Improved durability metallic-ceramic turbine air seals

Description

[0001] The present invention concerns a plasma sprayed graded metal-ceramic gas turbine air seal comprising starting from the substrate an initial metallic bond and a graded layer of ceramic material.

[0002] In a modern gas turbine engines working medium gases having temperatures in excess of 1093°C (2,000°F) are expanded across rows of turbine blading for extraction of power therefrom. A shroud, termed an outer air seal, circumscribes each row of turbine blading to inhibit the leakage of working medium gases over the blade tips. The limitation of the leakage of the working medium gases is crucial to the achievement of high efficiencies in such engines. The graded ceramic seals described herein were developed for specific application in gas turbine outer air seals, although other applications are clearly possible. Durable seals capable of long-term, reliable service in the hostile turbine environment were required. Specifically sought were high temperature capability and good resistance to thermal shock. In addition, the seal material must have adequate surface abradability to prevent destructive interference upon occurrence of rubbing contact of the seals by the circumscribed turbine blading.

[0003] The FR-A-918 141 describes a metal-ceramic component comprising a graded layered structure wherein the ceramic fraction changes from 100% at one interface to 0% at the other interface.

[0004] The publication "Patent Abstracts of Japan" vol. 7 No. 139 (C-171) (1284), 17th June 1983 discloses a graded metal-ceramic structure deposited onto the surface of a metal substrate by spraying, said structure comprising an undermost metal layer and an uppermost ceramic layer and therebetween intermediate layers formed so that the ceramic concentration increases upwardly.

[0005] US―A―3 091 548 to Dillion entitled "High Temperature Coatings"; 3 879 831 to Rigney et al entitled "Nickel Base High Temperature Abradable Material" 3 911 891 to Dowell entitled "Coating for Metal Surfaces and Method for Application"; 3 918 925 to McComas entitled "Abradable Seal"; 3 975 165 to Elbert et al entitled "Graded Metal-to-Ceramic Structure for High Temperature Abradable Seal Applications and a Method of Producing Same" and 4109031 to Marscher entitled "Stress Relief of Metal-Ceramic Gas Turbine Seals" are representative of the known concepts applicable to ceramic faced seals.

[0006] As is discussed in some of the above references and in particular detail in US―A―4 163 071 to Weatherly et al entitled "Method for Forming Hard Wear-Resistant Coatings", the temperature of the metallic substrate to which the ceramic coating is applied may be preheated to control either residual stress or coating density. Generally, such heating has been to a uniform temperature.

[0007] US-A-4.481 237 of common assignee with the present application, describes the production of discrete layered turbine seals wherein the seal is produced by plasma spraying discrete layers of essentially fixed composition on a metallic substrate while simultaneously varying the substrate temperature.

[0008] EP-A-0 183 638 broadens the concept and describes methods of continuous grading of mixed metal-ceramic materials.

[0009] Although many of the materials and methods described in the above patents are known to be highly desirable, the structures resulting therefrom have yet to achieve full potential, particularly in hostile environment applications. Significant research into yet improved materials and methods continues.

[0010] The plasma sprayed graded metal-ceramic gas turbine air seal of the present invention is characterized in that said bond coat is followed by a layer of constant composition of mixed alumina and MCrAIY, wherein M represents iron, nickel and cobalt and mixtures thereof, a graded layer wherein the MCrAIY concentration decreases while simultaneously the alumina concentration increases until a constant composition mixed layer of MCrAIY and A1₂0₃ is reached, a layer of predominately alumina and an outer layer of predominately zirconia.

[0011] According to the present invention, discrete graded layer seals of the type described in US patent 4 481 237 or continuously graded metal-ceramic seals of the type described in EP-A-0 183 638 are afforded substantially enhanced performance by employing as a ceramic material in the graded portion, a material having a low oxygen permeability at elevated temperatures such as alumina, mullite, or the MgO . A1₂0₃ spinel.

[0012] Additionally, oxidation resistant metallic materials are employed, particularly those of the MCrAIY type (where M is Fe, Ni or Co) and related materials.

[0013] Other concepts are described for enhancing the durability of mixed metal-ceramic seal systems. One such method involves reducing the surface area of the metallic constituent by either limiting the powder size to be relatively coarse and uniform (i.e., reducing the high surface area fine particle content), and/or employing plasma deposition parameters under which the metallic constituent does not melt completely so that upon impact it remains in a rounded form rather than assuming a high surface area splat configuration. Another approach is to preoxidize the metallic constituent.

