Shaft actuated swirling combustion system

Patent metadata

Field	Value
Publication number	US-10815883-B2
Application number	US-201916547779-A
Country	US
Kind code	B2
Filing date	Aug 22, 2019
Priority date	Feb 22, 2016
Publication date	Oct 27, 2020
Grant date	Oct 27, 2020

Abstract

A combustor having an ion transport membrane therein and an adjustable swirler, which is mechanically connected at an inlet of a combustion zone of the combustor; a combustion system comprising the combustor, a feedback control system adapted to adjust swirler blades of the combustor based on a compositional variation of a fuel stream, and a plurality of feedback control systems to control operational variables within the combustor for an efficient oxy-combustion; and a process for combusting a fuel stream via the combustion system. Various embodiments of the combustor, the combustion system, and the process for combusting the fuel stream are disclosed.

First claim

The invention claimed is:

1. A shaft actuated swirling combustion system, comprising:
a combustor comprising
a cylindrical vessel with an internal cavity,
an ion transport membrane that divides the internal cavity of said cylindrical vessel into a first and a second concentric cylindrical zone, wherein the first concentric cylindrical zone is a feed zone and the second concentric cylindrical zone is a combustion zone,
a first inlet and a first outlet located in the feed zone, and a second inlet and a second outlet located in the combustion zone, and
a swirler that is connected to the second inlet, wherein the swirler has a plurality of adjustable blades with adjustable angles, a shaft, an outer casing and an actuator that rotates the blades and is secured inside the shaft;

an oxygen supplier located upstream of and fluidly connected to the first inlet via a feed line for supplying an oxygen-containing stream;
a fuel supplier located upstream of and fluidly connected to the second inlet via a fuel line for supplying a fuel stream;
an expander located downstream of and fluidly connected to the second outlet via an exhaust line for expanding an exhaust stream to generate power;
a recycle line that fluidly connects the exhaust line to the fuel line;
a mixer located upstream of the combustor and fluidly connected to the fuel line and the recycle line configured to mix the fuel stream with the exhaust stream;
an oxygen-depleted line fluidly connected to the first outlet; and
a primary heat exchanger disposed on the recycle line and fluidly connected to the oxygen-depleted line, wherein the primary heat exchanger is located downstream of the first outlet and upstream of the mixer, and is configured to heat exchange the exhaust stream with an oxygen-depleted stream that egresses the first outlet to raise a temperature of the exhaust stream.

2. The combustion system of claim 1 , further comprising:
a swirler control unit comprising
a first gas analyzer disposed on the fuel line configured to determine a composition of the fuel stream,
a second gas analyzer disposed on the exhaust line configured to determine a composition of the exhaust stream, and
a processor that is configured to receive a first signal from the first gas analyzer and a second signal from the second gas analyzer, and to transmit a first output signal to the actuator,

wherein the swirler control unit is configured to adjust an angle of the adjustable blades based on the composition of the fuel stream and the exhaust stream.

3. The combustion system of claim 2 , further comprising:
a flow control unit comprising
the first gas analyzer disposed on the fuel line configured to determine the composition of the fuel stream,
a flowmeter disposed on the fuel line configured to determine a volumetric flow rate of the fuel stream,
a first control valve disposed on the feed line configured to control a volumetric flow rate of the oxygen-containing stream,
a flow controller that is configured to receive the first signal from the first gas analyzer and a flow rate signal from the flowmeter, and to transmit a second output signal to the first control valve,

wherein the flow control unit is configured to control the volumetric flow rate of the oxygen-containing stream based on a composition and volumetric flow rate of the fuel stream.

4. The combustion system of claim 3 , further comprising:
a temperature control unit comprising
a temperature sensor disposed on the exhaust line configured to determine the temperature of the exhaust stream,
a second control valve disposed on the recycle line configured to control a volumetric flow rate of the exhaust stream,
a temperature controller configured to receive a temperature signal from the temperature sensor, and to transmit a third output signal to the second control valve,

wherein the temperature control unit is configured to control a temperature of the fuel stream based on the temperature of the exhaust stream.

5. The combustion system of claim 1 , further comprising:
a secondary heat exchanger disposed on the feed line and fluidly connected to the oxygen-depleted line, wherein the secondary heat exchanger is located upstream of the first inlet and downstream of the first outlet, and is configured to heat exchange the oxygen-containing stream with the oxygen-depleted stream that egresses the first outlet.

6. The combustion system of claim 1 , further comprising:
a condenser located downstream of and fluidly connected to the expander via the exhaust line configured to separate a liquid phase from the exhaust stream.

7. The combustion system of claim 1 , wherein the combustor further comprises:
a third concentric cylindrical zone sandwiched between the first and the second concentric cylindrical zones, defining a sweep zone; and
a third inlet and a third outlet located in the sweep zone.

8. The combustion system of claim 7 , wherein the recycle line fluidly connects the exhaust line to the third inlet.

Assignees

• Univ King Fahd Pet & Minerals

Inventors

• Mokheimer Esmail M A
• Sanusi Yinka S

Classifications

• F23C7/002

  the air being submitted to a rotary or spinning motion (cyclonic combustion chamber F23C3/006) · CPC title

• F23N5/003

  using detectors sensitive to combustion gas properties (F23N5/02, F23N5/18 - F23N5/26 take precedence) · CPC title

• F02C7/224

  Heating fuel before feeding to the burner · CPC title

• F23R3/14

  by using swirl vanes · CPC title

• F02C3/22 Primary

  the fuel or oxidant being gaseous at standard temperature and pressure (F02C3/28 takes precedence) · CPC title