Patent Application
20100247005
The present invention is directed to a sealing segment according to claim 1 for sealingly connecting two structural components parts which are movable relative to one another, a sealing segment arrangement, and a flow machine with a sealing segment arrangement of this type.
Sealing segments for sealingly connecting adjacent structural component parts are known per se. A sealing segment allowing a relative movement of adjacent structural component parts with respect to one another is disclosed, for example, in DE 2453645. This sealing segment comprises a plurality of metal rings and plastic rings in a sandwich-type construction and should be able to sustain rotational loading while retaining the sealing action. One of the disadvantages of this sealing segment is the costly sandwich construction. It is further disadvantageous that this sealing segment only allows a rotational relative movement between the two structural component parts. The maximum relative movement of the two structural component parts with respect to one another is limited by the shear strength of the sealing segment. Therefore, with every relative movement the sealing segment is subjected to material fatigue which has a lasting negative impact on the life of the sealing segment.
It is an object of the present invention to provide a sealing segment that permits different relative movements between adjacent structural component parts and which has a long life, a sealing segment arrangement, and a flow machine with a sealing segment arrangement of this kind.
A sealing segment according to the invention for sealingly connecting two adjacent structural component parts which are movable relative to one another has two sealing bodies which are connected to one another by a web. The sealing bodies can be arranged in recesses of the structural component parts and, together with the latter, form a sliding bearing. The sealing segment is accordingly disposed in an articulated manner between the two structural component parts so that a swiveling movement and an axial movement of the two structural component parts relative to one another can be compensated. In so doing, the sealing segment is not warped or deformed so that it has a long life compared to the known solution. At the same time, a tight connection with respect to pressure and temperature is produced over the entire relative movement. Further, an offset between the structural component parts can be compensated without tension by the articulated construction of the sealing segments according to the invention.
A preferred material for the sealing segment is a metal.
The sealing bodies are preferably cylindrical and are constructed so as to be radially springing to enhance the sealing effect. Accordingly, the sealing surfaces of the sealing bodies can contact opposing inner surfaces of the recesses so as to be preloaded.
In particular, the sealing bodies extend axially parallel to one another, which makes it possible in principle to use them in longitudinal and annular grooves arranged parallel to one another in the opposing structural component parts.
In one embodiment, the sealing segment is formed integral with its sealing bodies and the web from a tubular body.
In another embodiment, the sealing segment with its sealing bodies and the web is formed from an individual sheet-like sealing element. Free end portions of the sheet-like sealing element can be guided along the web or can be at a distance from it.
In another embodiment, the sealing segment comprises two sheet-like sealing elements which are connected to one another in the web area. For technical reasons relating to manufacture, it is advantageous when the two sealing elements are identically shaped. Free end portions of the sealing elements can be at a distance from one another in the assembled state. When using a plurality of sealing segments axially one behind the other, the sealing effect between adjacent sealing segments can be enhanced in that the sheet-like sealing elements are arranged so as to be offset relative to one another in longitudinal direction, so that there is a step-like material overlapping between the sealing segments.
In another embodiment, a transverse slit that can extend up to the web is formed in at least one sealing body to increase the elasticity of the sealing segment. The elasticity can be further increased in that a plurality of transverse slits are alternately provided in one sealing body so as to extend along the web into the other sealing bodies.
To improve the cooling of the sealing segments and sealing surfaces, the sealing bodies can be at least partially perforated. Alternatively, they can also be profiled. It is also conceivable to form the web so as to have a large surface area with at least one through-hole which can be connected to a cooling air supply.
A plurality of sealing segments form a sealing segment arrangement according to the invention. It is especially advantageous for stabilizing the sealing segments relative to one another and for stabilizing the sliding bearings when a connection element is inserted into adjacent sealing bodies in axial direction. For example, the connection element can be a coil, a flexible rod or a bar with spherical end portions.
The sealing action of the sealing segment arrangement according to the invention is optimized in such a way that, when used in the hot gas path of a flow machine, hot gas blow-by, for example, in the connection area between the combustion chamber side and the turbine side, is prevented. Further, overheating and excessive consumption of cooling air can be prevented by the cooling of the sealing segments. The sealing segments permit a reproducible fuel distribution and air distribution and prevent blow-by in the hot gas path, so that high efficiencies of the flow machine can be reliably achieved.
Preferred embodiments of the invention will be described more fully in the following with reference to schematic drawings in which:
Each sealing segment 10, 12 has two axially parallel, cylindrical sealing bodies 14, 16 which are connected to one another in each instance by a web 18 which is constructed so as to have an extensive surface. The sealing bodies 14, 16 are radially springing and are partially enclosed in a U-shaped, rectangular longitudinal groove 20, 22 of the structural component parts with inner groove surfaces 28, 30 and 32, 34, respectively, extending parallel to one another in pairs. The sealing bodies 14, 16 form sealing surfaces 24, 26 on the circumference by which they sealingly contact the inner groove surfaces 28, 30, 32, 34 of the structural component parts in some areas accompanied by preloading.
