Language selection

Search

Patent 2498538 Summary

Third-party information liability

Some of the information on this Web page has been provided by external sources. The Government of Canada is not responsible for the accuracy, reliability or currency of the information supplied by external sources. Users wishing to rely upon this information should consult directly with the source of the information. Content provided by external sources is not subject to official languages, privacy and accessibility requirements.

Claims and Abstract availability

Any discrepancies in the text and image of the Claims and Abstract are due to differing posting times. Text of the Claims and Abstract are posted:

  • At the time the application is open to public inspection;
  • At the time of issue of the patent (grant).
(12) Patent: (11) CA 2498538
(54) English Title: VARIABLE FIRING RATE FUEL BURNER
(54) French Title: BRULEUR DE COMBUSTIBLE A REGLAGE VARIABLE
Status: Deemed expired
Bibliographic Data
(51) International Patent Classification (IPC):
  • F23D 14/02 (2006.01)
  • F28D 7/00 (2006.01)
(72) Inventors :
  • HALLIT, RAYMOND I. (United States of America)
(73) Owners :
  • RHEEM MANUFACTURING COMPANY (United States of America)
(71) Applicants :
  • RHEEM MANUFACTURING COMPANY (United States of America)
(74) Agent: BLAKE, CASSELS & GRAYDON LLP
(74) Associate agent:
(45) Issued: 2008-08-19
(22) Filed Date: 2001-10-11
(41) Open to Public Inspection: 2002-08-22
Examination requested: 2005-03-21
Availability of licence: N/A
(25) Language of filing: English

Patent Cooperation Treaty (PCT): No

(30) Application Priority Data:
Application No. Country/Territory Date
09/791,113 United States of America 2001-02-22

Abstracts

English Abstract



A variable firing rate fuel burner has a tubular body configuration defined by
a
central pilot tube coaxially circumscribed by intermediate and outer firing
tubes. A
pilot fuel-air mixture is flowed through the pilot tube and ignited to
maintain a pilot
flame at the open outlet end of the burner body. During firing of the burner,
separate fuel-air mixtures are flowed through an intermediate annulus between
the
intermediate firing tube and the pilot tube, and an outer annulus between the
intermediate firing tube and the outer firing tube. As these fuel-air mixtures
exit the
burner body they are ignited by the pilot flame, with the fuel-air mixture
exiting the
outer annulus serving as a flame shaping mechanism to provide the overall
burner
flame with a controlled, elongated shape. By using two separate fuel-air
mixture
flows surrounding the pilot fuel-air mixture flow, the firing rate of the
burner may be
easily modulated, and the burner may be simultaneously operated with two
different
types of fuel.


Claims

Note: Claims are shown in the official language in which they were submitted.





WHAT IS CLAIMED IS:


1. A variable firing rate fuel burner comprising:
a body having an outlet end and including:
a pilot tube extending along an axis and through which, during operation
of said burner, a pilot fuel/air mixture is flowed, discharged and ignited to
create a
central pilot flame extending laterally outwardly from said axis,
an inner firing tube coaxially circumscribing said pilot tube and laterally
defining therebetween a first annular flow space communicating with said
outlet end,
an outer firing tube coaxially circumscribing said inner firing tube and
laterally defining therebetween a second annular flow space communicating with
said
outlet end; and
a fuel/air mixture inlet plenum portion having an interior and being operative

to receive a fuel/air mixture during operation of said burner and discharge
the
received fuel/air mixture only into said first annular flow space, and

a fuel/air delivery system operative to force separate pre-mixed first and
second flows of fuel and air, formed externally of said inner and outer firing
tubes,
respectively through said first and second annular flow spaces, for ignition
by the
central pilot flame and discharge through said outlet end, to responsively
create a
main burner flame surrounding and extending axially past the central pilot
flame, said
fuel/air delivery system including:
an air inlet plenum structure having an interior and being externally
carried by said body,
a supply air fan having an outlet communicated with the interior of said
air inlet plenum structure,
separate first and second perforated mixing plenum structures disposed
within said air inlet plenum structure for receiving air forced into said air
inlet
plenum structure by said supply air fan, said separate first and second
perforated
mixing plenum structures having interiors respectively communicated with the



-8-



interior of said fuel/air mixture inlet plenum portion of said body and said
second
annular flow space, and
first and second fuel injectors respectively communicated with the
interiors of said separate first and second perforated mixing plenum
structures.


