IP Library › Granted Patent US 10,794,287
Granted Patent B2
US 10,794,287 · App. 16/077,333 · Granted Oct 6, 2020

Modular gas turbine system

Inventors: Marco Giancotti (Florence, IT); Andrea Righeschi (Florence, IT); Luciano Guidotti (Florence, IT); Michele Cecarini (Florence, IT)
Assignee: NUOVO PIGNONE TECNOLOGIE SRL
F02C7/143F01D25/285F02C7/18F25J1/0278F25J1/0283F25J1/0296F05D2220/32F05D2230/68F05D2240/91F05D2250/80F05D2260/20F05D2260/213F25J2290/42
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 10,794,287
App. No.
16/077,333
Granted
Oct 6, 2020
Kind
B2
Abstract

A modular gas turbine system is disclosed. The system includes a base plate and a gas turbine engine mounted on the base plate. The gas turbine engine has a rotation axis, a first air compressor section and a second air compressor section. A rotating load is mechanically coupled to the gas turbine engine and mounted on the base plate. A supporting frame extends above the base plate and supports a plurality of secondary coolers, which are fluid exchange relationship with an intercooler of the gas turbine engine.

Claims (21)

1. A modular gas turbine system, comprising:

a base plate;

mounted on the base plate, a gas turbine engine having a rotation axis, a first air compressor section and a second air compressor section;

at least one rotating load, mechanically coupled to the gas turbine engine and mounted on the base plate;

a supporting frame extending above the base plate;

an air intercooler fluidly coupled to the first air compressor section and second air compressor section, the air intercooler configured and arranged to cool partly compressed air from the first air compressor section in heat exchange relationship with a heat removal fluid;

wherein a plurality of secondary coolers are arranged on the supporting frame above the base plate at a level above at least one of the gas turbine engine and the load, and are in fluid exchange relationship with the intercooler, the heat removal fluid being in heat exchange relationship with a cooling medium in the secondary coolers.

2. The modular gas turbine system of claim 1 , wherein the secondary coolers are air coolers and the heat removal fluid is in heat exchange relationship with cooled ambient air in said secondary coolers.

3. The modular gas turbine system of claim 1 , further comprising at least one lube oil cooler arranged on the supporting frame.

4. The modular gas turbine system of claim 3 , wherein the at least one lube oil cooler is arranged at the same level as the secondary coolers.

5. The modular gas turbine system of claim 1 , further comprising a first bridge crane movably supported on the supporting frame.

6. The modular gas turbine system of claim 1 , further comprising a first bridge crane and a second bridge crane, both movable on the supporting frame.

7. The modular gas turbine system of claim 6 , wherein the first bridge crane and the second bridge crane are movable on common rails mounted on the supporting frame.

8. The modular gas turbine system of claim 6 , wherein at least one of the first bridge crane and second bridge crane is movable on rails extending substantially parallel to a rotation axis of the gas turbine engine.

9. The modular gas turbine system of claim 6 , wherein the first bridge crane is movable along first rails extending substantially parallel to the rotation axis of the gas turbine engine and the second bridge crane is movable along second rails extending substantially orthogonal to the rotation axis of the gas turbine engine.

10. The modular gas turbine system of claim 6 , wherein at least one of said first bridge crane and second bridge crane is movable on first rails extending substantially parallel to the rotation axis of the gas turbine engine and projecting horizontally beyond the footprint of the base plate up to a lay down area arranged on a side of the base plate.

11. The modular gas turbine system of claim 6 , wherein the first bridge crane has a lifting capacity higher than the second bridge crane.

12. The modular gas turbine system of claim 6 , further comprising a third bridge crane movably supported on the supporting frame.

13. The modular gas turbine system of claim 12 , wherein the first bridge crane and the second bridge crane are movably arranged on first rails supported by the supporting frame, the third bridge crane is movably arranged on second rails supported by the supporting frame, and the second rails are arranged above the first rails.

14. The modular gas turbine system of claim 1 , wherein the rotating load comprises at least one gas compressor.

15. The modular gas turbine system of claim 1 , wherein the modular gas turbine system is configured to be transportable.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 11, 2018
From: GIANCOTTI, MARCO; RIGHESCHI, ANDREA; GUIDOTTI, LUCIANO
To: NUOVO PIGNONE TECNOLOGIE SRL
Reel/Frame 047748/0531 →
Priority Claims (1)
IT 102016000016891 · Feb 18, 2016 · national
Continuity (1)
Related Publication 20190055887A1 · Feb 21, 2019