Patent Application
20160169012
This disclosure relates to methods for plating metallic layers onto molded polymeric articles for producing lightweight plated polymer components for gas turbine engines. More specifically, this disclosure relates to a method that includes molding a polymer article having a desired geometry and then plating the outer surface of the polymer article with metallic layers using electroless plating, electrolytic plating, or electroforming methods to produce lightweight metal parts that can be incorporated into gas turbine engines.
Metal parts tend to be heavy due to the high densities of most metals. In certain instances, removing material from a metal part can lead to weight savings. For example, the stresses imposed upon a metal part in service may be analyzed. Typically, there are areas of the metal part that have little or no stress as well as highly stressed areas. An ideal metal part may contain a sufficient amount of metal in highly stressed areas to transmit the necessary loads and perform the function of the part. However, such an ideal part would contain less or no material in areas with little or no stress, respectively, thereby reducing the weight of the metal part to an idealized minimum Therefore, there is a need for improved methods of providing metal parts that are lightweight but strong enough in high stress areas to perform the function of the part.
However, removing material from the metal part by conventional means, such as machining, laser drilling, etc., is both difficult and costly. Further, removing material from a metal part can lead to reduced material properties of the part, which may be unacceptable. Thus, simply removing metal from a formed metal part is less than ideal in certain parts and situations.
Gas turbine engines designed for aircraft include thousands of metal parts. Because the weight of an aircraft, including the engine, is directly related to fuel consumption, engine and aircraft manufacturers are constantly seeking new technologies that will help them reduce the weight of their engines and aircraft respectively. One strategy involves substituting traditional metal parts for lightweight polymer or composite parts. For example, non-metal containment structures for gas turbine engines may include, for example, KEVLAR® (a registered trademark of E.I. Dupont de Nemours & Company) or another ballistic fabric wrapped around a case. Containment systems that include fabric are more weight efficient than all-metal containment cases, but nonetheless add weight to the engine.
Additive manufacturing (AM) or three-dimensional (3D) printing is a process of making a three-dimensional solid object of virtually any shape from a digital model. AM is achieved by depositing successive layers of material in different cross-sectional shapes. AM is considered distinct from traditional machining techniques, which mostly rely on the removal of material by methods such as cutting or drilling, i.e., subtractive processes. A materials printer usually performs AM processes using digital technology. Since the start of the twenty-first century there has been a large growth in the sales of these machines, and while the price has dropped substantially, AM remains costly. Despite its high cost, though, AM is used in many fields, including aerospace.
Less costly alternatives to AM include various molding processes, such as blow molding, injection molding, compression molding, and others that will be apparent to those skilled in the art. Blow molding processes begin with melting the molding material and forming it into a parison or preform. The parison is a tube-like piece of plastic with a hole in one end through which compressed air can pass through. The parison is clamped into a mold and air is pumped into the parison. The air pressure pushes the molding material outwards to match the interior surface of the mold. Once the molding material has cooled and hardened, the mold opens and the part is ejected. In contrast, injection molding includes injecting molding material for the part into a heated barrel, mixing, and forcing the molding material into a mold cavity where the molding material cools and hardens to the configuration of the cavity. Compression molding is a method of molding in which the preheated molding material is placed in an open mold cavity. The mold is closed and pressure is applied to force the material into contact with all mold areas, while heat and pressure are maintained until the molding material has cured.
For many molding processes, hard tooling is used to form the mold or die. While hard tooling can provide a high dimensional repeatability, hard tooling is very heavy and cumbersome and can present a safety hazard when moved or handled. Further, fabricating hard tooling is time consuming and costly. As a result, hard tooling is normally too expensive and time consuming for short production runs and/or for the fabrication of test parts. Thus, the ability to quickly fabricate tooling to support short production runs and/or test runs of composite materials is desired.
Blow molding and injection molding cannot be used if the polymer to be molded is in the form of a composite with a plurality of layers or plies, i.e., a composite layup structure. Composites are materials made from two or more constituent materials with significantly different physical or chemical properties that, when combined, produce a material with characteristics different from the individual components. The individual components remain separate and distinct within the finished structure. Typically, composite layup structures can be molded or shaped using compression molding, resin transfer molding (RTM) or vacuum assisted resin transfer molding (VARTM), all of which utilize hard tooling that typically include details machined into one or more blocks of metal that form the mold.
Composites can also include reinforcing fibers or matrices. The fibers or matrices may be formed from ceramic, metal, combinations of ceramic and metal, concrete and various other inorganic and organic materials. Organic matrix composites (OMCs) may include polyimides and/or bismaleimides (BMIs) because they can be used at higher temperatures than other commonly used organic reinforcing materials, such as epoxies. Such high-temperature OMCs may be processed by autoclave molding, compression molding, or resin-transfer molding. These processes all require lengthy cure and post-cure cycles as well as hard tooling that is difficult and costly to make. Further, only tooling with limited geometrical complexity can be produced. Thus, improved methods for molding OMCs are also desired.
One inexpensive method of forming a metallic layer on a surface of a molded polymer article is electroless plating. To ensure adhesion of the plated film to the molded polymer article, the surface of the polymer article may need to be prepared by etching, abrading, or ionic activation. The most common types of metals used for plating on polymers are copper, silver, and nickel, although other metals can be used.
Electrolytic plating is the deposition of a metal on a conductive material using an electric current. A molded polymer article must first be made conductive to be electrolytically plated. This can be done through electroless plating or by the use of conductive additives such as carbon. The article to be electrolytically plated is immersed in a solution of metal salts connected to a cathodic current source, and an anodic conductor is immersed in the bath to complete the electrical circuit. Electric current flows from the cathode to the anode, and the electron flow reduces the dissolved metal ions to pure metal on the cathodic surface. The anode is usually made from the same metal, and can dissolve during the electroplating process, thereby replenishing the bath.
The operating temperature of a plated polymer article, component or part may be limited by the polymeric substrate. Thus, parts for a gas turbine engine may not be able to be fabricated from a polymer material or a reinforced polymer material if the part is within a line-of-sight to a heat source, such as a combustor, which may transfer heat to the part by radiation. Because of the operating conditions of a gas turbine engine and the need to save weight, lightweight polymer parts that can withstand relatively high operating temperatures for polymers (>150° C.) are needed in the aircraft and/or gas turbine engine industries.
