U.S. patent number 3,832,086 [Application Number 05/351,622] was granted by the patent office on 1974-08-27 for particle separator with scroll scavenging means.
This patent grant is currently assigned to General Electric Company. Invention is credited to Thomas Neil Hull, Jr., James Leroy Nye.
United States Patent |
3,832,086 |
Hull, Jr. , et al. |
August 27, 1974 |
PARTICLE SEPARATOR WITH SCROLL SCAVENGING MEANS
Abstract
A particle separator for removing extraneous matter from the
inlet flow to the compressor of a gas turbine engine has improved
efficiency provided by a scroll type of scavenging means. The
scroll scavenging means provides for removal of the particles from
the collection chamber of the separator and limits the
circumferential travel of the particles within the collection
chamber before removal, so as to reduce the likelihood that the
particles will be rebounded back out into the engine inlet. The
invention herein described was made in the course of or under a
contract or subcontract thereunder, (or grant) with the Department
of the Army.
Inventors: |
Hull, Jr.; Thomas Neil
(Marblehead, MA), Nye; James Leroy (Marblehead, MA) |
Assignee: |
General Electric Company (Lynn,
MA)
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Family
ID: |
26896729 |
Appl.
No.: |
05/351,622 |
Filed: |
April 16, 1973 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
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201421 |
Nov 23, 1971 |
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Current U.S.
Class: |
415/121.2;
55/306; 137/15.1; 60/39.091 |
Current CPC
Class: |
F02C
7/052 (20130101); B04C 3/06 (20130101); Y10T
137/0536 (20150401) |
Current International
Class: |
B04C
3/00 (20060101); B04C 3/06 (20060101); F02C
7/04 (20060101); F02C 7/052 (20060101); B04b
001/04 (); F04d 029/00 () |
Field of
Search: |
;60/39.9P ;137/15.1
;55/306,396,397,399,456,457 ;415/121G |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Raduazo; Henry F.
Parent Case Text
CROSS REFERENCES TO RELATED APPLICATIONS
This application is a continuation of Application Ser. No. 201,421
filed Nov. 23, 1971 now abandoned.
Claims
What is claimed is:
1. In a gas turbine engine assembly wherein an improved engine
inlet particle separator includes a pair of spaced apart wall
members defining an annular inlet and an annular outlet for
communication with the engine inlet, wall means defining a
collection chamber in flow communication with the annular
passageway for receiving and removing extraneous matter from the
stream of air supplied to the engine inlet through the passageway
and means for centrifuging the extraneous matter out of the air
stream within the passageway into the collection chamber, the
improvement comprising:
scroll scavenging means having a plurality of turning vanes with
the leading edge of each vane spaced upstream of the trailing edge
of an adjacent vane to divide the collection chamber and define an
annular extraction manifold at the downstream portion thereof
thereby reducing the likelihood that particles of extraneous matter
entrained within the extraction manifold are rebounded back into
the passageway, whereby all particles entering the collection
chamber may be inhibited from rebound back into the passageway
after only limited circumferential travel around the collection
chamber, and
means for continuously ducting extraneous matter from the
extraction manifold including a blower for establishing a vacuum
within the extraction manifold and drawing out the extraneous
matter entrained within the manifold.
2. The improved inlet separator of claim 1 wherein the wall means
defining the collection chamber includes spaced apart inner and
outer generally axially extending circumferential wall members and
an interconnecting wall member, and the plurality of turning vanes
extend radially from the inner wall member to the outer wall member
with the leading edge of each vane spaced axially forward of the
trailing edge of an adjacent vane, thereby dividing the collection
chamber so as to define the annular extraction manifold at the aft
portion thereof.
3. The improved inlet separator of claim 1 wherein the scroll
scavenging means comprises:
a plurality of axially extending turning vanes with the leading
edge of each vane spaced radially inward of the trailing edge of an
adjacent vane thereby dividing the collection chamber and, in
combination with the outer wall of the collection chamber, defining
the annular extraction manifold.
4. An improved particle separator for removing extraneous matter
from a fluid stream comprises:
means forming an axially extending passageway having an inlet and
an outlet at opposing ends thereof;
wall means defining a collection chamber around the passageway in
flow communication with the passageway for receiving and removing
extraneous matter from a fluid stream flowing through said
passageway;
means adjacent said inlet for imparting swirl to the fluid stream
flowing through said passageway whereby extraneous matter is
centrifuged out of the fluid stream into the collection chamber,
and
scroll scavenging means having a plurality of turning vanes with
the leading edge of each vane spaced upstream of the trailing edge
of an adjacent vane to divide the collection chamber and define an
annular extraction manifold at the downstream portion thereof
thereby reducing the likelihood that particles of extraneous matter
entrained within the, extraction manifold are rebounded back into
the passageway, whereby all particles entering the collection
chamber may be inhibited from rebound back into the passageway
after only limited travel around the collection chamber,
and means for continuously ducting extraneous matter from the
extraction manifold including a blower for establishing a vacuum
within the extraction manifold and drawing out the extraneous
matter entrained within the manifold.
