JP5947687B2 - SEALING DEVICE AND GAS TURBINE HAVING SEALING DEVICE - Google Patents

Description

  The present invention relates to a sealing device, and more particularly to a sealing device used for a gas turbine.

  The gas turbine is configured to generate a working fluid compressed by a compressor, add fuel to the working fluid by a combustor, and burn it to obtain a hot working fluid to drive the turbine. The member exposed to the high-temperature working fluid is cooled to an allowable temperature or lower by a low-temperature fluid so that the member does not melt or crack due to oxidation or thermal stress. In addition, the gas turbine is constituted by a member divided into a plurality of parts so as to relieve stress concentration due to thermal deformation of the member and facilitate inspection, maintenance, and replacement of parts.

  In such a gas turbine, a high-pressure and low-temperature fluid is supplied to the outside of the member so that the high-temperature working fluid does not leak out of the gap between the members. Generally, in a gas turbine, such a low-temperature fluid is extracted from a compressor, and if this extraction fluid is increased unnecessarily, the high-temperature working fluid that drives the turbine will decrease, so the entire gas turbine Leading to reduced efficiency.

  For this reason, a seal structure is provided between adjacent constituent members, and in the case of stationary members, they are generally connected by inserting a seal plate into seal grooves provided on surfaces facing each other. A technique for suppressing the leakage of the bleed fluid is employed. (See Patent Document 1 etc.)

JP-A 62-45904 JP-A-10-212904

  In the technique of Patent Document 1 described above, the adjacent component members are sealed by a metal seal plate that is prevented from being detached by a pin. However, there is a gap in the groove depth direction of the seal groove, and there is a deviation in the amount of thermal elongation between adjacent constituent members, which may cause a deviation in the seal groove. When the seal groove is displaced, the seal plate inserted so as to straddle the seal groove between adjacent components is inclined, and the contact state with the seal groove wall surface changes from surface contact to line contact, and the sealing performance is improved. descend. In addition, when the radial position and the axial position of the turbine are shifted at the same time and the seal plate rotates in the plate surface within the seal groove, the contact state between the seal plate and the seal groove is point contact or non-contact. Since it also becomes a state, there exists a possibility that sealing performance may fall further.

  In the technique of Patent Document 2, a plurality of seal grooves are provided between the same members, a plurality of thin plate-like seal plates are stacked, and each seal plate is appropriately moved in the groove depth direction of the seal groove. The sealing performance is improved by enlarging the width of the seal groove in the depth direction. However, since it becomes easier to follow the groove displacement with respect to the amount of thermal elongation, the groove displacement is further increased and the sealing performance may be deteriorated. Moreover, since each thin plate-shaped seal plate has low strength, there is a possibility that the seal plate itself may be damaged due to the shift of the seal groove.

  This invention is made | formed in view of such a situation, and is providing the sealing device which can maintain favorable sealing performance, when deviation arises in the amount of thermal elongation between structural members.

  To achieve the above object, the present invention provides a seal groove provided on each of opposing surfaces of adjacent constituent members, and the other constituent member from the seal groove provided on one of the constituent members. A control plate for controlling movement of the component members so that the seal grooves face each other. It has a member on the said opposing surface, It is characterized by the above-mentioned.

  ADVANTAGE OF THE INVENTION According to this invention, even when deviation arises in the amount of thermal expansion between structural members, the sealing device which can maintain favorable sealing performance can be provided.

Sectional drawing of the sealing device which concerns on one embodiment of this invention. The side view of the adjacent surface of the sealing device which concerns on one embodiment of this invention. Sectional drawing of the sealing device which concerns on the form of the application example of this invention. The permeation | transmission figure of the control member which concerns on the form of the application example of this invention. Sectional drawing of the sealing device which concerns on the form of the application example of this invention. The permeation | transmission figure of the control member which concerns on the form of the application example of this invention. Sectional drawing of the sealing device which concerns on the form of the application example of this invention. The perspective view showing the structure of the sealing device which concerns on the form of the application example of this invention. The perspective view showing the structure of the sealing device which concerns on the form of the application example of this invention.

  Hereinafter, embodiments of the present invention will be described with reference to the drawings. 1 and 2 are explanatory views of a sealing device according to an embodiment of the present invention. Adjacent components 1 and 2 are configured to delimit a low-temperature fluid (hereinafter referred to as seal air) 6 and a gas path 7 through which a high-temperature working fluid flows. A fluid having a pressure higher than that of the gas path 7 is supplied as the seal air 6 so that the high-temperature main flow 7 does not leak from the gap between the members to the outside of the operating region.