2. The variable firing rate fuel burner of Claim 1 wherein:
said fuel/air delivery system is operative to utilize different fuels in said
separate first and second fuel/air mixtures.


3. The variable firing rate fuel burner of Claim 1 wherein:
said inner and outer firing tubes have downstream ends, and
the downstream end of said outer firing tube is axially offset from the
downstream end of said inner firing tube in a downstream direction.


4. The variable firing rate fuel burner of Claim 1 wherein said body is
configured
in a manner such that said second fuel/air mixture, when discharged from said
second
annular flow space, functions to laterally constrain the main burner flame.


5. The variable firing rate fuel burner of Claim 4 wherein said second
fuel/air
mixture, when discharged from said second annular flow spaced, functions to
provide
the main burner flame with an axially elongated shape.


6. The variable firing rate fuel burner of claim 1 wherein:
the second fuel/air mixture is discharged from said second annular flow space
in a substantially non-swirling pattern.


7. Fuel-fired heat exchange apparatus comprising:
a heat exchanger through which, during operation of said fuel-fired heat
exchange apparatus, a fluid to be heated is flowed, said heat exchanger having
an
interior space for receiving a fuel burner flame from which combustion heat is

transferred to the fluid being flowed through said heat exchanger; and
a variable firing rate fuel burner including:
a body having an outlet end and including:



-9-




a pilot tube extending along an axis and through which, during
operation of said burner, a pilot fuel/air mixture is flowed, discharged
and ignited to create a central pilot flame extending laterally outwardly
from said axis,
an inner firing tube coaxially circumscribing said pilot tube and
laterally defining therebetween a first annular flow space
communication with said outlet end,
an outer firing tube coaxially circumscribing said inner firing tube
and laterally defining therebetween a second annular flow space
communication with said outer end, and
a fuel/air mixture inlet plenum portion having an interior and
being operative to receive a fuel/air mixture during operation of said
burner and discharge the received fuel/air mixture only into said first
annular flow space, and
a fuel/air delivery system operative to force separate pre-mixed
first and second flows of fuel and air, formed externally of said inner
and outer firing tubes, respectively through said first and second annular
flow spaces, for ignition by the central pilot flame and discharge through
said outlet end, to responsively create a main burner flame surrounding
and extending axially past the central pilot flame, said fuel/air delivery
system including:
an air inlet plenum structure having an interior and being
externally carried by said body,
a supply air fan having an outlet communicated with the
interior of said air inlet plenum structure,
separate first and second perforated mixing plenum
structures disposed within said air inlet plenum structure for receiving
air forced into said air inlet plenum structure by said supply air fan, said
separate first and second perforated mixing plenum structures having
interiors respectively communicated with the interior of said fuel/air



-10-




mixture inlet plenum portion of said body and said second annular flow
space, and
first and second fuel injectors respectively communicated
with the interiors of said separate first and second perforated mixing
plenum structures.


8. The fuel-fired heat exchange apparatus of Claim 7 wherein:
said fuel/air delivery system is operative to utilize different fuels in said
separate first and second fuel/air mixtures.


9. The fuel-fired heat exchange apparatus of Claim 7 wherein:
said inner and outer firing tubes have downstream ends, and
the downstream end of said outer firing tube is axially offset from the
downstream end of said inner firing tube in a downstream direction.


10. The fuel-fired heat exchange apparatus of Claim 7 wherein said body is
configured in a manner such that said second fuel/air mixture, when discharged
from
said second annular flow space, functions to laterally constrain the main
burner
flame.