[0014] The final concept relates to minimizing the swelling resulting from oxidation of the metallic constituent by deliberately inducing porosity into the material by cospraying a fugitive material along with the metallic-ceramic material.

[0015] In addition to the specific details relating to the mixed metal-ceramic layer, the invention also teaches the use of a thin 100% alumina layer on the mixed layer for purposes of affording total resistance to oxygen penetration and the use of a abradable ceramic layer such as zirconia as the outer seal constituent to provide abradable rubbing contact upon interaction with the moving turbine blading and to provide improved temperature capabilities.

[0016] The foregoing features and advantages of the present invention will be made more evident in light of the following description of the best mode for carrying out the invention and the accompanying drawings.

Figure 1 shows the composition profile for a seal according to the invention;

Figure 2 is a photomicrograph (25x) of a turbine air seal;

Figure 3 shows a -schematic illustration of a turbine air seal;

Figure 4 shows the variation in substrate temperature during deposition of the seal according to Figure 1; and

Figure 5 shows the oxygen permeability of zirconia and alumina.

[0017] The requirements for producing a successful graded metal-ceramic seal may be organized in two categories. The first is the physical requirements of the seal, particularly composition. The second relates to the residual strain which may be built into the system through control of substrate temperature during plasma deposition. This invention is directed at the first category, namely, the physical properties of the graded metal-ceramic layer. Aspects of the second category, namely the control of residual strain will be described as necessary to permit an understanding of the best mode of practicing the invention. These strain control aspects are described in US-A-4,481,237 (which is incorporated herein by reference) for the discrete layer case and in EP-A-0183638 (which is incorporated herein by reference) for the case of continuous grading.

[0018] Figure 1 illustrates the composition versus thickness of the best seal known to the inventors at the time of the filing of this application. Starting from the substrate and going outwards, the X axis shows seal thickness in mils and the total seal thickness is approximately 3,81 mm (150 mils). Since the seal is deposited by a plasma deposition, the seal thickness will actually vary in a stepwise fashion from one layer to the next, however, since each layer is in the order of 25.4 µm (1 mil) thick the continuous curve of Figure 1 is a more than adequate description of the seal composition.

[0019] Starting from the substrate there is an initial metallic bond coat of a composition known as Metco 443 which is a commercially available material formed from an agglomeration of nickel chromium powder and aluminum powder which upon plasma spraying undergoes an exothermic reaction which is believed to aid in the adherence of the bond coat to the substrate. Following the deposition of the bond coat the next 508 µm (20 mils) are of a constant composition of 60% CoCrAIY (nominal composition of Co-23cr-13AI-0.65Y) having a particule size of 0.044 to 0.149 mm (-100+325 U.S. Standard Sieve) and 40% alumina. Following the deposition of this constant composition layer, continuous grading occurs over the next 6.35 um (25 mils) or so until a composition of 20% CoCrAIY and 80% alumina is reached. This composition is maintained constant for about 254 µm (10 mils) then the grading continues until a composition of 100 alumina is achieved. One layer (25.4±12.7 µm) (1±.5 mil) of 100% alumina is then deposited, it has been found that the absence of all alumina layer detracts from oxidation performance but that multiple layers are detrimental to mechanical behavior. Finally an outer layer of zirconia is applied to provide abradability and temperature capability (A1₂0₃ melts at -2000°C while Zr0₂ melts at -2700°C). Alumina is a harder, stronger material than zirconia and alumina as the outer layer would not have the desired abradable qualities. To further increase the abradability of the zirconia deliberate porosity is induced in the zirconia in the outer portion thereof, pososity on the order of about 19%. This is accomplished by adding a fugitive material (such as Metco 600 polyester or DuPont Lucite®), to the ceramic material and subsequently removing the fugitive by baking at a high temperature to vaporize the fugitive material. Accordingly, Figure 1 describes in some detail the apparent physical characteristics of a preferred embodiment of the present invention. It should also be apparent that the various details of the present invention could be readily applied to the discrete layered system described in US-A-4,481,237.

Figure 2 is a photomicrograph of the resultant structure. The metallic constituent is light in color, the alumina is dark gray, the zirconia is light gray and the porosity is black.

Figure 3 is a schematic or a turbine air seal showing the arrangement or layers, the plasma torch and the substrate heating.

