U.S. patent number 3,751,911 [Application Number 05/133,492] was granted by the patent office on 1973-08-14 for air inlet arrangement for gas turbine engine combustion chamber.
This patent grant is currently assigned to Motoren-Und Turbinen Union Munich GmbH. Invention is credited to Peter De Tartaglia.
United States Patent |
3,751,911 |
De Tartaglia |
August 14, 1973 |
AIR INLET ARRANGEMENT FOR GAS TURBINE ENGINE COMBUSTION CHAMBER
Abstract
A combustion chamber to gas turbine engines equipped with a
flame tube provided with air inlet openings for combustion and
mixing air; further air inlet openings are provided in the flame
tube at the level of the combustion chamber end wall, through which
small quantities of air are adapted to be blown radially inwardly
toward the discharge point of the fuel injection nozzle. This
invention relates to a combustion chamber for gas turbine engines,
whose flame tube contains air inlet openings for the supply of
combustion and mixing air. As a rule, the ratio of the
cross-sectional areas of the primary and secondary air inlet
openings is so chosen that the fuel-air mixture in the combustion
zone of the combustion chamber is approximately stoichiometric. It
is well known, however, that in this case frequently zones of a
richer fuel-air mixture occur so that combustion in these zones is
only incomplete, with resulting deposits of carbon black on the end
wall of the combustion chamber and/or pollution of the exhaust
gases. This is particularly true for combustion chambers
incorporating a flameholder, since in the same there is little or
no air introduced into the spraying zones of the fuel injector.
Among the known measures that have been employed to avoid such
carbon deposits are an increase in the proportion of primary air
and the use of additional small air inlet ports in the susceptible,
endangered zones. Both of these measures, however, can be used only
to a limited extent because an increased proportion of primary air
will result in a poor LEAN extinction limit and also because the
use of too large and/or too many air inlet ports has been known to
disturb the reduced pressure zone behind the flameholder. The
purpose of this invention is, therefore, to eliminate the
above-mentioned drawbacks of the known types of combustion chambers
and to provide a combustion chamber which offers, in addition to a
high degree of combustion at partial load and a good LEAN
extinction limit, a combustion which produces neither carbon
deposits nor a pollution of the exhaust gases. It is proposed
according to the invention for this purpose, to provide air inlet
openings in the flameholder arranged at the level of the combustion
chamber end wall, which will blow small quantities of air radially
into the flame tube in the direction of the discharge tip of the
fuel injector nozzle. According to a further feature of the
invention, the flame tube may be equipped with tubes and/or ribs
arranged coaxially to the air inlet openings in the flame tube. The
air flowing inward at a high velocity will have the following
effect: 1. The excess fuel existing directly adjacent to the end
wall of the combustion chamber will be removed; 2. A zone of high
turbulence will be created adjacent to the combustion chamber end
wall, which will have a favorable effect on the combustion process;
and 3. Any carbon black particles which may still be produced will
be prevented from depositing.
Inventors: |
De Tartaglia; Peter
(Munich-Karlsfeld, DT) |
Assignee: |
Motoren-Und Turbinen Union Munich
GmbH (Munich, DT)
|
Family
ID: |
5768415 |
Appl.
No.: |
05/133,492 |
Filed: |
April 13, 1971 |
Foreign Application Priority Data
|
|
|
|
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Apr 18, 1970 [DT] |
|
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P 20 18 641.8 |
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Current U.S.
Class: |
60/756; 60/760;
60/758 |
Current CPC
Class: |
F23R
3/10 (20130101); F23R 3/54 (20130101); F23R
3/04 (20130101) |
Current International
Class: |
F23R
3/00 (20060101); F23R 3/10 (20060101); F23R
3/54 (20060101); F23R 3/04 (20060101); F02g
003/00 () |
Field of
Search: |
;60/39.74,39.65,DIG.8,39.69,39.36,39.66 ;431/352 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
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|
|
|
|
|
|
205,220 |
|
May 1956 |
|
AU |
|
545,787 |
|
Sep 1957 |
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CA |
|
836,117 |
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Jun 1960 |
|
GB |
|
Primary Examiner: Croyle; Carlton R.
