U.S. patent number 3,698,186 [Application Number 05/101,225] was granted by the patent office on 1972-10-17 for afterburner combustion apparatus.
This patent grant is currently assigned to United Aircraft Corporation. Invention is credited to David J. Beane, John H. Gastler.
United States Patent |
3,698,186 |
Beane , et al. |
October 17, 1972 |
**Please see images for:
( Certificate of Correction ) ** |
AFTERBURNER COMBUSTION APPARATUS
Abstract
A power plant with an afterburner has a combustion apparatus
therein which comprises a flameholder-spraybars extending radially
into the afterburner at a plurality of locations. A third of the
flameholder-spraybars are full length and extend to a center body,
a third are of medium length and extend to the center of a hot
exhaust, and a third are short and extend inwardly to a point
rearwardly of a splitter separating the hot exhaust from a cooler
fan duct air. The medium length flameholder-spraybars are divided
into two fuel injection compartments and the full length
flameholder-spraybars are divided into three fuel injection
compartments. For primary zone burning fuel is admitted to the
innermost compartment of each of the full length
flameholder-spraybars; for secondary zone burning, the inner
compartments of the medium length flameholder-spraybars and the
middle compartments of the full length flameholder-spraybars then
also have fuel directed thereto; and for tertiary zone burning,
fuel is then also directed to the outermost compartment of each of
the full length and medium length flameholder-spraybars and to the
short length flameholder-spraybars.
Inventors: |
Beane; David J. (North Palm
Beach, FL), Gastler; John H. (Portland, CT) |
Assignee: |
United Aircraft Corporation
(East Hartford, CT)
|
Family
ID: |
22283584 |
Appl.
No.: |
05/101,225 |
Filed: |
December 24, 1970 |
Current U.S.
Class: |
60/746; 60/749;
60/764 |
Current CPC
Class: |
F23R
3/00 (20130101); F23R 3/20 (20130101) |
Current International
Class: |
F23R
3/20 (20060101); F23R 3/02 (20060101); F23R
3/00 (20060101); F02k 003/10 () |
Field of
Search: |
;60/39.74R,39.72R,226,261,39.32,262 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Hart; Douglas
Claims
We claim:
1. In a combustion chamber having an inlet and outlet a plurality
of flameholder-spraybars, said flemholder-spraybars extending
radially into said combustion chamber at a plurality of locations,
each flameholder-spraybar comprising a spraybar assembly which is
fixedly mounted to said combustion chamber, a flameholder assembly
being positioned over each spraybar assembly and fixed thereto, a
plurality of fuel nozzles located along the length of each spraybar
assembly, an opening in each flameholder assembly opposite each
nozzle to permit fuel exiting from the nozzle to be directed
therethrough into the combustion chamber, said
flameholder-spraybars being of different lengths around said
combustion chamber, some spraybars are full length and extend
across the full radius of the inlet of the combustion chamber while
others extend for substantially two-thirds of said length and
one-third of said length.
2. An apparatus as set forth in claim 3 wherein said inlet is
annular and the full length spraybars are guided at their inner end
by a center body structure positioned in the combustion
chamber.
3. In a combustion chamber having an inlet and outlet a plurality
of flameholder-spraybars, said flameholder-spraybars extending
radially into said combustion chamber at a plurality of locations,
each flameholder-spraybar comprising a spraybar assembly which is
fixedly mounted to said combustion chamber, a flameholder assembly
being positioned over each spraybar assembly and fixed thereto, a
plurality of fuel nozzles located along the length of each spraybar
assembly, an opening in each flameholder assembly opposite each
nozzle to permit fuel exiting from the nozzle to be directed
therethrough into the combustion chamber, said
flameholder-spraybars being of at least two different lengths
around said combustion chamber, said longer of said
flameholder-spraybars having its spraybar divided into
compartments, the outer compartment being the length of the shorter
spraybars, each extra inner compartment having conduit means for
directing fuel thereto.