Another issue associated with gas turbine engines is noise. Suppression of gas turbine engine noise has become an important field of research due to airport regulations and aircraft noise certification requirements that govern the maximum noise level that aircraft are allowed to produce. Further, because the principal sources of noise from a commercial aircraft are the engines, reducing noise emitted by such engines is desirable. Thus, there is a need for gas turbine engine structural components that are both lightweight and that include sound attenuation properties.
Plated polymer components for gas turbine engines are disclosed. The disclosed components may include a molded polymeric substrate plated with at least one metallic layer and, optionally, at least one polymer layer.
Methods are also disclosed for fabricating such plated polymer components of gas turbine engines. The disclosed methods may include forming a polymer into a desired shape having an outer surface. The method may further include preparing the outer surface to receive a catalyst and activating the outer surface with the catalyst. The method may then include plating a first metal onto the outer surface and the catalyst to form a structure, and optionally followed by plating one or more additional layers until a desired thickness is reached. The plated structure may optionally be coated with a polymeric coating.
In accordance with an aspect of the disclosure, a gas turbine engine component is provide. The component may include a first at least one polymeric substrate forming the gas turbine engine component and having a first at least one exposed surface. A first at least one metallic plating layer may be deposited on the first at least one exposed surface of the first at least one polymeric substrate.
In accordance with another aspect of the disclosure, the at first least one polymeric substrate may be formed into a housing for one of a full authority digital engine control (FADEC), an induction head, a computer, a radio, an electrical actuator, a pump, and a valve.
In accordance with yet another aspect of the disclosure, the first at least one metallic plating layer may be ferro-magnetic.
In accordance with still yet another aspect of the disclosure, the first at least one polymeric substrate may be formed into one of an instrumentation probe, a waveguide, a heat exchanger, and a piston rod.
In further accordance with another aspect of the disclosure, the first at least one polymeric substrate may be formed into a diffuser case. The first at least one metallic plating layer may be highly polished to reflect radiant heat.
In further accordance with yet another aspect of the disclosure, the first at least one polymeric substrate may surround a central conductor.
In further accordance with still yet another aspect of the disclosure, the first at least one polymeric substrate may be formed into a support tubing. The support tubing may have a central channel. The first at least one metallic plating layer may be surrounded by a first at least one polymeric layer. The at least one polymeric layer may be surrounded by a second at least one metallic plating layer.
In further accordance with an even further aspect of the disclosure, the first at least one metallic plating layer may be a first at least one metallic plating wire.
In further accordance with yet an even further aspect of the disclosure, the second at least one metallic plating layer may be a second at least one metallic plating wire.
In further accordance with still yet an even further aspect of the disclosure, the first and second at least one metallic plating wire may be in a spiral configuration.
In even further accordance with another aspect of the disclosure, the first at least one polymeric substrate forming the support tubing may include gear-like teeth. The gear-like teeth may include insulating channels between teeth. The first at least one metallic plating layer may be deposited in one of the insulating channels.
In even further accordance with yet another aspect of the disclosure, a connector may be bonded to the first at least one metallic plating layer and to the second at least one metallic plating layer.
In accordance with another aspect of the disclosure, a gas turbine engine is provided. The engine may include a full authority digital engine control (FADEC) housing including a first at least one polymeric substrate having a first at least one exposed surface. A first at least one metallic plating layer may be deposited on the first at least one exposed surface.
In accordance with yet another aspect of the disclosure, the engine may further include at least one gas turbine engine component. The component may include a second at least one polymeric substrate having a second at least one exposed surface and a second at least one metallic plating layer deposited on the second at least one exposed surface. The second at least one polymeric substrate may be formed into one of an induction head housing, a computer housing, a radio housing, an electrical actuator housing, a pump housing, a valve housing, an instrumentation probe, a waveguide, a heat exchanger, a piston rod, and a diffuser case.
In accordance with another aspect of the disclosure, a method of fabricating a component for a gas turbine engine is provided. The method entails forming a first at least one polymeric substrate in a desired shape of the component. Antoher step may be depositing a first at least one metallic plating layer on a first at least one exposed surface of the first at least one polymeric substrate.
In accordance with yet another aspect of the disclosure, the desired shape may be one of a full authority digital engine control (FADEC) housing, an induction head housing, a computer housing, a radio housing, an electrical actuator housing, a pump housing, a valve housing, an instrumentation probe, a waveguide, a heat exchange, a piston rod, and a diffuser case.
In accordance with still yet another aspect of the disclosure, the desired shape may be a cable surrounding a central conductor.
In accordance with an even further aspect of the disclosure, the desired shape may be a supporting tube having a central channel.
In accordance with still an even further aspect of the disclosure, another step may be coating the first at least one metallic plating layer with a first at least one polymeric layer.
In accordance with still yet an even further aspect of the disclosure, another step may be depositing a second at least one metallic plating layer on the first at least one polymeric layer.
Other aspects and features of the disclosed systems and methods will be appreciated from reading the attached detailed description in conjunction with the included drawing figures. Moreover, selected aspects and features of one example embodiment may be combined with various selected aspects and features of other example embodiments.
Electrical cables are involved in transmitting electrical signals between locations to provide power or electrical communication for various applications such as automotive and aerospace applications. The traditional construction of an electrical cable consists of a signal-conducting central core surrounded by a heavy shielding of a conductive material. The central conductor may consist of copper or aluminum and the shielding may consist of copper or a conductive polymer. The shielding layer may shield the central conductor from external electromagnetic noise and may also be involved in signal transmission. Between the central conductor and the shielding layer may be an insulating layer which may insulate the central conductor and the shielding, while also providing mechanical protection to these conductive layers. However, as masses of cables may be bundled and draped around structures in some applications, the heavy shielding employed in standard cable designs may introduce substantial weight burdens in weight-sensitive applications such as aerospace and automotive applications. At least from the standpoint of fuel efficiency and cost savings, lighter-weight and more flexible designs for electrical cables are clearly needed.