Assistant Examiner: Koczo, Jr.; Michael
Claims
I claim:
1. A combustion chamber arrangement for a gas turbine engine
comprising: a flame tube and an end wall forming a combustion
chamber space, fuel injector nozzle means having a fuel discharge
point located centrally of said end wall for injecting fuel into
said combustion chamber space in a downstream direction, air
introducing means for supplying combustion and mixing air to said
combustion chamber space, said air introducing means including
first air inlet means arranged in the flame tube for introducing
air in an upstream direction parallel to and along said end wall
toward said discharge point and second air inlet means for
introducing air into said combustion chamber space in a downstream
direction, said end wall being tapered conically outwardly in the
downstream direction from said discharge point to adjacent the
first air inlet means, and an outer casing surrounding said flame
tube with an annular space between said outer casing and said flame
tube for conducting mixing and combustion air to said air
introducing means, said second air inlet means being constructed as
an annular opening between said end wall and said flame tube, said
end wall being formed by an extension of said outer casing.
2. An arrangement according to claim 1, wherein said first air
inlet means includes a plurality of cylindrical inlet tubes
extending from said annular space across said annular opening
inwardly into said combustion chamber space.
3. An arrangement according to claim 1, wherein said first air
inlet means includes a plurality of part-cylindrical rib means
extending from openings leading from said annular space and across
said annular opening.
4. An arrangement according to claim 2, wherein said air
introducing means includes third air inlet means for introducing
air into said combustion chamber space, said third air inlet means
including a plurality of openings in said flame tube means which
communicate with said annular space and said combustion chamber
space at a position downstream of said first and second air inlet
means.
5. An arrangement according to claim 3, wherein said air
introducing means includes third air inlet means for introducing
air into said combustion chamber space, said third air inlet means
including a plurality of openings in said flame tube means which
communicate with said annular space and said combustion chamber
space at a position downstream of said first and second air inlet
means.
6. A combustion chamber arrangement for a gas turbine engine
comprising: a flame tube and an end wall forming a combustion
chamber space, fuel injector nozzle means having a fuel discharge
point located centrally of said end wall for injecting fuel into
said combustion chamber space in a downstream direction, said end
wall being tapered conically outwardly in the downstream direction
from said discharge point to adjacent the downstream end of said
end wall, and air introducing means for supplying combustion and
mixing air to said combustion chamber space, said air introducing
means including first air inlet means arranged in the flame tube
for introducing air in an upstream direction parallel to and along
said end wall toward said discharge point and second air inlet
means for introducing air into said combustion chamber space in a
downstream direction, said second air inlet means being formed by
an annular opening between said flame tube and said downstream end
of said end wall, said first air inlet means including means
extending across said annular opening for precluding intermixing of
the flow from said first and second air inlet means, whereby flow
from said first air inlet means is not interrupted by flow from
said second inlet means such that it can effectively remove any
excess fuel adjacent said end wall, prevent depositing of carbon
black particles on said end wall, and create a zone of high
turbulence adjacent said end wall.
7. An arrangement according to claim 6, wherein said means
extending across said annular opening includes a plurality of
cylindrical inlet tubes extending inwardly into the combustion
chamber space through said flame tube means.
8. An arrangement according to claim 7, wherein said inlet tubes
are circumferentially spaced from one another around the
circumference of said flame tube means.
9. An arrangement according to claim 6, wherein said means
extending across said annular opening includes a plurality of
part-cylindrical rib means extending inwardly into the combustion
chamber space from openings in said flame tube means.
10. An arrangement according to claim 9, wherein said rib means are
circumferentially spaced from one another around the circumference
of said flame tube means.
