Information
-
Patent Grant
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6799945
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Patent Number
6,799,945
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Date Filed
Friday, January 31, 200321 years ago
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Date Issued
Tuesday, October 5, 200420 years ago
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Inventors
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Original Assignees
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Examiners
- Look; Edward K.
- White; Dwayne
Agents
- Oblon, Spivak, McClelland, Maier & Neustadt, P.C.
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CPC
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US Classifications
Field of Search
US
- 415 155
- 415 156
- 415 159
- 415 160
- 415 161
- 415 162
- 415 148
- 403 1093
- 403 3594
- 403 205
- 403 187
- 403 144
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International Classifications
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Abstract
A spring (15) of angular shape is placed between the lug (17) of a connecting rod (10) controlling the orientation of a stator blade and the pivot (3) of said blade, such that its edge (18) bends against one edge face (19) of the connecting rod (10) and the washer (16) moves the pivot (3) in the play of the bore (21) of the connecting rod and sets and maintains the contact between two plane faces (12 and 13), so as to reduce the differences in angular displacements between the connecting rod and pivot due to the play remaining in the bore (21).
Description
This invention relates to a stator blade pivoting arrangement in a turbomachine.
The stator blades, stationary in a turbomachine and used to rectify the gas flow before the next rotor blade stage, may be of the variable locking type, i.e. their orientation is controlled as a function of the operating mode of the machine. They are then mounted on outer pivots which project outside the stator casing and are connected to connecting rods rotated at will by a common control ring, surrounding the stator casing. The rotation of the connecting rods produces a similar rotation of the blades. The transmission of the rotation is acquired by a suitable adjustment liable to comprise mutual support of plane faces established on an end section of the pivot of the blade and on a bore at the end of the connecting rod: this end section and the bore are frequently squares.
The documents U.S. Pat. Nos. 4,767,264 and 4,668,165-A disclose connecting rod arrangements sufficiently thin to be flexible to the twisting to which they are subjected by the rotation of the control ring. These connecting rods are equipped with lateral ribs curved like tongs and which penetrate into the grooves of the pivots. These ribs are responsible for rotating the pivots with an engagement which is only slightly different to that of the square sections.
However, it is observed that the slightest adjustment play between the bore of the connecting rod and the pivot of the blade delays the rotational drive markedly, and a drive defect of several tenths of an angular degree is frequently reached. Since the blade should be oriented with great precision in order to obtain a good machine output, it can be concluded that an improvement is desirable to reduce the square adjustment play.
A solution is offered with the invention, which consists in its broadest definition of a stator blade pivoting arrangement in a turbomachine, comprising a blade pivot having one end projecting outside the stator and comprising a plane face section, and a control connecting rod engaged onto the end of the blade pivot via a bore limited by plane faces associated with the plane faces of the pivot, characterised in that it comprises a spring stressed between the pivot and the connecting rod and arranged so as to press one of the plane faces of the pivot against one of the plane faces of the connecting rod.
The above-mentioned documents do not clearly disclose the nature of the ribs, and in particular their rigidity. It is not stated that they have an elasticity which would be used to keep them in contact with the base of the grooves and ensure the angular position of the blade pivot with respect to the connecting rod with sufficient force.
The assemblies in these documents are also of a special type. The spring according to the invention is an autonomous part, distinct from the rest of the conventional square section assembly which does not need to be modified, the spring being simply added.
It is favourably envisaged that the springs will comprise a bored washer placed on the connecting rod and engaged around the end of the blade pivot, and a flexible edge of the washer, engaged on an edge face of the connecting rod opposite one of the faces of the pivot against which the washer abuts, making with the washer a wider angle than in the idle state of the spring.
The invention will now be described with reference to the figures, wherein:
FIG. 1
is an overall view of the arrangement according to the invention,
FIG. 2
is a more detailed view of the main components of the invention,
and
FIG. 3
is a blown-up view of said components.
With reference to
FIG. 1
, a turbomachine portion comprises a stator casing
1
comprising stationary blades
2
but which can be oriented by pivots
3
, located at the outer ends of the blades
2
and in bearings
4
passing through the casing
1
; the inner ends of the blades
2
are joined by a ring
5
engaged around an inner pivot
6
and which helps hold the circular stages of the blades
2
in place.