Referring now to
As best shown in
The metal plating layers 18 may be formed from highly conductive metals such as, but not limited to, silver, copper, and gold, and each metal plating layer 18 in the cable 10 may have the same composition or different compositions. Due to the high conductivity of the metal plating layers 18, they may be made thin enough to maintain sufficient flexibility in the cable 10, allowing it to bend while still transmitting a signal. The thicknesses of the metal plating layers 18 may be engineered to provide a desired level of flexibility in the cable 10. Suitable thicknesses for the metal plating layers 18 may be less than about 0.001 inches (about 0.025 mm) However, the metal plating layers 18 may also have thicknesses greater than this range when stiffer cables with greater mechanical strength and less flexibility are desired. In addition, the outermost metal plating layer 18 may have a thickness greater than this range to provide resistance against erosion and/or the option to customize the surface finish of the cable 10 by polishing, machining, or other finishing processes.
The polymeric layers 16 may be formed from a thermoplastic material or a thermoset material. Suitable thermoplastic materials may include, but are not limited to, polyetherimide (PEI), thermoplastic polyimide, polyether ether ketone (PEEK), polyether ketone ketone (PEKK), polysulfone, polyamide, polyphenylene sulfide, polyester, polyimide, or combinations thereof. Suitable thermoset materials may include, but are not limited to, condensation polyimides, addition polyimides, epoxy cured with aliphatic and/or aromatic amines and/or anhydrides, cyanate esters, phenolics, polyesters, polybenzoxazine, polyurethanes, polyacrylates, polymethacrylates, silicones (thermoset), and combinations thereof. If desired, the thermoplastic or thermoset materials forming the polymeric layers 16 may be optionally reinforced with reinforcing materials such as carbon or glass. Each of the polymeric layers 16 in the electrical cable 10 may have the same or different compositions.
A method of fabricating the cable 10 in accordance with the present disclosure is shown in
As an optional step, an outer polymeric layer 16 may be coated on the outer surface of a previously deposited metal plating layer 18 to provide non-conductive outer coating on the cable 10, according to an optional block 28. The outer polymeric layer 16 may be coated on the outer surfaces of the previously deposited metal plating layer 18 at a desired thickness using conventional polymeric coating methods such as spray coating or dip coating. An outer polymeric layer 16 may be desired, for example, in situations requiring protection of the cable 10 from abrasion or certain fluids, whereas an outer metal plating layer 18 may be desired, for example, in situations requiring protection of the cable 10 from erosion. In addition, an outer metal plating layer 18 on the cable 10 may provide the option to later customize the surface finish of the electrical cable 10. As another optional step, additional features (e.g., end connectors, etc.) may be attached to the electrical cable following the block 24 (or the block 28) according to an optional block 30, as shown.
From the foregoing, it can therefore be seen that the present disclosure can find industrial applicability in many situations such as, but not limited to, weight-critical applications. The electrical cable design as disclosed herein utilizes one or more plated polymeric layers to provide electromagnetic shielding and insulation for a central conductor. In addition, the metal plating layers in the plated polymeric layers may replace heavier shielding layers typically used for electrical cable construction. Furthermore, the thicknesses of the metal plating layers in the plated polymeric layers may be engineered to provide desired levels of cable flexibility, cable strength, resistance against erosion, or other desired properties. The technology as disclosed herein offers an approach to produce lightweight and flexible electrical and/or communication cables and may find wide industrial applicability in a wide range of areas such as aerospace industries, automotive industries, and other industries which may benefit from lightweight and flexible cable constructions.
Current aircraft and automotive engine designs, as well as many other systems, use bundles of electrical cables and tubing wrapped around and anchored to various engine structures for support. The electrical cables may be responsible for providing power or electrical communications for a range of applications, while the tubing may be involved in transporting fluids such as fuel, oil, or gas to various locations. These masses of electrical cables and tubing may be heavy and may add weight to weight-sensitive systems such as aircraft and automotive systems. Furthermore, the bundles of electrical cables and tubing required for proper system operations may give some engines a cluttered appearance and may also be prone to handling damage. Clearly, from a fuel efficiency and safety standpoint, there is a need for lighter-weight and more durable electrical cable and fluid tubing constructions which offer the ability to save space and reduce clutter.
Referring now to
As shown in
On the surface of the support tubing 38 may be one or more metal plating layers 42 which may be conductive and involved in transmitting electrical signals. Surrounding the metal plating layer(s) 42 on the support tubing 38 may be one or more polymeric layers 44 having one or more metal plating layers 42 on their outer surfaces, as shown in
The metal plating layers 42 may be formed from one or more highly conductive metals such as copper, gold, or silver, and they may be thin enough to maintain sufficient flexibility in the hybrid conductive tubing 35. In some applications, the outermost metal plating layer 45 may be conductive and involved in electrical signal transmission. In other applications where electromagnetic interference (e.g., radio-frequency signals) is a concern, the outermost metal plating layer 45 may be either conductive or non-conductive and may act to shield the conductive metal plating layers 42 in the hybrid conductive tubing 35 from the external electromagnetic interference. If the outer metal plating layer 45 is conductive, it may be covered by a polymeric coating or other insulating layer for protection.
An alternative hybrid conductive tubing 50 is shown in
The metal plating wires 52 in the hybrid conductive tubing 50 may be formed from one or more highly conductive metals such as, but not limited to, copper, gold, or silver, and each metal plating wire 52 may have the same or different composition. In addition, the number, thickness, and spacing of the metal plating wires 52 on the surfaces of the support tubing 38 and the polymeric layers 44 may, of course, vary depending on the application. Deposition of the metal plating wires 52 with a desired thickness and spacing on the outer surfaces of the support tubing 38 and the polymeric layer(s) 44 may be achieved using conventional metal deposition processes (e.g., electroplating, electroless plating, electroforming, physical vapor deposition, etc.) combined with masking techniques to block selected surfaces of the support tubing 38 from being plated with metal. In some embodiments, the metal plating wires 52 on the outer surface of the hybrid conductive tubing 50 may not be conductive and may shield metal plating wires 52 inside of the hybrid conductive tubing 50 from external electromagnetic interference. In other embodiments, the metal plating wires 52 on the outer surface of the hybrid conductive tubing 50 may be conductive and may be covered by a polymer coating or other insulating layer (e.g., a layer of varnish, etc.) for protection.