11. The fuel-fired heat exchange apparatus of Claim 10 wherein said second
fuel/air mixture, when discharged from said second annular flow spaced,
functions to
provide the main burner flame with an axially elongated shape.


12. The fuel-fired heat exchange apparatus of Claim 11 wherein:
said heat exchanger has a series of interior heating tubes through which the
fluid to be heated may be flowed, said series of interior heating tubes
circumscribing
said interior space and longitudinally extending parallel to said axis.



-11-




13. The fuel-fired heat exchange apparatus of claim 7 wherein:
the second fuel/air mixture is discharged from said second annular flow space
in a substantially non-swirling pattern.



-12-

Description

Note: Descriptions are shown in the official language in which they were submitted.



CA 02498538 2001-10-11
Docket No.: RPAK-0004DIV 1 CN

VARIABLE FIRING RATE FUEL BURNER
BACKGROUND OF THE INVENTION

The present invention generally relates to combustion apparatus and, in a
preferred embodiment thereof, more particularly relates to a specially
designed
variable firing rate fuel burner.

Fuel burners are utilized in a variety of heating applications in which the
burner operates to transfer combustion heat to a heat exchanger to thereby
heat a
1o fluid being flowed through the heat exchanger during firing of the burner.
In some of
these heating applications it is desirable that the pattern of the flame
emanating
from the outlet of the burner be considerably elongated parallel to the axis
of the
burner to suit the interior geometry of the heat exchanger and/or to satisfy
certain
heat transfer efficiency desigri parameters.

One previously proposed technique used to provide the burner flame with the
requisite elongated shape was to coaxially attach to the outlet end of the
burner a
tubular ceramic flame shaper that axially projected a considerable distance
beyond
the outlet end of the burner body. While this technique provided the burner
flame
with the desired elongated shape, it had certain problems, limitations and
disadvantages such as being fragile, relatively expensive, and undesirably
increasing
the overall length of the burner body.

In burner-fired heat exchanger applications of this general type it is often
desirable to vary the firing rate of the burner. However, in conventional fuel
burner
design it is often difficult to substantially reduce the firing rate of the
burner without
potentially creating undesirable flame "flashback".


CA 02498538 2001-10-11

In view of the foregoing it can be seen that a need exists for an improved
fuel
burner which eliminates or at least substantially reduces the above-mentioned
problems, limitations and disadvantages commonly associated with fuel burners
of
conventional constructions. It is to this need that the present invention is
directed.

SUMMARY OF THE INVENTION

In carrying out principles of the present invention, in accordance with a
preferred embodiment thereof, an improved fuel burner apparatus is provided
which
comprises a body having an outlet end and including a pilot conduit extending
along
an axis and through which a pilot fuel/air mixture may be flowed, discharged
through
the outlet end, and ignited to create a pilot flame. An inner firing conduit
circumscribes the pilot conduit and laterally defines therebetween a first
flow space
communicating with the body outlet end. An outer firing conduit circumscribes
the
inner firing conduit and laterally defines therebetween a second flow space
communicating with the body outlet end.

The fuel burner apparatus also includes a fuel/air delivery system operative
to
force fuel and air through each of the first and second body flow spaces, for
discharge
through the body outlet end and ignition by the pilot flame, to responsively
create a
main burner flame. Accordirig to a key aspect of the present invention, the
burner
body is configured in a manner such that the flow of fuel and air discharged
from the
second body flow space functions to laterally constrain the main burner flame,
representatively providing the main burner flame with a relatively thin,
axially
elongated configuration. The inner and outer firing conduits have downstream
ends,
and the downstream end of the outer firing conduit is preferably axialLy
offset from
the downstream end of the inner firing conduit in a downstream direction to
aid in
the shaping of the main burner flame.

-2-


CA 02498538 2001-10-11

According to other aspects of the present invention, the fuel/air delivery
system is operative to force separate first and second fuel/air mixtures
respectively
through the first and second burner body flow spaces, and the fuel/air
delivery
system is operative to utilize different fuels in the separate first and
second fuel/air
mixtures.