4. A flameholder-spraybar assembly adapted to be positioned in a
combustion chamber having a wall and a forward end and an after end
and including:
1. a fuel spraybar comprising a hollow tube member adapted to
extend into said combustion chamber, and having:
a. first aperture means extending through the hollow tube member
for fuel flow therethrough,
2. means to support one end of said spraybar with respect to said
combustion chamber wall,
3. a flameholder of gutter-shaped cross-section and being of
selected shape and length to be sleeved over said spraybar in
scabbard fashion and having its closed end projecting in a forward
direction, and having:
a. second aperture means oriented to communicate with said first
aperture means for fuel flow to said combustion chamber,
4. slip joint means supporting one end of the flameholder with
respect to said one end of said spraybar,
5. means to connect the other end of the flameholder to the other
end of the spraybar.
5. Apparatus according to claim 10 and including an inner
combustion chamber wall forming an annular section, means to
position said other end of said flameholder with respect to said
inner combustion chamber wall.
6. Apparatus according to claim 4 wherein said flameholder has its
open end closed by a closure member forming a long closed
compartment therein, an opening in the closed forward part of its
outer portion so as to receive flow from the outer part of the
combustion chamber, an exhaust opening at its inner portion to
exhaust flow at the inner part of the combustion chamber.
7. A flameholder-spraybar assembly as set forth in claim 4 wherein
said first aperture means comprises a fuel nozzle means.
8. In combination, a combustion chamber between inner and outer
walls positioned concentrically about an axis:
1. a plurality of flameholder-spraybar assemblies extending
radially across said combustion chamber and positioned in spaced
circumferential positions therearound and with the
flameholder-spraybar assemblies being of different lengths selected
so as to form a flameholder-spraybar assembly pattern
circumferentially about said combustion chamber,
2. each of said flameholder-spraybar assemblies comprising:
a. a spraybar comprising a hollow tube member adapted to extend
into a combustion chamber and having:
1. aperture means extending through the wall of the hollow tube
member and oriented to communicate with the combustion chamber,
b. means to connect one end of said spraybar to the combustion
chamber outer wall,
c. a flameholder of gutter-shaped cross-section and being of
selected shape and length to be sleeved over said spraybar in
scabbard fashion and having its closed end projecting in a forward
direction,
d. slip joint means supporting one end of the flameholder with
respect to said one end of said spraybar,
e. means to connect the other end of the flameholder to the other
end of the spraybar so that with said last-named means removed,
said flameholder may be sleeved free of said slip joint means and
off of said spraybar.
9. Apparatus according to claim 8 and wherein said spraybar
apertures are oriented to extend substantially transversely of the
combustion chamber and wherein said flameholders include a
plurality of apertures positioned and sized so that a flameholder
aperture is positioned adjacent each spraybar aperture so that fuel
from the interior of the spraybar will pass through both the
spraybar and the flameholder apertures in passing into the
combustion chamber.
10. In combination, in an engine, a combustion chamber, said
chamber having an inwardly facing wall, said chamber having an
inlet and outlet, a plurality of flameholder-spraybars, said
flameholder-spraybars extending radially into said combustion
chamber from said wall at a plurality of locations, each
flame-holder-spraybar comprising a spraybar assembly which is
fixedly mounted with respect to said combustion chamber, each
spraybar assembly comprising a spraybar extending radially into the
combustion chamber, a flameholder assembly being mounted over each
spraybar and supported by the spraybar assembly, a plurality of
fuel nozzles located along the length of each spraybar, an opening
in each flameholder assembly spaced from each nozzle to permit fuel
exiting from the nozzle to be directed therethrough into the
combustion chamber.
11. A combination as set forth in claim 10 wherein each spraybar
assembly has a plate member fixed to each spraybar which is
removably attached with respect to said combustion chamber, an
opening in each plate member connects the interior of its attached
spraybar to the exterior of said plate member, means are provided
for directing a fuel to the interior of each spraybar, each
flameholder-spraybar being removable as a unit.
12. A combination as set forth in claim 10 wherein said inlet is
divided by a splitter located radially inwardly from said inwardly
facing wall forming two inlet sections, said outer annular inlet
section having cool gas pass therethrough while the inner inlet
section has relatively hot gases pass therethrough.
