U.S. patent number 3,604,818 [Application Number 04/883,819] was granted by the patent office on 1971-09-14 for centrifugal compressor diffuser.
This patent grant is currently assigned to Avco Corporation. Invention is credited to Val Cronstedt, Gary M. Gron.
United States Patent |
3,604,818 |
Cronstedt , et al. |
September 14, 1971 |
CENTRIFUGAL COMPRESSOR DIFFUSER
Abstract
The disclosure illustrates an annular diffuser assembly that
receives gas discharged from a compressor impeller at supersonic
velocity. The diffuser consists of a series of passages extending
in a direction generally tangential to the impeller and spaced
around the impeller so that their inlet ends intersect. The
passageways each have a straight-sided polygon cross-sectional
shape so that the diffuser passages have a series of generally
V-shaped entrances. The diffuser passages may be formed with a
particular cross-sectional shape to compensate for the variations
in velocity of the airstream discharged from the impeller. The
passageways may be formed from intersecting tubular elements or may
be formed in opposing faces of a pair of sandwiched discs.
Inventors: |
Cronstedt; Val (Williamsport,
PA), Gron; Gary M. (Cincinnati, OH) |
Assignee: |
Avco Corporation (Williamsport,
PA)
|
Family
ID: |
25383388 |
Appl.
No.: |
04/883,819 |
Filed: |
December 10, 1969 |
Current U.S.
Class: |
415/207;
415/208.3 |
Current CPC
Class: |
F04D
29/441 (20130101); F04D 21/00 (20130101) |
Current International
Class: |
F04D
29/44 (20060101); F04D 21/00 (20060101); F04d
001/00 (); F04d 017/08 (); F04d 029/00 () |
Field of
Search: |
;415/211,207,204,206 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Raduazo; Henry F.
Claims
We claim:
1. In a centrifugal compressor, a diffuser receiving air from the
periphery of a circular impeller, said diffuser comprising:
means for forming around the periphery of said impeller a plurality
of identical spaced diffuser passageways intersecting adjacent
their inlet ends and extending generally tangentially from the
periphery of said impeller;
said passageways having a straight sided polygon cross-sectional
shape symmetrical about diagonal line that extends through the
median axis of and defines the height of said passageways, said
diagonal line being parallel to the axis of rotation of said
impeller;
each of said passageways having at least two walls on either side
of said diagonal line intersection at corners defining the width of
said passageways, the walls of adjacent passageways intersecting so
that adjacent corners intersect to form the apex of V-shaped
entrance wedges between adjacent passageways.
2. Apparatus as in claim 1 wherein said passageways are square in
cross-sectional shape and have one diagonal thereof parallel to the
axis of rotation of said impeller.
3. Apparatus as in claim 1 wherein said diffuser passageway means
comprises a plurality of intersecting tubular elements extending
from an annular plate surrounding said impeller.
4. Apparatus as in claim 1 in combination with an impeller
wherein:
said impeller comprises a plurality of radial blades extending in
an axial direction from a disc toward a fixed annular shroud, the
velocity distribution of the fluid flow from said impeller being
biased toward said disc;
said diffuser passageways each have a four-sided polygon
cross-sectional shape symmetrical about said diagonal defining the
height of said passageways, said diagonal being parallel to the
axis of rotation of said impeller;
the walls of said passageway extending from said diagonal to apexes
defining the width of said passageways, the apexes being positioned
from the midpoint of the passageway height toward the disc of said
impeller;
whereby the generally V-shaped entrances to said passageways have
their most downstream point positioned to accommodate the biased
distribution of fluid flow from said impeller.
5. Apparatus as in claim 1 wherein said diffuser passageway means
comprises:
a pair of sandwiched discs, each having an interior hole for
surrounding the periphery of said impeller and grooves in opposing
faces of the discs extending from the interior hole to the exterior
of said disc, the grooves in each disc shaped to define said
diffuser passageways when said discs are sandwiched together.
6. Apparatus as in claim 5 wherein:
The inlet end of said passageways is generally square in
cross-sectional shape and has one of its diagonals defining the
height of said passageway, said diagonal being parallel to the axis
of rotation of said impeller;
the downstream portion of said passageways is of equal height with
the inlet ends and has a pair of parallel sides normal to said
diagonal and having diverging edges;
whereby divergent passageways are formed in the downstream end of
said diffuser.
