Fluid-cooled mechanical face seal rotor
A fluid-cooled seal rotor is described for a seal assembly that includes a seal case, a seal stator, and wherein the rotor has a sealing face on a first side and a heat-transfer structure on a second side. The heat-transfer structure may be a roughened surface. The heat-transfer structure may have p...
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Main Authors | , , , |
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Format | Patent |
Language | English |
Published |
29.11.2005
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Online Access | Get full text |
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Abstract | A fluid-cooled seal rotor is described for a seal assembly that includes a seal case, a seal stator, and wherein the rotor has a sealing face on a first side and a heat-transfer structure on a second side. The heat-transfer structure may be a roughened surface. The heat-transfer structure may have protrusions which may be fins, including fins with roughened surfaces. The heat-transfer structure may have additional heat-transfer structures thereon to create complex, including fractal, structures. The fins may be shaped as impellers to move oil over the heat-transfer structure. Channels between fins may have a width greater than twice the boundary layer thickness for the fluid engaged by the fins. The fluid-cooled rotor, the seal assembly having the fluid-cooled rotor, an air turbine starter having the seal assembly, air turbine starters and other machines with rotating shafts using the seal are within the scope of the invention. |
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AbstractList | A fluid-cooled seal rotor is described for a seal assembly that includes a seal case, a seal stator, and wherein the rotor has a sealing face on a first side and a heat-transfer structure on a second side. The heat-transfer structure may be a roughened surface. The heat-transfer structure may have protrusions which may be fins, including fins with roughened surfaces. The heat-transfer structure may have additional heat-transfer structures thereon to create complex, including fractal, structures. The fins may be shaped as impellers to move oil over the heat-transfer structure. Channels between fins may have a width greater than twice the boundary layer thickness for the fluid engaged by the fins. The fluid-cooled rotor, the seal assembly having the fluid-cooled rotor, an air turbine starter having the seal assembly, air turbine starters and other machines with rotating shafts using the seal are within the scope of the invention. |
Author | Kincheloe, Todd A Geck, Kellan P Giesler, William L Langston, Todd A |
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References | Lipschitz (5143384) 19920900 Flaherty et al. (6257589) 20010700 Lebeck et al. (4836561) 19890600 Wiese (3813103) 19740500 Amundson et al. (4889348) 19891200 Sedy (5702110) 19971200 Flaherty et al. (5941532) 19990800 (PCT/US2004/028042) 20050400 Pecht et al. (5217233) 19930600 Sato (4123089) 19781000 Gardner (3499653) 19700300 Pecht et al. (5090712) 19920200 Lahrman (5174584) 19921200 Langston et al. (6623238) 20030900 Takenaka et al. (4423879) 19840100 Ullah (5639096) 19970600 B. M. Steinetz; R. C. Hendricks; J Munson; Advanced Seal Technology Role in Meeting Next Generaton Turbine Engine Goals; NASA/TM-1998-206961; AVAT-PPS Paper No. 11; NATO Research and Technology Agency; Toulouse, France, May 11-15, 1998. Lebeck et al. (4887395) 19891200 |
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Snippet | A fluid-cooled seal rotor is described for a seal assembly that includes a seal case, a seal stator, and wherein the rotor has a sealing face on a first side... |
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Title | Fluid-cooled mechanical face seal rotor |
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