13. A combination as set forth in claim 12 wherein some spraybars
extend radially inward to the radius of said splitter, and some
spraybars extend radially inward across said outer annular inlet
section and into said inner inlet section.
14. A combination as set forth in claim 13 wherein the spraybars
which extend into said inner inlet section have a plurality of
compartments therein, one compartment extends inwardly
approximately to the radius of said splitter, a second compartment
is located inwardly of said splitter extending further inwardly of
said combustion chamber, means for directing fuel directly to said
inner compartment.
15. A combination as set forth in claim 14 wherein means are
provided to direct fuel to only the inner compartments of the
spraybars at a given time, and means are provided to direct fuel to
the outer compartments of the spraybars and the spraybars which
extend only to the splitter at another given time.
Description
BACKGROUND OF THE INVENTION
This invention relates to flameholders for gas turbine engines and
is located in the afterburner of a fan engine. An afterburner
including a flameholding arrangement for a bypass gas turbine
engine is shown in U.S. Pat. No. 3,485,045.
SUMMARY OF INVENTION
A primary object of the present invention is to provide an
afterburner combustion apparatus having combined
flameholder-spraybars extending radially inwardly from the outer
casing of an engine, said flameholder-spraybars acting as
cantilevered beams. This close coupling of spraybars within
flameholders eliminates the need for a separate heat shield.
In accordance with the present invention, each flameholder-spraybar
is separately removable and replaceable. The absence of
circumferential flameholders connected to said radial flameholders
prevents distortion and buckling due to the transport hoop.
In accordance with a further aspect of the present invention,
cooling is obtained by having air flow from the cooler fan air
section into the interior of the flameholder and over the
cooperating spraybar to a discharge. This operates efficiently
since the fan air is at a high pressure and the hot exhaust is at a
lower pressure.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a view of a fan engine showing the location of the
flameholder-spraybars in the afterburner.
FIG. 2 is a schematic view taken along the line 2--2 of FIG. 1
showing the position of the different lengths of
flameholder-spraybars.
FIG. 3 is an enlarged view, partially in section, of the full
length flameholder-spraybar shown in FIG. 1.
FIG. 4 is a cross-sectional view taken along the line 4--4 of FIG.
3.
FIG. 5 is a view taken along the line 5--5 of FIG. 3 showing a fuel
nozzle.
FIG. 6 is a view taken along the line 6--6 of FIG. 3.
FIG. 7 is an enlarged view, partially in section, of the medium
length flameholder-spraybar.
FIG. 8 is an enlarged view, partially in section, of the short
flameholder-spraybar.
DESCRIPTION OF THE PREFERRED EMBODIMENT
The power plant shown in FIG. 1 comprises a conventional fan engine
1 with an afterburner 2 and nozzle 4. Turbine engine exhaust flows
from the engine at A between the rear end of the splitter 6 and the
tail cone 10. Fan air flows from the outer fan duct at B between
the splitter 6 and the outer casing 12. Both of these flows, then
enter the flameholder-spraybars arranged as a plurality of radially
extending composite members fixed to the outer casing 12 and
extending toward the tail cone. A cooling liner 16 extends around
the inner surface of the outer casing 12 and is fixed thereto by a
plurality of spacing members 17 along its length. Flow from the
outer fan duct passes between the liner 16 and outer casing 12.
As shown in FIG. 2, there are thirty flameholder-spraybars, ten of
them are full length flameholder-spraybars 14A, ten of them are
medium length flameholder-spraybars 14B, extending about two-thirds
of the length of the full length flameholder-spraybars, and ten of
them are short length flameholder-spraybars 14C extending about
one-third of the length of the full length flameholder-spraybar.
The short flameholder-spraybars 14C extend in length approximately
to the circumference of the rear end of the splitter 6 which
separates the fan air and turbine engine exhaust. The medium
spraybars, 14B, extend to a point midstream of the distance between
the rear end of the splitter 6 and tail cone 10. The full length
flameholder-spraybars 14A extend approximately to a circular flange
20 which extends rearwardly from a rear surface 18 of the tail cone
10 and are guided therein in a manner to be hereinafter
described.
