초록 ▼

A turbine blade assembly, in particular of a gas turbine, is provided. The turbine blade assembly includes a turbine disc with rotor blades inserted into notches of the turbine disc and locking plates that are placed inside circular grooves with rims in the turbine disc and in the rotor blade. The e

A turbine blade assembly, in particular of a gas turbine, is provided. The turbine blade assembly includes a turbine disc with rotor blades inserted into notches of the turbine disc and locking plates that are placed inside circular grooves with rims in the turbine disc and in the rotor blade. The edges of the locking plates that are oriented towards the center of the turbine disc are castellated by providing teeth and accordingly a part of the rim of the circular groove of the turbine disc is also castellated by providing gaps and whereby the gaps of the rim match the teeth of the locking plates. The locking plates have a spring-back force to provide both locking and sealing capabilities during engine operation.

대표청구항 ▼

1. A turbine blade assembly, comprising: a turbine disc with a rotor blade inserted into a notch of the turbine disc; anda locking plate, placed inside a plurality of circular grooves with a plurality of rims located in both the turbine disc and in the rotor blade,wherein an edge of the locking plat

1. A turbine blade assembly, comprising: a turbine disc with a rotor blade inserted into a notch of the turbine disc; anda locking plate, placed inside a plurality of circular grooves with a plurality of rims located in both the turbine disc and in the rotor blade,wherein an edge of the locking plate that is oriented towards a center of the turbine disc is castellated by providing a plurality of teeth,wherein a part of a rim of the circular groove of the turbine disc is also castellated by providing a plurality of gaps and in that the plurality of gaps of the rim match the plurality of teeth of the locking plate, wherein the locking plate is sprung and thereby is engaged and further comprises a bent portion which is located at or near the castellated edge and/or the bent portion is located at or near an edge lying opposite to the castellated edge, the bent portion extending into the plurality of teeth. 2. A turbine blade assembly as claimed in claim 1, wherein the turbine blade assembly is a gas turbine. 3. A turbine blade assembly as claimed in claim 1, wherein the locking plate further comprises a flat body with a plurality of rounded corners. 4. A turbine blade assembly as claimed in claim 1, wherein the locking plate provides a spring-back force, andwherein when the locking plate is inserted into the plurality of grooves, the spring-back force presses the flat body of the locking plate against a face of the turbine disc providing a sealing effect. 5. A turbine assembly as claimed in claim 1, wherein the bent portion is formed in the plurality of teeth. 6. A turbine assembly as claimed in claim 1, wherein the locking plate is flat outside the bent portion. 7. A turbine assembly as claimed in claim 1, wherein the locking plate is formed from a sheet metal. 8. A turbine assembly as claimed in claim 1, wherein the locking plate is held in place by a deformable closing plate, wherein the deformable closing plate is placed in a castellated part of the rim of the circular groove of the turbine disc to secure the locking plate in a circumferential direction. 9. A turbine assembly as claimed in claim 1, further comprising a closing plate which closes a further gap formed between two adjacent locking plates.