  A seal groove 3 is provided on a side surface of the component member 1 facing the component member 2. Further, a seal groove 4 is provided on a side surface of the component member 2 facing the component member 1. The seal grooves 3 and 4 are provided so as to be opposed to each other, and a seal member (for example, a plate) 5 is spanned between the seal grooves 3 and 4, thereby separating the high-pressure part and the low-pressure part, and sealing The air 6 is prevented from leaking to the gas path 7 unnecessarily. The width of the seal member 5 and the width of the seal grooves 3 and 4 in the leak direction (the direction of the arrow of the seal air 6), which is the direction from the high pressure portion to the low pressure portion, are different. A seal gap δ is provided between them so as not to be damaged by thermal deformation of the constituent members.

  In the sealing device of the present embodiment, a cylindrical control pin 10 is fixed to a pin fixing portion 11 provided on an end surface of the component member 1 (side surface facing the component member 2) by means such as welding and welding, and is convex. A member is formed. It is inserted into a concave pin insertion portion 12 provided on the end surface of the adjacent component member 2. Between the control pin 10 and the pin insertion part 12, a control gap δc is provided in the direction perpendicular to the seal groove 3 so as to be assembled. At this time, the control gap δc is strictly controlled so as to be sufficiently small, and is configured to be at least smaller than the seal gap δ. As shown in FIG. 2, the control pins 10 are provided at a plurality of positions at positions parallel to the seal groove 3.

  Below, the effect | action of the sealing apparatus of a present Example is demonstrated. During operation of the gas turbine, the constituent members 1 and 2 become hot and cause thermal deformation. At this time, conventionally, since the seal groove 4 can move in the vertical direction within the range of the seal gap δ with respect to the seal groove 3, a level difference or twist occurs in the seal grooves 3, 4, and the contact surface of the seal member 5. Is not kept.

  On the other hand, in the present embodiment, since the control pin 10 is inserted into the pin insertion portion 12, the movement of the constituent members 1 and 2 is controlled, and the relative movement of the seal groove 4 with respect to the seal groove 3 is controlled by the seal gap. The control gap can be suppressed to be smaller than δ or less than δc. Thus, even when a deviation occurs in the amount of thermal expansion between the constituent members 1 and 2, it is possible to always keep the contact surface between the seal grooves 3 and 4 and the seal member 5 without damaging the seal plate. , The deterioration of the sealing performance can be suppressed.

  Furthermore, since the change in the relative position of the seal grooves 3 and 4 is suppressed to a minute control gap δc or less, the load applied to the seal plate is reduced. Therefore, the life of the seal plate can be extended, and the reliability of the seal device can be improved. Further, since the restriction on the strength of the seal plate is relaxed, it is possible to reduce the thickness and complexity of the seal plate, thereby improving the sealing performance.

  Note that if the width of the control pin 10 in the leak direction is made as large as the width of the pin insertion portion 12, the control gap δc becomes extremely small, so that better sealing performance can be maintained. The same size as used in the present application does not necessarily indicate only the same size but also includes a case where there is a tolerance for assembling.

  Further, since the cylindrical control pin 10 is fixed to the pin fixing portion 11 provided on the end face of the component member 1, it is possible to prevent the control pin 10 from dropping off during assembly.

  Furthermore, if the sealing device of this embodiment is applied to a gas turbine that handles a high-temperature working fluid, the reliability and efficiency of the gas turbine can be improved by improving the reliability and performance of the sealing device.

  As other configuration examples for obtaining such an effect, configurations shown in FIGS. 3 to 9 described below can be considered. In the example shown in FIG. 3, the pin insertion portion of the component member 2 is a single square groove 13 extending parallel to the seal groove. FIG. 4 is a perspective view of the control pin 10, the pin fixing portion 11, and the pin insertion groove 13 as seen through the constituent members. Since the control pin 11 and the pin insertion groove 13 suppress the movement of the seal groove 4 in the vertical direction with respect to the seal groove 3 to a minute control gap δc or less, the contact surface between the seal grooves 3, 4 and the seal member 5 is always provided. It is possible to keep, and it is possible to suppress a decrease in sealing performance. Although the seal groove 4 can move in the horizontal direction with respect to the seal groove 3, the contact surface between the seal grooves 3 and 4 and the seal member 5 is maintained, so that the seal performance is not affected.

