초록 ▼

On production of a component, two primary pieces must often be fixed together to give one piece. In order to achieve the above, it is important that the two primary pieces are oriented in a particular manner during the fixing process, which provides some difficulties. According to the invention, a p

On production of a component, two primary pieces must often be fixed together to give one piece. In order to achieve the above, it is important that the two primary pieces are oriented in a particular manner during the fixing process, which provides some difficulties. According to the invention, a plug body is fixed to the component by a mounting, whereby the position of the plug body relative to the component remains unchanged during a fixing process.

대표청구항 ▼

The invention claimed is: 1. A method for production of a gas turbine blade component having a surface, comprising: introducing a filling element into the component through a first side of the surface of the component; connecting the filling element to the component by a soldering method; during th

The invention claimed is: 1. A method for production of a gas turbine blade component having a surface, comprising: introducing a filling element into the component through a first side of the surface of the component; connecting the filling element to the component by a soldering method; during the soldering method of the filling element and component, using a an M shaped holder that connects the filling element to the component temporarily, wherein the holder has a first holding point on the first side of the surface of the component and a second holding point on the filling element; and removing the holder after the filling element and component have been fixed by soldering, wherein the filling element is introduced into a groove in the component, and between the filling element and the component in the grove there is a gap, wherein a first end of the M shape of the holder is fixed to a first holding point on the component, a middle of the M shape of the holder is fixed to a second holding point on the filling element, a second end of the M shape of the holder is fixed to a third holding point on the component, and the filling element is a permanent plug wherein the filling element is arranged such that a further gap is formed between a bottom of the filling element and a base of the groove in the component, wherein the further gap traverses the entirety of the base of the filling element. 2. The method as claimed in claim 1, wherein two holders are used. 3. A method for production of a gas turbine blade component having a surface, comprising: introducing a filling element into the component through a first side of the surface of the component; connecting the filling element to the component by a soldering method; during the soldering method of the filling element and component, using a holder that connects the filling element to the component temporarily, wherein the holder has a first holding point on the first side of the surface of the component and a second holding point on the filling element; and removing the holder after the filling element and component have been fixed by soldering, wherein the filling element is introduced into a groove in the component, there is a gap between the filling element and the component in the grove, and the holder is M shape, and the filling element is a permanent plug wherein the filling element is arranged such that a further gap is formed between a bottom of the filling element and a base of the groove in the component, wherein the further gap traverses the entirety of the base of the filling element. 4. The method as claimed in claim 3, wherein two holders are used. 5. The method as claimed in claim 3, wherein a first end of the M shape of the holder is fixed to a first holding point on the component, the middle of the M shape of the holder is fixed to a second holding point on the filling element, and a second end of the M shape of the holder is fixed to a third holding point on the component. 6. The method as claimed in claim 1, wherein the filling element is arranged between the first and third holding points. 7. A method for production of a gas turbine blade component having a surface, comprising: introducing a filling element into a grove the component through a first side of the surface of the component; attaching a holder to temporarily connect the filling element to the component; connecting the filling element to the component by a soldering method; during the soldering method of the filling element and component, using the holder that connects the filling element to the component; and removing the holder after the filling element and component have been fixed by soldering, wherein wherein the holder has a first holding point on the first side of the surface of the component and a second holding point on the filling element; a spacer is arranged in the groove between the filling element and the component such that a gap is formed in the groove between the filling element and the component, and the holder is M shaped, and the filling element is a permanent plug wherein the filling element is arranged such that a further gap is formed between a bottom of the filling element and a base of the groove in the component, wherein the further gap traverses the entirety of the base of the filling element. 8. The method as claimed in claim 7, wherein the spacer is arranged in a vicinity of the surface of the gas turbine blade component. 9. A method for production of a gas turbine blade component having a surface, comprising: introducing a filling element into a grove the component through a first side of the surface of the component: attaching a holder to temporarily connect the filling element to the component; connecting the filling element to the component by a soldering method; during the soldering method of the filling element and component, using the holder that connects the filling element to the component; removing the holder after the filling element and component have been fixed by soldering; and removing the spacer after the attaching of the holder, wherein wherein the holder has a first holding point on the first side of the surface of the component and a second holding point on the filling element; a spacer is arranged in the groove between the filling element and the component such that a gap is formed in the groove between the filling element and the component, the holder is M shaped. 10. The method as claimed in claim 7, wherein a plurality of spacers are arranged to provide a uniform gap between sides of the filling element and component.