Since the flameholder-spraybars 14A, 14B and 14C are similar in
construction, except for the length, the full length
flameholder-spraybar 14A will be described fully and the other
flameholder-spraybars 14B and 14C will be described as they differ
from it. Each flameholder-spraybar is removable through an opening
22 in the outer casing 12 and an axially aligned similar fixed
opening 23 in the cooling liner 16. The full length
flameholder-spraybar 14A comprises two main parts, the spraybar
assembly 30 and the flameholder assembly 32.
The spraybar assembly 30 comprises a cover plate 34 which covers
the opening 22 in the outer casing 12 and is removably attached
thereto by bolts 36. This cover plate 34 has a thickened center
portion with passages therethrough which provide for the connection
of the fuel lines mounted externally of the outer casing 12 and the
fuel transfer lines within said outer casing 12. A guide member 35
is fixed around the thickened center portion of the cover plate 34
and extends inwardly through the opening 23 of the cooling line 16
a short distance for receiving a mating end 37 of the flameholder
assembly 32.
A spraybar 38 extends inwardly from the thickened portion of the
cover plate 34. The spraybar 38 is a hollow member with two
partitions 40 therein dividing it into three compartments 42, 44
and 46. Compartment 42 extends for approximately the first
one-third of the length of the spraybar 38, compartment 44 extends
for approximately the second one-third of its length, and
compartment 46 extends for the last remaining one-third of its
length. The inner end of the spraybar is closed by a boss member 48
having an opening 50 therethrough for a purpose to be hereinafter
described. The outer end of the compartment 42 is connected by a
conduit section 41 to one of the three passageways in the thickened
center portion of the cover plate 34. The other end of this
passageway is connected to a conduit 53 which is in turn connected
to an annular manifold 55. Fuel is directed to the manifold 55 from
the fuel control 57.
A fuel line 52 extends inwardly from the thickened portion of the
cover plate 34 and is connected at its inner end to the interior of
the compartment 46 adjacent partition 40 by a right angle connector
54. The outer end of the fuel line 52 is connected around one of
the other passageways in the thickened center portion of the cover
plate 34. The other end of this passageway is connected to a
conduit 65 which is in turn connected to an annular manifold 59.
Fuel is directed to the manifold 59 from the fuel control 57.
A fuel line 56 extends inwardly from the thickened portion of the
cover plate 34 and is connected at its inner end to the interior of
the compartment 44 adjacent partition 40 by a right angle connector
58. The outer end of the fuel line 56 is connected around one of
the other passageways in the thickened center portion of the cover
plate 34. The other end of this passageway is connected to a
conduit 61 which is in turn connected to an annular manifold 63.
Fuel is directed to the manifold 63 from the fuel control 57. The
fuel lines 52 and 56 are connected to the spraybar 38 along their
lengths adjacent connector 58 by rearwardly extending flange 60. A
similar support 62 supports fuel line 52 adjacent connector 54.
Each compartment contains three fuel nozzles 70 which spray fuel at
90.degree. to the axis of the spraybar 38. Each fuel nozzle 70
comprises a stem 72 and an opening 74 in the side of the spraybar
38 which acts as a valve seat. A contoured end of the stem 42
coacts with the opening 74 to provide a variable nozzle opening.
The stem 72 can be adjusted to obtain the opening desired for
afterburner operation. The stem can be adjusted axially since it is
threadably mounted in a boss 76 fixed to the spraybar 38. In each
of the figures, the position of the fuel nozzle is shown by a small
dotted circle.
The flameholder assembly 32 comprises a combination heat shield and
flameholder which is positioned over the spraybar assembly. The
outer end of said flameholder assembly has a mating guide member 37
which is formed to slidably engage guide member 35 on the cover
plate 34. When these are properly positioned, two bushings 80 and
82 at the inner end of the flameholder assembly have openings
therein which are aligned with the opening 50 in the boss member 48
mentioned hereinbefore. A pin member 86 therethrough maintains the
flameholder-spraybars in their proper relationship.
