk disposed proximate the seal, the seal backup disk including an orifice surrounding an outside diameter of the rotatable shaft. 14. The method of claim 13, further comprising providing the seal backup disk with an orifice having a diameter between 0.191 inch and 0.193 inch. 15. The method of claim 13, further comprising coupling a universal head to a downstream portion of the rotatable shaft. 16. A rotating nozzle assembly, comprising: a rotatable shaft having a bore to transport a cryogenic fluid therethrough, the rotatable shaft having an upstream portion associated with a feed chamber and a downstream portion; a seal disposed within the feed chamber and surrounding at least a portion of the rotatable shaft; a seal backup disk disposed proximate the seal, the seal backup disk including an orifice surrounding an outside diameter of the rotatable shaft, the orifice having a diameter such that, when the cryogenic fluid is flowing through the bore of the rotatable shaft, the rotatable shaft can freely rotate while the seal prevents the cryogenic fluid from seeping past the seal; and one or more bearings disposed within a bearing chamber and operable to allow the rotation of the rotatable shaft, wherein the one or more bearings are located downstream of the seal backup disk and are lubricated with a cryogenically-rated aerospace grease.