Description
The present invention relates to essentially radial outflow
centrifugal compressor diffusers and more particularly to diffusers
adapted to receive supersonic flow.
In recent years the centrifugal supersonic compressor has been used
for gas turbine engines because if is mechanically simple and
produces substantial pressure increases necessary for high
performance. The adoption of compressors of this type has prompted
a substantial amount of development work in the area of diffusers
which are particularly adapted to receive a supersonic gas flow
discharged from a rotating impeller.
One result of this development has been the patent to Vrana, U.S.
Pat. No. 3,333,762, entitled "Diffuser for Centrifugal Compressor."
In that patent a diffuser is formed by a series of curvilinearly
enclosed passages surrounding an impeller. These passages are
closely spaced so that their inlet ends form a vaneless diffuser
space adjacent the periphery of the impeller and a series of
scalloped leading edges to the passages. This type of diffuser
offers significant advantages in producing high pressure rises at
high efficiency.
The above diffuser is manufactured by machining a series of holes
around the periphery of a blank which would appear to be a
relatively simple manufacturing process.
An object of the present invention is to provide a diffuser of the
above general type which has a configuration also making it capable
of highly simplified, economical and accurate manufacture.
In the broader aspects of the present invention the above ends are
achieved by providing a diffuser which comprises a means for
forming a plurality of diffuser passageways extending generally
tangentially from the periphery of an impeller surrounded by the
diffuser passageways. The passage ways are spaced from one another
around the periphery of the impeller so that they intersect each
other at their inlet ends. The passageways have straight-sided
polygon cross-sectional shapes that form generally V-shaped
entrances to the diffuser passageways.
The above and other related objects and features of the present
invention will be apparent from a reading of the description of the
disclosure shown in the accompanying drawings and the novelty
thereof pointed out in the appended claims.
IN THE DRAWINGS:
FIG. 1 is a transverse cross-sectional view of a centrifugal
compressor with a diffuser embodying the present invention;
FIG. 2 is a view taken on lines 2--2 of FIG. 1;
FIG. 3 is a fragmentary view of FIG. 1 taken on lines 3--3 of FIG.
1;
FIG. 4 is a cross-sectional view of a passageway that is
incorporated in a diffuser embodying the present invention;
FIG. 5 is a longitudinal section view of the passageway in FIG. 4
illustrating the shape of the generally V-shaped inlet wedge which
results when the passageway of FIG. 4 intersects an adjacent
passageway;
FIG. 6 is a transverse view of another diffuser illustrating an
alternate embodiment of the present invention;
FIG. 7 is a view taken on lines 7--7 of FIG. 6.
Referring particularly to FIGS. 1, 2 and 3, there is shown a
compressor including an impeller 10 mounted on a shaft 12. The
shaft 12 may receive a rotating input from a suitable source, such
as a turbine wheel of a gas turbine engine. A series of radial
blades 14 extend axially from the disc 10 towards a fixed annular
shroud 16. When the compressor is incorporated in a gas turbine
engine the shroud 16 may form, in part, the outer casing for the
engine.
An annular ring 20 surrounding the periphery of the impeller blades
is attached to flange 18. A series of tubular passageways,
generally indicated by reference character 22, extend from the
annular ring 20 in a direction generally tangential to the
periphery 15 of the impeller. The passageways 22 are spaced around
the periphery of the ring 20 so that they intersect one another
adjacent their inlet ends 24. The tubular passageways 22 may be
secured to the ring 20 and to each other by welding, as
illustrated.
As shown in FIG. 2, the inlet portions of the passageways 24 have a
straight-sided polygon cross-sectional shape. This results in
generally straight V-shaped entrances 26 to the plurality of
diffuser passageways around the periphery (see FIG. 3). For
supersonic flow into the diffuser it is desirable that the inlet
portions 24 be of constant cross-sectional area and that the
downstream portions 28 and 30 be divergent to diffuse the air
flowing therethrough.
As illustrated in FIG. 2, the straight-sided polygon
cross-sectional shape of the passages 22 is in the form of a square
having one diagonal d parallel to the axis of rotation of the
impeller disc 10. As illustrated in the specification and in the
claims, the diagonal d defines the height of the passageways and
the distance of the walls from the diagonal d determines the width
of the particular passageways.