The flameholder assembly 32 is formed by a V-shaped member 41 with
a flat U-shaped member 43 fixed adjacent the rear end thereof
forming a long closed compartment 45 and rearwardly open trough 47.
A plate 49 covers the outer end of the compartment 45. The V-shaped
member 41 has an opening 100 adjacent its outer end in its
forwardly facing portion to receive air from the outer fan duct. A
second opening 102 is located in the U-shaped member 43 adjacent
its inner end so that the cooling air entering opening 100 can flow
from the compartment 45. The flat U-shaped member 43 extends at the
inner end of the flameholder assembly into an opening 51 in the
circular flange 20 of the tail cone 10 to provide for proper
spacing and support of the full length flameholder-spraybars 14A.
The sides of the opening 51 are made so as to slidably engage the
outer side of the U-shaped member. This permits unrestricted radial
growth of the flameholder-spraybars.
FIG. 7 shows the medium length flameholder-spraybar 14B and it
comprises only two compartments with one fuel line 90 necessary.
The outer end of the outer compartment is connected by a conduit
section 87 to one of the passageways in the thickened center
portion of its cooperating cover plate. It is noted that the cover
plate for the medium length flameholder-spraybar has only two
passageways therein. The other end of this passageway is connected
to a conduit 89 which is in turn connected to the annular manifold
55.
The fuel line 90 extends inwardly from the thickened portion of the
cover plate and is connected at its inner end to the interior of
the outer compartment adjacent partition 40 by a right angle
connector 91. The other end of the fuel line 90 is connected around
the other passageway in the thickened center portion of the cover
plate. The other end of this passageway is connected to a conduit
93 which is in turn connected to the annular manifold 63.
The inner end of the flameholder assembly is attached in a
different manner than that of the full length flameholder-spraybar
14A. In the medium length construction, a projection 92 extends
into a bushing member 94 with a pin 96 being placed through aligned
openings therein. A cooling arrangement similar to that shown in
FIG. 3 for the full length flameholder-spraybar is incorporated in
the medium length flameholder-spraybar.
The short flameholder-spraybar 14C of FIG. 8 has a similar
arrangement at its inner end to that in FIG. 7 for connecting the
spraybar assembly and the flameholder assembly. It is noted that
this section does not have the cooling flow through the flameholder
assembly. This short flameholder-spraybar comprises only one
compartment which is similar to the outer compartments of the other
spraybars. This compartment is connected by conduit section 95 to
the one passageway in the thickened center portion of its
cooperating cover plate. It is noted that the cover plate for the
short length flameholder-spraybar has only one passageway therein.
The other end of this passageway is connected to a conduit 97 which
is in turn connected to the annular manifold 55.
It can be seen that the outer compartments of the full length and
medium length flameholder-spraybars are connected to the same
manifold 55 as the single compartment of the short length
flameholder-spraybar so that when fuel is directed to the annular
manifold 55 fuel is then delivered to all of the compartments of
all of the flameholder-spraybars which are located downstream of
the outer fan duct. The center compartment of the full length
flameholder-spraybars and the inner compartment of the medium
length flameholder-spraybars are connected to the same manifold 63
so that when fuel is directed to the annular manifold 63 fuel is
then delivered to all of the compartments of the full length and
medium length flameholder-spraybars which are located downstream of
the outer portion of the turbine engine hot exhaust flow. The inner
compartments of the full length flameholder-spraybars are connected
to the annular manifold 59 so that when fuel is delivered to the
annular manifold 59 fuel is then delivered to all of the
compartments of the full length flameholder-spraybars which are
located downstream of the inner portion of the turbine engine hot
exhaust flow.
When fuel is admitted to the annular manifold 59 a primary zone of
afterburning is obtained. When the fuel control then supplies fuel
to the annular manifold 63 a secondary zone is brought in, and when
fuel is directed to the annular manifold 55 a tertiary zone is
brought in.
* * * * *