A sealing arrangement for a gas turbine and configured for sealing between a first component and a second component of the gas turbine, the sealing arrangement comprising: a first outer seal comprising a main body , which is generally circumferentially coextensive with an outer portion of an aft frame of a pair of circumferentially arranged transition ducts , a circumferentially oriented frame rail , an axially oriented leaf , a frame rail extension that extends circumferentially beyond the main body , and a leaf extension that extends circumferentially beyond the main body ; a second outer seal adjacent to the first outer seal , the second outer seal comprising a main body , which is generally circumferentially coextensive with an outer portion of the aft frame of the pair of circumferentially arranged transition ducts , a circumferentially oriented frame rail , an axially oriented leaf , a frame rail extension that extends circumferentially beyond the main body , and a leaf extension that extends circumferentially beyond the main body , the second outer seal circumferentially aligned with the first outer seal ; and a side seal radially disposed between the first outer seal and the second outer seal , the side seal comprising an elongate radially oriented main body , an axially oriented leaf , a projection , and a notch defined by the elongate radially oriented main body , an axial portion of the projection , and a radial portion of the projection ; characterized by a first deflection limiter radially inward of the leaf extension of the first outer seal , wherein the first deflection limiter is configured to reinforce a corner extension of the leaf extension of the first outer seal to avoid or minimize the corner extension bending radially inward; and a second deflection limiter radially inward of the leaf extension of the second outer seal , wherein the second deflection limiter is configured to reinforce a corner extension of the leaf extension of the second outer seal to avoid or minimize the corner extension bending radially inward. a first outer seal comprising a main body , which is generally circumferentially coextensive with an outer portion of an aft frame of a pair of circumferentially arranged transition ducts , a circumferentially oriented frame rail , an axially oriented leaf , a frame rail extension that extends circumferentially beyond the main body , and a leaf extension that extends circumferentially beyond the main body ; a second outer seal adjacent to the first outer seal , the second outer seal comprising a main body , which is generally circumferentially coextensive with an outer portion of the aft frame of the pair of circumferentially arranged transition ducts , a circumferentially oriented frame rail , an axially oriented leaf , a frame rail extension that extends circumferentially beyond the main body , and a leaf extension that extends circumferentially beyond the main body , the second outer seal circumferentially aligned with the first outer seal ; and a side seal radially disposed between the first outer seal and the second outer seal , the side seal comprising an elongate radially oriented main body , an axially oriented leaf , a projection , and a notch defined by the elongate radially oriented main body , an axial portion of the projection , and a radial portion of the projection ; characterized by a first deflection limiter radially inward of the leaf extension of the first outer seal , wherein the first deflection limiter is configured to reinforce a corner extension of the leaf extension of the first outer seal to avoid or minimize the corner extension bending radially inward; and a second deflection limiter radially inward of the leaf extension of the second outer seal , wherein the second deflection limiter is configured to reinforce a corner extension of the leaf extension of the second outer seal to avoid or minimize the corner extension bending radially inward. <EOS>