Jose Adan Guillen

US Patent:

20230045567, Feb 9, 2023

Filed:

Oct 18, 2022

Appl. No.:

17/968784

Inventors:

- Schenectady NY, US
Balakrishnan Ponnuraj - Sugar Land TX, US
Vineet Sethi - Sugar Land TX, US
Jose Emmanuel Guillen - Humble TX, US
Tho Vankhanh Nguyen - Cypress TX, US
Douglas Alan Jones - Bellaire TX, US
Abhinash Reddy Konatham - Sugar Land TX, US

International Classification:

F01D 25/30
F01D 9/06

Abstract:

One or more cooling systems for ventilating a turbine and rotary shaft of a gas turbine system is provided. The gas turbine system includes a gas turbine engine and a turbine exhaust collector in separate enclosures. A first cooling system includes an educator that sucks exhaust gas through a diffuser and directs it out of the turbine exhaust collector enclosure based on suction pressure created from the high velocity of exhaust gas. A second cooling system include struts that enable the exhaust gas to flow from the diffusers to a ventilation flow stack. A third cooling system includes exhaust gas sucked from an opening to a top duct based on suction pressure created from the rotation of the rotary shaft disposed about a coupling. A guideway associated with the third cooling system also directs the exhaust gas to flow to the top duct.

US Patent:

20210317784, Oct 14, 2021

Filed:

Apr 8, 2020

Appl. No.:

16/843848

Inventors:

- Schenectady NY, US
Balakrishnan Ponnuraj - Sugar Land TX, US
Vineet Sethi - Sugar Land TX, US
Jose Emmanuel Guillen - Humble TX, US
Tho Vankhanh Nguyen - Cypress TX, US
Douglas Alan Jones - Bellaire TX, US
Abhinash Reddy Konatham - Sugar Land TX, US

International Classification:

F02C 7/18
F01D 25/12

Abstract:

One or more cooling systems for ventilating a turbine and rotary shaft of a gas turbine system is provided. The gas turbine system includes a gas turbine engine and a turbine exhaust collector in separate enclosures. A first cooling system includes an educator that sucks exhaust gas through a diffuser and directs it out of the turbine exhaust collector enclosure based on suction pressure created from the high velocity of exhaust gas. A second cooling system include struts that enable the exhaust gas to flow from the diffusers to a ventilation flow stack. A third cooling system includes exhaust gas sucked from an opening to a top duct based on suction pressure created from the rotation of the rotary shaft disposed about a coupling. A guideway associated with the third cooling system also directs the exhaust gas to flow to the top duct. These cooling systems are designed to increase the efficiency of ventilating the turbine and rotary shaft, prevent misalignments of the rotary shaft, which may result in thermal stresses, and allow the use of the gas turbine systems in higher ambient temperature environments.

US Patent:

20180328279, Nov 15, 2018

Filed:

Jul 23, 2018

Appl. No.:

16/043081

Inventors:

- Schenectady NY, US
Vineet Sethi - Houston TX, US
Raymond Kalok Fong - Houston TX, US
Jose Emmanuel Guillen - Houston TX, US
Robert Allen Baten - Baytown TX, US
Donald Gordon Laing - Houston TX, US

International Classification:

F02C 6/00
F16M 3/00
F02B 63/04
F16M 5/00
B62D 53/00
H02K 7/18
F02C 3/04
B60D 1/00

Abstract:

A system a first mobile body configured to support a turbine engine and an auxiliary skid communicatively and fluidly coupled to the turbine engine. The auxiliary skid includes one or more interconnects configured to support a turbine engine component. The system also includes a second mobile body configured to support a generator. The first and second mobile bodies are configured to align a removable coupling between the turbine engine and the generator.

US Patent:

20180080376, Mar 22, 2018

Filed:

Sep 21, 2016

Appl. No.:

15/272050

Inventors:

- Schenectady NY, US
Vineet Sethi - Houston TX, US
Raymond Kalok Fong - Houston TX, US
Jose Emmanuel Guillen - Houston TX, US
Robert Allen Baten - Baytown TX, US
Donald Gordon Laing - Houston TX, US

International Classification:

F02C 6/00
H02K 7/18
F02C 3/04

Abstract:

A system includes a first mobile body configured to support a turbine engine and an air intake section coupled to the turbine engine. The system also includes a second mobile body configured to support a generator. The first and second mobile bodies are configured to guide a removable coupling between the turbine engine and the generator. The system also includes a third mobile body configured to support one or more partially assembled components associated with the turbine engine and the generator.

US Patent:

20180080377, Mar 22, 2018

Filed:

Sep 21, 2016

Appl. No.:

15/272100

Inventors:

- Schenectady NY, US
Vineet Sethi - Houston TX, US
Raymond Kalok Fong - Houston TX, US
Jose Emmanuel Guillen - Houston TX, US
Robert Allen Baten - Baytown TX, US
Donald Gordon Laing - Houston TX, US

International Classification:

F02C 6/00
F02C 3/04
H02K 7/18

Abstract:

A system a first mobile body configured to support a turbine engine and an auxiliary skid communicatively and fluidly coupled to the turbine engine. The auxiliary skid includes one or more interconnects configured to support a turbine engine component. The system also includes a second mobile body configured to support a generator. The first and second mobile bodies are configured to align a removable coupling between the turbine engine and the generator.