To compensate for different thermal expansions between the sealing segments 10, 12 and the structural component parts 4, 6, at least one sealing body 14, 16 is disposed at a distance from the groove base 36, 38; i.e., the distance between the groove bases 36, 38 of the opposite longitudinal grooves 20, 22 is greater than the extension of the sealing segments 10, 12 along their transverse axis 40.
According to the invention, the sealing bodies 14, 16 together with the structural component parts 4, 6 form a sliding bearing and are accordingly supported therein in an articulated manner. The longitudinal grooves 20, 22 serve as bearing shells which allow a relative movement of the structural component parts 4, 6 with respect to one another axially along a longitudinal axis 42 of the longitudinal grooves 20, 22 and a swiveling movement 44 around the longitudinal axis 42. The springing construction of the sealing bodies 14, 16 generates a preloading force which produces a tight connection between the sealing surfaces 24, 26 and the inner groove surfaces 28, 30 and 32, 34, respectively, with respect to pressure and temperature regardless of the respective relative movements between the structural component parts 4, 6 so that the gap 8 between the structural component parts 4, 6 is sealingly closed. At the same time, an offset between the longitudinal grooves 20, 22 can be compensated by the articulated bearing support of the sealing segments 10, 12 without tension being introduced into them.
As is shown in
It should be noted that a cooling of the sealing segments mentioned above by way of example is not limited to at least one through-hole in the web 18, but rather other cooling variants are also conceivable. Among these, for example, is a perforation of the sealing surfaces 24, 26 of the sealing bodies 14, 16, which leads in particular to an improvement in the cooling of the inner groove surfaces 28, 30, 32, 34. A circumferential profiling of the sealing surfaces 24, 26 of the sealing bodies 14, 16 also causes a deliberate cooling of the inner groove surfaces 28, 30, 32, 34. Of course, the individual embodiment examples for cooling mentioned above can also be combined.
It is further noted that the use of the sealing segments and sealing segment arrangements 2, 78 mentioned above by way of example is not limited to axial, rectangular longitudinal grooves 20, 22. For example, it is also conceivable to form longitudinal grooves 20, 22 whose inner groove surfaces 28, 30 and 32, 34, respectively, are inclined relative to the groove base 36, 38 in such a way that the longitudinal grooves 20, 22 are widened proceeding from their groove opening in direction of their groove base 36, 38.
The use of the sealing segments or sealing segment arrangements 2, 78 according to the invention is also not limited to longitudinal grooves, per se; rather, they can also be used in annular grooves so that annular gaps between adjacent structural component parts 4, 6 can be tightly closed. In this regard, it is advantageous when the individual sealing segments have an arc shape in longitudinal direction corresponding to the respective annular groove and/or a corresponding plurality of transverse slits. An example of the use of the sealing segment arrangements according to the invention in front annular grooves is their use in flow machines, particularly in the hot gas path between combustion chamber components and turbine components such as the initial blading. The corresponding combustion chamber component has an annular groove at its end face directed toward the guide vane stage for receiving the sealing body 14 of the sealing segment arrangements according to the invention. The guide vane stage likewise has in its end face directed toward the combustion chamber component an annular groove for receiving the sealing body 16. When relative movements occur between the combustion chamber side and the turbine side owing, for example, to thermal stresses, these relative movements are compensated by the articulated construction of the sealing segments according to the invention while retaining the required tightness relative to pressure and temperature and without introducing loads, for example, tensile forces or shearing forces, into the sealing segments.
It is also noted that the elastic connection elements are not limited to coils; rather, elastic rods or bars with spherical end heads are also conceivable, for example.
It is further noted that the sealing segments can also be produced from a material other than metal. The material is primarily determined by the anticipated environmental conditions and may also be a plastic, for example. Further, it is conceivable to provide the sealing bodies 14, 16 in particular with a corrosion-resistant, low-friction coating, for example.
Disclosed herein is a sealing segment for sealingly connecting two adjacent structural component parts which are movable relative to one another, the sealing segment has two sealing bodies which are connected to one another by a web and are arranged in recesses of the structural component parts in an articulated manner, and a sealing segment arrangement with a plurality of sealing segments of this kind, and a flow machine with a sealing segment arrangement of this kind.
The invention is not limited by the embodiments described above which are presented as examples only but can be modified in various ways within the scope of protection defined by the appended patent claims.
PRIORITY CLAIM This is a U.S. national stage of application No. PCT/EP2008/009257, filed on Nov. 3, 2008. Priority is claimed on the following application: Country: Germany, Application No.: 10 2007 062 681.0, Filed: Dec. 24, 2007, the content of which is/are incorporated here by reference.
| Filing Document | Filing Date | Country | Kind | 371c Date |
|---|---|---|---|---|
| PCT/EP08/09257 | 11/3/2008 | WO | 00 | 4/19/2010 |
