Stator blade pivoting arrangement in a turbomachine

Information

  • Patent Grant
  • 6799945
  • Patent Number
    6,799,945
  • Date Filed
    Friday, January 31, 2003
    21 years ago
  • Date Issued
    Tuesday, October 5, 2004
    20 years ago
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)
Number Name Date Kind
4668165 Ludwick May 1987 A
4767264 Kisling et al. Aug 1988 A
5024580 Olive Jun 1991 A
5211537 Langston et al. May 1993 A
6019574 DiBella Feb 2000 A
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