DEVICE FOR THE MUTUAL FIXING OF TWO COMPONENTS

Abstract

A device is provided for the mutual fixing of two components, which are interconnected via a flanged joint, for preventing a relative movement of the components in relation to each other in the connecting plane of the flanged joint. The device includes a key which engages in both components in a form-fitting manner in the region of the flanged joint. A simplified and flexible application is achieved by the key being guided in one of the components by means of a precision fit, whereas in the other of the components the form fit can be adjusted by adding shims.

Claims

1.-6. (canceled)

7. A method for connecting together casing components of a casing of a gas turbine, the method comprising: providing two finish-machined casing components, each casing component including a flange, the flanges forming a flanged joint, wherein the casing components have a first recess formed in an outer surface of a first flange of a first casing component of the two casing components and a second recess formed in an outer surface of a second flange of a second casing component of the two casing components, wherein the first and second recesses face each other across the flanged joint; inserting a finish-machined key into the first and second recesses in a radial direction toward a machine axis of the gas turbine, wherein after insertion into the recesses the key is in contact with at least two sides of the first recess and the key inserted alone being displacable in the second recess in a circumferential direction in relation to the first casing component; and inserting shims in the second recess to adjust the fit of the key in the second recess for preventing relative movement of the first and second casing components in a connecting plane of the flanged joint.

8. The method according to claim 7, comprising: inserting the key substantially orthogonal to the flanged joint.

9. The method as claimed in claim 7, comprising: arranging the key on an outer periphery of the flanged joint.

10. The method as claimed in claim 7, comprising: arranging the key to extend between the components in a direction parallel with the machine axis.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0009] The invention shall subsequently be explained in more detail based on exemplary embodiments in conjunction with the drawing. In the drawings:

[0010] FIG. 1 shows in a partially sectioned, perspective view a stationary gas turbine with sequential combustion, as is suitable for application of the invention;

[0011] FIG. 2 shows in a side view a concentric flanged joint with an adjustable key device according to an exemplary embodiment of the invention and (for comparison) a conventional round key, and

[0012] FIGS. 3a-3d show in a number of sub-figures the installation of an adjustable key according to an exemplary embodiment of the invention in a flanged joint of the type shown in FIG. 2.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS INTRODUCTION TO THE EMBODIMENTS

[0013] It is therefore an object of the invention to create a generic-type device which avoids the disadvantages of previously used devices and is distinguished particularly by a simple and flexible application.

[0014] The device according to the invention for the mutual fixing of two componentswhich are interconnected via a flanged jointfor preventing a relative movement of the components in relation to each other in the connecting plane of the flanged joint, comprises a key which engages in both components in a form-fitting manner in the region of the flanged joint. In the device according to the invention the key is guided in one of the components by means of a precision fit, whereas in the other of the components the form fit can be adjusted by adding shims.

[0015] In one embodiment of the device according to the invention, in the one component, provision is made for a first recess for the precision-fit seating of the key, and in the other component, provision is made for a second recess which accommodates the key with a clearance parallel to the connecting plane of the flanged joint.

[0016] In another embodiment, the key is arranged on the outer periphery of the flanged joint.

[0017] In a further embodiment, the flanged joint is formed concentrically to an axis, and the key extends between the components in the axial direction.

[0018] The device according to the invention is used in a gas turbine which has a casing extending along a machine axis and assembled from a plurality of sections which are arranged axially in series and interconnected in each case by a vertical flanged joint.

DETAILED DESCRIPTION

[0019] An essential element of the inventive idea is the installation of adjustable keys in components which are to be connected, which keys are delivered in an already finish-machined state. After assembly of the components, adjustable keys are installed. These keys are guided in one of the components by means of a precision fit and on the adjacent component are adjusted by shims.

[0020] During assembly, no additional machining is necessary. The components can be replaced without any difficulty; only the keys have to be readjusted.

[0021] The surface areas which are acted upon by forces are larger than in the case of round keys, which allow the transfer of greater forces.

[0022] FIG. 2 shows an exemplary flanged joint 18, which is formed concentrically to an axis 26, between two adjoining components 24 and 25. Such a flanged joint for example connects the individual sections of the casing 27 of the gas turbine 10 from FIG. 1.

[0023] According to the previous solution, round keys 19 (shown by a dotted line in FIG. 2) were inserted for the relative fixing of the two flanges 18a and 18b in relation to each other, which round keys engage in a form-fitting manner in both flanges 18a and 18b and are arranged in a radial hole. This type of fixing has the disadvantages listed in the introduction.

[0024] According to the invention, an adjustable key device 20 is now used instead, the installation of which is illustrated in detail in FIGS. 3a-3d. According to FIG. 3a, components 24 and 25 are delivered for assembly, the flanges 18a and 18b of the components already being provided with recesses 20a, b in each case for accommodating an adjustable key. The one recess 20a in this case is designed in terms of its dimensions so that it accommodates the key (21 in FIG. 3b) with the desired fit (arrows in FIG. 3b). The other recess 20b, in contrast, is dimensioned so that with the key 21 inserted the associated component 25 can be displaced or rotated in the circumferential direction in relation to the other component 24, as is shown in FIG. 3c.

[0025] If the desired relative positioning of the two components 24 and 25 in relation to each other is achieved, then according to FIG. 3c the key 21 is also fixed in the other recess 20b by corresponding shims 22, 23 being inserted, as is gathered from FIG. 3d. The shims may consist of thin plates or small plates 22, 23, for example, which are inserted successively into the gaps between the key 21 and the circumferentially delimiting walls of the recess 20b until the desired fit is achieved.

[0026] If, for example, one of the components 24, 25 is exchanged, a new fixing can be achieved in a simple manner by the shims 22 and 23 being exchanged or modified. Remachining of the components is not necessary in this case.

LIST OF DESIGNATIONS

[0027] 10 Gas turbine (e.g. Alstom GT26 type) [0028] 11 Air inlet [0029] 12 Compressor [0030] 13, 15 Combustion chamber [0031] 14, 16 Turbine [0032] 17 Exhaust housing [0033] 18 Flanged joint [0034] 18a, b Flange [0035] 19 Round key [0036] 20 Adjustable key device [0037] 20a, b Recess [0038] 21 Key [0039] 22, 23 Shim [0040] 24, 25 Component [0041] 26 Axis of the flanged joint [0042] 27 Casing [0043] 28 Machine axis