Modular gas turbine plant with a heavy duty gas turbine

Patent metadata

Field	Value
Publication number	US-10151244-B2
Application number	US-201314406328-A
Country	US
Kind code	B2
Filing date	Jun 7, 2013
Priority date	Jun 8, 2012
Publication date	Dec 11, 2018
Grant date	Dec 11, 2018

Abstract

A transportable gas turbine module including a baseplate supporting at least a gas turbine and a load drivingly connected to the gas turbine. The module further comprises a structure surrounding the gas turbine and the load and connected to the baseplate. The baseplate is designed such that it can support a heavy duty as turbine having a rated power of not less than 80 MW.

First claim

What is claimed is:

1. A gas turbine module, the gas turbine module comprising:
a baseplate supporting at least one heavy duty gas turbine having a rated power of not less than 80 MW and a load drivingly connected to the at least one heavy duty gas turbine; and
a structure surrounding the at least one heavy duty gas turbine and the load and connected to the baseplate, wherein:
the baseplate comprises a plurality of longitudinal beams, extending parallel to a direction of a rotation axis of the at least one heavy duty gas turbine, and a plurality of transverse beams, extending transversely and spaced longitudinally along the rotation axis, wherein the plurality of longitudinal beams and the plurality of transverse beams define a primary lattice structure, on which the at least one heavy duty gas turbine and the load are placed,
the at least one heavy duty gas turbine and the load are placed on and supported by a first pair of longitudinal beams of the plurality of longitudinal beams;
the at least one heavy duty gas turbine is constrained to a turbine base support, wherein the turbine base support is connected to the baseplate of the gas turbine module through a plurality of feet, and the plurality of feet are constrained to the first pair of longitudinal beams; and
a foundation having a planar surface of support for the baseplate, wherein the planar surface of support is discontinuous, wherein the foundation has channels running parallel to a plurality of longitudinal beams, and wherein the channels are arranged and configured for the insertion of lifting and moving trailers,
wherein the foundation further comprises a plurality of side supports and an intermediate support,
wherein the first pair of the plurality of longitudinal beams, on which the heavy duty gas turbine and the load are placed, rest on the intermediate support, and
one of a plurality of transverse beams rests on the side supports.

2. The gas turbine module according to claim 1 , wherein the load comprises an electric generator.

3. The gas turbine module according to claim 1 , wherein the first pair of the plurality of longitudinal beams are located in an intermediate position in the primary lattice structure between a second pair of longitudinal beams of the plurality of longitudinal beams.

4. The gas turbine module according to claim 1 , wherein the plurality of transverse beams and the plurality of longitudinal beams define a top planar surface of the baseplate.

5. The gas turbine module according to claim 4 , wherein the plurality of transverse beams and the first pair of the plurality of longitudinal beams have substantially the same height and define a bottom planar surface of the baseplate, the bottom planar surface forming a rest surface on the foundation.

6. The gas turbine module according to claim 1 , wherein the baseplate is divided into baseplate sections, wherein each of the baseplate sections is aligned to one another in a direction parallel to the rotation axis of the at least one heavy duty gas turbine and connected to one another to form a rigid baseplate structure.

7. The gas turbine module according to claim 6 , wherein each transverse beam of the plurality of transverse beams has a length corresponding to a width of the baseplate and each longitudinal beam of the plurality of longitudinal beams is formed by a plurality of longitudinal beam portions aligned along the direction of the rotation axis of the at least one heavy duty gas turbine, each longitudinal beam portion of the plurality of longitudinal beam portions extending between respective transverse beams of the plurality of transverse beams, wherein the plurality of longitudinal beam portions of each longitudinal beam is connected to one another by welding to respective transverse beams of the plurality of transverse beams.

8. The gas turbine module according to claim 1 , wherein the primary lattice structure has a plurality of substantially rectangular meshes, wherein in at least some of the plurality of substantially regular meshes, a secondary lattice structure is provided, wherein the secondary lattice structure is formed by secondary beams running parallel to the plurality of transverse beams of the primary lattice structure and the plurality of longitudinal beams of the primary lattice structure.

9. The gas turbine module according to claim 1 , wherein the primary lattice structure has a plurality of substantially rectangular meshes, wherein in at least some of the plurality of substantially rectangular meshes, bracings are arranged in a plane parallel to the baseplate and are inclined with respect to both the plurality of longitudinal beams and the plurality of transverse beams.

10. The gas turbine module according to claim 1 , wherein the plurality of transverse beams and the plurality of longitudinal beams forming the primary lattice structure each comprise a central web welded to upper and lower flanges.

11. The gas turbine module according to claim 1 , further comprising spherical washers between the turbine base support and the plurality of feet for adjusting an inclination of the at least one heavy duty gas turbine with respect to the baseplate of the transportable gas turbine module.

12. The gas turbine module according to claim 1 , further includes a plurality of auxiliary transverse connection beams provided under the at least one heavy duty gas turbine, to transversely connect the first pair of the plurality of longitudinal beams.

13. The gas turbine module according to claim 1 , wherein the load is placed on a plurality of load base supports constrained to a pair of intermediate longitudinal beams of the plurality of longitudinal beams, wherein the plurality of load base supports extends parallel to the plurality of transverse beams.

14. An on-shore gas turbine plant comprising a gas turbine module comprising:
a baseplate supporting at least one heavy duty gas turbine having a rated power of not less than 80 MW and a load drivingly connected to the at least one heavy duty gas turbine; a structure surrounding the at least one heavy duty gas turbine and the load and connected to the baseplate; and
a foundation, having a planar surface of support for the gas turbine module, wherein the planar surface of support is discontinuous and the foundation has channels running parallel to a plurality of longitudinal beams, wherein the channels are arranged and configured for the insertion of lifting and moving trailers,
wherein the foundation further comprises a plurality of side supports and an intermediate support,
wherein a pair of the plurality of longitudinal beams, on which the heavy duty gas turbine and the load are placed, rest on the intermediate support and
wherein one of a plurality of transverse beams rests on the side supports.

15. The on-shore gas turbine plant according to claim 14 , wherein the side supports and the intermediate support comprise recesses housing sole plates grouted in the recesses, wherein said sole plates form resting surfaces for the plurality of transverse beams and the plurality of longitudinal beams.

16. The on-shore gas turbine plant according to claim 15 , wherein the foundation comprises stud bolts grouted therein and arranged for connection to the baseplate.

17. The on-shore gas turbine plant according to claim 14 , wherein the baseplate comprises a plurality of shear keys, horizontally anchoring the baseplate to the foundation.

18. The on-shore gas turbine plant according to claim 17 , further comprising:
a first set of shear keys, of the plurality of shear keys, de

Assignees

• Nuovo Pignone Srl

Inventors

• Giancotti Marco
• Caverni Stefano

Classifications

• F16M5/00

  Engine beds, i.e. means for supporting engines or machines on foundations · CPC title

• F05D2260/12

  Testing on a test bench · CPC title

• F01D25/28

  Supporting or mounting arrangements, e.g. for turbine casing · CPC title

• F02C7/20 Primary

  Mounting or supporting of plant; Accommodating heat expansion or creep · CPC title

• F16M1/04 Primary

  for rotary engines or similar machines · CPC title