5. The improved particle separator of claim 4 wherein the wall
means defining the collection chamber includes spaced apart inner
and outer generally axially extending circumferential wall members
and an interconnecting wall member, and the scroll scavenging means
includes a plurality of turning vanes which radially extend from
the inner wall member to the outer wall member with the leading
edge of each vane spaced axially forward of the trailing edge of an
adjacent vane thereby dividing the collection chamber so as to
define the annular extraction manifold at the aft portion
thereof.
6. The improved inlet separator of claim 3 wherein the scroll
scavenging means comprises:
a plurality of axially extending turning vanes with the leading
edge of each vane spaced radially inward of the trailing edge of an
adjacent vane thereby dividing the collection chamber and, in
combination with the outer wall of the collection chamber, defining
the annular extraction manifold.
Description
BACKGROUND OF THE INVENTION
This invention generally relates to an improved engine inlet
particle separator, and more particularly to an improved inlet
particle separator for use with a gas turbine engine wherein the
improvement comprises a scroll scavenging means disposed within the
collection chamber of the particle separator for reducing the
likelihood that particles of extraneous matter entrained within the
collection chamber are rebounded back into the engine inlet.
Aircraft gas turbine engines are particularly susceptible to damage
from foreign objects introduced into the air inlets of the engines.
This problem has been most acute in the past with respect to
relatively large foreign objects such as stones, gravel, birds,
hail and the like. With the advent of gas turbine powered
helicopters and other vehicle take-off and landing (VTOL) aircraft,
smaller particles of foreign matter such as sand and water have
become increasingly troublesome due primarily to the conditions
under which such aircraft may be operated. Because of its VTOL
capability, this type of aircraft may be utilized in areas where
conventional airfields are nonexistent, such as in combat zones,
and in other isolated areas. Helicopters and other VTOL aircraft
are also especially suited for certain low altitude missions on
both land and sea, including close combat support, search and
rescue, and anti-submarine warfare. Under these and related
conditions, substantial quantities of small foreign objects such as
sand and dust particles and droplets of water may become entrained
in the air stream supplied to the gas turbine engine. These
particles, which individually have little effect on the engine, can
cause very substantial damage when introduced into the engine in
large quantities. For example, it has been found that the engine of
a helicopter operating at low altitude in a desert environment can
lose performance rapidly due to erosion of the engine blading by
high velocity particles. In addition to erosion, extraneous matter,
particularly salt water, introduced into the engine in this manner
can cause rapid and destructive erosion.
It is, therefore, desirable to provide means for separating out the
particles of sand, dust, water and the like before the air stream
is supplied to the engine. To be satisfactory, it is essential that
the separator chosen to provide this function be effective in
removing the unwanted particles from the air stream. High
efficiency is particularly desirable in an aircraft separator in
view of the large quantities of air and, consequently, the large
quantities of extraneous particles consumed by a gas turbine
engine.
Heretofore, particle separators have included collection chambers
which either retained the extraneous matter until the engine was
shut down, whereupon the particles were removed through a clean-out
port by means of a vacuum hose, or alternatively removed the
particles during engine operation through a single outlet port.
Retaining particles of extraneous matter within the collection
chamber of the separator during engine operation is disadvantageous
due to the likelihood that particles striking the walls of the
collection chamber will eventually be rebounded back into the
passageway and hence into the engine inlet. Also, the collection
chamber of the separator may fill and overflow into the passageway.
Removal of the particles from the collection chamber through a
single outlet during engine operation eliminates the possibility of
the collection chamber overflowing, but still retains the risk that
particles might rebound back into the passageway before passing
through the outlet port. The likelihood of particles rebounding
back into the passageway increases with the circumferential
distance that the particles must travel before exiting through the
outlet port. In conventional separators, many of the particles must
travel entirely around the collection chamber before being
evacuated through the outlet port which increases the probability
that the particles will strike an interior surface and rebound back
into the passageway.
Therefore, it is an object of this invention to provide an improved
engine inlet separator wherein separator efficiency is materially
increased by reducing the risk that particles entrained within the
collection chamber of the separator will be rebounded back into the
engine inlet.
It is also an object of this invention to provide an improved
engine inlet separator wherein the risk of entrained particles
rebounding back out of the collection chamber is reduced by
limiting the circumferential distance which the particles need
travel before evacuation from the chamber.
It is a further object of this invention to provide an improved
engine inlet separator having a scroll type of scavenging means
communicating with the collection chamber of the separator so as to
limit the circumferential distance traveled by the particles before
evacuation from the chamber.
