Injection systems for fuel and gas

Patent metadata

Field	Value
Publication number	US-10107498-B2
Application number	US-201414567753-A
Country	US
Kind code	B2
Filing date	Dec 11, 2014
Priority date	Dec 11, 2014
Publication date	Oct 23, 2018
Grant date	Oct 23, 2018

Abstract

Embodiments of the present disclosure provide injection systems for fuel and air. According to one embodiment, an injection system can include a mixing zone embedded within a surface of a turbine nozzle and positioned between a first outlet and a second outlet, the turbine nozzle separating a combustor of a power generation system from a turbine stage of the power generation system, wherein the first outlet is oriented substantially in opposition to the second outlet; a first injection conduit for delivering a carrier gas to the mixing zone through the first outlet; and a second injection conduit for delivering a fuel to the mixing zone through a second outlet; wherein the carrier gas and the fuel intermix within the mixing zone upon leaving the first injection conduit and the second injection conduit.

First claim

What is claimed is:

1. An injection system comprising:
a combustor of a power generation system having a reaction chamber, wherein the reaction chamber includes a reaction section and an aft section;
a turbine nozzle positioned downstream of the combustor of the power generation system, such that the aft section of the reaction chamber is interposed directly between the reaction section of the reaction chamber and the turbine nozzle, wherein the turbine nozzle separates the reaction chamber from a turbine blade stage of the power generation system;
an injector assembly within the turbine nozzle, downstream of a high pressure turbine, and upstream of a low pressure turbine of the power generation system, wherein the injector assembly includes:
a mixing chamber beneath a pressure side surface or a suction side surface of the turbine nozzle, wherein the mixing chamber includes a discharge outlet through the pressure side surface or the suction side surface of the turbine nozzle;
a first injection conduit for delivering a carrier gas to the mixing chamber through a first outlet; and
a second injection conduit for delivering a fuel to the mixing chamber through a second outlet;

wherein a diameter of the discharge outlet is less than a diameter of the mixing chamber, and wherein the first outlet is oriented substantially in opposition to the second outlet,
and wherein the carrier gas and the fuel intermix within the mixing chamber upon leaving the first injection conduit and the second injection conduit, and wherein the mixing chamber is in fluid communication with a flow of a post-combustion fluid within the aft section of the reaction chamber.

2. The injection system of claim 1 , wherein the mixing chamber is embedded within a dimple of the pressure side surface or suction side surface of the turbine nozzle.

3. The injection system of claim 1 , wherein a contour of the discharge outlet prevents fluid communication of a combusted gas outside of the turbine nozzle into the mixing chamber.

4. The injection system of claim 1 , wherein the combustor comprises a reheat combustor of the power generation system, and the pressure side surface or suction side surface of the turbine nozzle is exposed to a flow of fluid through the reheat combustor, wherein the power generation system comprises a gas turbine system.

5. The injection system of claim 1 , wherein at least one of the first injection conduit and the second injection conduit is composed of a thermally conductive material, such that the carrier gas of the first injection conduit or the fuel of the second injection conduit absorbs heat from the pressure side surface or suction side surface of the turbine nozzle.

6. An injection system comprising:
a combustor of a power generation system having a reaction chamber, wherein the reaction chamber includes a reaction section and an aft section;
a turbine nozzle positioned downstream of the combustor of the power generation system, such that the aft section of the reaction chamber is interposed directly between the reaction section of the reaction chamber and the turbine nozzle, wherein the turbine nozzle separates the reaction chamber from a turbine blade stage of the power generation system;
an injector assembly within the turbine nozzle, downstream of a high pressure turbine and upstream of a low pressure turbine of the power generation system, wherein the injector assembly includes:
a mixing chamber including a housing positioned outside a pressure side surface or a suction side surface of the turbine nozzle, wherein the mixing chamber includes a discharge outlet through the housing outside the pressure side surface or the suction side surface of the turbine nozzle;
a first injection conduit for delivering a carrier gas to the mixing chamber through a first outlet;
at least one second injection conduit for delivering a fuel to the mixing chamber through at least one second outlet; and

wherein a diameter of the discharge outlet is less than a diameter of the mixing chamber, and wherein the first injection conduit and the at least one second injection conduit are in fluid communication with a flow of a post-combustion fluid within the aft section of the reaction chamber upstream of the turbine blade stage.

7. The injection system of claim 6 , wherein the first injection conduit is composed of a thermally conductive material, such that the carrier gas of the first injection conduit or the fuel of the at least one second injection conduit absorbs heat from the pressure side surface or suction side surface of the turbine nozzle through the thermally conductive material.

8. An injection system comprising:
a reheat combustor of a power generation system having a reaction chamber, wherein the reaction chamber includes a reaction section and an aft section;
a turbine nozzle positioned downstream of the reheat combustor, such that the aft section of the reaction chamber is interposed directly between the reaction section of the reaction chamber and the turbine nozzle, wherein the turbine nozzle separates the reaction chamber from a turbine blade stage of the power generation system; and
an injector assembly within the turbine nozzle, downstream of a high pressure turbine, and upstream of a low pressure turbine of the power generation system, wherein the injector assembly includes:
a mixing chamber beneath a pressure side surface of a suction side surface of the turbine nozzle, wherein the mixing chamber includes a discharge outlet through the pressure side surface or the suction side surface of the turbine nozzle;
a first injection conduit for delivering a carrier gas to the mixing chamber through a first outlet; and
a second injection conduit for delivering a fuel to the mixing chamber through a second outlet, the second outlet being oriented substantially in opposition to the first outlet;

wherein a diameter of the discharge outlet is less than a diameter of the mixing chamber, the mixing chamber is positioned between the first outlet and the second outlet, upstream of the turbine blade stage, and wherein the carrier gas and the fuel intermix within the mixing chamber upon exiting the first outlet and the second outlet, and wherein the mixing chamber is in fluid communication with a post-combustion fluid within the aft section of the reaction chamber.

9. An injection system comprising:
a reheat combustor of a power generation system having a reaction chamber, wherein the reaction chamber includes a reaction section and an aft section; and
a turbine nozzle positioned downstream of the reheat combustor, such that the aft section of the reaction chamber is interposed directly between the reaction section of the reaction chamber and the turbine nozzle, wherein the turbine nozzle separates the reaction chamber from a turbine blade stage of the power generation system; and
an injector assembly within the turbine nozzle, downstream of a high pressure turbine and upstream of a low pressure turbine of the power generation system, wherein the injector assembly includes:
a mixing chamber including a housing positioned outside a pressure side surface or a suction side surface of the turbine nozzle, wherein the mixing chamber includes a discharge outlet through the housing outside the pressure side surface or the suction side surface of the turbine nozzle;
a first injection conduit for delivering a carrier gas to the mixing chamber through a first outlet disposed on the pressure side surface or the suction side surface of the turbine nozzle,
at least one second injection conduit for delivering a fuel to the mixing chamber through at least one second outlet the at least one second outlet being disposed on the pressure side surface or the suction

Assignees

• Gen Electric

Inventors

• Widener Stanley Kevin
• Davis Jr Lewis Berkley
• Foster Gregory Thomas
• Graham Kaitlin Marie
• Venkataraman Krishnakumar

Classifications

• F23R3/34

  Feeding into different combustion zones · CPC title

• F23R3/286 Primary

  having fuel-air premixing devices (F23R3/30 takes precedence) · CPC title

• F02C7/222

  Fuel flow conduits, e.g. manifolds · CPC title

• F01D9/06

  Fluid supply conduits to nozzles or the like · CPC title

• F23R2900/03341

  Sequential combustion chambers or burners · CPC title