U.S. patent number 3,610,778 [Application Number 04/813,235] was granted by the patent office on 1971-10-05 for support for rotor blades in a rotor.
This patent grant is currently assigned to Sulzer Brothers, Ltd.. Invention is credited to Peter Suter.
United States Patent |
3,610,778 |
Suter |
October 5, 1971 |
SUPPORT FOR ROTOR BLADES IN A ROTOR
Abstract
The blades are held in slots of the rotor along with baffle
elements which are placed between each pair of blades. Each element
is elastically connected in a yieldable manner to each blade of a
pair of blades at points on opposite sides of the element while
simultaneously filling the slot to prevent leakage between the
blades. The elements can be slotted or provided with elevations at
opposite ends to enhance the yieldability.
Inventors: |
Suter; Peter (Schottikon, ZH,
CH) |
Assignee: |
Sulzer Brothers, Ltd.
(Winterthur, CH)
|
Family
ID: |
4379003 |
Appl.
No.: |
04/813,235 |
Filed: |
April 3, 1969 |
Foreign Application Priority Data
|
|
|
|
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Aug 9, 1968 [CH] |
|
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12011/68 |
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Current U.S.
Class: |
416/210R;
416/221; 416/500; 416/193A |
Current CPC
Class: |
F01D
5/22 (20130101); F01D 5/3007 (20130101); Y10S
416/50 (20130101) |
Current International
Class: |
F01D
5/00 (20060101); F01D 5/22 (20060101); F01D
5/30 (20060101); F01D 5/12 (20060101); F01d
005/32 () |
Field of
Search: |
;253/77CK,77PM
;416/221,219,220,210,212,500 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Powell, Jr.; Everette A.
Claims
What is claimed is:
1. The combination of a rotor having a plurality of
circumferentially spaced slots; a plurality of turbine blades
mounted in respective slots of said rotor, each blade having a base
received in a respective slot, a baseplate and a necklike extension
between said base and baseplate; and a plurality of elements, each
said element being of approximately the same axial length as said
necklike extensions and positioned between a pair of adjacent
blades between said necklike extensions, each said element having a
pair of spaced-apart elevations projecting therefrom, one of said
elevations contacting one blade at a first contact point and the
other of said elevations contacting the other blade of said pair of
blades at a second contact point, and each said element being
elastically yieldable between said points of contact and said
elevations.
2. The combination as set forth in claim 1, wherein said element
includes a pair of spaced plates between said pair of blades and a
crosspiece joining said plates.
3. The combination as set forth in claim 2, wherein each baseplate
is disposed radially over said elements and wherein said crosspiece
mounts said elevations on an upper surface thereof with each said
elevation extending along not more than one-quarter of the length
of said crosspiece.
4. The combination as set forth in claim 3, wherein said crosspiece
includes at least one slot therein between said contact points.
5. The combination as set forth in claim 3, wherein said crosspiece
has a reduced cross section centrally thereof.
6. The combination as set forth in claim 2, wherein one of said
plates of each element has a lug projecting therefrom in contact
with the side of an adjacent blade.
7. The combination as set forth in claim 1, wherein said element
includes an axial slot in the upper part between said contact
points.
8. The combination as set forth in claim 1, wherein said slots are
obliquely disposed in said rotor.
9. The combination as set forth in claim 1 wherein said slots are
axially disposed in said rotor.
Description
This invention relates to a support for rotor blades in a rotor.
More particularly, this invention relates to a support for rotor
blades of a turboengine rotor.
Turboengine rotors have been known wherein a plurality of turbine
blades have been mounted in slots within the rotor with wedgelike
baffle elements therebetween. For example, blades have been
constructed with a baseplate, a necklike extension below the
baseplate and a base below the extension which has been shaped to
mate within an axial or oblique slot in the rotor. In order to
prevent leakage between these blades, the baffle elements have been
sized to fit within the space between the necklike extension of two
adjacent blades. Further, such baffle elements have been sized and
fitted so as to obtain as smooth as possible a transition between
the baseplates and rotor.
However, it has been found that under the influence of centrifugal
force, the heretofore used baffle elements have been pressed with
such force against the baseplates as to behave in a manner as if
they were rigidly interconnected with the baseplates. Such rigid
connections have frequently exerted unfavorable influence on the
vibration behavior of the rotor in that the natural vibration
frequency of a row of blades has become excessively high.
Accordingly, it is an object of the invention to mount the blades
of a rotor in place in an elastic manner.