As shown in
As yet another alternative arrangement, a hybrid conductive tubing 58 may have one or more metal plating wires 52 wrapped around the outer surface of the support tubing 38 in a spiral configuration, as shown in
A polymeric layer 44 may surround the outer surface of the support tubing 38 of the hybrid conductive tubing 58 and it may have one or more metal plating wires 52 deposited on its outer surface in a spiral configuration, as shown in
A hybrid conductive tubing 60 having one or more metal plating wires 52 deposited in channels formed on the surface of the support tubing 38 is depicted in
One or more polymeric layers 44 may also surround the support tubing 38 of the hybrid conductive tubing 60, offering further electrical insulation, as shown in
Based on the above description, those skilled in the art will understand that various combinations of the above-described hybrid conductive tubing arrangements also fall within the scope of this disclosure. For example, mixtures of metal plating layers 42, metal plating wires 52 in various configurations (e.g., straight, curved, or spiral), and/or metal plating wires 52 formed in the gaps between gear-like teeth on the surface of the support tubing 38 and/or polymeric layers 44 may exist in different orders in the hybrid conductive tubing. Furthermore, in any of the above-described hybrid conductive tubing arrangements or combinations thereof in which the metal platings layers 42 or the metal plating wires 52 are exposed on the outer surface of the hybrid conductive tubing, they may be conductive or non-conductive and shielding. If they are conductive, they may be covered by a polymeric coating or another insulating layer for protection.
Various arrangements may also be employed for collecting the electrical signals carried by the metal plating layers 42 and/or metal plating wires 52 of the hybrid conductive tubings disclosed herein. As shown in
Another alternative electrical signal collection arrangement is depicted in
A method for fabricating the above-described hybrid conductive tubings is shown in
If the support tubing 38 is polymeric, the outer surfaces (and potentially the inner surfaces) of the support tubing 38 which are selected for plating may be suitably activated and metallized using processes well-known in the industry according to a block 72. If the support tubing 38 is formed from metal, its outer surfaces may first be coated with a polymer layer according to a block 71 prior to the block 72, as shown. The polymer layer may be formed from the thermoplastic or thermoset materials described above (with optional fiber reinforcement) and may be applied to the outer surfaces of the support tubing 38 by conventional processes such as spray coating or dip coating.
One or more metal plating layers 42 or one or more metal plating wires 52 may then be deposited on the outer surface of the support tubing 38 according to block 74. As described above, the metal plating layers 42 and the metal plating wires 52 may consist of one or more highly conductive metals such as copper, gold, or silver. Deposition may be carried out using any metal deposition process apparent to those of ordinary skill in the art such as, but not limited to, electrolytic plating, electroless plating, electroforming, spray coating, and plasma vapor deposition. Notably, if metal plating wires 52 are deposited, deposition may be carried out using masking techniques to block certain surfaces of the support tubing 38 from being plated, as will be understood by those skilled in the art. Moreover, the metal plating wires 52 may be formed in straight lines, in curved lines, or in spiral configurations (see, for example,
According to a next block 76, the outer surfaces of the support tubing 38 may then be coated with a polymeric layer 44. The polymeric layer 44 may be formed from selected thermoplastic materials or thermoset materials described above with optional reinforcement with carbon or glass. It may be applied to the outer surfaces of the support tubing 38 using conventional processes such as, but not limited to, spray coating or dip coating.
At block 76, further alternating arrangements of insulating polymeric layers 44 and conductive layers (e.g., metal plating layers 42 or metal plating wires 52) may be built-up according to optional blocks 78, 80, and 82. More specifically, the polymeric layer 44 may first be suitably activated and metallized on selected outer surfaces (block 78) and one or more metal plating layers 42 or metal plating wires 52 (with masking) may be deposited theron (block 80), using the surface activation/metallization and metal deposition processes described above. The blocks 76, 78, and 80 may be repeated as desired to build up the desired number of alternating insulating and conductive layers in the hybrid tubing according to the block 82, as shown. If the outer metal plating layer 42 or metal plating wires 52 are conductive, the outer surface of the hybrid conductive tubing may then be coated with a protective polymeric coating or another insulating layer according to an optional block 84, as shown. If, however, the outer metal plating layer 42 or metal plating wires are shielding and non-conductive, they may remain exposed.
From the foregoing, it can therefore be seen that the hybrid conductive tubings as disclosed herein can find industrial applicability in many situations including, but not limited to, aerospace engine and automotive engine construction. The hybrid conductive tubings as disclosed herein are multi-purpose tubings capable of both transporting a fluid (gas or liquid) and transmitting electrical signals. Therefore, in some situations, the technology disclosed herein may eliminate the need for separate fluid-transfer tubings and electrical cables. The disclosed hybrid conductive tubing arrangements have alternating insulating polymeric layers and metal conductive layers. Moreover, the metal conductive layers may be deposited on the surface of the polymeric layers as solid layers or as wires in various configurations which may offer structural support to the tubing. The technology as disclosed herein offers a lightweight, high-strength, and space-saving alternative for fluid-transfer tubings and electrical cables and may find wide industrial applicability in a wide range of areas.
Moving along,
The gas turbine engine 110 may include a core engine C within a core nacelle 112 that houses a low-pressure spool 114 and a high-pressure spool 124. The low-pressure spool 114 may include a low-pressure compressor 116 and low pressure turbine 118. The low-pressure spool 114 may be coupled to drive a fan 120 either directly or through a gear train 122. The high-pressure spool 124 may include a high-pressure compressor 126 and a high-pressure turbine 128. A combustor 130 may be arranged between the high-pressure compressor 126 and the high-pressure turbine 128. The low and high-pressure spools 114 and 124 may rotate about an engine axis A.
The engine 110 may be a high-bypass geared architecture aircraft engine. Airflow enters a fan nacelle 134, which at least partially surrounds the core nacelle 112. The fan 120 communicates airflow into the core nacelle 112 to power the low-pressure compressor 116 and the high-pressure compressor 126. Core airflow compressed by the low-pressure compressor 116 and the high-pressure compressor 126 is mixed with the fuel in the combustor 130 and expanded over the high-pressure turbine 128 and low-pressure turbine 118. The turbines 128 and 118 are coupled to the spools 124 and 114 to rotationally drive the compressors 126 and 116, respectively, and the fan section 120 through the optional gear train 122. A core engine exhaust exits the core nacelle 112 through a core nozzle 138 disposed between the core nacelle 112 and the tail cone 132.
