U.S. patent number 3,791,137 [Application Number 05/253,023] was granted by the patent office on 1974-02-12 for fluidized bed powerplant with helium circuit, indirect heat exchange and compressed air bypass control.
This patent grant is currently assigned to The Secretary of State for Defense in Her Britannic Majesty's Government. Invention is credited to Albert Jubb, David Eyre Williams.
United States Patent |
3,791,137 |
Jubb , et al. |
February 12, 1974 |
FLUIDIZED BED POWERPLANT WITH HELIUM CIRCUIT, INDIRECT HEAT
EXCHANGE AND COMPRESSED AIR BYPASS CONTROL
Abstract
A power unit consists basically of two gas turbine engines. In
the first which is a closed cycle the working fluid (helium) is
heated by passing it through a duct embedded in a fluidized bed.
The exhaust gas is passed through a conventional heat exchanger
before being returned to the compressor. In the second engine,
consisting of a compressor and a turbine, air from the compressor
is passed through the particulate material of the fluidised bed
with fuel which maintains combustion in the fluidised bed. The
exhaust gas from the turbine of the second engine is passed through
a conventional heat exchanger and then to atmosphere. The two
engines each drive an alternator.
Inventors: |
Jubb; Albert (Kenilworth,
EN), Williams; David Eyre (Rugby, EN) |
Assignee: |
The Secretary of State for Defense
in Her Britannic Majesty's Government (London,
EN)
|
Family
ID: |
22958521 |
Appl.
No.: |
05/253,023 |
Filed: |
May 15, 1972 |
Current U.S.
Class: |
60/39.181;
60/39.463; 122/4D |
Current CPC
Class: |
F02C
1/10 (20130101); F02C 3/205 (20130101); F02C
1/05 (20130101) |
Current International
Class: |
F02C
1/05 (20060101); F02C 3/20 (20060101); F02C
1/10 (20060101); F02C 1/00 (20060101); F02c
001/04 (); F02c 003/00 () |
Field of
Search: |
;60/39.18A,39.18B,39.18C,39.18R,39.46 ;122/4D ;23/288S |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Croyle; Carlton R.
Assistant Examiner: Olsen; Warren
Attorney, Agent or Firm: Cushman, Darby & Cushman
Claims
We claim:
1. A gas turbine engine power plant comprising:
compressor means,
fluidised bed combustion means,
said fluidised bed combustion means being connected to receive
working fluid compressed by said compressor means in heat exchange
relationship with said fluidised bed,
turbine means,
said turbine means being connected to receive and be driven by said
working fluid heated by said fluidised bed combustion means, said
turbine means also being drivingly connected to said compressor
means,
said turbine means and said compressor means being connected to
form a closed cycle,
further compressor means,
said further compressor means being adapted to supply said
fluidised bed combustion means with compressed air to support
combustion therein,
further turbine means,
said further turbine means being connected to receive and be driven
by the combustion products of the fluidised bed combustion
means,
said further compressor means being connected to be driven by said
further turbine means,
control valve means,
said control valve means being operative to permit at least a part
of the compressed air compressed by said further compressor means
to by-pass said fluidised bed combustion means and flow to said
further turbine means,
auxiliary combustion means connected to receive and heat compressed
air from said further compressor before said fluidised bed
combustion means, and
further auxiliary combustion means connected to receive and heat
combustion products from said fluidised bed combustion means before
said further turbine.
2. A power plant as claimed in claim 1 having throttle valve means
connected between the outlet of the further compressor means and
the fluidised bed combustion means.
3. A power plant as claimed in claim 2 having further control valve
means operable to permit at least a part of the compressed air
compressed by the further compressor means to by-pass the fluidised
bed combustion bed combustion means and flow to the inlet of the
further auxiliary combustion means.
4. A power plant as claimed in claim 1 having condenser means and
pump means connected in series between the outlet of the first
mentioned turbine means and the fluidised bed combustion means.
5. A power plant as claimed in claim 1 in which the gas in the
closed cycle is helium.
6. A power plant as claimed in claim 1 having heat exchange means
connected to receive exhaust gases from the further turbine means
in heat exchange relationship with the working fluid compressed by
the further compressor means prior to its heating by the fluidised
bed combustion means.
7. A power plant as claimed in claim 6 having further heat exchange
means connected to receive exhaust gases from the further turbine
means in heat exchange relationship with the air compressed by the
first mentioned compressor means.
8. A power plant as claimed in claim 7 having a recuperator
connected to receive the working fluid compressed by the further
compressor means prior to its heating by the fluidised bed
combustion means, the recuperator being connected between the
compressor means and the first mentioned heat exchange means.
9. A power plant as claimed in claim 7 in which the heat exchange
means and the further heat exchange means are connected in flow
series.
10. A power plant as claimed in claim 7 in which the heat exchange
means and the further heat exchange means are connected in
parallel.
