T 0680/09 10-07-2009

1. Admissibility of the appeal

The decision under appeal rejected the sole request for both lack of inventive step in the subject matter of claim 1 and for lack of conciseness of the claims due to repetition (Article 84 EPC 1973). The arguments in the appellant's grounds of appeal concerning the reasons for which the subject matter of claim 1 involved an inventive step provided sufficient substantiation for the Board to understand why the appellant was of the opinion that the decision should be overturned in that regard. Concerning the objection to conciseness, the appellant stated in its appeal grounds that "the claims have been amended for conciseness by cancelling the subject matter of previous claim 3". Thus the Board can recognise that this was an attempt to overcome the objection to conciseness of the claims when seen as a whole, and is thus able to understand why the appellant was of the opinion that the decision should be overturned in that regard by means of its amendment. By way of claim deletion being performed specifically to meet this objection when supplying its grounds of appeal, a substantiation for overturning the decision in this regard is thus present.

Since no other matters concerning the admissibility of the appeal arise in this matter, the Board concludes that the appeal is admissible.

2. Main request

2.1 In view of the amendments made to the claims, whereby only a single dependent claim remained which does not repeat any of the features in claim 1, the objection to lack of conciseness (Article 84 EPC 1973) is overcome.

2.2 In respect of inventive step and of the documents cited, D1 is considered to be the closest prior art starting point and this is also agreed by the appellant.

2.2.1 Contrary to the appellant's submission however, D1 indeed concerns the repair of "blisks" (i.e. an integral rotor disk with blades, as described in the application at paragraph [0004]). In particular, D1 discloses the repair process in the specific context of the "repair of blades for integral rotor disks of a turboengine" as being a preferred use (see e.g. column 5, lines 33 to 40). D1 even provides an example (Example 1) specifically describing the process carried out on such an integral rotor disk (see column 6, lines 35 to 42). The appellant's argument in this regard that the process of D1 was only intended for use in repairing separate disk blades mounted on a rotor disk finds no support in D1, and the repair of separate rotor blades mounted on a rotor disk is merely given as an alternative to the repair of blisks.

2.2.2 The appellant further argued that D1 did not disclose a predetermined notch location, but merely a notch size. The Board is however unconvinced by the appellant's argument. In column 6, lines 35 to 41 of D1, it is disclosed that "one or more standardized separation cuts 10 - 15, are made", whereby separation cut 15 is a semicircular cut (see column 6, lines 46 to 53). Moreover, standardizing of the cuts is explained in column 7, lines 6 to 10 as being such that the cuts "do not have to be adapted individually to each blade". Thus the cuts are predetermined in both size and location, as anything else would require being adapted individually for each blade and thus contrary to D1.

Whilst D1 also discloses, very generally, in column 1, lines 13 to 21 that the separation of the damaged portion depends on how and where the blade is damaged, this does not detract from the fact that in the specific case of Example 1 it is explained how standardizing is performed.

2.2.3 D1 also discloses (see column 6, lines 43 to 61) that "the standardizing of the separation cuts is obtained on the basis of" distribution of stress, reasons of accessibility and on the occurrence of damage due to effects of foreign objects, and that the separation is performed so as to leave a blade stump of sound material. As is evident from this, the separation cuts are therefore of such a size and in such a location that the separation is made outside areas of maximum stress, because the distribution of stress is taken into account when providing the standardized separation cuts which results in the stump of sound material.

2.2.4 The last feature of claim 1, according to which the notch size is uniform for all of said airfoils in said blisk irrespective of damage area therein, is also known from D1, since the cuts are "standardised" and in as far as the word "uniform" in claim 1 can be understood, this has the same meaning as "standardized" in this context because the standardizing in D1 is such that no individual adaptation is required for each blade.

2.2.5 The step of welding a repair in said airfoil to fill said notch by means of a multi-axis numerically controlled welding machine is also disclosed, since in Example 1 three welding types may be used (see e.g. column 8, lines 1 to 6) and in column 5, lines 25 to 32 it is explained that a seam tracking system for detection and automatic butt welding is provided, whereby also curved welds can be precisely produced. This was also not disputed by the appellant.

2.3 Since, in Example 1, it is only stated that the removal of material is by way of a laser beam (column 7, line 21 to 53), the only features of claim 1 which are not disclosed in D1 are the following:

(a) machining away damage is accomplished in a multi-axis numerically controlled milling machine;

(b) initiating and terminating said repair welding outside said notch.