Containment Cases and Other Structural Components Made from Plated Polymeric Substrates
Referring to
Because it does not experience high operating temperatures, the fan case 146 may be fabricated from one or more shaped polymer articles, each in the form of a reinforced polymeric substrate that has been coated with one or more metallic layers. Suitable thermoplastic materials may include, but are not limited to: polyetherimide (PEI), polyimide, polyether ether ketone (PEEK), polyether ketone ketone (PEKK), polysulfone, polyamide, polyphenylene sulfide, polyester, polyimide, and combinations thereof. Suitable thermoset materials may include, but are not limited to, condensation polyimides, addition polyimides, epoxy cured with aliphatic and/or aromatic amines and/or anhydrides, cyanate esters, phenolics, polyesters, polybenzoxazine, polyurethanes, polyacrylates, polymethacrylates, silicones (thermoset), and combinations thereof. Optionally, the polymeric material of the polymeric substrate 52 may be structurally reinforced with materials that may include carbon, metal, or glass. The fiber-reinforced polymeric substrate may be molded or may include a plurality of layers to form a composite layup structure.
An exemplary case 146 may include a metallic layer 196 plated onto the polymeric substrate 195 as shown in
A polymeric substrate 195 may be molded into a desired shape. One or more metallic layers 196 may be deposited onto the polymeric substrate 195 to form a part for a gas turbine engine, such as a fan case 146. As will be apparent to those skilled in the art, other parts may be fabricated using this technique as well. The metallic layer(s) 196 may be applied by electroless plating, electroplating, or electroforming with a thickness ranging from about 0.01 inches (0.254 mm) to about 0.5 inches (12.7 mm) This thickness range may provide sufficient resistance to wear and impact and/or provide sufficient material for post machining to meet tight tolerance requirements.
The plated metallic layer(s) 196 may include one or more layers. The plating may consist of one or more metals selected from nickel, cobalt, copper, iron, gold, silver, palladium, rhodium, chromium, zinc, tin, cadmium, and alloys with any of the foregoing elements comprising at least 50 wt. % of the alloy, and combinations thereof. Plating may be performed in multiple steps by masking certain areas of the molded article to yield different thicknesses or no plating in certain areas. A customized plating thickness profile can also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.). Tailored racking allows for an optimization of properties for the case 146 with respect to heat resistance, structural support, surface characteristics, etc. without adding undue weight to the case to accommodate each of these properties individually. Thus, plating thicknesses may be tailored to the structural requirements of the case 146. In addition, a thicker plated metallic layer allows for more aggressive machining, finishing, etc. to achieve the desired surface roughness, tolerances, etc. in certain locations of the case 146. Use of a multi-step process allows for optimization of cover properties, with respect to fire, structural support, surface characteristics, etc. without adding undue weight to the case 146.
Some mounting features (e.g., flanges, bosses, mounting holes, integral fittings) may be bonded to the molded polymer article using a suitable adhesive after molding but before plating. Further, the polymeric substrate can be fabricated in multiple segments that are joined by any conventional process (e.g., by welding, adhesive, mitered joint with or without adhesive, etc.) before plating. Furthermore, molded composite articles may be produced and plated separately and subsequently bonded by transient liquid phase (TLP) bonding. In addition, features such as bosses or inserts may be added (using an adhesive, riveting, etc.) to the plated structure after the plating has been carried out. The polymeric substrate may have a thickness ranging from about 0.05 inches (1.27 mm) to about 2 inches (50.8 mm).
Referring to
The gearbox 160 houses a gear system that couples a towershaft 166 to a layshaft 168. The layshaft 168 is disposed within a layshaft cover 176, which is a cylindrical or tubular structure as shown in
A composite layup structure may be compression molded into a desired shape to form a shaped composite article that will serve as a substrate. One or more metallic layers may be deposited onto the composite shaped article to form a part, such as a layshaft cover 176. As will be apparent to those skilled in the art, other parts may be fabricated using this technique as well. The metallic layer(s) may be applied by electroless plating, electroplating, or electroforming with a thickness ranging from about 0.004 inches (0.102 mm) to about 0.05 inches (1.27 mm) This thickness range may provide sufficient resistance to wear and impact and/or provide sufficient material for post machining to meet tight tolerance requirements. As noted above, the plated metallic layer(s) may include one or more layers.
Plating may be performed in multiple steps by masking certain areas of the molded article to yield different thicknesses or no plating in certain areas. A customized plating thickness profile can also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.). Tailored racking allows for an optimization of properties for the part or layshaft cover 176 with respect to heat resistance, structural support, surface characteristics, etc. without adding undue weight to the layshaft cover 176 to accommodate each of these properties individually. Thus, plating thicknesses may be tailored to the structural requirements of the layshaft cover 176.
For example, a thicker plated metallic layer can be provided on the one side of the cover 176 for structural integrity during a fire. In addition, a thicker plated metallic layer allows for more aggressive machining, finishing, etc. to achieve the desired surface roughness, tolerances, etc. in certain locations of the cover 176. Use of a multi-step process allows for optimization of cover properties, with respect to fire, structural support, surface characteristics, etc. without adding undue weight to the cover 176.
Some mounting features (e.g., flanges, bosses, mounting holes, integral fittings) may be bonded to the molded composite article using a suitable adhesive after molding but before plating. Further, the shaped polymer or composite article can be fabricated in multiple segments that are joined by any conventional process (e.g., by welding, adhesive, mitered joint with or without adhesive, etc.) before plating. Furthermore, molded composite articles may be produced and plated separately and subsequently bonded by transient liquid phase (TLP) bonding. In addition, features such as bosses or inserts may be added (using an adhesive, riveting, etc.) to the plated structure after the plating has been carried out. When the shaped polymer article is formed from a composite material and is to be used as a substrate to be plated for use as a part like a layshaft cover 176, the molded composite article may have a thickness ranging from about 0.05 inches (0.127 mm) to about 2 inches (50.8 mm).
