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Shaped face thermal expansion

The turbine exhaust E seal was replaced with a segmented cylindrical piston ring seal, which became typical of all other seals. The turbine vertical inlet face seal was replao with two horizontal segmented cylindrical piston ring seals between the turbocompressor and a new adapter. These seals, located above and below the hot duct, are the same type as the turbine exhaust seal. The tee-shaped adapter also interfaces to the hot duct with a segmented piston ring seal that replaces the hot duct bellows that was previously used to accommodate thermal expansion. [Pg.61]

Suppose that a thin film is bonded to one surface of a substrate of uniform thickness hs- It will be assumed that the substrate has the shape of a circular disk of radius R, although the principal results of this section are independent of the actual shape of the outer boundary of the substrate. A cylindrical r, 0, z—coordinate system is introduced with its origin at the center of the substrate midplane and with its z—axis perpendicular to the faces of the substrate the midplane is then at z = 0 and the film is bonded to the face at z = hs/2. The substrate is thin so that hs R, and the film is very thin in comparison to the substrate. The film has an incompatible elastic mismatch strain with respect to the substrate this strain might be due to thermal expansion effects, epitaxial mismatch, phase transformation, chemical reaction, moisture absorption or other physical effect. Whatever the origin of the strain, the goal here is to estimate the curvature of the substrate, within the range of elastic response, induced by the stress associated with this incompatible strain. For the time being, the mismatch strain is assumed to be an isotropic extension or compression in the plane of the interface, and the substrate is taken to be an isotropic elastic solid with elastic modulus Es and Poisson ratio Vs the subscript s is used to denote properties of the substrate material. The elastic shear modulus /Xg is related to the elastic modulus and Poisson ratio by /ig = Es/ 1 + t s). [Pg.94]


See other pages where Shaped face thermal expansion is mentioned: [Pg.298]    [Pg.288]    [Pg.443]    [Pg.298]    [Pg.321]    [Pg.74]    [Pg.229]    [Pg.22]    [Pg.120]    [Pg.406]   
See also in sourсe #XX -- [ Pg.115 ]




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