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A blade for an axial-flow turbomachine with a gap-side blade area I which transits into a free blade end and with a hub-side or casing-side blade area II, respectively. Blade 3 forms a flow line profile section with leading edge VK and trailing edge HK which establish forward end point V and rearwar

A blade for an axial-flow turbomachine with a gap-side blade area I which transits into a free blade end and with a hub-side or casing-side blade area II, respectively. Blade 3 forms a flow line profile section with leading edge VK and trailing edge HK which establish forward end point V and rearward end point H, respectively, by a tangent normal to and intersecting with the profile chord, with the distance between these end points being profile depth L. Blade 3 includes an enlargement of profile depth L at a tip of the free blade end which is at least +10 percent and decreases to zero in the blade central section, with the values being non-negative throughout, with the profile enlargement at trailing edge HK being larger than zero at the tip in the gap-side peripheral section.

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1. A stator/rotor blade for a fluid-flow machine, the blade having a free blade end blade area adjacent to a tip clearance gap positioned between a blade tip and a main gas path boundary of one of a hub and a casing, and a fixed blade end blade area structurally connected to the main gas path bounda

1. A stator/rotor blade for a fluid-flow machine, the blade having a free blade end blade area adjacent to a tip clearance gap positioned between a blade tip and a main gas path boundary of one of a hub and a casing, and a fixed blade end blade area structurally connected to the main gas path boundary of one of the hub and the casing, the blade transmitting energy to the working fluid and being cambered to turn flow from high relative whirl to lower relative whirl, the blade being defined by flow line profile sections with a leading edge and a trailing edge which establish a forward end point and a rearward end point, respectively, each given by a tangent normal to and intersecting with a respective profile chord, with a distance between these end points being a respective profile depth, and the free end blade area and the fixed end blade area meeting at a central meridional flow line profile of the blade, the blade having an enlargement of the profile depth at the free blade end blade area which, in relation to a profile depth of the blade at a central meridional flow line of the blade, is at least +10 percent at a tip of the free blade end blade area and decreases to zero by the central meridional flow line of the blade, with the enlargement values being ≧0 throughout, the profile depth enlargement being provided across substantially all of a length of the free blade end blade area and continuously increasing in a continuous concave curve from the central meridional flow line to the tip of the free end blade area on each of the leading edge and the trailing edge to provide structural stress and aerodynamic loading continuity across the blade length, the profile depth enlargement sized to avoid local distortion of the blade leading edge and trailing edge shape meridional projections, the profile depth enlargement at the trailing edge of the tip of the free blade end blade area being >0. 2. A blade in accordance with claim 1, wherein the fixed blade end blade area includes a profile depth reduction over at least a portion thereof, as compared to the profile depth of the blade at the central meridional flow line of the blade. 3. A blade in accordance with claim 2, wherein the fixed blade end blade area includes a profile depth enlargement over at least a portion thereof, as compared to the profile depth of the blade at the central meridional flow line of the blade. 4. A blade in accordance with claim 3, wherein the fixed blade end blade area has a profile depth at its base of greater than 85%, as compared to the profile depth of the blade at the central meridional flow line of the blade. 5. A blade in accordance with claim 1, wherein the profile depth enlargement at the leading edge of the tip of the free blade end blade area is at least +10 percent, as compared to the profile depth of the blade at the central meridional flow line of the blade. 6. A blade in accordance with claim 5, wherein the ratio of the profile depth enlargement of the leading edge to the trailing edge at the tip of the free blade end blade area is between 1.5 to 4.0. 7. A blade in accordance with claim 6, wherein the profile depth enlargement at the tip of the free blade end blade area results in a trailing edge of the blade at the free blade end blade area which, in the meridional direction, is further downstream in the turbomachine than the trailing edge of the blade at the central meridional flow line of the blade. 8. A blade in accordance with claim 5, wherein the profile depth enlargement at the tip of the free blade end blade area results in a trailing edge of the blade at the free blade end blade area which, in the meridional direction, is further downstream in the turbomachine than the trailing edge of the blade at the central meridional flow line of the blade. 9. A blade in accordance with claim 1, wherein the fixed blade end blade area includes a profile depth reduction over at least a portion thereof, as compared to the profile depth of the blade at the central meridional flow line of the blade, and the fixed blade end blade area has a profile depth at its base of greater than 85%, as compared to the profile depth of the blade at the central meridional flow line of the blade. 