For some parts with complex geometries and/or that are large, multi-piece mold toolings are required because the molded part cannot be reliably released from a single mold. Thus, to fabricate tooling for such a part with complex geometry and/or that is large, the part may be divided into a plurality of segments, which may be coupled. Possible weak points caused by the joining of two segments together may be overcome by joining the two segments using one or more joints in combination with an adhesive that remains within the joint so that the adhesive is not exposed or “visible” to a subsequent plating process. The types of joints that may be suitable for coupling two such polymer segments together include mitered joints, angled joints, angled-mitered joints, welded joints, mitered joints with low-angle boundaries, mitered joints with accommodation channels for accommodating extra adhesive, welded joints with a cover, slot-type attachments with or without an additional fastener, and others as will be apparent to those skilled in the art. Types of welded joints may include, but are not limited to ultrasonic, laser, friction, friction-stir, and traditional welded joints. Adhesive may also be used to couple the substrates or shaped polymer articles together. Then, the joined segments are plated using one of the plating methods described above. By plating one or more layers over the joint and over the outer surfaces of two segments, possible structural weak points created by the coupling of the two segments can be avoided. Suitable adhesives include epoxy-based adhesives in liquid, paste, or film form, with long-term service temperatures of up to 121° C. (250° F.), and bismaleimide-based adhesives with service temperatures up to 177° C. (350° F., in paste or film form). In addition, cyanoacrylates and polyurethanes could be used in certain situations, depending upon the strength and rigidity requirements.
The plating material and thickness may be selected such that a structural analysis would indicate that the plated metallic layer 196 will take the majority of the loads that the part experiences. Furthermore, geometric features are optionally added into the design to mitigate any weakness caused by joining segments together prior to plating.
Portions of the metallic layer(s) 196 may be purposefully weakened (or the polymeric substrate can be masked before plating) to provide paths for outgassing and expansion of the polymeric substrate during a fire. As will be apparent to those skilled in the art, such weakened portions should not reside near areas of the part that are significantly stressed and such weakened portions may be masked areas, scored lines, one or more large holes, smaller holes, etc. to provide appropriate redirection of thermally induced stresses and strains away from critical load paths.
Turning to
As shown in
As shown in
Thus, improved fan blades are disclosed that may be fabricated from a variety of materials including metals, polymers, polymeric composites, and ceramics. The strength of the roots of such fan blades may be enhanced by selectively plating at least part of the fan blade root, especially at the pressure faces, as discussed above. Plated molded thermoplastic or composite airfoils, airfoil clusters, and inlet guide vane assemblies offer cost and weight savings compared to traditional metal components.
Turning to
The compressor(s) 116, 126 each include airfoils or airfoil clusters as shown in
A disclosed airfoil cluster 260 may be formed from a polymeric substrate 195 and at least one plated metallic layer 196 as shown in
The plated metallic layer 196 may include one or more layers. The plated metallic layer 196 may be applied by electroless plating, electroplating, or electroforming to a thickness ranging from about 0.001 to about 0.05 inches (from about 25.4 to about 1270 microns), locally. The average plating thickness may range from about 0.004 to about 0.025 inches (from about 101.6 to about 635 microns). Thicknesses within these ranges provide resistance to erosion, impact, FOD, etc. and the option to finish more aggressively to meet tight tolerances, surface finish requirements, etc. The plated metallic layer 196 may include any number of metals or alloys including, but not limited to, The plating may consist of one or more metals selected from nickel, cobalt, copper, iron, gold, silver, palladium, rhodium, chromium, zinc, tin, cadmium, and alloys with any of the foregoing elements comprising at least 50 wt. % of the alloy, and combinations thereof.
Plating may be performed in two steps by masking certain areas of the airfoil cluster to yield different thicknesses in areas of interest, such as the cluster platforms. This customized plating thickness profile can also be achieved by tailored racking (includes shields, thieves, etc.). In addition, a thicker plated metallic layer allows for more aggressive machining, finishing, etc. to achieve the desired surface roughness, tolerances, etc. This multi-step process allows for optimization of airfoil cluster properties, with respect to fire, structural support, surface characteristics, etc. without adding undue weight to the part to completely accommodate each of these properties.
More broadly, the airfoil cluster 260 can be fabricated in multiple segments that are joined by any conventional process (e.g., ultrasonic, laser, friction, friction-stir welding; traditional welding processes; adhesive; mitered joint with or without adhesive) before plating. Furthermore, the airfoils 263 and shrouds 261, 262 may be produced and plated separately and subsequently bonded by transient liquid phase (TLP) bonding.
Plated polymer parts offer cost and/or weight savings compared to traditional materials and processes. For example, plating provides built-in erosion protection and superior resistance to loads. Further, additional savings can be realized given the high-throughput of currently available molding and plating processes. Finally, complex geometries can be accommodated by producing the airfoil clusters 260 in multiple polymer segments and joining them together before plating.
Thus, airfoil clusters are disclosed that may be fabricated from a variety of materials including metals, polymers, polymer composites and ceramics. The strength of the shrouds of such airfoil clusters may be enhanced by selectively plating at least part of the airfoil cluster shrouds. Plated molded thermoplastic or composite airfoils, airfoil clusters and inlet guide vane assemblies offer cost and weight savings compared to traditional metal components.
Hybrid airfoils for gas turbine engines are used to replace metal airfoils to reduce weight and manufacturing costs. For example, US20120082553 discloses an airfoil with a polymer core and an outer nanocrystalline metal shell that covers the polymer core and which defines an outer surface of the airfoil. The nanocrystalline metal shell has a thickness ranging from about 0.001 to about 0.125 inches (from about 25.4 to about 3175 microns). U.S. Pat. No. 4,815,940 discloses another hybrid airfoil having a graphite fiber-reinforced polyetherimide core covered by a very thin copper conductive layer that is covered by a nickel, cobalt or nickel-cobalt plated layer having a thickness ranging from about 0.002 to about 0.02 inches (from about 50.8 to about 508 microns). As the need to replace heavy metal parts with lighter composite and composite plated parts for gas turbine engines continues to exist, additional hybrid airfoil designs are needed.
Plated injection molded thermoplastic airfoils are disclosed that reduce manufacturing and operating costs of a gas turbine engine and that provide integral erosion and foreign object damage (FOD) resistance. Further, the plating can be locally varied in thickness to allow the airfoil structural properties to be tailored to the specific need. Further, the disclosed airfoils provide improved bond strength relative to the prior art because the plating contributes to the structural integrity of the airfoil versus being simply an erosion protection layer.
Turning to
The metallic layer 342 may include one or more layers. The metallic layer(s) 342 may be applied by electroless plating, electroplating, or electroforming to a thickness ranging from about 0.001 to about 0.025 inches (from about 25.4 to about 635 microns), locally. An average plating thickness may range from about 0.003 to about 0.02 inches (from about 76.2 to about 508 microns). These thickness ranges provide resistance to erosion, impact, FOD, etc. and the option to finish more aggressively to meet tight tolerances, surface finish requirements, etc.