SUMMARY OF THE INVENTION
A gas turbine engine assembly includes an improved engine inlet
particle separator for removing extraneous matter from the stream
of air supplied to the compressor. The particle separator includes
a pair of spaced apart walls which define an annular passageway
therebetween, having at opposite ends thereof, an annular inlet and
an annular outlet for flow communication with the engine inlet.
Additional wall means define a collection chamber in flow
communication with the annular passageway for receiving and
removing extraneous matter from the stream of air supplied to the
engine inlet through the passageway. Means for centrifuging the
extraneous matter out of the air stream within the passageway into
the collection chamber are also provided. The improvement comprises
a scroll scavenging means communicating with the collection chamber
for reducing the likelihood that particles of extraneous matter
entrained within the collection chamber are rebounded back into the
passageway. The scroll scavenging means acts to inhibit particles
which enter the collection chamber from rebounding back into the
passageway by limiting the circumferential travel of the particles
around the collection chamber.
DESCRIPTION OF THE DRAWINGS
While the specification concludes with claims distinctly claiming
and particularly pointing out the invention described herein, it is
believed that the invention will be more readily understood by
reference to the discussion below and the accompanying drawings in
which:
FIG. 1 is a cutaway perspective view of the improved particle
separator of this invention as attached to the inlet of a gas
turbine engine.
FIG. 2 is a cross-sectional view of an alternate embodiment of the
separator of FIG. 1 as attached to the inlet of a gas turbine
engine.
FIG. 3 is a cross-sectional view taken along the line 3--3 of FIG.
2.
FIG. 4 is a cross-sectional view of still another alternate
embodiment of the separator of FIG. 1.
DESCRIPTION OF THE PREFERRED EMBODIMENT
Referring to FIG. 1 there is shown the inlet portion of a gas
turbine engine assembly 10 including a gas turbine engine inlet 12
and an axial flow separator 14 having improved scroll scavenging
means 16 formed in accordance with the present invention. The
engine, of which only the inlet portion is shown, typically
includes in axially spaced serial flow arrangement, a compressor,
an annular combustor, a gas generator turbine for driving the
compressor and a power turbine for driving an output shaft, all of
which are conventional and well known to the gas turbine art. The
turboshaft engine described may be suited for helicopter
applications in which a helicopter rotor (not shown) is driven by
the output shaft through suitable speed reduction means (not
shown).
The improved separator of this invention is a static component
having no moving parts. More particularly, the separator 14 has an
outer casing or housing indicated generally by the numeral 18 and
an inner fairing 20, defining therebetween an axially extending
annular passageway 22 having at opposite ends thereof an annular
inlet 24 and an annular outlet communicating with the engine inlet
12 and an annular particle collection chamber 26. A row of
circumferentially spaced, radially extending turning vanes 27,
having a desired turning configuration which will be described
presently, is located adjacent the annular inlet 24. Another row of
circumferentially spaced, radially extending, compressor inlet
guide vanes 28 is located adjacent the engine inlet 12, the vanes
28 also having a required turning configuration. The annular
particle collection chamber 26 is defined by the outer surface of
the engine housing 30, a first axially and circumferentially
extending wall 32, a second radially and circumferentially
extending wall 34, and a third radially and circumferentially
extending wall 36 connecting with the separator housing 18 so as to
form a radially outward extending gutter.
The improved scroll scavenging means includes a plurality of
circumferentially spaced turning vanes 38 which radially extend
from the engine housing 30 to the axially and circumferentially
extending wall 32. The vanes 38 axially divide the particle
collection chamber 26 and define an annular extraction manifold 40
at the aft portion of the collection chamber. Means for ducting
extraneous matter from the extraction manifold 40 is provided by a
scavenge duct 42 which cummunicates with the manifold, and
preferably extends in a tangential direction away from the outer
periphery of the extraction manifold 40. The outside end of the
scavenge duct is in flow communication with a scavenge blower (not
shown) for establishing a reduced pressure within the duct, and
drawing out extraneous matter entrained within the annular
manifold.
During operation of the gas turbine engine, the low pressure area
existing at the inlet 12 of the engine causes air to flow through
the annular passageway 22 at high velocity. As the air passes over
the stationary turning vanes 27, it is turned or centrifuged
circumferentially such that downstream of the vanes 27 the air
stream has both angular and axial velocity. This is known as
imparting "swirl" to the fluid stream. Small particles of foreign
matter entrained in the air stream are also centrifuged, this
centrifuging resulting primarily from the particles, which have
small mass, being carried along with the swirling air. To assure
that particles having greater mass are also centrifuged by the
turning vanes, it may be desirable to overlap adjacent vanes
circumferentially so that a particle cannot pass axially between
adjacent vanes without striking a vane and thereby being turned. A
particle entrained in the air stream and centrifuged will have both
tangential and axial velocity downstream of the turning vanes 27.