Description
This invention relates to power plants, and is particularly but not
exclusively concerned with a closed cycle gas turbine engine power
plant.
According to the present invention, a power plant comprises
fluidised bed combustion means connected to receive a working fluid
in heat exchange relationship with the fluidised bed, turbine means
connected to receive and be driven by the working fluid heated by
the fluidised bed combustion means, compressor means connected to
supply compressed air to the fluidised bed combustion means to
support the combustion therein, further turbine means which is
connected to receive and be driven by the combustion products from
the fluidised bed combustion means and which is drivingly connected
to the compressor means, and control valve means operative to
permit at least a part of the compressed air compressed by the
compressor means to by-pass the fluidised bed combustion means and
flow to the inlet of the further turbine means.
There may be provided throttle valve means connected between the
outlet of the compressor means and the fluidised bed combustion
means so as to control the quantity of compressed air supplied to
the latter.
In a preferred embodiment of the invention, the power plant
additionally comprises auxiliary combustion means connected between
the throttle valve means and the fluidised bed combustion means so
as to heat the compressed air supplied to the latter prior to its
entry therein.
There may also be provided further auxiliary combustion means
adapted to heat the combustion products from the fluidised bed
combustion means prior to their entry into the further turbine
means.
The power plant may also comprise further control valve means
operative to permit at least a part of the compressed air
compressed by the compressor means to by-pass the fluidised bed
combustion means and flow to the inlet of the further auxiliary
combustion means.
The fluidised bed combustion means and the firstmentioned turbine
means may be arranged to form a closed cycle for the working fluid
thereof.
Thus there may be provided condenser means and pump means connected
in series between the outlet of the firstmentioned turbine means
and the fluidised bed combustion means so as to form a closed steam
cycle.
Alternatively, there may be provided further compressor means
connected in series between the outlet of the firstmentioned
turbine means and the fluidised bed combustion means so as to form
a closed cycle gas, e.g. helium, cycle.
Preferably there is provided heat exchange means connected to
receive exhaust gases from the further turbine means in heat
exchange relationship with the working fluid compressed by the
further compressor means prior to its heating by the fluidised bed
combustion means: additionally or alternatively there may be
provided further heat exchange means connected to receive exhaust
gases from the further turbine means in heat exchange relationship
with the air compressed by the firstmentioned compressor means.
The heat exchange means and the further feat exchange means may be
connected in flow series or in parallel.
There may also be provided a recuperator connected to receive the
working fluid expanded in the firstmentioned turbine means in heat
exchange relationship with the working fluid compressed by the
further compressor means prior to its heating by the fluidised bed
combustion means, the recuperator preferably being connected
between the compressor means and the firstmentioned heat exchange
means.
The invention will now be described, merely by way of example, with
reference to the accompanying drawing, which is a schematic block
diagram of a gas turbine engine power plant in accordance with the
invention.
The gas turbine engine power plant shown in the drawing comprises,
in flow series, a low pressure compressor 10, a high pressure
compressor 12, a fluidised bed combustion apparatus 14, a
compressor-driving turbine 16 drivingly connected to the
compressors 10 and 12 by a shaft 18 and a free power turbine 20
which is drivingly connected to an alternator 22, the compressors
10, 12, the combustion apparatus 14 and the turbine 16, 20 being
connected to form a closed cycle flow path for the working fluid of
the power plant. The working fluid is preferably helium.
A precooler 24 is provided in flow series with the inlet of the
compressor 10 while an intercooler 26 is provided between, and in
flow series with, the compressors 10 and 12, the helium being
passed in heat exchange relationship with cooling water in the
coolers 24, 26. A recuperator 28 having two flow paths 30, 32 in
heat exchange relationship is arranged so that the path 30 is
connected in flow series between the outlet of the compressor 12
and the inlet of the fluidised bed combustion apparatus 14, and the
path 32 is connected in flow series between the outlet of the
turbine 20 and the inlet of the precooler 24.
The fluidised bed combustion apparatus 14 comprises a chamber 34
containing a particulate material 36 constituted by a particulate
fuel such as granular coal or coke (about 1/8 inch diameter),
although non-combustible particular material such as sand, soaked
in or supplied with a light fuel such as kerosene or a gaseous fuel
such as methane, may be used. The chamber 34 has an inlet 37
through which air compressed by a compressor 38 to a pressure of
about six atmospheres enters the chamber and flows upwards through
the particulate fuel 36. The particulate fuel 36 is thus fluidised,
and burns continuously. The ash rises to the top, and is removed
continuously by means not shown, while additional particulate fuel
is continuously supplied by means not shown. Embedded in the
particulate fuel 36 are a number of conduits (indicated
diagrammatically at 39) through which the helium flows to be
heated.