It is another object of the invention to permit vibration of a
turbine blade with respect to a baffle element adjacent the blade
within a rotor.
It is another object of the invention to reduce the natural
vibration frequency of a blade secured in a rotor.
Briefly, the invention provides a baffle element for turbine blades
in a rotor which is situated between a pair of blades and contacts
each blade at a point in an elastic yieldable manner opposite the
contact point of the other blade. This allows the blades to vibrate
more or less freely with respect to the baffle element. In effect,
an elastic yieldable section is provided in the baffle element
between the contact points with the respective turbine blades. As a
result, the blades are able to oscillate more or less freely with
respect to the baffle element while their natural frequency is
reduced. Depending on the configuration of the intermediate baffle
elements, the natural vibration frequency of the blades can be
adjusted to a desired value within certain limits. Also, depending
on the vibration form of particular interest, various
configurations of the baffle elements can likewise be elastically
effective.
These and other objects and advantages of the invention will become
more apparent from the following detailed description taken in
conjunction with the accompanying drawings in which:
FIG. 1 illustrates a fragmentary side view of a rotor having blades
mounted in place by baffle elements according to the invention;
FIG. 2 illustrates a view taken on line A-B of FIG. 1;
FIG. 3 illustrates a perspective view of the baffle element of FIG.
1;
FIGS. 4 to 6 respectively illustrate perspective views of modified
baffle elements according to the invention; and
FIG. 7 illustrates a view similar to FIG. 1 of another modified
baffle element according to the invention.
Referring to FIG. 1, the rotor 1 is provided with a plurality of
circumferentially spaced axial or oblique slots 2 each of which
receives a complementary shaped base 3 of a turbine blade 4. In
addition to the shaped base 3, each blade 4 has a baseplate 5 and a
necklike extension 6 between the base 3 and baseplate 5. The
necklike extensions 6 of each pair of adjacent blades 4 are spaced
apart to provide an interspace for a baffle element 7. Each baffle
element 7 serves to fill up the interspace between the blade
extensions 6.
Referring to FIG. 3, each baffle element 7 has a pair of plates 8,
which are joined together in spaced relation by a crosspiece 9 of
substantially T-shaped cross section. In addition, elevations 11,
16 are provided at either end of the crosspiece 9 to extend over a
part of the length of the crosspiece 9, for example, one-quarter of
the crosspiece length. The elevations 11, 16 are further disposed
diagonally opposite each other on the top of the crosspiece 9.
Thus, one elevation 11 comes in contact with the baseplate 3 of one
turbine blade 4 while the other elevation 16 comes in contact with
the baseplate 3 of the other turbine blade 4 of an adjacent pair of
blades. Also, one of the plates 8, i.e., the front plate, of each
baffle element 7 has a lug 18 extending therefrom in the same plane
which abuts the side of a blade 4 so as to prevent axial
displacement of the baffle element 7. Since each of the baffle
elements 7 contacts the baseplates 5 of adjacent blades 4 at
separated points and is of a shape to elastically yield under
stress, the baseplates 5 can move with respect to one another, for
example, under a torsional vibration.
Referring to FIG. 4 in order to increase the elastic yieldability,
the baffle element 7 is provided with a slot 14 substantially in
the center of the crosspiece 9 which passes upwardly through the
upper part of the cross section of the crosspiece 9. Alternatively,
a plurality of slots (not shown) can be distributed uniformly or
nonuniformly over the length of the crosspiece 9.
Referring to FIG. 5, the elastic yieldability of the baffle element
7 can also be increased by reducing the cross-sectional area of the
center of the crosspiece 9 in the upper part. For example, as
shown, the flat horizontal upper part of the crosspiece can be
centrally interrupted.
Referring to FIG. 6, the elastic yieldability of the baffle element
can be increased by positioning the two elevations 12 on the same
side of the crosspiece 9. This allows the baffle element 7 to bear
against only one of the two adjacent blades 4 during operation
while the contact point of the baffle element 7 with the other
blade 4 lies between the plates 8 and the necklike extension 6
substantially in the area 13, as shown, opposite the lug 18.
Referring to FIG. 7, a baffle element 7' having an axial slot 20
can also be fitted between the necklike extensions 6 of a pair of
blades 4. This allows an elastic yieldable connection to be formed
at the contact points 19 between the upper surfaces of the element
7' on opposite sides of the slot 20 and the baseplates 5 of the
blades 4.
* * * * *