In an illustrated preferred embodiment of the fuel burner, the fuel/air
delivery
system includes first and second fuel injectors respectively communicated with
the
first and second flow spaces and operative to receive fuel from at least one
source
thereof. An air inlet plenum structure is carried by the burner body, and
first and
second mixing plenum structures extend through the air inlet plenum structure,
the
first and second mixing plenum structures being respectively coupled to the
first and
second fuel injectors, having air inlet openings therein, and respectively
communicating with the first and second burner body flow spaces. The fuel
burner
further includes an air delivery structure operatively coupled to the first
and second
flow spaces, the air delivery structure representatively including an air
supply fan
having an outlet communicated with the interior of the air inlet plenum
structure.

According to another aspect of the present invention, the outlet end of the
2o burner body is operatively cciupled to a heat exchanger through which a
fluid to be
heated may be flowed, the heat exchanger having an interior space for
receiving the
main burner flame from which combustion heat may be transferred to the fluid
being
flowed through the heat exchanger. Representatively, the heat exchanger has a
series of interior heating tubes through which the fluid to be heated may be
flowed,
the series of interior heating tubes circumscribing the burner flame-receiving
interior
space of the heat exchanger and longitudinally extending parallel to the axis
of the
burner body. The axial elonglation of the main burner flame injected into the
interior
of the heat exchanger parallel to the heat exchanger tubes substantially
enhances the
overall heat transfer efficiency of the overall fuel-fired heat exchange
apparatus.

-3-


CA 02498538 2007-02-28
BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1(Prior Art) is a simplified cross-sectional view of an outlet end
portion of
a conventional fuel burner;
FIG. 2 (Prior Art) is a view similar to that in FIG. 1, but with a tubular
ceramic
flame shaper operatively connected to the outlet end of the conventional fuel
burner;
FIG. 3 is a simplified cross-sectional view of an outlet end portion of a
specially
designed variable firing rate fuet burner embodying principles of the present
invention; and
FIG. 4 is a simplified, somewhat schematic full cross-sectional view through
the
variable firing rate fuel burner of the present invention operatively
connected to a
representative heat exchanger, only a portion of which is iliustrated.

DETAILED DESCRIPTION

As iliustrated in FIGS. 3 and 4, this invention provides a specially designed
variable firing rate fuel burner 10. Burner 10 is illustratively depicted in a
downfire
orientation and is representatively connected at its outlet to the upper end
of a
schematically depicted, vertically elongated heat exchanger structure 12 (see
FIG. 4),
only a vertical portion of which is illustrated. Burner 10 constitutes a
substantiat
improvement of the prior art fuel burner 14 shown in FIG. 1, burner 14 being
similar
in some regards to the burner shown in FIG. 12 of U.S. Patent 5,658,139.
The prior art burner 14 had several
problems such as (1) its main outlet flame 16 being too laterally divergent
(i.e., wide)
for use in, for example, the vertically elongated heat exchanger structure 12
(see FIG.
4), and (2) its firing rate being difficult to modulate.

To a certain extent the desirable narrowing of the burner outlet flame 16 was
sotved, as itlustrated in FIG. 2 (Prior Art), by attaching to the outlet of
the prior art
burner 14 a tubular ceramic flame shaper 18 which "shapes" the outlet flame 16
to
the indicated narrower configuration 16a. However, the ceramic flame shaper 18
was
-4-


CA 02498538 2001-10-11

expensive, fragile, and undesirably increased, the overall burner length.
Additionally,
the flame shaper did nothing to add firing rate modulation capabilities to the
burner
14.