Thus, airfoils are disclosed that may be fabricated from a variety of materials including metals, polymers, polymer composites and ceramics. The strength of the roots of such airfoils may be enhanced by selectively plating at least part of the airfoil root, especially at the pressure faces, as discussed above. Plated molded thermoplastic or composite airfoils, airfoil clusters and inlet guide vane assemblies offer cost and weight savings compared to traditional metal components.
The inlet air duct 255 of the gas turbine engine 110 of
Similar to the airfoil cluster 260 discussed above, the disclosed inlet guide vane assembly 270 may be a hand layed-up, compression molded, two-dimensional laminate of a graphite-epoxy material system. As noted above, this manufacturing process tends to be rather complex (e.g., ply orientations have to be tightly and repeatably controlled, and are applied manually). Therefore, a disclosed inlet guide vane assembly 270 may be formed from a polymeric substrate 195 and at least one plated metallic layer 196 as shown in
Further, the substrate 195 may be a two-dimensional woven laminated composite that includes carbon fibers or glass fibers in combination with an epoxy resin or a similar matrix material. Metal inserts may be incorporated into the substrate 195 to enhance the load-carrying capability of the resultant structure.
The plated metallic layer 196 may include one or more layers. The plated metallic layer 196 may be applied by electroless plating, electroplating, or electroforming to a thickness ranging from about 0.001 to about 0.003 inches (from about 25.4 to about 762 microns), locally. The average plating thickness may range from about 0.003 to about 0.025 inches (from about 76.2 to about 635 microns). Thicknesses within these ranges provide resistance to erosion, impact, FOD, etc. and the option to finish more aggressively to meet tight tolerances, surface finish requirements, etc. The plated metallic layer 196 may include any number of metals or alloys including, but not limited to, nickel, cobalt, copper, iron, gold, silver, palladium, rhodium, chromium, zinc, tin, cadmium, and alloys with any of the foregoing elements comprising at least 50 wt. % of the alloy, and combinations thereof.
Plating may be performed in two steps by masking certain areas of the airfoil cluster to yield different thicknesses in areas of interest, such as the cluster platforms. This customized plating thickness profile can also be achieved by tailored racking (includes shields, thieves, etc.). In addition, a thicker plated metallic layer allows for more aggressive machining, finishing, etc. to achieve the desired surface roughness, tolerances, etc. This multi-step process allows for optimization of airfoil cluster properties, with respect to fire, structural support, surface characteristics, etc. without adding undue weight to the part to completely accommodate each of these properties.
More broadly, the inlet guide vane assembly 270 may be fabricated in multiple segments that are joined by any conventional process (e.g., ultrasonic, laser, friction, friction-stir welding; traditional welding processes; adhesive; mitered joint with or without adhesive) before plating. Furthermore, the vanes 273 and shrouds 271, 272 may be produced and plated separately and subsequently bonded by transient liquid phase (TLP) bonding.
Plated polymer parts offer cost and/or weight savings compared to traditional materials and processes. For example, plating provides built-in erosion protection and superior resistance to loads. Further, additional savings can be realized given the high-throughput of currently available molding and plating processes. Finally, complex geometries can be accommodated by producing the inlet guide vane assembly 270 in multiple polymer segments and joining them together before plating.
Thus, improved inlet guide vanes are also disclosed that may be fabricated from a variety of materials including metals, polymers, polymer composites and ceramics. The strength of the shrouds of such inlet guide vanes may be enhanced by selectively plating at least part of the shrouds. Plated molded thermoplastic or composite airfoils, airfoil clusters and inlet guide vane assemblies offer cost and weight savings compared to traditional metal components.
Because of its lightweight and high specific strength, metal plated polymers (PP) may be used replace some metal materials in gas turbine engines. Currently available PP materials, however, are limited thermally by commonly employed polymeric substrates. For example, polyethyleneimine (PEI) is not recommended for use at temperatures exceeding 149° C. (300° F.), which may restrict its applications in gas turbine engines in certain areas of the engine, such as those areas that are in line-of-sight of a radiant heat source, e.g., the combustor.
However, highly polished metal plated polymer (PP) surface is proposed for use in gas turbine engines within line-of-sight of radiant heat sources. The highly polished plated metallic layer can significantly increase emissivity and thus reduce radiation heating to a component that is in line-of-radiation sight with a heat source. Thus, the disclosed PP materials may be highly polished to expand their use in gas turbine engines.
Thus, plated polymer articles and parts may be highly polished for purposes of reflecting radiant heat, such as radiant heat emitted from a combustor so that a plated polymer article, part or component may be disposed within line of sight of a radiant heat source. Further, plated polymer components may be highly polished for purposes of reducing drag, which is particularly applicable to aerospace applications.
Components with very smooth surfaces are desirable in aerospace applications to reduce drag. However, metal components, which can be polished to a very low roughness, are heavy. On the other hand, while polymeric substrates are lightweight compared to a metal, polymeric substrates cannot be polished to a very small surface roughness to reduce drag. Coatings may be applied to a polymer article to reduce the surface roughness, but they cannot achieve the low surface roughness possible with metals.
A disclosed lightweight high-strength super-polished article may be created by applying typical polishing methods (i.e., grinding, lapping, honing, micromachining, etc.) to a plated polymer article. A disclosed polished article may include a polymeric substrate 195 and at least one metallic layer 196 as shown in
The metallic layer(s) 196 may be applied by electroless plating, electroplating, or electroforming to a thickness ranging from about 0.001 to about 0.05 inches (from about 25.4 to about 1270 microns, locally. An average plating thickness may range from about 0.004 to about 0.04 inches (from about 101.6 to about 1016 microns. These thickness ranges may provide resistance to erosion, impact, FOD, etc. and provide the option to finish very aggressively to meet very tight tolerances, surface finish requirements, etc.
The metallic layer(s) 196 may be plated in multiple steps by masking certain areas of the polymeric substrate to yield different thicknesses (or no plating) in areas of interest. Such a customized plating thickness profile may also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.). Such a multiple-step process may provide for optimization of properties for the polished article with respect to structural support, etc., without adding undue weight to the part.
