Turbine component cooling system

US9879600B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9879600-B2
Application numberUS-201213460001-A
CountryUS
Kind codeB2
Filing dateApr 30, 2012
Priority dateApr 30, 2012
Publication dateJan 30, 2018
Grant dateJan 30, 2018

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

Systems for cooling turbine components via fluid filled conduits are disclosed. Various embodiments include a system having: a set of fan systems for cooling a set of conduits, the set of conduits fluidly connected with a turbine component; a temperature sensor operably connected to the turbine component, the temperature sensor for obtaining a temperature indicator of the turbine component; and a control system operably connected to the set of fan systems and the temperature sensor, the control system for modifying a speed of at least one fan system in the set of fan systems across a range of speeds in response to determining the temperature indicator deviates from a predetermined range of temperature values.

First claim

Opening claim text (preview).

We claim: 1. A system comprising: a gas turbine system including a gas turbine and at least one gas turbine component; a set of conduits configured to provide a cooling fluid to the at least one gas turbine component, the cooling fluid cooling the at least one gas turbine component; a set of fan systems for cooling the set of conduits, the set of conduits fluidly connected with the at least one gas turbine component wherein each fan system includes: a fan; a fan motor operably connected with the fan; and a variable frequency drive for modifying an operating speed of the fan motor; a temperature sensor operably connected to the at least one gas turbine component, the temperature sensor for obtaining a temperature indicator of the at least one gas turbine component; and a control system operably connected to the set of fan systems and the temperature sensor, the control system for modifying a speed of at least one fan system in the set of fan systems across a range of speeds by providing instructions to the variable frequency drive to: increase the operating speed of the fan motor in response to determining the temperature indicator exceeds an upper limit of the predetermined range; and decrease the operating speed of the fan motor in response to determining the temperature indicator is below a lower limit of the predetermined range. 2. The system of claim 1 , wherein at least two fan systems in the set of fan systems are arranged in parallel. 3. The system of claim 1 , wherein the set of fan systems includes two distinct groups of serially connected fans, the two distinct groups being arranged in parallel. 4. The system of claim 1 , wherein each conduit in the set of conduits includes a heat exchange element. 5. The system of claim 1 , wherein the control system is configured to perform the following: set a speed of the set of fan systems to a first speed in the range of speeds; and reduce the speed of a fan system in the set of fan systems to a second speed below the first speed in response to determining the temperature indicator is below the predetermined range of temperature values. 6. The system of claim 5 , wherein the control system is further configured to reduce the speed of an additional fan system in the set of fan systems in response to determining a subsequent temperature indicator is below the predetermined range of temperature values. 7. The system of claim 1 , wherein the control system is configured to perform the following: set a speed of a first fan system in the set of fan systems to a first speed in the range of speeds; and set a speed of a second fan system in the set of fan systems to a second speed less than the first speed in response to determining the temperature indicator deviates from the predetermined range of temperature values. 8. A system comprising: a gas turbine system including a gas turbine and at least one gas turbine component; a cooling fluid provided to the at least one gas turbine component, the cooling fluid cooling the at least one gas turbine component; a control system operably connected to a set of fan systems configured to cool the cooling fluid, wherein each fan system in the set of fan systems includes: a fan; a fan motor operably connected with the fan; and a variable frequency drive for modifying an operating speed of the fan motor, the control system configured to: modify a speed of at least one fan system in the set of fan systems across a range of speeds by providing instructions to the variable frequency drive to: increase the operating speed of the fan motor in response to determining a temperature of the cooling fluid exceeds an upper limit of the predetermined range, and to decrease the operating speed of the fan motor in response to determining the temperature of the cooling fluid is below a lower limit of the predetermined range. 9. The system of claim 8 , wherein at least two fan systems in the set of fan systems are arranged in parallel. 10. The system of claim 8 , wherein the set of fan systems includes two distinct groups of serially connected fans, the two distinct groups being arranged in parallel. 11. The system of claim 8 , wherein the control system is further configured to perform the following: set a speed of the set of fan systems to first speed in the range of speeds; and reduce the speed of a fan system in the set of fan systems to a second speed less than the first speed in response to determining the temperature is below the predetermined range of temperature values. 12. The system of claim 11 , wherein the control system is further configured to reduce the speed of an additional fan system in the set of fan systems in response to determining a subsequent temperature indicator is below the predetermined range of temperature values. 13. A system comprising: a gas turbine system including a gas turbine and at least one gas turbine component; a set of conduits containing a cooling fluid, the set of conduits fluidly connected to the at least one gas turbine component, the cooling fluid cooling the at least one gas turbine component; at least one computing device configured to control a set of fan systems wherein the set of fan systems is configured to cool the cooling fluid, wherein each fan system in the set of fan systems includes: a fan; a fan motor operably connected with the fan; and a variable frequency drive for modifying an operating speed of the fan motor, by performing the following: determining a temperature of the cooling fluid; and modifying a speed of at least one fan system in the set of fan systems across a range of speeds in response to determining the temperature of the cooling fluid deviates from a predetermined range of temperature values. 14. The system of claim 13 , wherein the at least one computing device is further configured to perform the following: set a speed of the set of fan systems to first speed in the range of speeds; and reduce the speed of a fan system in the set of fan systems to a second speed less than the first speed in response to determining the temperature is below the predetermined range of temperature values. 15. The system of claim 14 , wherein the at least one computing device is further configured to reduce the speed of an additional fan system in the set of fan systems in response to determining a subsequent temperature indicator is below the predetermined range of temperature values.

Assignees

Inventors

Classifications

  • Temperature · CPC title

  • F02C7/12Primary

    Cooling of plants (of component parts, see the relevant subclasses, e.g. F01D; cooling of engines in general F01P) · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US9879600B2 cover?
Systems for cooling turbine components via fluid filled conduits are disclosed. Various embodiments include a system having: a set of fan systems for cooling a set of conduits, the set of conduits fluidly connected with a turbine component; a temperature sensor operably connected to the turbine component, the temperature sensor for obtaining a temperature indicator of the turbine component; and…
Who is the assignee on this patent?
Stovall Steven David, Gilchrist Iii George Martin, Hains John Victor, and 1 more
What technology area does this patent fall under?
Primary CPC classification F02C7/12. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jan 30 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).