Figure 4 illustrates the temperature control of the substrate which is employed during plasma spraying to attain the desired and necessary substrate prestrain conditions. The substrate temperature is maintained at a relatively high level during deposition of the bond coat and is then reduced. Thereafter the substrate temperature is increased generally in parallel with the ceramic content and eventually reaches a level above that employed during deposition of the bond coat and then tapers off during the deposition of the outer abradable ceramic material.

[0020] A primary aspect of this invention is the substitution of a material which is resistant to the diffusion of oxygen at elevated temperatures. Three such materials have been identified for seal application. These are alumina, mullite and the MgO - A1₂0₃ spinel.

[0021] Figure 5 shows the permeability of stabilized zirconia and alumina over a temperature range at 6666 Pa (50 Torr) partial pressure of oxygen. It can be seen that at 1600°C the permeability of oxygen in alumina is less than about 10^-10 and it is about 3 orders of magnitude less than the permeability of oxygen in zirconia at the same temperature. The other suggested materials, mullite and the spinel, both have oxygen permeability which are less than 10% of that of zirconia at elevated temperatures.

[0022] Additionally, oxidation resistant materials selected from the group consisting of the MCr materials where chromium ranges from about 20 to about 40% the MCrAI materials where chromium ranges from about 15 to about 45% and aluminum ranges from about 7 to about 15%; the MCrAIY materials where chromium ranges from about 15 to about 45%, aluminum ranges from about 6 to about 20% and yttrium ranges from about 0.1 to about 5%; and the MCrAIHf materials where chromium ranges from about 15 to about 45%, aluminum ranges from about 7 to about 15% and hafnium ranges from about 0.5 to about 7%. In all of these materials "M" is selected from the group consisting of nickel, cobalt, iron and mixtures thereof with mixtures of nickel and cobalt being particularly favored, the yttrium (when present) may be partly or wholly replaced by lanthanum, cerium, Misch metal and mixtures thereof, additionally, up to 10% of a material selected from the group consisting of platinum, tungsten, rhenium, silicon, tantalum and manganese may be added to any of these materials are utilized.

[0023] Table I presents oxidation data for two compositions based on ceramic-CoCrAIY materials. In one composition the ceramic is zirconia and the other the ceramic is alumina, in both compositions the CoCrAIY content was the same volume percent. These materials were tested at 1038°C (1900°F) for 150 hours. The results are presented in the table. It can be seen that the zirconia base material gained 3.3% in weight due to oxidation of the metallic constituent and underwent a longitudinal expansion of 3.4% due to swelling of the material caused by the oxidation of the metallic constituent. Under the same condition the alumina based material gained 2.1% in weight, (a reduction of 37% compared to the zirconia based material), and shrank 0.5% in length. The information in Table I supports the basic premise of the invention which that the substitution of alumina for the commonly used zirconia material in mixed metal-ceramic systems provides substantial seal performance benefits.

[0024] Table II shows the benefit obtained through minimizing the surface area of the metallic constituent by sieving out the fine particles. In Table II both compositions were based on the zirconia ceramic which serves as a valid baseline for demonstrating the benefits obtained by employing coarse particles. Table II shows the weight change results of two materials both of which had the same composition of 85% zirconia, 15% CoCrAIY, the difference between the two samples being that one was produced from a wide size range metallic powder composition of 0.044 to 0.149 mm (-100+325 mesh) while the other was produced from metallic material having 0.074 to 0.149 mm (-100+200 mesh) (the mesh sizes referred to are those described in the U.S. Standard Sieve Series; -100 describes all those particles which will pass through a wire mesh having square openings 0.149 millimeters on a side, +325 mesh means that the material will be retained on a wire mesh having average openings of 0.044 millimeters and +200 mesh means the material will be retained on a mesh having an average opening of 0.074 millimeters on a side). Thus the essential difference between the two compositions is that the particles which would pass through the 0.074 mm (200 mesh) screen were rejected in the second composition but were retained in the first composition. From Table 11 it is clear that the elimination of fine particles plays a significant role in reducing weight change due to oxidation. In this experiment the dimensional changes were not evaluated.

[0025] Very preliminary experiments were performed using CoCrAIY material which had been deliberately preoxidized for about 6 hours at about 204°C (400°F) to produce an alumina layer on the surface of the powder which would serve to retard further oxidation. It appears from the very preliminary work done that a reduction in oxidation of about 20% can be achieved through this technique.