In theory, a particle leaving the vanes 27 with both tangential and
axial velocity, and not being subject to any external forces, will
follow a straight line path to the outer periphery of passageway 22
at some point downstream of the vanes. In practice, however, the
swirling air has a significant effect on the particle's trajectory
which can be compared roughly to that of a helix having increasing
diameter in the downstream direction. The compressor inlet guide
vanes 28 may be configured as deswirl vanes to remove the
circumferential velocity component of the main air stream before
entering the compressor.
In the preferred practice of the present invention, the turning
vanes 27 have a turning configuration which will cause the
entrained extraneous matter to reach the outer periphery of the
passageway 22 upstream of the engine housing 30, and either flow
directly into the collection chamber 26 or strike the interior
surface of the separator housing 18 and rebound therefrom into the
chamber 26. Once the particles enter the chamber 26, they are
prevented from rebounding back into the passageway 22 by
entrainment through the turning vanes 38, and into the extraction
manifold from which the particles are scavenged through the duct 42
by means of a blower. Turning vanes 38 are arranged to maintain the
same circumferential direction of flow initially imparted to the
input air stream by turning vanes 27. To assure that particles do
not rebound from the extraction manifold 40 back into the
passageway and hence to the engine inlet, turning vanes 38 may also
be overlapped circumferentially so that a particle cannot pass
axially between adjacent vanes without striking a vane and thereby
rebounding back into the manifold. It has been found that the
scroll scavenging means of this invention provides significantly
improved separator efficiency to the extent that particles entering
the engine passage have been reduced from 20 percent to 12 percent
of the total mass of particles entering the separator inlet when
using standard AC coarse test dust.
The turning vanes of the scroll scavenging means of this invention
limit the circumferential distance which particles must travel
before entrainment within the manifold 40 so as to reduce the
likelihood that the particles will rebound back into the engine
inlet. As becomes readily obvious from the drawings, once a
particle travels aft of the turning vanes into the extraction
manifold, nearly all possible rebound paths back into the engine
inlet are blocked by the turning vanes. For the configuration of
FIG. 1 showing three turning vanes each of which extends an arcuate
distance of approximately 120.degree., it can be seen that no
particle need travel more than a cirumferential distance of
120.degree. before entering the extraction manifold from which the
likelihood of rebound back into the engine inlet is substantially
reduced. The intended scope of invention is by no means limited to
the number of turning vanes shown and the scroll scavenging means
may include any number of turning vanes as required to meet a
particular separator efficiency.
Referring to FIGS. 2 and 3 where like numerals refer to previously
described elements, there is shown generally at 16' an alternate
embodiment for the scroll scavenging means of this invention. A
plurality of circumferentially spaced and radially extending inlet
openings 50 are disposed around the outer periphery of the
collection chamber 26. Each opening 50 communicates with a scavenge
duct 52 wherein the outside end of each scavenge duct is in flow
communication with a scavenge blower (not shown) for establishing a
vacuum within the duct and drawing out extraneous matter entrained
within the collection chamber. Each scavenge duct is defined by a
circumferentially extending inner wall 54 and a circumferentially
extending outer wall 56 wherein each inner wall gradually extends
radially outward from the inlet opening to the outer wall of the
adjacent duct. The walls of each duct may be either curvilinear or
rectilinear in cross-section, and are not particularly limited, so
long as an enclosed fluid passageway is defined therebetween for
drawing out particles entrained within the collection
passageway.
For the arrangement of FIGS. 2 and 3, showing three openings, each
of which is circumferentially spaced approximately 120.degree.
apart, it can be seen that no particle entrained within the
collection chamber need travel more than a circumferential distance
of 120.degree. before entering a scavenge duct from which the
likelihood of rebound back into the engine inlet is substantially
reduced. Again the intended scope of invention is by no means
limited to the number of openings and the scroll scavenging means
may include any number of openings as required to meet a particular
separator efficiency.
FIG. 4 shows generally at 16" still another embodiment for the
scroll scavenging means of this invention whereby circumferentially
spaced, axially extending, turning vanes 60 are provided instead of
openings 50 as shown in FIGS. 2 and 3. The turning vanes 60 in
combination with the outside axially and circumferentially
extending wall 32 define an annular extraction manifold 62
therebetween, which functions in substantially the same manner as
previously described. Again particles entering the colletion
chamber need only travel a limited circumferential distance before
passing radially outward into the extraction manifold from which
the likelihood of rebound back into the engine inlet is
substantially reduced.
Having above described preferred embodiments of the invention
though not exhaustive of all possible equivalents, what is desired
to be secured by Letters Patent is distinctly claimed and
particularly pointed out in the claims appearing below.
* * * * *