The pivots
3
pass through the stator casing
1
and end with an outer end
7
wherein one section
8
has a square shape. Further out, the end
7
is threaded and receives a nut
9
. A connecting rod
10
is articulated between the end
7
and a control ring
11
around the stator casing
1
and at a close distance to the blade
2
. The control ring
11
surrounds the stator casing
1
, and it is rotated by known means such as cylinders according to the machine drive. It rotates the connecting rod
10
around the pivot
3
, along with said pivot and the entire blade
2
. Indeed, the connecting rod
10
comprises a square-shaped bore
13
at its end lug
17
, and which comprises plane faces resting against the plane faces of the pivot
3
to rotate it. Two opposing plane faces of the pivot
3
have the reference
12
, and the two corresponding plane faces of the bore
13
have the reference
14
.
In accordance with the invention, a spring
15
is added to the device. It is separate from the other parts of the assembly, particularly the connecting rod
10
and the pivot
3
, and it consists of a washer
16
placed on the lug
17
of the connecting rod
10
and an edge
18
roughly at a right angle with the washer
16
which extends along one lateral edge face
19
of the washer
16
. The edge
18
comprises an undulation
20
oriented towards the lateral edge face
19
and wherein the top touches said face. A square bore
21
is provided via the washer
16
. In addition, the proportions of the spring
15
are selected such that the edge
18
is pushed back when the bore
21
is engaged onto the square section
8
of the end of the pivot
3
, while one of the edge faces of the bore
21
touches one of the plane faces
12
(opposite the lateral edge face
19
) of the square section
8
, and the plane face
12
of the square section
8
which is opposite the latter touches the complementary plane face
13
of the connecting rod lug
17
. In other words, a tension is exerted on the spring
15
, by means of which the angle of the washer
16
and the edge
18
is opened with respect to an idle state, and it is reflected by a contact pressure between a pair of plane faces
12
and
13
of the pivot
3
and the connecting rod
10
, which persists during all the machine operating statuses. In this way, the connecting rod
10
and the blade
2
remain at a stationary mutual angular position.
All the blades
2
of the stage controlled by the ring
11
are equipped with a similar spring
15
. It may be useful to check that all the springs
15
are mounted in the same way, to prevent differences in placement of the play between the bore
21
and the square section
8
of the pivot
3
. For this it is possible to add a tab
22
to the spring
15
, which is attached to the washer
16
and directed perpendicular to it like the edge
18
already encountered, but which is not intended to be deformed elastically when the spring is positioned, but to perform a fool-proof device function allowing positioning of the spring
15
only on one side. The tab
22
extends along the outer edge faces
23
of the connecting rod
10
when the spring
15
has been positioned correctly, but it prevents the washer
16
from resting on the lug
17
of the connecting rod
10
otherwise.
The invention would be practicable with other polygonal sections of the blade pivot and the connecting rod bore.
A very marked reduction in the angular drive defect of stator blades was observed by applying the invention.
Claims
- 1. Stator blade (2) pivoting arrangement in a turbomachine, comprising a blade pivot (3) having one end projecting outside the stator and comprising a plane face section (8), and a control connecting rod (10) engaged onto the end of the blade pivot via a bore limited by plane faces (13) associated with the plane faces (12) of the pivot, characterised in that it comprises a spring (15) stressed between the pivot and the connecting rod and arranged so as to press one of the plane faces of the pivot against one of the plane faces of the connecting rod.
- 2. Stator blade pivoting arrangement according to claim 1, characterised in that the spring comprises a bored washer (16) placed on the connecting rod and engaged around the end of the blade pivot, and a flexible edge (18) of the washer, engaged on an edge face of the connecting rod opposite one of the faces of the pivot against which the washer abuts, making with the washer a wider angle than in the idle state of the spring.
- 3. Stator blade pivoting arrangement according to claim 2, characterised in that the spring comprises a tab (22) engaged on another top edge face of the connecting rod.
- 4. Stator blade pivoting arrangement according to claim 2, characterised in that the edge of the spring is engaged on the edge of the connecting rod by an undulation (20).
Priority Claims (1)
Number |
Date |
Country |
Kind |
0201459 |
Feb 2002 |
FR |
|
US Referenced Citations (5)
Foreign Referenced Citations (3)
Number |
Date |
Country |
2 029 859 |
Feb 1972 |
DE |
0 545 656 |
Jun 1993 |
EP |
1 156 227 |
Nov 2001 |
EP |