Patent Application
20140202170
The disclosure relates to gas turbine engines. More particularly, the disclosure relates to fluid ducts.
In an exemplary gas turbine engine, ducting can be fabricated using a variety of processes, such as a composite layup or forming a sheet metal to the desired shape using a combination of cutting, bending, welding, and/or stamping processes. US8273430B2 discloses an alternative in which ducting is formed of a metallic inner layer and a polymeric outer layer by a stamping process.
One aspect of the disclosure involves an article having a polymeric substrate and a coating system. The coating system includes a metallic plating and a polymeric coating atop the metallic plating. The metallic plating has a thickness of at least 0.05 mm.
In further embodiments of any of the foregoing embodiments: the coating system comprises the polymeric coating atop the metallic plating along a majority of an interior surface area; and along a majority of an exterior surface area, the coating system comprises the metallic plating without the polymeric coating.
In further embodiments of any of the foregoing embodiments, the matrix is a thermoplastic material forming a majority of the substrate by weight.
In further embodiments of any of the foregoing embodiments, the substrate comprises polyetherimide, thermoplastic polyimide, or polyether ether ketone (PEEK).
In further embodiments of any of the foregoing embodiments: the substrate comprises polyetherimide or thermoplastic polyimide; and the polymeric coating comprises PEEK.
In further embodiments of any of the foregoing embodiments, the substrate has a thickness of 1.27-6.35 mm.
In further embodiments of any of the foregoing embodiments, the metallic plating forms at least 30% by weight of the article.
In further embodiments of any of the foregoing embodiments, the metallic plating comprises nickel as a largest by-weight content.
In further embodiments of any of the foregoing embodiments, the metallic plating has a thickness of at least 0.25 mm.
In further embodiments of any of the foregoing embodiments, the metallic plating imparts the principal strength of the article.
In further embodiments of any of the foregoing embodiments, the polymeric coating comprises PEEK.
In further embodiments of any of the foregoing embodiments, the polymeric coating has a thickness of 0.5-2.0 mm.
In further embodiments of any of the foregoing embodiments, the article is a turbine engine duct having: a first flange having an opening; a second flange having an opening; and a conduit connecting the openings.
In further embodiments of any of the foregoing embodiments, the turbine engine duct is at least one of: an air oil cooler inlet duct; an air oil cooler outlet duct; a precooler inlet duct; and an active clearance control inlet duct.
In further embodiments of any of the foregoing embodiments, a gas turbine engine has: a compressor section; a combustor downstream of the compressor section along a core flowpath; a turbine section downstream of the combustor along the core flowpath and coupled to the compressor section to drive the compressor section and the article as an air duct.
In further embodiments of any of the foregoing embodiments, a method for manufacturing the article comprises: molding the substrate; plating the molded substrate to form the metallic plating; and applying the polymeric coating to the metallic plating.
In further embodiments of any of the foregoing embodiments, the applying comprises spraying.
In further embodiments of any of the foregoing embodiments, the plating is electroless plating, electrolytic plating, or electroforming.
The details of one or more embodiments are set forth in the accompanying drawings and the description below. Other features, objects, and advantages will be apparent from the description and drawings, and from the claims.
Like reference numbers and designations in the various drawings indicate like elements.
The core flowpath 522 proceeds downstream to an engine outlet 36 through one or more compressor sections, a combustor, and one or more turbine sections. The exemplary engine has two axial compressor sections and two axial turbine sections, although other configurations are equally applicable. From upstream to downstream there is a low pressure compressor section (LPC) 40, a high pressure compressor section (HPC) 42, a combustor section 44, a high pressure turbine section (HPT) 46, and a low pressure turbine section (LPT) 48. Each of the LPC, HPC, HPT, and LPT comprises one or more stages of blades which may be interspersed with one or more stages of stator vanes.
