U.S. patent number 3,689,178 [Application Number 05/091,869] was granted by the patent office on 1972-09-05 for apparatus for protection of rotor vanes against surface erosion caused by impingement of high speed liquid drops.
This patent grant is currently assigned to Aktiengesellschaft Brown. Invention is credited to Carlo Maggi, Guy Faber.
United States Patent |
3,689,178 |
|
September 5, 1972 |
APPARATUS FOR PROTECTION OF ROTOR VANES AGAINST SURFACE EROSION
CAUSED BY IMPINGEMENT OF HIGH SPEED LIQUID DROPS
Abstract
The surface of a structural part such as for example the leading
edge portion of a turbine vane or airplane wing is protected
against erosion which would otherwise be caused by impingement of
high speed liquid drops thereon by positioning an array of flexible
baffles in front of the surface. These baffles which are slightly
spaced from the surface of the vane or wing serve to intercept the
liquid drops resulting in a division thereof into smaller drops
which are simultaneously decelerated as a result of flexation of
the baffles.
Inventors: |
Guy Faber (Oberrohrdorf,
CH), Carlo Maggi (Baden, CH) |
Assignee: |
Aktiengesellschaft Brown
(Boveri & Cie, Baden)
|
Family
ID: |
4437164 |
Appl.
No.: |
05/091,869 |
Filed: |
November 23, 1970 |
Foreign Application Priority Data
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Dec 23, 1969 [CH] |
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19070/69 |
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Current U.S.
Class: |
416/224;
416/228 |
Current CPC
Class: |
B64C
3/26 (20130101); F01D 5/286 (20130101); F01D
5/288 (20130101); F01D 25/32 (20130101); F01D
5/141 (20130101); Y02T 50/60 (20130101); Y02T
50/671 (20130101); Y02T 50/673 (20130101) |
Current International
Class: |
F01D
25/00 (20060101); B64C 3/00 (20060101); B64C
3/26 (20060101); F01D 5/14 (20060101); F01D
25/32 (20060101); F01D 5/28 (20060101); F01d
005/28 () |
Field of
Search: |
;416/62,224,228
;415/168 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
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311010 |
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Feb 1, 1919 |
|
DE (Pre-1945) |
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233693 |
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Jul 1, 1969 |
|
Soviet Union |
|
Primary Examiner: Everette A. Powell, Jr.
Attorney, Agent or Firm: Pierce, Scheffler & Parker
Claims
We claim:
1. A device for protecting the vanes of a rotor against surface
erosion caused by impingement of liquid drops thereon at high speed
which comprises an array of thin flexible baffles positioned in
front of and spaced from the surface of each vane, said baffles
serving to intercept and decelerate the droplets prior to striking
the vane surface as a result of flexation of said baffles, and said
baffles also serving to divide the droplets into smaller masses,
thereby to reduce their impact force upon the vane surface.
2. A device as defined in claim 1 for protecting the vanes of a
rotor against surface erosion wherein said baffles are constituted
by an array of parallel spaced thin flexible wires enveloping the
leading edge portion of the vane and extending in a radially
outward direction, said wires being spaced from the vane surface
and being secured thereto only at their ends.
3. A device as defined in claim 2 for protecting the vanes of a
rotor against surface erosion wherein said wires are tapered in the
radially outward direction.
4. A device as defined in claim 1 for protecting the vanes of a
rotor against surface erosion wherein said baffles are constituted
by the wires of a thin flexible wire grid, said grid enveloping the
leading edge portion of the vane and being secured thereto in
spaced relation.
Description
This invention relates to an improved device for the protection of
the vanes of a rotor against erosion which are imperiled by liquid
drops impinging thereon at high speed.
When liquid drops impinge on metals or other materials at very high
speeds, they cause erosion, that is, small particles of material
break off after a certain time. The erosion effect depends mainly
on the speed of impingement of the drops, their diameter, the angle
of incidence on the surface of the structural part, and the
specific properties of the eroding material. Due to the removal,
the surface first becomes rough, then peaks opposed to the
impinging drops form, which are now removed more slowly but
continue to be removed. The friction losses of a flow along such
eroded surfaces are correspondingly great.
Low pressure vanes on steam turbines, running temporarily or
permanently in the saturated steam zone, are very susceptible to
erosion. Especially the radially external portion of the entrance
edge may be eroded intensively, and this leads to a loss of
efficiency. It should be taken into consideration also that eroded
vanes can hardly be repaired.
