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Publication numberUS2729422 A
Publication typeGrant
Publication dateJan 3, 1956
Filing dateMar 26, 1952
Priority dateApr 6, 1951
Publication numberUS 2729422 A, US 2729422A, US-A-2729422, US2729422 A, US2729422A
InventorsHerbert Scharf
Original AssigneeMaschf Augsburg Nuernberg Ag
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Shaped article of ceramic material
US 2729422 A
Abstract  available in
Previous page
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Claims  available in
Description  (OCR text may contain errors)

Jan. 3, 1956 H. SCHARF 2,729,422

SHAPED ARTICLE OF CERAMIC MATERIAL Filed March 26, 1952 INVENTOR HERBERT Scnmzr ATTORNEYS SHAPED ARTICLE OF CERAMIC MATERIAL Herbert Scharf, Augsburg, Germany, assignor to Maschinenfabrik Augsburg-Numberg A. G., Augsburg, Germany, a corporation of Germany Application March 26, 1952, Serial No. 278,559 Claims priority, application Germany April 6, 1951 4 Claims. 01. 253-77 This invention relates to certain improvements in the shaping of engine parts or machine elements of ceramic material, more particularly, in the form of blades for gas turbines.

In engineering practice, ceramic materials are used primarily where in addition to mechanical stresses the parts are exposed to very high temperatures exceeding the upper temperature limit admissible for metallic materials. The mechanical strength of shaped articles of ceramic materials is not substantially changed by heating them from room temperature to very high temperature. However, in view of the relatively low mechanical strength of ceramic materials, it is necessary to pay special attention to the factors determining the rated fatigue limit of the respective part. This is especially true in case of highly stressed engine parts, such as, turbine blades or vanes. The main difiiculty consists in the fact that the slightest peak strains which have been neglected in the design will cause break-down of the ceramic element if such peak load exceeds the strength of the material.

More particularly, it has been found that the equilibrium of the structural or internal strain which originates from the firing and is a characteristic feature of ceramic materials is disturbed by the machining of individual surfaces of the ceramic part, for instance by grinding, whereby the rated fatigue limit is substantially reduced. The critical points of a partly ground workpiece are at the transitions between the ground surface and the non-injured or unwrought natural surface or skin of the shard produced by the firing.

It is an object of the present invention to provide a design which offers optimum conditions as to the mechanical strength of engine parts or other shaped articles of the type referred to.

With this and further objects in view, according to the present invention the place of transition between the machined supporting or seating surface or surfaces and the unwrought surface or surfaces of the engine part, more particularly, of the root of a turbine blade, is shaped in the form of a hollow or flute. According to a further feature of the invention, such flute is arranged to have its center point, or its center axis, respectively, on a plane which is flush, or nearly flush, with the ground surface. It has been found that the deleterious influence of ground surfaces on the mechanical strength can be compensated particularly eifectively in this way. Generally speaking, the ground surface should form a right angle with the returning non-ground surface. The machining or tooling allowance which is indispensable with ceramic materials for rendering it possible to adhere safely to the dimensions indicated in the drawing in spite of the large tolerances caused by the manufacturing process, and by the large shrinking diflerences inherent to this material, should be dimensioned so that after grinding to the specified measure the centers of the flutes are not located substantially above the plane of the ground surfaces. The important thing is to arrange the surfaces in such a way that the compressive forces act on the machined surfaces 2,729,422 iiatented Jan. 3, 1956 in a normal direction while non-stressed parts of the shard adjacent to the surface acted upon by the force are avoided.

It will be understood that the invention is not restricted to its application in ceramic turbine blades but it may be used for other ceramic engine parts or machine elements as well.

Other and further objects, features and advantages of the invention will be pointed out hereinafter and appear in the appended claims forming part of the application:

One embodiment of the invention is illustrated by way of example and purely schematically in the accompanying drawing, showing a fragmentary sectional view of a conventional turbine wheel and a ceramic turbine blade seated in a dovetail groove of the turbine wheel.

Referring to the drawing, it will be seen that the turbine blade, consisting of a blade portion 1 and a root portion 2, is inserted in a dovetail groove 3 of a turbine rotor 4 and supported by means of its main seating surfaces or load carrying faces 5 on the supporting surfaces of the rotor 4.

Adjacent to the ground seating surfaces 5 the unwrought surface of the root of the blade is provided with hollows or flutes 8, the centers X of the circles defining the curvature of the flutes 8 being located in the same plane as the respective ground seating surfaces 5. It is not absolutely necessary for the flute to be cylindrical or for its center axis to be disposed accurately in the plane of the seating surface. The important thing is that the compressive forces P acting upon the seating surface 5 are introduced into these surfaces in a normal, i. e., perpendicular direction.

It will be noted from the dotted line 5 that the seating surfaces 5 are projected or extended outwardly from the conventional wedge shape blade root construction, and that, as noted above, a tangent T to the flutes or hollows 8 at the point of intersection thereof with the seating surfaces 5 forms a right angle with the seating surfaces.