In the exemplary engine, the blade stages of the LPC and LPT are part of a low pressure spool mounted for rotation about the axis 500. The exemplary low pressure spool includes a shaft (low pressure shaft) 50 which couples the blade stages of the LPT to those of the LPC and allows the LPT to drive rotation of the LPC. In the exemplary engine, the shaft 50 also directly drives the fan. In alternative implementations, the fan may be driven via a transmission (e.g., a fan gear drive system such as an epicyclic transmission between the fan and the low pressure spool) to allow the fan to rotate at a lower speed than the low pressure shaft. Also, although shown as an axial two-spool engine, other spool counts and configurations may be used.
The exemplary engine further includes a high pressure shaft 52 mounted for rotation about the axis 500 and coupling the blade stages of the HPT to those of the HPC to allow the HPT to drive rotation of the HPC. In the combustor 44, fuel is introduced to compressed air from the HPC and combusted to produce a high pressure gas which, in turn, is expanded in the turbine sections to extract energy and drive rotation of the respective turbine sections and their associated compressor sections (to provide the compressed air to the combustor) and fan.
The duct 74 includes a sidewall 128 extending between the flanges 122 and 126 and cooperating therewith to define respective inlet and outlet ports 130 and 132.
Each of the exemplary flanges 122 and 126 has a front (mounting) face 134, 136 and a rear face 138, 140.
One or both of the exemplary flanges may include mounting holes 142. Additionally, the duct may include ports and/or integral fittings (of which an exemplary integral fitting 144 is shown) and/or further mounting features.
The article comprises a substrate 160 and a coating 162 (
The exemplary substrate is an injection-molded or compression-molded piece formed of: at least one of polyetherimide (e.g., trademark ULTEM of SABIC Innovative Plastics Holding BV, Pittsfield, Mass.); thermoplastic polyimide (e.g., trademark EXTEM of SABIC Innovative Plastics Holding BV, Pittsfield, Mass.; polyether ether ketone (PEEK); or any of the foregoing with fiber reinforcement e.g., carbon fiber or glass-fiber). An exemplary substrate comprises a single one of the forgoing as a by-weight majority (more particularly as just a single material and not in a block co-polymer).
In a particular example of an AOC inlet duct, or other embodiment, an initial precursor is molded by injection (or compression) molding using RTP 2185, a carbon-fiber-reinforced grade of ULTEM polyetherimide. The mold will include at least two retractable (or removable) inserts to achieve the desired angled internal flow path and mounting features (additionally or alternatively, some such features (e.g., flanges or bosses) may be bonded on using a suitable adhesive after molding but before plating to simplify the mold tooling). Holes for attachment (e.g., by bolt, rivets, etc.) are machined in the molded part (unless they were included in the mold tooling; however, there might be finish machining of molded holes or other features). It is preferable that no mold release, or comparable chemical agents, be used during the molding process to facilitate a strong bond between the plating and polymer (however, in certain instances, depending on mold release formulation and/or part requirements, a mold release could be used and/or a cleaning process may remove mold release residue).
Exemplary substrate thickness Ts is 0.05-0.2 inch (1.3-5 mm, more particularly 2.0-4.0 mm). The thickness may be a local thickness or a thickness over a majority of a surface area of the substrate or as a mean, median or modal value over the substrate. The substrate may be formed with various flanges, ribs, gussets, bosses and the like. These may cause substantial local departures in substrate thickness, coating gaps, etc.
The exemplary metallic layer 164 provides fire protection and imparts the principal strength of the article (as indicated by mechanical test results of representative test specimens or part cut-ups as compared to mechanical test results of the polymeric part with no or little plating). The exemplary metallic layer 164 also forms at least 30% by weight of the article, more particularly 40%-80% or 55%-70%.