For protection against erosion, therefore, steam turbine vanes are
produced either of an erosionproof material, e.g. hardened 12
percent chromium steel, or they are provided at the entrance edge
with a soldered on hard metal plate (stellite). When using titanium
or plastic vanes, hardening is not possible. The application of
stellite shields involves difficulties in the case of titanium
vanes because of the temperature influences during brazing, and in
the case of plastic vanes because of the weight. Also, in the case
of stellites, the properties of a material determinant for the
erosion resistance, namely strength combined with toughness, can
hardly be increased any further, so that at increased
circumferential speeds greater erosions are to be expected even
with stellites.
When airplanes fly through rain clouds at supersonic speed, the
wing noses are so intensively eroded by the rain drops that already
after several times the planking consisting of a light metal alloy
must be exchanged. The only remedy is seen in increasing the
erosion resistance of the metals used.
The principal object underlying the present invention is to protect
against the erosion of structural parts endangered by drop impact
without having to subject the material to a special treatment and
without having to replace it in the specially affected areas by a
more erosion-resistant material.
This problem is solved according to the invention in that the drops
are divided and, at the same time, decelerated before they impinge
on the structural parts.
A device for carrying out this method is characterized by baffle
bodies of small mass which are arranged, viewed in the direction of
incidence of the drops, ahead of the endangered structural
parts.
Instead of a fixed, stiff, solid erosion shield, there are used,
according to the invention, baffle bodies which, due to their small
mass, and because they do not rest on anything except for their
attachment to the structural part to be protected, are flexible and
hence can be elastically deflected in the direction of incidence or
laterally thereto when a drop impinges. This yielding of the baffle
bodies upon impingement of a drop gives the same effect as a lower
impingement speed. Due to the narrow and usually also curved
impingement surface offered to the drops, the angle of incidence is
more favorable than in the case of impingement normal to the
impingement surface. The drops are divided and so slowed in their
velocity that the erosion effect on the imperiled structural parts
behind the baffle bodies is greatly reduced.
If these structural parts are, for example, the impellers of a
low-pressure turbine, running in the saturated steam zone, they can
be protected by preceding fixed baffle bodies installed in the flow
path, e.g. a wire mesh. However, the effect is greater if the
baffle bodies co-rotate in the same direction of rotation as the
vanes, preferably at the same speed. They may be fastened either to
the rotor or to the vanes themselves. As the vanes are endangered
by drop impact mainly toward the tip, it may sometimes be
sufficient to protect only their radially external portion. The
stress of the baffle bodies caused by the centrifugal force is
thereby greatly reduced; yet it is advantageous to taper them
conically in radial direction outwardly.
The drops impinge close to the stagnation or ram point of the
profile, and therefore, if the baffle bodies are fastened on the
rotor or on the vanes, they are provided only in this region. Also
it is not necessary to protect each vane separately, as five or six
vanes are covered together and are sufficiently protected by baffle
bodies mounted in front.
The baffle bodies may be made, for example, of cold-drawn stainless
steel. Experiments have shown that the erosion effect greatly
decreases with decreasing wire diameter. A thickness of the baffle
bodies of 1 mm is to be regarded practically as the upper limit. A
few millimeters distance of the baffle bodies from the imperiled
structural parts are sufficient for adequate protection.
Two examples of construction of the invention are illustrated in
simplified form in the accompanying drawings, wherein:
FIG. 1 shows a steam turbine vane in front view;
FIG. 2, a single baffle body on a larger scale; and
FIG. 3, an airplane wing in partial view.
According to FIG. 1, the entrance edge of the turbine vane 1 is
protected at its radially external portion by wires 2, which are
secured to the ribs 3,4. They extend at a small distance from the
vane approximately parallel with one another. Because of the high
stress exerted by the centrifugal forces, a careful attachment to
the ribs 3 is necessary.
An example of this is illustrated in FIG. 2. It shows a single wire
2 greatly enlarged, especially the thickness being much
exaggerated. The outwardly tapering wire is welded into the rib 3,
while at rib 4 it is fastened only by spot welding, because there
only relatively small forces must be absorbed. According to the
occurring stress, the wire may alternatively be jointed to the ribs
by brazing or otherwise.
Instead of providing the rib 3, the profile may be recessed at this
point, the wires extending in the original profile line, whereby
the necessary spacing and the desired flexibility are established.
Also, the wires may extend over the full length of the vane blade
and may be held, for example, in a bottom plate, which is fastened
to the root of the vane. Another possibility, already mentioned,
consists in fastening the wires directly to the rotor, that is, in
front of the vane root.
FIG. 3 shows another possible use of the baffle bodies. Before the
nose of an airplane wing 5 a wire grid 6 is applied, which protects
the planking against impinging rain drops.
Other uses of the baffle bodies are conceivable wherever high
speeds occur, especially greater than Mach 1, and liquid drops are
contained in the gaseous medium. Exchangeability of the baffle
bodies is of advantage in most cases.
* * * * *