[0026] Table III present basic information on the effect of including deliberate porosity on the performance of alumina-CoCrAIY composites produced by plasma spraying. From Table III it is evident that material 'which contained 4% polyester and therefore contains some amount of porosity (about 2%) exhibited slightly increased weight change due to oxidation but rather significantly decreased dimensional changes. Thus, the deliberate inclusion of porosity is an area which will require careful attention by the skilled artisan.

[0027] 

[0028] The final suggested technique for reducing oxidation and resultant swelling is to perform the plasma spraying under conditions which do not entirely melt the metallic constituent so that the metallic constituent will retain a more nearly spheroidal configuration within the graded coating rather than assuming a completely flattened splat configuration which will result if total melting occurs. Observed aspect ratios (length:thickness) in totally melted materials are from about 5:1 to about 10:1, reduced surface areas result when aspect ratios of about 3:1 or less are produced. This result may be accomplished by adjusting the position within the plasma torch where the metallic constituent is injected so that the metallic constituent has a short residence time within the plasma zone and does not melt completely. The use of coarse particles also assists in controlling aspect ratio.

[0029] The effective commercial production of -the graded seal described in Figures 1 and 2 at the beginning of this section requires some refined plasma spraying techniques which are not known in the art and which are the subject of commonly assigned EP-A-0 183 637 and EP-A-0 183 638. EP-A-0 183 638 describes the temperature management schemes, for continuously graded coatings, which were previously mentioned with respect to Figure 1 and which produce the necessary prestrain in the coating which permit the coating to withstand severe conditions at elevated temperatures without spallation. EP-B-0 185 604 deals with a plasma spray powder management system which has been employed to produce the mixed powder combinations in a highly controllable and reproducible fashion. The essentials of the system are accurate measurements of carrier gas flow and pressure coupled with x-ray measurements of the gas plus powder stream, these measurements are supplied to a controlling microcomputer which generates signals necessary to control the flow and the flow of the various powders. EP-A-0 183 637 deals with the powder flow gauging techniques which are used to measure the actual powder streams and to control their flow. Briefly, the x-ray gauging system uses flow and pressure sensors to provide accurate measurements of carrier gas flow and uses a transmission x-ray apparatus to give an indication of the total mass flow of powder plus carrier gas. From these measurements the mass flow rate can be accurately calculated. Knowing the actual powder mass flow rate one can employ control circuitry to control and constrain the powder flow rate to follow a predetermined schedule.

Claims

1. A plasma sprayed graded metal-ceramic gas turbine air seal comprising starting from the substrate an initial metallic bond and a graded layer of ceramic material, characterized in that said bond coat is followed by a layer of constant composition of mixed alumina and MCrAIY, wherein M represents iron, nickel and cobalt and mixtures thereof, a graded layer wherein the MCrAIY concentration decreases, while simultaneously the alumina concentration increases until a constant composition mixed layer of MCrAIY and A1₁0₃ is reached, a layer of pre- dominantely alumina and an outer layer of pre- dominantely zirconia.

2. The gas turbine air seal according to claim 1 characterized in that it contains up to 20%, by volume, of porosity so as to accommodate swelling resulting from oxidation of the metallic constituent.

3. The gas turbine air seal according to claim 1 characterized in that the graded layer is present in the form of discrete layers of essentially constant composition.

4. The gas turbine air seal according to claim 1 characterized in that the deposited metallic particles have an aspect ratio of less than about 3:1.

5. The gas turbine air seal according to claim 1 characterized in that the graded layer varies in essentially a continuous fashion from metallic to ceramic.

6. The gas turbine air seal according to claim 1 characterized in that the ceramic material has an oxygen permeability constant which is less than about 10-⁸ gm cm-¹ sec-1 at 1600°C and 6666 Pa (50 Torr) oxygen partial pressure as the ceramic constituent so that the metallic constituent is isolated and protected from oxygen and the graded structure is thereby rendered more durable at elevated temperature under oxidizing conditions.

7. The gas turbine air seal according to claim 1 characterized in that the outer layer of zirconia is a layer of stabilized zirconia.

Ansprüche

1. Plasmagespritzte, gestaffelte Metall-Keramik-Gasturbinenluftabdichtung mit, ausgehend von dem Substrat, einer anfänglichen metallischen Bindung und einer gestaffelten Schicht keramischen Materials, dadurch gekennzeichnet, daß sich an den Bindungsüberzug eine Schicht konstanter Zusammensetzung aus Aluminiumoxid gemischt mit MCrAIY, wobei M Eisen, Nickel and Kobalt sowie Gemische derselben darstellt, eine gestaffelte Schicht, in der die MCrAIY-Konzentration abnimmt, während gleichzeitig die Aluminiumoxidkonzentration zunimmt, bis eine eine konstante Zusammensetzung aufweisende gemischte Schicht aus MCrAIY und A1₂0₃ erreicht ist, eine Schicht aus überwiegend Aluminiumoxid und eine äußere Schicht aus überwiegend Zirkonoxid anschließen.