Turning now to FIGS. 3 and 4, the improved, variable firing rate fuel burner
10
of the present invention incorporates the general structure of the FIG. I
burner 14 as
a tubular inner body portion of the improved burner 10 which comprises an
inner
firing tube or conduit 20, a pilot tube or conduit 22 outwardly circumscribed
by the
firing tube 20 and creating an annular flow space 24 therewith, a bluff body
26
carried on the lower end of the pilot tube 22, and an annular array of
circumferentially spaced flame-holding swirl vanes 28 disposed at the lower
end of
the annular flow space 24.

Burner 10 also includes an outer firing tube or conduit 30 that outwardly
circumscribes the inner firing tube 20 and creates an annular flow space 32
therewith.
As illustrated, the open lower end of the outer firing tube 30 is preferably
downwardly offset from the open lower end of the inner firing tube 20.

A blank-off plate 34 (see FIG. 4) internally located at an upper end portion
of
the burner 10 blocks the upper end of the outer annular flow space 32 and
separates
the flow space 32 from an upper end chamber 36 in the burner body which is
communicated at its lower side with the inner annular flow space 24. Upper end
chamber 36 and an upper end portion of the outer annular flow space 32
communicate with the interior of an air inlet plenum structure 38 disposed at
the
upper end of the burner 10 and coupled to the outlet of an air supply fan 40.

Fuel injectors 42,44 are operatively connected to mixing plenum structures
46,48 disposed in the air inlet plenum structure 38 and respectively
communicated
with the upper end chamber 36 and an upper end portion of the outer annular
flow
space 32. Each of the mixing plenum structures 46,48 has a series of air inlet
openings 50 formed therein.
-5-


CA 02498538 2001-10-11

During operation of the burner 10, a- fuel-air mixture is flowed downwardly
through the pilot tube 22 to maintain a pilot flame 52 adjacent the lower end
of the
burner 10. Pilot flame 52 is initiated by a suitable igniter structure (not
shown). Fuel
from a source thereof is forced into the fuel injectors 42 and 44, and
combustion air
54 is forced into the inlet plenum structure 38 by the fan 40. The air 54
entering the
plenum 38 is forced into the mixing plenum structures 48,50 through their air
inlet
openings 50 and mixed with fuel discharged from the injectors 42,44 to form
(1) a
first or inner premixed fuel-air flow 56 that is forced downwardly through the
inner
annutar flow space 24 for downward discharge therefrom and ignition by the
pilot
flame 52, and (2) a second or outer premixed fuel-air flow 58 that is forced
downwardly through the outer annular flow space 32 for discharge therefrom and
ignition at the lower end of the burner 10.

This forcibLe discharge of the annular outer premixed fuel-air flow 58
outwardly around the discharged inner premixed fuel-air flow 56 causes the
outer
premixed fuel-air flow 58 to function as a flame shaping structure that takes
the
place of the previously described ceramic flame shaper 18 (see FIG. 2) and
operates
to cause the resulting main burner flame 60 to assume the desired long, narrow
shape without the use of the ceramic flame shaper 18.
Additionally, the use of the two premixed fuel-air mixture flows 56,58
provides
the burner 10 with substantially enhanced firing rate adjustment capabilities
by
simply reducing or increasing the amount of fuel supplied to the injector 44
and/or
reducing the air supply to the burner. Further, the dual premixed fuel-air
flow
capability permits the burner 10 to be simultaneously operated with two
different
types of fuel simply by supplying each injector 42,44 with a different type of
fuel.

In addition to its enhanced firing rate adjustment capability and dual-fuel
operational capability, the unique structure of the burner 10 just described
provides
it with a variety of other advantages compared to conventionally configured
fuel
-6-


