Gas turbine having a lifting mechanism

Abstract

A crane system having a gas turbine that has a manhole on the outer housing thereof, the manhole being designed to open up a maintenance access to hot gas parts of the gas turbine in the open state of the manhole, which is provided with a fastening section; the crane system further has a hoisting mechanism that includes a mating fastening section which is connected to the fastening section of the manhole in such a way that the hoisting mechanism introduces weights that same has to lift into the outer housing of the gas turbine.

Claims

1. A crane system comprising: a combustion gas turbine comprising an outer housing, a plurality of burner openings in the outer housing, and a manhole on the outer housing, the manhole comprising a fastening section; and a lifting mechanism comprising a mating fastening section, a pillar, and at least one boom arm, wherein the mating fastening section of the lifting mechanism is configured to be connected to the fastening section of the manhole, wherein, when the mating fastening section of the lifting mechanism is connected to the fastening section of the manhole, the lifting mechanism introduces weight forces onto the outer housing of the combustion gas turbine such that the weight forces are distributed onto the outer housing of the combustion gas turbine, and wherein, when the mating fastening section of the lifting mechanism is connected to the fastening section of the manhole, the at least one boom arm is positionable above the plurality of burner openings in the outer housing.

2. The crane system as claimed in claim 1, wherein the mating fastening section comprises a mating fastening section flange, and wherein the fastening section comprises a fastening section flange configured to be screwed to the mating fastening section flange.

3. The crane system of claim 2, wherein the fastening section flange has a thickened region via which the weight forces are further directed.

4. The crane system as claimed in claim 1, wherein the manhole is arranged at a vertex of the outer housing.

5. The crane system as claimed in claim 1, wherein the mating fastening section is fitted to one end of the pillar.

6. The crane system as claimed in claim 1, wherein the lifting mechanism comprises at least two boom arms which comprise a pivotable design.

7. The crane system as claimed in claim 6, wherein at least one boom arm of the at least two boom arms comprises a multi-part design comprising individual parts, wherein the individual parts are pivotable with respect to one another.

8. The crane system of claim 1, further comprising: the pillar secured to the mating fastening section, and the boom arm pivotably secured to the pillar.

9. The crane system of claim 8, wherein the boom arm comprises two boom parts pivotally secured to each other so that the two boom parts pivot about a vertical pivot axis.

10. The crane system of claim 1, wherein the fastening section located on the outer housing is adapted to support loads to be lifted and is adapted to provide an introduction of force into a foundation upon which the combustion gas turbine is already positioned, wherein the foundation is designed for loading with large weight forces.

11. The crane system of claim 1, wherein the at least one boom arm is pivotable on the pillar such that the at least one boom arm is positionable above the plurality of burner openings in the outer housing.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) In the drawings:

(2) FIG. 1 shows a first embodiment of the crane system according to the invention with an embodiment of the lifting mechanism according to the invention in a perspective view from the side;

(3) FIG. 2 shows a further embodiment of the crane system according to the invention with a further embodiment of the lifting mechanism according to the invention in a perspective side view;

(4) FIG. 3 shows the embodiment of the crane system according to the invention illustrated in FIG. 2 together with the embodiment of the lifting mechanism according to the invention in an operating position which differs from that in FIG. 2;

(5) FIG. 4 shows a flow chart of a first embodiment of the method according to the invention for producing a crane system.

DETAILED DESCRIPTION OF INVENTION

(6) FIG. 1 shows a first embodiment of the crane system 100 according to the invention with an embodiment of the lifting mechanism 30 according to the invention, which mechanism is fitted to a fastening section 25 of a manhole 20 on the outer housing 11 of the gas turbine 10 on a foundation 50 via a mating fastening section 35. Besides the manhole 20, the outer housing 11 provides a further number of housing opening's 60 (burner openings), which are not provided with reference signs, via which the interior of the gas turbine 10 and thus the components acted upon by hot gas can be reached by the maintenance personnel.

(7) The lifting mechanism 30 itself is designed as a pillar crane, which has a pillar 31 which has the mating fastening section 35 in question at one end, said mating fastening section being connected to the fastening section 25 of the manhole 20. The connection of the two sections 25, 35 is realized by means of a flange connection, since the fastening section 25 is designed as a fastening flange and the mating fastening section 35 is designed as a mating fastening flange. Both flanges are securely connected to one another, for example via suitable threaded bolts. The flange may have a thickened region 51.