While the invention has been described in detail with respect to a now preferred example and embodiment of the invention it will be understood by those skilled in the art after understanding the invention that various changes and modifications may be made without departing from the spirit and scope of the invention and it is intended, therefore, to cover all such changes and modifications in the appended claims.

What is claimed is:

1. A ceramic turbine blade having a working portion and a root portion extending therefrom for affixing said blade in position in use in a groove in the rim of a turbine, said root portion having a generally wedge shape dovetail configuration outwardly flared from said working portion and including load carrying surfaces outward ly projecting from said dovetail configuration and positioned to receive perpendicularly thereto substantially the entire forces acting on said root portion in use, said outwardly projecting surfaces being machine finished and bounded on opposite sides by concave arcuate walls which are not machine finished and the radii of curvature of which do not substantially exceed the extent of projection of said surfaces, and a tangent to said concave walls at the points of intersection with said load carrying surfaces forming substantially a right angle with said surfaces.

2. In a turbine having ceramic blades aflixed around the rim of a turbine rotor, the combination which comprises seating surfaces in said rotor rim, corresponding dovetail seating surfaces on said blade for load bearing engagement with said rotor'seating surfaces, said blade seating surfaces being outwardly and downwardly projecting from said blade and having accurately machined surfaces for fitting engagement with said rotor surfaces,

said outwardly projecting blade seating surfaces being bounded on. opposite sides by v concave curved wall portions the centers of curvature of which are substantially in the planes of said projecting seating surfaces, and said curved walls being unrnachined and 1 meeting said seating;

lie/substantially nofurther from thecenter line of saidceramic part than-saidmachine finished portions, and said concaveiarcuate walls meeting said machine finished portions at substantially a right angle.

4. A. ceramic machine part subject to substantial load stress inuse comprising a machine finished surface portion of substantial area for transmitting said load stress,

another. surface portion which is-notmachine finishedand extends beyond'said machine finished area, and concave arcuate walls joining said machine finished portion with said unmachined'portion, the centers of curvature ofsaid concavewallslying substantially no further from the center line of said ceramic part than said machine finished portion and said concave arcuate walls being unmaehined and meeting said machine finished portions at substantially a right angle.

References-Cited in the file of this patent UNITED STATES. PATENTS 1,491,079 Champion Apr. 22, 1924 2,118,795 Littleton May 24, 1938 2,183,699 Schweiker Dec. 19, 1939 2,317,338,- Rydmark Apr. 20, 1943 2,363,448 Siesel Nov. 21, 1944 FOREIGN PATENTS 664,986 Great Britain Jan. 16, 1952 821,735 Germany Nov.,19, 1951 892,785 France May 19, 1944 OTHER REFERENCES Ser; No. 285,333; Schutte' (A. P; C.), published May 25; 1943.

Ser. No. 385,334, Schutte; (A. 1 0), published May 25', 1943;

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US1491079 *Jan 20, 1921Apr 22, 1924Ac Spark Plug CoDevice for and method of forming ceramic objects
US2118795 *Sep 21, 1931May 24, 1938Corning Glass WorksInsulator
US2183699 *Apr 14, 1936Dec 19, 1939Franklin Tile CompanyMethod of fashioning tiles
US2317338 *Feb 7, 1942Apr 20, 1943Westinghouse Electric & Mfg CoTurbine blade fastening apparatus
US2363448 *Apr 27, 1943Nov 21, 1944William M SieselApparatus for manufacturing ceramic coil forms
DE821735C *Oct 2, 1948Nov 19, 1951Maschf Augsburg Nuernberg AgMehrstufige Turbine mit keramischen Laufschaufeln
FR892785A * Title not available
GB664986A * Title not available
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3025037 *Oct 24, 1957Mar 13, 1962Bert F BeckstromGas turbine
US3037458 *Apr 15, 1957Jun 5, 1962Goulds PumpsGlass pump
US4164102 *Jan 26, 1977Aug 14, 1979Daimler-Benz AktiengesellschaftProcess for the manufacture of a ceramic axial turbine wheel
US5141401 *Sep 27, 1990Aug 25, 1992General Electric CompanyStress-relieved rotor blade attachment slot
US5191711 *Dec 23, 1991Mar 9, 1993Allied-Signal Inc.Compressor or turbine blade manufacture
US5435694 *Nov 19, 1993Jul 25, 1995General Electric CompanyStress relieving mount for an axial blade
US6106188 *Jun 29, 1998Aug 22, 2000Asea Brown Boveri AgJoint between two joint partners, and its use
EP0478234A1 *Sep 20, 1991Apr 1, 1992General Electric CompanyStress-relieved rotor blade attachment slot
U.S. Classification416/219.00R, 416/241.00R, 29/889.7, 415/217.1, 416/215
International ClassificationF01D5/28, F01D5/00, F01D5/30
Cooperative ClassificationF01D5/3084, F01D5/284
European ClassificationF01D5/28C, F01D5/30K