CA 02498538 2001-10-11

burners. These other advantages include lowered NOx emission rates, enhanced
stability, better fuel/air mixing characteristics and a lowered burner
pressure drop.
The unique configuration and operation of the burner 10 also enhances the
performance of the elongated heat exchanger 12 (see FIG. 4) due to the
correspondingly elongated burner flame 60. Representatively, the heat
exchanger 12
has a vertically elongated cylindrical body 62 with a header section 64 at its
upper
end, the outlet end of the burner 10 being operatively connected to the header
section 64. The elongated burner flame 60 is forced downwardly into a
vertically
io elongated firing space 66 disposed in the interior of the heat exchanger
body 62 and
surrounded by a circumferentially spaced array of vertically oriented heat
exchanger
tubes 68 disposed in the interior of the heat exchanger 12 (only two of the
tubes 68
being shown). During operation of the heat exchanger 12, a fluid (for example,
water) to be heated is ftowed through the tubes 68 and receives combustion
heat
from the burner outlet flame 60. Due to the unique flame shaping capability of
the
burner 10 described above, the elongated flame 60 is generally parallel to the
lengths
of the tubes 68, thereby desirably enhancing the heat transfer efficiency of
the heat
exchanger 12.

The foregoing detailed description is to be clearly understood as being given
by
way of illustration and example, the spirit and scope of the present invention
being
limited solely by the appended claims.

-7-

Representative Drawing
A single figure which represents the drawing illustrating the invention.
Administrative Status

For a clearer understanding of the status of the application/patent presented on this page, the site Disclaimer , as well as the definitions for Patent , Administrative Status , Maintenance Fee  and Payment History  should be consulted.

Administrative Status

Title Date
Forecasted Issue Date 2008-08-19
(22) Filed 2001-10-11
(41) Open to Public Inspection 2002-08-22
Examination Requested 2005-03-21
(45) Issued 2008-08-19
Deemed Expired 2010-10-12

Abandonment History

There is no abandonment history.

Payment History

Fee Type Anniversary Year Due Date Amount Paid Paid Date
Request for Examination $800.00 2005-03-21
Registration of a document - section 124 $100.00 2005-03-21
Application Fee $400.00 2005-03-21
Maintenance Fee - Application - New Act 2 2003-10-14 $100.00 2005-03-21
Maintenance Fee - Application - New Act 3 2004-10-12 $100.00 2005-03-21
Maintenance Fee - Application - New Act 4 2005-10-11 $100.00 2005-09-26
Maintenance Fee - Application - New Act 5 2006-10-11 $200.00 2006-09-19
Maintenance Fee - Application - New Act 6 2007-10-11 $200.00 2007-09-21
Final Fee $300.00 2008-06-03
Maintenance Fee - Patent - New Act 7 2008-10-14 $200.00 2008-09-17
Owners on Record

Note: Records showing the ownership history in alphabetical order.

Current Owners on Record
RHEEM MANUFACTURING COMPANY
Past Owners on Record
HALLIT, RAYMOND I.
Past Owners that do not appear in the "Owners on Record" listing will appear in other documentation within the application.
Documents

To view selected files, please enter reCAPTCHA code :



To view images, click a link in the Document Description column. To download the documents, select one or more checkboxes in the first column and then click the "Download Selected in PDF format (Zip Archive)" or the "Download Selected as Single PDF" button.

List of published and non-published patent-specific documents on the CPD .

If you have any difficulty accessing content, you can call the Client Service Centre at 1-866-997-1936 or send them an e-mail at CIPO Client Service Centre.


Document
Description 
Date
(yyyy-mm-dd) 
Number of pages   Size of Image (KB) 
Cover Page 2008-08-06 2 44
Abstract 2001-10-11 1 25
Description 2001-10-11 7 318
Claims 2001-10-11 5 172
Drawings 2001-10-11 2 50
Representative Drawing 2005-05-03 1 6
Cover Page 2005-05-04 1 40
Claims 2007-02-28 5 172
Description 2007-02-28 7 318
Correspondence 2005-06-15 1 14
Correspondence 2009-07-16 6 294
Correspondence 2005-04-01 1 36
Assignment 2001-10-11 3 95
Prosecution-Amendment 2006-11-22 2 79
Prosecution-Amendment 2007-02-28 6 238
Correspondence 2008-06-03 2 50
Correspondence 2009-08-12 1 13
Correspondence 2009-08-12 1 26