(8) The lifting mechanism 30 designed as a pillar crane further has a boom arm 36 which is connected at one end to the pillar 31 via a joint or pivot hinge (not further provided with a reference sign). The boom arm 36, which has a double-T profile or even an MSH profile in cross section (perpendicular to the direction of longitudinal extent), allows a motor 41 which is connected to an input unit 42 on the pillar 31 by a suitable electrical supply line 40, to perform lifting operations. For example, the motor 41 can be moved along the boom arm 36 via suitable running rollers (not provided with further reference signs), wherein, at the same time, a load cable (not shown in more detail) for lifting or supporting loads can be used, for example. By means of suitable handling, it is possible, for example, to move the boom arm 36 to a location, for example above the burner openings shown, such that, following suitable positioning of the motor along the boom arm 36, this arm can be directly positioned above the designated burner opening in an extended state. On account of the pillar structure, there is sufficient space available in the region of the burner openings for the maintenance personnel or a further maintenance device.

(9) FIG. 2 shows a further embodiment of the crane system according to the invention with another embodiment of the lifting mechanism 30 according to the invention. The lifting mechanism 30 has two boom arms 36, 37, which are both fastened to a pillar 31, in each case via a pivot joint (not further provided with a reference sign). The pivot joint allows pivoting of the boom arm 36, 37 in question through more than 180, such that again all regions of the outer housing 11 of the gas turbine 10 required for maintenance can be reached by means of both boom arms 36, 37. At the same time, the lifting mechanism 30 provides two boom arms 36 and 37, which are also used at the same time. Consequently, the flexibility is increased when using the present embodiment. Alternatively, it is also possible for a plurality of boom arms 36, 37 to be provided for the purpose of further increasing the flexibilization of the use of the lifting mechanism 30.

(10) The two boom arms 36, 37 are again of multi-part design, wherein the individual parts are again fastened in a pivotable manner with respect to one another. In order to pivot individual parts of a boom arm 36, 37 with respect to one another, joints 38 and 39 are provided in the respective boom arms 36 and 37. The joints 38 and 39 thus define the individual parts (not provided with reference signs) of the respective boom arm 36, 37.

(11) The adjustment or pivoting of the boom arms 36, 37 can take place manually, with or without auxiliary means. Auxiliary means are, for example, suitable guide cables which are fitted to the boom arms 36, 37.

(12) In order to further increase the flexibility with regard to the carrying out of maintenance work, the parts of the boom arms 36, 37 provided with the respective motors 41 can be of telescopic design. Likewise, it may also be sufficient for these end parts of the respective boom arms 36, 37 to have, in cross section, a double-T profile or an MSH profile, along which the respective motor 41 can be moved.

(13) The fastening of the lifting mechanism 30 to the outer housing 11 of the gas turbine 10 is again realized by means of a suitable mating fastening section 35 which is fitted to the fastening section 25 of a manhole 20. In the present case too, the manhole 20 is arranged at a vertex of the outer housing 11 in a comparable manner to the embodiment shown in FIG. 1. This can be readily understood from the shown curvature of the outer housing 11.

(14) FIG. 3 shows the embodiment of the crane system 100 according to the invention already illustrated in FIG. 2 together with the corresponding embodiment of the lifting mechanism 30 according to the invention. The operating position illustrated in FIG. 3 differs from that illustrated in FIG. 2 solely in that the individual parts of the boom arms 36 and 37 have been pivoted via the joints 38 and 39 in such a manner that the parts belonging to one boom arm 36, 37 are largely oriented parallel to one another. On the basis of this illustration, it is readily apparent that not only regions of the outer housing 11 of the gas turbine 10 that are at a large distance from the manhole 20 can be reached by the boom arms 36, 37, but also maintenance regions that are situated in the immediate vicinity of the manhole. In addition, the operating state shown in FIG. 3 can also represent a standby position, in which the crane system 100 provides relatively little hindrance for other maintenance work that does not require the crane system 100. The present operating position can equally be a transport position in which the crane system 100 can be taken off the gas turbine 10 or mounted on it without hindering the installation work.

(15) It should furthermore be pointed out that the pillar 31 of the lifting mechanism 30 is of height-adjustable design, such that the lifting mechanism 30 can, as a complete unit, also be adjusted in height.

(16) FIG. 4 shows a flow chart of an embodiment of the method according to the invention for producing a crane system. Here, the following steps are provided:opening a manhole 20 on the outer housing 11 of a gas turbine 10 (first method step 101);fastening a mating fastening section 35 of a lifting mechanism 30 to a fastening section 25 of the manhole 20 (second method step 102).

(17) Further embodiments can be gathered from the subclaims.