The combustion products resulting from the combustion of the
particulate fuel 36 pass from the chamber 34 into a turbine 40
which is drivingly connected to the compressor 38 and to a further
alternator 42. After being expanded in the turbine 40, the
combustion products pass to atmosphere through a first flow path 44
of a heat exchanger 46 having a second flow path 48 connected, for
the flow of helium, in series between the flow path 30 of the
recuperator 28 and the inlet to the conduits 39 of the fluidised
bed combustion apparatus 14. The considerable waste heat in the
exhaust from the turbine 40 is thus injected into the closed helium
cycle.
It will be appreciated that the flow path 48 may be arranged
upstream of the flow path 30. Additionally, or alternatively, there
may be provided a further heat exchanger (shown dotted at 50)
having a first flow path 52 connected to receive the combustion
products from the turbine 40 in heat exchange relationship with a
second flow path 54 connected between the outlet of the compressor
38 and the inlet 37 of the chamber 34. The flow path 52 may be
connected in series or in parallel with the flow path 44.
A throttle valve 56 and auxiliary combustion equipment 58 which is
adapted to be supplied with liquid or gaseous fuel are connected in
flow series between the outlet of the compressor 38 and the inlet
37 of the fluidised bed combustion apparatus 14, the throttle valve
56 being upstream of, and the combustion equipment 58 being
downstream of, the flow path 54 if the flow path 54 is present.
Further auxiliary combustion equipment 62 and a mixing chamber 64
are connected in flow series between the outlet of the chamber 34
of the fluidised bed combustion apparatus 14 and the inlet of the
turbine 40, while a by-pass conduit 66 containing a by-pass control
valve 68 is connected between the outlet of the compressor 38 and
the mixing chamber 64. A further conduit 69 containing a shut-off
valve 70 communicates between the outlet of the compressor 38 and
the inlet of the combustion equipment 62.
The combustion equipment 58, 62 are preferably such that the gas
passing therethrough (i.e. the compressed air or combustion
products respectively) is indirectly heated, for example by passing
through ducts in the combustion equipment 58, 62 which ducts are
heated by the combustion of the fuel in the combustion equipment
58, 62.
When the power plant is to be started, the particulate fuel 36 in
the fluidised bed combustion apparatus 14 is cold. The valve 56 is
set fully open, the valves 68 and 70 are closed, and fuel is
supplied to and burnt in the combustion equipment 58. Hot
fluidising gas is thus supplied to the fluidised bed combustion
apparatus 14, which hot gas rapidly heats the particulate fuel 36
to a temperature at which self-sustaining combustion can commence.
At this point the supply of fuel to the combustion equipment 58 can
be gradually reduced to zero. Before self-sustaining combustion of
the particulate fuel 36 has commenced the temperature of the
combustion products leaving the chamber 34 may be too low for
satisfactorily driving the turbine 40. In this case, fuel may
additionally be supplied to and burnt in the combustion equipment
62.
An alternative method of starting the power plant comprises
adjusting the valves 56 and 68 so that only about 20 percent of the
air compressed by the compressor 38 is supplied to the fluidised
bed combustion apparatus 14. Fuel is supplied to the combustion
equipment 58 and 62, and the very hot combustion products leaving
the combustion equipment 62 are diluted and cooled in the mixing
chamber 64 by air passing through the valve 68 to a temperature
suitable for driving the turbine 40.
During the normal running of the power plant, no fuel is supplied
to the combustion equipment 56 or 62, the valve 56 is fully open
and the valves 68 and 70 are closed. Should there be a sudden
decrease in the load, by-pass valve 68 is rapidly opened while the
throttle valve 56 is closed, thus rapidly reducing the temperature
at the inlet of the turbine 40 and within the particulate fuel 36
of the fluidised bed combustion apparatus 14. Fine control of the
overall power output of the power plant is exercised by adjusting
the valve 68 alone or by simultaneously adjusting the valves 56 and
68 in opposite senses.
If it is desired to service or repair the main power producing part
of the power plant, i.e. the compressors 10, 12 and their
associated equipment, the turbines 16, 20, the alternator 22 and
the fluidised bed combustion apparatus 14, the power plant can
still be used to produce at least some power by closing the valves
56 and 68, opening the valve 70 and supplying fuel to the
combustion equipment 62. The compressor 38, combustion equipment 62
and turbine 40 then act as an independently operable gas turbine
engine to drive the alternator 42.
It will be appreciated that the invention is applicable to power
plants other than gas turbine engine power plants. For example, the
closed helium cycle part of the power plant could be replaced by a
closed steam cycle. In this case the compressors 10, 12 and their
associated equipment would be replaced by a condenser and a water
pump, the turbines 16, 20 would be replaced by a steam turbine or
turbines, and the fluidised bed combustion apparatus 14 would act
as a boiler for the water supplied to the conduits 39.
* * * * *