10. A blade in accordance with claim 5, wherein the fixed blade end blade area includes a profile depth reduction over at least a portion thereof, as compared to the profile depth of the blade at the central meridional flow line of the blade, and the fixed blade end blade area has a profile depth at its base of greater than 85%, as compared to the profile depth of the blade at the central meridional flow line of the blade. 11. A blade in accordance with claim 6, wherein the fixed blade end blade area includes a profile depth reduction over at least a portion thereof, as compared to the profile depth of the blade at the central meridional flow line of the blade, and the fixed blade end blade area has a profile depth at its base of greater than 85%, as compared to the profile depth of the blade at the central meridional flow line of the blade. 12. A blade in accordance with claim 7, wherein the fixed blade end blade area includes a profile depth reduction over at least a portion thereof, as compared to the profile depth of the blade at the central meridional flow line of the blade, and the fixed blade end blade area has a profile depth at its base of greater than 85%, as compared to the profile depth of the blade at the central meridional flow line of the blade. 13. A blade in accordance with claim 8, wherein the fixed blade end blade area includes a profile depth reduction over at least a portion thereof, as compared to the profile depth of the blade at the central meridional flow line of the blade, and the fixed blade end blade area has a profile depth at its base of greater than 85%, as compared to the profile depth of the blade at the central meridional flow line of the blade. 14. A blade in accordance with claim 1, wherein the fixed blade end blade area includes a profile depth enlargement over at least a portion thereof, as compared to the profile depth of the blade at the central meridional flow line of the blade. 15. A blade in accordance with claim 14, wherein the profile depth enlargement at the leading edge of the tip of the free blade end blade area is at least +10 percent, as compared to the profile depth of the blade at the central meridional flow line of the blade. 16. A blade in accordance with claim 15, wherein the ratio of the profile depth enlargement of the leading edge to the trailing edge at the tip of the free blade end blade area is between 1.5 to 4.0. 17. A blade in accordance with claim 16, wherein the profile depth enlargement at the tip of the free blade end blade area results in a trailing edge of the blade at the free blade end blade area which, in the meridional direction, is further downstream in the turbomachine than the trailing edge of the blade at the central meridional flow line of the blade. 18. A blade in accordance with claim 1, wherein the profile depth continues from the free blade end blade area past the central meridional flow line into the fixed blade end blade area in a continuous concave curve on each of the leading and trailing edges to create a profile depth reduction on each of the leading and trailing edges over at least a portion of the fixed blade end blade area adjacent the central meridional flow line, and then continues in a continuous concave curve on each of the leading and trailing edges to create a profile depth enlargement on each of the leading and trailing edges at a base of the fixed blade end blade area, as compared to the profile depth of the blade at the central meridional flow line of the blade. 19. A blade in accordance with claim 18, wherein the blade is a rotor blade. 20. A blade in accordance with claim 1, wherein the blade is a rotor blade. 21. A method for positively influencing a radial gap flow for a free blade end of a stator/rotor blade for a fluid-flow machine, comprising: providing a blade having: a free blade end blade area adjacent to a tip clearance gap positioned between a blade tip and a main gas path boundary of one of a hub and a casing, anda fixed blade end blade area structurally connected to the main gas path boundary of one of the hub and the casing,the blade transmitting energy to the working fluid and being cambered to turn flow from high relative whirl to lower relative whirl,the blade being defined by flow line profile sections with a leading edge and a trailing edge which establish a forward end point and a rearward end point, respectively, each given by a tangent normal to and intersecting with a respective profile chord, with a distance between these end points being a respective profile depth, and the free end blade area and the fixed end blade area meeting at a central meridional flow line profile of the blade,the blade having an enlargement of the profile depth at the free blade end blade area which, in relation to a profile depth of the blade at a central meridional flow line of the blade, is at least +10 percent at a tip of the free blade end blade area and decreases to zero by the central meridional flow line of the blade, with the enlargement values being ≧0 throughout,reducing losses due to radial gap flow, and providing structural stress and aerodynamic loading continuity across the blade length, by providing the profile depth enlargement across substantially all of a length of the free blade end blade area and continuously increasing the profile depth enlargement in a continuous concave curve from the central meridional flow line to the tip of the free end blade area on each of the leading edge and the trailing edge, sizing the profile depth enlargement to avoid local distortion of the blade leading edge and trailing edge shape meridional projections, the profile depth enlargement at the trailing edge of the tip of the free blade end blade area being >0.