Exemplary metal is nickel or by-weight majority nickel with an ultimate tensile strength of at least 60 ksi (414 MPa). Exemplary metal is applied by electroless plating, electroplating or electroforming (specifications for electroforming are sometimes more applicable to thick platings than electroplating specifications are) to a thickness TM of 2-50 thousandths of an inch (0.05-1.3 mm, more narrowly 0.25-1.0 mm, or alternatively at least 0.25 mm yet thinner than the substrate while still at least 0.05 mm, or alternatively, at least 0.20 mm). The thickness may be a local thickness or a thickness over a majority of a surface area (either of the substrate as a whole or of the plated portion of the substrate) or as a mean, median or modal value over the substrate as a whole or a plated portion thereof.
The molded precursor can be masked to provide localized areas that are unplated (e.g., that are not conductive, can be bonded using adhesives that are well-suited for polymers, and/or allow for outgassing of the polymer during high-temperature excursions), if desired, although the amount of masking should be minimal (to maximize strength and structural integrity). The plating material is typically pure Ni or a hardened Ni applied from a Ni sulfamate solution. Other plating materials, such as Ni—P or Ni—Co, can be applied to achieve certain results. Also, different plating solutions, such as Ni sulfate, can be used to deposit the plating resulting in a different set of properties. A typical plating for this application would be a low-stressed Ni plating (per AMS 2424) or a hardened Ni plating (per AMS 2423) applied using a Ni sulfamate bath.
In the example, plating is applied to internal passages and holes in the part, provided they are sufficiently large for the plating solution to deposit material. If desired, holes can be machined into the plated polymer structure to accommodate attachment, etc. rather than incorporating holes in the mold or machining them before plating.
In the particular example or other embodiment, there may be a post-plating cleaning/washing to remove any plating solution.
The exemplary polymer coating 166 protects the metal against impact or foreign object damage and environmental corrosion. The outer polymer coating may provide the first line of defense against nicks, dents, and scratches, helping to prolong part life by delaying damage to the plating that can eventually lead to crack initiation and propagation.
The exemplary polymer coating 166 is a PEEK coating (e.g., trademark VICOTE of Victrex plc., Lancashire, GB).
The polymer coating may be applied by spraying (e.g., thermal spray or electrostatic or dispersion spray) to a thickness of Tc of 0.1-2.0 mm, more narrowly 0.25-1.0 mm. The thickness may be a local thickness or a thickness over a majority of a surface area (either of the substrate as a whole or of the plated and coated portion of the substrate) or as a mean, median or modal value over the substrate as a whole or a plated and coated portion thereof.
If desired, the part can be masked before spraying to apply the polymer coating only in areas of interest. For example, the portions of the duct ultimately exposed to an external environment may be masked to leave the ultimate duct with exposed metal exterior for fire-resistance (e.g., only the internal passage of the duct will be coated).
Relative to a pure metal article, the composite may be easier to manufacture. Complex shapes might require complex machining, stamping/bending, welding, or other steps. In contrast, a polymeric part may be easier to mold in a convoluted shape. In addition, the polymer-metal composite part has a lower weight than a metal part of the same size and geometry. Further, in many cases, injection molding and conventional plating processes have lower unit costs than composite layups or metal forming, welding, etc. Also, the process may allow for simple modular changes by using a different polymer in the molding process and/or a different plating bath setup to achieve a range of desired properties.
Relative to a pure polymeric article or an article with only a thin metal layer, the composite may be thinner, thereby providing greater use flexibility where a thicker structure would not fit. Also the metal may increase resistance to particular impact or foreign object damage (FOD). Furthermore, the thicker plating provides structure that is capable of significantly higher loads, in excess of those typical of injection-molded polymers in the flow direction (best-case property, not achieved throughout a molded part). The thicker plating is also capable of maintaining part geometry while under load during a fire.
The AOC exhaust duct 76 of
The precooler inlet duct 84 of
The ACC inlet duct 92 of
One or more embodiments have been described. Nevertheless, it will be understood that various modifications may be made. For example, when implemented as a replacement for a baseline part, details of the baseline may influence details of any particular implementation. Accordingly, other embodiments are within the scope of the following claims.
