Cmc vane assembly apparatus and method
WebA CMC vane airfoil (22) is formed, cured, and slid over the strut (64). The spring ( 74 ) urges continuous contact between the strut ( 64 ) and airfoil ( 66 ), eliminating vibrations …
Cmc vane assembly apparatus and method
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WebOct 8, 2024 · CMC Vane Assembly Apparatus and Method: 2010-03-18: Schiavo et al. 7452189: Ceramic matrix composite turbine engine vane: 2008-11-18: Shi et al. 7185433: Turbine nozzle segment and method of repairing same: 2007-03-06: Miller: 29/889.22: 7101150: Fastened vane assembly: 2006-09-05: Bash et al. 20040120811: Methods … WebNov 22, 2016 · CMC vane assembly apparatus and method. Patent Schiavo, Anthony L; Gonzalez, Malberto F; Huang, Kuangwei; ... A metal vane core or strut (64) is formed …
WebThese include a CMC combustor liner, a CMC high pressure turbine vane, and a CMC exhaust nozzle. Advanced EBCs specifically tailored to the needs of the CMC combustor and vane are also being developed. The primary objectives are to address commercial manufacturability of the complex-shaped components and to evaluate their WebFeb 18, 2024 · Turbine engine blade or vane made of composite material, ... A pre-form CMC cavity and method of forming pre-form CMC cavity for a ceramic matrix component includes providing a mandrel, applying a base ply to the mandrel, laying-up at least one CMC ply on the base ply, removing the mandrel, and densifying the base ply and the at …
WebJan 1, 2005 · A CMC turbine vane with internal cooling path was tested on this burning rig. The results showed that the CMC vane could withstand the 1200 ℃ thermal cycling test … WebJan 1, 2005 · A CMC turbine vane with internal cooling path was tested on this burning rig. The results showed that the CMC vane could withstand the 1200 ℃ thermal cycling test but the coating was disappeared.
WebA CMC vane airfoil (22) is formed, cured, and slid over the strut (64). The spring (74) urges continuous contact ... CMC VANE ASSEMBLY APPARATUS AND METHOD CROSS …
Webfabrication methods to be developed. The objective of this research was to demonstrate design and fabrication techniques, developed under UEET, have made significant progress toward the application of CMC in cooled aerodynamic parts. Previous analysis of CMC vane shapes subjected to the turbine environment [ 5 ] indicated that downloads facturiWebA method of forming a ceramic matrix composite component having an internal cooling circuit includes wrapping at least a first sheet around a first mandrel, wrapping at least a second sheet around a second mandrel, creating a first plurality of holes in the first sheet corresponding to a plurality of openings in the first mandrel, creating a second plurality of … downloads facetimeWebComplete Patent Searching Database and Patent Data Analytics Services. downloads factuurWebCmc Vane Assembly Apparatus and Method: A metal vane core or strut (64) is formed integrally with an outer backing plate (40). ... A CMC vane airfoil (22) is formed, cured, … downloads fanatecWebCMC Vane Assembly Apparatus and Method US20100196160A1 (en) 2009-01-30: 2010-08-05: United Technologies Corporation: Cooled turbine blade shroud ... Bladed disk assembly method and impact device US20080206057A1 (en) * 2007-02-27: 2008-08-28: Siemens Power Generation, Inc. Blade shroud vibration monitor ... downloads fa treuhandWebThe fibers and the matrix are initially contained in a green stage, which is generally pliable until processed or cured into the final ceramic state. The nozzle assembly 100 includes a pair of CMC vanes, a first vane 110 and a second vane 120. The nozzle assembly 1 00 may be used in the second stage nozzle 30 or elsewhere. downloads failing firefoxWebSep 10, 2013 · Rather, as the temperature of the vane assembly increases/decreases, it will be appreciated that the CMC vane 30 is allowed to slide radially with respect to the rod 33 (and within the cutout 38 of the outer ring 31), due to the different coefficients of thermal expansion of the CMC vane 30 and the metallic rings 48 and 31, respectively. downloads facturen