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In order to configure the bending of a plate in an intermediate space between two blade rings, arranged along an axis of a compressor and having blades extending along a radius in a simpler and more effective manner, the novel concept provides a bending device which can be positioned in the intermed

In order to configure the bending of a plate in an intermediate space between two blade rings, arranged along an axis of a compressor and having blades extending along a radius in a simpler and more effective manner, the novel concept provides a bending device which can be positioned in the intermediate space and has, according to the invention, a fixing element for the bending device, a hydraulic system and a punch which can be actuated by the hydraulic system. Accordingly, a method for bending a plate in the intermediate space provides for a bending device to be positioned in the intermediate space, for the bending device to be fixed in the intermediate space, and for a punch of the bending device to be hydraulically actuated for bending the plate, the punch being moved toward the plate to be bent, and the plate being bent under the effect of the punch.

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The invention claimed is: 1. A gas turbine engine locking plate bending system, comprising: a hydraulic system; a hydraulic punch arranged along a longitudinal axis of the turbine in an intermediate space between adjacent rotor stages, and actuated by the hydraulic system; and a fixing element arra

The invention claimed is: 1. A gas turbine engine locking plate bending system, comprising: a hydraulic system; a hydraulic punch arranged along a longitudinal axis of the turbine in an intermediate space between adjacent rotor stages, and actuated by the hydraulic system; and a fixing element arranged between the hydraulic punch and an adjacent down stream rotor stage that secures the hydraulic punch to the rotor in the intermediate space. 2. The bending system as claimed in claim 1, wherein the entire bending device is sized and configured to fit in the intermediate space between adjacent rotor stages. 3. The bending system as claimed in claim 2, wherein the bending device is portable. 4. The bending system as claimed in claim 3, wherein the hydraulic pump is exchangeable. 5. The bending system as claimed in claim 4, wherein the punch is exchangeable. 6. The bending system as claimed in claim 1, wherein the fixing element is a clamping element which enables the hydraulic punch to be clamped in place in the intermediate space. 7. The bending system as claimed in claim 6, wherein the fixing element is adapted to fit into different sized intermediate spaces between rotor stages. 8. The bending system as claimed in claim 1, wherein the punch extends in the radial direction. 9. A method for bending a gas turbine blade locking plate, comprising: positioning a hydraulically actuated bending device in an intermediate space between two stages of a rotor extending along a radius of the rotor; fixing the bending device to the rotor in the intermediate space; hydraulically actuating the bending device to move toward the locking plate; and bending the locking plate due to a force exerted by the bending device on the locking plate. 10. The method as claimed in claim 9, wherein the entire bending device is fixed in the intermediate space along the axis. 11. The method as claimed in claim 9, wherein a punch of the bending device moves in the radial direction toward the locking plate. 12. The method as claimed in claim 9, wherein the locking plate is displaced into a groove of an impeller to lock the blade in place. 13. A portable turbine rotor blade locking plate bending system, comprising: a portable bending device arranged coaxial with a longitudinal axis of a turbine rotor in an intermediate space between adjacent rotor stages, the bending device containing a punch that moves in the radial direction toward the locking plate; an actuation device that energizes the punch; and a fixing element arranged between the portable bending device and an adjacent down stream rotor stage that secures the portable bending device to the rotor. 14. The portable bending system as claimed in claim 13, wherein the power actuated punch is hydraulically energized. 15. The portable bending system as claimed in claim 13, wherein the portable bending device is arranged radially outboard of the turbine rotor blade locking plate and the punch acts radially inward to deform the locking plate. 16. The portable bending system as claimed in claim 13, wherein the portable bending device incorporates a sealing tip protector located on a radially inward oriented surface of the bending device. 17. The portable bending system as claimed in claim 16, wherein the tip protection is a polymer or metal coating. 18. The portable bending system as claimed in claim 13, wherein the fixing element is formed in unity with the bending device. 19. The portable bending system as claimed in claim 13, wherein the fixing element is a hydraulic cylinder or a screw clamp.