2.4 The appellant stated that the objective problem to be solved over D1 was to provide a high quality weld repair in an automated manner. However, the Board finds that this problem is not objective, since no evidence has been provided that D1 does not itself produce a high quality weld, and the weld is quite evidently already produced in an automated manner.

2.4.1 The two features (a) and (b) identified above do not solve a common problem, but independent problems; feature (a) solving the problem of providing an alternative method of automated cutting of an airfoil, and feature (b) solving the problem of avoiding non-homogeneous locations at the start and end of a weld.

2.4.2 Regarding feature (a), the use of numerically controlled milling as a method of removing material in an airfoil for its subsequent repair is known from D5 (see e.g. page 9, lines 5 to 8) where it is given as an alternative to a procedure of cutting by erosion. A skilled person wishing to provide an alternative method of automated cutting of an airfoil is thus taught that numerically controlled milling is a suitable method for this purpose and would apply such a method where the circumstances make it appropriate, without needing to use inventive skill. It is also implicit that a numerical controlled machine has several degrees of freedom. This feature was also found to be obvious by the examining division when considering the teaching of D5 and the appellant has not challenged that finding.

2.4.3 Regarding feature (b), the skilled person is taught by e.g. D3 (see column 8, lines 50 to 54), that run-off tabs are used for starting and stopping a weld since at those locations metallurgical defects may be caused. A skilled person wishing to solve the problem of avoiding non-homogeneous locations would thus adopt the teaching of D5 and use this in the method of D1. As stated with regard to feature (a), this feature was also found to be obvious by the examining division when considering the teaching of D3 and the appellant has not challenged that finding.

2.5 The appellant argued that D1 involved building up a weld repair in layers by adding several plates radially and that this was not the same as the method described in the patent. However, nothing in claim 1 defines the manner of performing a repair which differs over D1; claim 1 merely defines "welding a repair in said airfoil". How the repair material is constructed in a way which might be different from D1 is not defined.

2.6 The subject matter of claim 1 consequently lacks an inventive step such that the requirement of Article 56 EPC 1973 is not fulfilled. The main request is therefore not allowable.

3. Auxiliary request

3.1 Of the additional features added to claim 1 of the main request, the feature "said notch is positioned along leading or trailing edges of said airfoil, and spaced outboard from a root thereof, said notch having an arcuate profile along said airfoil" is disclosed already in D1, due to the fact that notch 15 is semicircular, and is located well away from the root (almost half way up the airfoil) on the trailing edge (see e.g. Figure 1b and column 6, lines 48 to 53).

3.2 Thus, the only feature added to claim 1 of the main request which is not disclosed in D1 is "said repair being formed in layers to fill said notch".

Starting from D1, this feature solves the problem of making the repair by an alternative method of forming a weld compared to the welding of a plate, wherein such welding should result in defect-free welded layers (see e.g. the published application column 7, lines 6 to 14).

3.3 D3 discloses the feature of providing a weld repair by forming a repair in layers (see e.g. column 3, lines 44 to 50 and the Figures). In D3, the specific embodiment concerns the repair of a turret type connection of a turbine blade to a disk, but in column 1, lines 38 to 41 it is disclosed that the method also relates to repair procedures for worn or damaged surface of turbine components and to welding techniques for building up these worn surfaces with sound metal deposits. Thus, contrary to the appellant's submission, D3 is not incompatible with D1 as its teaching to a skilled person clearly is that it is applicable to turbine components in general and not merely repairing a damaged turret (steeple) connection, such that whilst D3 is not directed specifically to the repair of a notch, D3 teaches building up of layers to provide a weld with minimised defects in a turbine. This teaching would thus equally be applied to the repair of a notch in a turbine application. In particular, there is no feature of the notch defined in claim 1 which alters this opinion, as the notch is merely defined as being arcuate and thus implies nothing which might cause the method of D3 not to be compatible with some aspect thereof. Likewise, nothing in D3 indicates that such a method would be incompatible with the welding of the notch as shown in D1.

Further, D3 notes (see e.g. column 1, lines 51 and 52) that prior art repairs are already known involving welding of individual pieces to worn rotors or discs, and that the invention in D3 (see e.g. column 3, lines 1 to 62) relates to minimization of defects and achieves this by welding in layers.

The skilled person is therefore taught by D3 that an alternative to welding a plate in place as a repair is to use welding in layers, and that this minimises defects. The skilled person would thus use this teaching in place of the method of welding in a plate as in D1, and thus arrive at the subject matter of claim 1 without using inventive skill.

3.4 Consequently, the subject matter of claim 1 does not involve an inventive step and thus does not fulfil the requirement of Article 56 EPC 1973.

The request is therefore not allowable.