11. An arrangement according to claim 6, further comprising an
outer casing surrounding said flame tube means with an annular
space between said outer casing and said flame tube means for
conducting mixing and combustion air to said air introducing
means.
12. An arrangement according to claim 10, wherein said means
extending across said annular opening includes a plurality of
cylindrical inlet tubes extending from said annular space across
said annular opening inwardly into said combustion chamber
space.
13. An arrangement according to claim 10, wherein said means
extending across said annular opening includes a plurality of
part-cylindrical rib means extending from openings leading from
said annular space and across said annular opening.
14. An arrangement according to claim 11, wherein said air
introducing means includes third air inlet means for introducing
air into said combustion chamber space, said third air inlet means
including a plurality of openings in said flame tube means which
communicate with said annular space and said combustion chamber
space at a position downstream of said first and second air inlet
means.
15. An arrangement according to claim 11, wherein said end wall is
formed by an extension of said outer casing.
Description
These and other objects, features and advantages of the present
invention will become more apparent from the following description
when taken in conjunction with the accompanying drawing which
shows, for purposes of illustration only, two embodiments in
accordance with the present invention, and wherein:
FIG. 1 is a longitudinal sectional view of a reverse flow
combustion chamber incorporating a flameholder;
FIG. 2 is a cross-section taken along line A - B of FIG. 1, and
FIG. 3 is a modified embodiment for the cross-section taken along
line A - B of FIG. 1.
Referring now to the drawing wherein like reference numerals are
used throughout the various views, and more particularly to FIG. 1,
this figure illustrates the invention in connection with a reverse
flow combustion chamber whose outer casing terminates at the
right-hand portion of the drawing, in a flameholder 2 with the fuel
injection nozzle 3 installed in its center. The outer casing 1
houses coaxially to its longitudinal axis 4 the flame tube 5 which
terminates, in the right-hand portion of the drawing, between the
outer casing 1 and the flameholder 2, in a rim-like or bulge-like
deflector 6 which produces a favorable flow reversing section 7 for
the primary air duct. Secondary air is supplied through air inlet
ports 8 of circular area.
The primary air enters through the primary air reversing duct 7 in
the direction of arrow E (downstream direction with respect to the
flow of combustion chamber products) between the flameholder 2 and
the flame tube 5 into the primary zone 9 of the combustion chamber,
producing the reverse flow zone 10 in which the fuel 11 injected by
the fuel injector nozzle 3 is combusted.
Air flows radially inwardly through the air inlet openings 12
proposed by the invention, in the direction of arrows F (upstream
direction with respect to the combustion chamber flow) towards the
discharge tip of the fuel injector nozzle 3, i.e., toward the point
of fuel discharge. The air inlet openings 12 are arranged at the
level of the conically flaring rear wall 15 of the combustion
chamber formed by flameholder 2. Any deflection of the airstreams
from the direction of arrows F under the influence of the primary
air inlet stream in the direction of arrow E will be prevented by
tubes 13 (FIGS. 1 and 2) and/or ribs 14 (FIG. 3) suitably welded
into the flame tube 5.
The tubes 13 and the ribs 14 further assist the directional flow of
the air towards the discharge tip of the fuel injector nozzle 3 by
their radially inward arrangement inclined in the direction of the
fuel injector nozzle 3. The invention can also be applied to
annular combustion chambers as well as to combustion chambers
having an annular outer casing housing several individual
combustion chambers.
While I have shown and described only two embodiments of the
present invention, it is understood that the latter is not limited
thereto but is susceptible of numerous changes and modifications as
known to those skilled in the art, and I therefore do not wish to
be limited to these details as shown and described but intend to
cover all such changes and modifications as are encompassed by the
scope of the appended claims. It is further noted that the terms
upstream and downstream refer to the direction of flow of
combustion chamber products in the flame tube, both in the
specification and in the claims.
* * * * *