2. Gasturbinenluftabdichtung nach Anspruch 1, dadurch gekennzeichnet, daß sie bis zu 2 Vol.-% Porosität aufweist, um eine Schwellung zu kompensieren, welche aus der Oxidation des metallischen Bestandteils resultiert.

3. Gasturbinenluftabdichtung nach Anspruch 1, dadurch gekennzeichnet, daß die gestaffelte Schicht in Form von diskreten Schichten mit im wesentlichen konstanter Zusammensetzung vorliegt.

4. Gasturbinenluftabdichtung nach Anspruch 1, dadurch gekennzeichnet, daß die aufgetragenen metallischen Partikel ein Längenverhältnis von weniger als etwa 3:1 haben.

5. Gasturbinenluftabdichtung nach Anspruch 1, dadurch gekennzeichnet, daß sich die gestaffelte Schicht auf im wesentlichen kontinuierliche Weise vom Metall zur Keramik verändert.

6. Gasturbinenluftabdichtung nach Anspruch 1, dadurch gekennzeichnet, daß das keramische Material eine Sauerstoffpermeabilitätskonstante hat, die kleiner als etwa 10-⁸ g cm-¹ s^-1 bei 1600°C und 6666 Pa (50 Torr) Sauerstoffpartialdruck im keramischen Bestandteil ist, so daß der metallische Bestandteil vom Sauerstoff getrennt und vor dem Sauerstoff geschützt ist und dadurch die gestaffelte Struktur bei erhöhter Temperatur unter oxidierenden Bedingungen dauerhafter gemacht wird.

7. Gasturbinenluftabdichtung nach Anspruch 1, dadurch gekennzeichnet, daß die äußere Schicht aus Zirkonoxid eine Schicht aus stabilisiertem Zirkonoxid ist.

Revendications

1. Joint étanche à l'air échelonné en métal/ matière céramique pour une turbine à gaz, pulvérisé sous plasma et comprenant, à partir du substrat, une liaison métallique initiale et une couche échelonnée de matière céramique, caractérisé en ce que ce revêtement de liaison est suivi d'une couche d'une composition constante d'alumine mixte et de MCrAIY où M représente le fer, le nickel et le cobalt, ainsi que leurs mélanges, une couche échenlonnée dans laquelle la concentration en MCrAIY diminue tandis que, dans le même temps, la concentration en alumine augmente jusqu'à ce qu'on atteigne une couche mixte de composition constante de MCrAIY et d'A1₂0₃ une couche constituée principalement d'alumine et une couche extérieure constituée principalement d'oxyde der zirconium.

2. Joint étanche à l'air pour une turbine à gaz selon la revendication 1, caractérisé en ce qu'il contient jusqu'à 20% en volume de porosité de façon à faire face au gonflement résultant de l'oxydation du constituant métallique.

3. Joint étanche à l'air pour une turbine à gaz selon la revendication 1, caractérisé en ce que la couche échelonnée est présente sous forme de couches discrètes d'une composition essentiellement constante.

4. Joint étanche à l'air pour une turbine à gaz selon la revendication 1, caractérisé en ce que les particules métalliques déposées ont un rapport d'élancement inférieur à environ 3:1.

5. Joint étanche à l'air pour une turbine à gaz selon la revendication 1, caractérisé en ce que la couche échelonnée varie essentiellement de manière continue du métal à la matière céramique.

6. Joint étanche à l'air pour une turbine à gaz selon la revendication 1, caractérisé en ce que la matière céramique a une constante de perméabilité à l'oxygène inférieure à environ 10-⁸ gm cm-¹ sec ' à 1.600°C et sous une pression partielle d'oxygène de 6.666 Pa (50 Torrs) comme constituant céramique, si bien que le constituant métallique est isolé et protégé contre l'oxygène, tandis que la structure échelonnée est ainsi rendue plus durable à une température élevée et dans des conditions oxydantes.

7. Joint étanche à l'air pour une turbine à gaz selon la revendication 1, caractérisé en ce que la couche extérieure d'oxyde de zirconium est une couche d'oxyde de zirconium stabilisé.

Drawing