It has been found that the flow discharged from the impeller blades
14 varies in velocity and direction along the axial termination of
the impeller blades 14. The fixed shroud 16 creates a boundary
layer which substantially reduces the radial velocity of the air
immediately adjacent its surface. The air towards the center of the
blades 14 has a greater velocity and the air adjacent the surface
of the impeller disc 10 is reduced due to another boundary layer.
However, its reduction is not as great because the impeller 10 is
rotating with the stream. The result of this is that the velocity
distribution of air across the axial extent of the blades 14 is
biased towards the disc of the impeller 10. This biasing of the
velocity across the axial extent of the impeller blades also causes
a variation in the direction of the velocity vectors across the
axial termination of the impeller blades 14.
The passageway cross-sectional shape shown in FIG. 4 is
particularly adapted to conform to the above velocity distribution.
The passageway inlet 24' is a four-sided polygon symmetrical about
a diagonal d' which is parallel to the axis of rotation of impeller
10 and which defines the height h of the passageway. The sidewalls
32 and 34 are symmetrical about the diagonal d' and extend towards
apexes 36 which define the width w of the passageways.
The apexes 36 are positioned towards the bottom side 38 of the
passageway which is adjacent the periphery of the impeller disc 10.
When a plurality of these passageways are positioned around the
periphery of the impeller, as in FIG. 1, a series of generally
V-shaped entrances 26' are formed, as shown in FIG. 5. It is
apparent that these inlet edges 26' have a downstream point 40
which is positioned towards the bottom wall 38 of the passageway
24'. This particular shape conforms approximately to the velocity
and flow distribution of the air discharged from the impeller.
The straight-sided polygon cross-sectional shape of the diffuser
passageways 22 and 22' enables a substantial degree of simplicity
in their manufacture. As shown in FIG. 1, the passageways may be
formed from tubular elements welded or brazed to one another at
their points of intersection and secured as by welding to the inner
ring 20. In addition to being manufactured out of tubular stock, a
diffuser may be fabricated as illustrated in FIGS. 6 and 7.
In these figures the diffuser comprises a pair of annular discs 44
(only one of which is shown in FIG. 6) which have a circular outer
periphery 46 and an inner hole 48 which surrounds the periphery of
the impeller blades 14'. Each of the discs 44 has a series of
grooves, generally referred to by reference characters 50, formed
in one of their faces. These grooves define one half of the
diffuser passageway and when the discs 44 are sandwiched together,
as shown in FIG. 7, the opposing grooves 50 define the diffuser
passageway.
As particularly illustrated in FIGS. 6 and 7, the passageways have
a square cross-sectional shape at their inlet ends 52. Downstream
from the inlet section 52, walls 54 and 56 diverge from one another
but have the same angular relationship as the walls in the inlet
sections 52. As a result, a passageway of equal height is formed
and the increasing flow area is provided for through top and bottom
walls 58 having diverging edges. This feature is even more
emphasized in the outlet end of the passageway having the sidewalls
60 and 62 and top and bottom walls 64.
Thus it is apparent that the increase in cross-sectional area of
the individual passageways may be accomplished without an increase
in the axial dimension of the diffuser. This has two advantages,
the first of which is that it provides an extremely compact
diffuser assembly and the second of which is that it utilizes more
of the annular space within the disks 44 thereby reducing their
cost.
The forming of the straight grooves 50 and the opposite discs 44
enables the use of highly accurate and automated machines which are
capable of producing in a rapid fashion passageways of highly
accurate dimensions. This enables a significant reduction in the
cost of the diffuser.
Because the diffuser passageways have straight sides they lend
themselves to inexpensive manufacture. This manufacturing advantage
is achieved while at the same time providing a diffuser with flow
paths that will provide a high level of performance. In addition,
the straight-sided passageways enable the selection of V-shaped
entrance edges which accept the biased velocity distribution from a
supersonic impeller. Furthermore, the passageways may be formed
with diverging downstream portions without increasing the axial
dimension of the impeller.
While the preferred embodiment of the present invention has been
described, it is apparent that those skilled in the art may employ
diffusers other than those specifically shown without departing
from the spirit of the present invention. Therefore, its scope
should be determined solely by the appended claims.
* * * * *