  In the example shown in FIG. 5, the pin fixing portion 11 provided on the end face of the component member 1 has a quadrangular prism shape, and the quadrangular prism-shaped control pin 10 is also fixed by means such as welding and welding. FIG. 6 is a perspective view of the control pin 10, the pin fixing portion 11, and the pin insertion groove 13 as seen through the constituent members. Since the vertical movement of the seal groove 4 with respect to the seal groove 3 is suppressed to a minute control gap δc or less, the contact surface between the seal grooves 3 and 4 and the seal member 5 can always be maintained, and the sealing performance is deteriorated. Can be suppressed.

  Further, since the control pin 10 has a quadrangular prism shape, it is possible to receive a load for suppressing a deviation in the amount of thermal elongation. Thereby, since the local load concerning the control pin 10 or the pin fixing | fixed part 11 can be eased, the reliability of a sealing device can further be improved.

  In the example shown in FIG. 7, the pin fixing portion 14 provided on the end face of the component member 1 is formed into one square groove shape, and one control plate 15 is fixed by means such as welding and welding. FIG. 6 is a perspective view of the control plate 15, the pin fixing groove 14, and the pin insertion groove 13 as seen through the constituent members. Since the vertical movement of the seal groove 4 with respect to the seal groove 3 is suppressed to a minute control gap δc or less, the contact surface between the seal grooves 3 and 4 and the seal member 5 can always be maintained, and the sealing performance is deteriorated. Can be suppressed.

  In the example shown in FIG. 9, the projecting portion 16 is integrally formed with the constituent member 1 by machining on the end face of the constituent member 1 and is inserted into the insertion groove 13 provided on the end face of the adjacent constituent member 2. As the shape of the protrusion 16, as in FIGS. 3, 5, and 7, a cylindrical shape, a quadrangular prism shape, a plate shape, and the like are conceivable.

  As described above, according to the present embodiment, the contact state between the seal groove and the seal member can always be kept in the surface contact state even when the adjacent component member is thermally deformed. It is possible to effectively suppress leakage of cooling air from the gap and maintain good sealing performance. Therefore, the reliability and efficiency of the gas turbine can be improved.

DESCRIPTION OF SYMBOLS 1, 2 ... Gas path component 3, 4 ... Seal groove 5 ... Seal member 6 ... Seal air 7 ... Gas path 10 ... Control pin 11 ... Pin fixing part 12 ... Pin insertion part 13 ... Pin insertion groove 14 ... Pin fixing groove 15 ... Control plate 16...

Claims (7)

A seal groove provided on each of the opposing surfaces of the adjacent component members;
A seal plate that is attached so as to span from the seal groove provided on one of the constituent members to the seal groove provided on the other constituent member, and that separates the high-pressure portion and the low-pressure portion;
A control member for controlling the movement of the component members so that the seal grooves face each other, on the facing surface;
As the control member, having a convex member attached so as to protrude from the facing surface of one of the constituent members,
The opposing surface of the other component member has a concave portion, and the convex member is inserted into the concave portion,
The control gap, which is the difference between the width of the convex member and the width of the concave portion in the leak direction from the high pressure portion toward the low pressure portion, is the difference between the width of the seal plate and the width of the seal groove. A sealing device characterized by being configured to be smaller than a seal gap. The sealing device according to claim 1 ,
The sealing device according to claim 1, wherein a width of the convex member and a width of the concave portion in the leak direction are configured to be approximately the same. The sealing device according to claim 1 ,
As the convex member, a plurality of columnar members are provided on the facing surface. The sealing device according to claim 1 ,
As the convex member, one or a plurality of quadrangular prism members are provided on the facing surface. The sealing device according to claim 1 ,
The sealing device, wherein the convex member is integrally formed with a member constituting the facing surface on which the convex member is provided. The sealing device according to claim 1 ,
The sealing device, wherein the concave portion has a groove shape having a depth in a direction parallel to the seal groove. A compressor that generates compressed air; a combustor that combusts the compressor from the compressor together with fuel; and a turbine that obtains shaft power by combustion gas from the combustor, and a plurality of stationary turbines constituting the turbine In a gas turbine having a seal device that is attached so as to span a seal plate in seal grooves provided on opposing surfaces between the constituent members, and separates the high-pressure part and the low-pressure part,
It said sealing device, have a control member for controlling movement of the components such that the seal grooves are opposed to each other on the facing surface,
As the control member, having a convex member attached so as to protrude from the facing surface of one of the constituent members,
The opposing surface of the other component member has a concave portion, and the convex member is inserted into the concave portion,
The control gap, which is the difference between the width of the convex member and the width of the concave portion in the leak direction from the high pressure portion toward the low pressure portion, is the difference between the width of the seal plate and the width of the seal groove. A gas turbine characterized by being configured to be smaller than a seal gap .