Some mounting features (e.g., flanges or bosses) may be bonded on using a suitable adhesive after molding but before plating to simplify the mold tooling. The polished article may be fabricated in multiple segments that are joined by conventional processes (e.g., ultrasonic, laser, friction and friction-stir welding; traditional welding processes; adhesives; mitered joints with or without adhesive) before plating. The polished article may be produced in multiple components, plated separately and subsequently bonded by transient liquid phase (TLP) bonding. Features such as bosses or inserts may be added (using an adhesive, riveting, etc.) to the article after the plating process.
Thus, plated polymer articles and parts may be highly polished for purposes of reflecting radiant heat, such as radiant heat emitted from a combustor so that a plated polymer article, part or component may be disposed within line of sight of a radiant heat source. Further, plated polymer components may be highly polished for purposes of reducing drag, which is particularly applicable to aerospace applications.
Referring to
Referring to
The metallic layer 196 may include one or more layers. The metallic layer 196 may be applied by electroless plating, electroplating, or electroforming to a thickness ranging from about 0.001 to about 0.100 inches (from about 25 to about 2540 microns), which provides resistance to erosion, impact, foreign object damage, etc., and the option to finish aggressively to meet tight tolerances, surface finish requirements, etc. Plating may be performed in two steps by masking certain areas of the segment 190 to yield different thicknesses in areas of interest. Such a customized plating thickness profile can also be achieved by tailored racking (includes shields, thieves, anodes, etc.). In addition, a thicker plated metallic layer 196 allows for more aggressive machining, finishing, etc. to achieve the desired surface roughness, tolerances, etc. Such a multi-step process allows for optimization of the properties of the fan nacelle 134, with respect to fire, structural support, surface characteristics, etc. without adding undue weight to the segment 190.
The forward segment 190 of the fan nacelle 134 and/or fan inlet duct 193a may be fabricated in multiple segments that are joined by any conventional process (e.g., ultrasonic, laser, friction, friction-stir welding; traditional welding processes; adhesive; mitered joint with or without adhesive) before plating as discussed above. Furthermore, the forward segment 190 can be produced in multiple segments that are plated separately and subsequently bonded by transient liquid phase (TLP) bonding. The metallic layer(s) 196 of the forward segment 190 may be highly polished to achieve or promote a laminar flow profile around the nacelle 134.
In addition to the forward segment 190 and fan inlet duct 193a, other parts of the fan nacelle 134 or nacelle assembly N can be fabricated from a plated polymer structure. For example, the bulkheads 197, 198, fixed structure 199, thrust reverser doors 203 (only one of two doors being shown in
As an alternative shown in
As shown in
The fan inlet duct 193a of the gas turbine engine 110 of
Further, the substrate 195 may be a two-dimensional woven laminated composite that includes carbon fibers or glass fibers in combination with an epoxy resin or a similar matrix material. Metal inserts may be incorporated into the substrate 195 to enhance the load-carrying capability of the resultant structure.
The plated metallic layer 196 may include one or more layers. The plated metallic layer 196 may be applied by electroless plating, electroplating, or electroforming to a thickness ranging from about 0.001 to about 0.03 inches (from about 25.4 to about 762 microns), locally. The average plating thickness may range from about 0.003 to about 0.025 inches (from about 76.2 to about 635 microns). Thicknesses within these ranges provide resistance to erosion, impact, FOD, etc. and the option to finish more aggressively to meet tight tolerances, surface finish requirements, etc. The plated metallic layer 196 may consist of one or more metals including, but not limited to nickel, cobalt, copper, iron, gold, silver, palladium, rhodium, chromium, zinc, tin, cadmium, and alloys with any of the foregoing elements comprising at least 50 wt. % of the alloy, and combinations thereof.
Plating may be performed in two steps by masking certain areas of the airfoil cluster to yield different thicknesses in areas of interest, such as the cluster platforms. This customized plating thickness profile can also be achieved by tailored racking (includes shields, thieves, etc.). In addition, a thicker plated metallic layer allows for more aggressive machining, finishing, etc. to achieve the desired surface roughness, tolerances, etc. This multi-step process allows for optimization of airfoil cluster properties, with respect to fire, structural support, surface characteristics, etc. without adding undue weight to the duct.
More broadly, the fan inlet duct 193a may be fabricated in multiple segments that are joined by any conventional process (e.g., ultrasonic, laser, friction, friction-stir welding; traditional welding processes; adhesive; mitered joint with or without adhesive) before plating. Furthermore, components of the fan inlet duct 193a may be produced and plated separately and subsequently bonded by transient liquid phase (TLP) bonding.
Plated polymer parts offer cost and/or weight savings compared to traditional materials and processes. For example, plating provides built-in erosion protection and superior resistance to loads. Further, additional savings can be realized given the high-throughput of currently available molding and plating processes. Finally, complex geometries can be accommodated by producing the fan inlet duct 193a in multiple polymer segments and joining them together before plating.
Turning to
The pylon P connects the engine 110 to the wing W. During maintenance of the engine 110 or its accessories, the C-shaped ducts formed by the bifurcated fan nacelle 134 and core nacelle 112 may be pivoted open in a conventional manner. The pylon P is coupled to the fan nacelle 134 and core nacelle 112 through an upper bifurcation 209. A lower bifurcation 210 provides an opening for the passage of various types of equipment such as electrical lines, hydraulic lines, etc.
To reduce the weight of the fan nacelle 134 and/or core nacelle 112, at least part of the inner barrel 212 of the fan nacelle 134 and at least part of the outer barrel 207 of the core nacelle 112 may be fabricated using the disclosed plated polymeric substrates of
The outer fixed structure 207 of the core nacelle 112 provides substantial weight and cost savings as compared to the prior art, which teaches a solid aluminum sheet inner wall that is thickly sprayed with an ablative coating. Similarly, the inner barrel 212 of the fan nacelle 134 may be fabricated using the structure shown in
In addition, the sprayed ablative layer shown at 213 may be quite heavy and the thickness of the ablative layer is typically set by burn through testing. The burn through testing is made more difficult by the use of a solid aluminum inner wall, which is a very good heat conductor. Once the ablative is consumed, the aluminum wall conducts the heat to the honeycomb, which is typically glued in place. Once the glue fails, the honeycomb will rapidly disbond causing a structural failure. In contrast, the plated polymeric substrates 195e, 196f act as heat insulators that supplement the ablative coating 213, thereby contributing to the thermal isolation of the glue that holds the honeycomb layer 201 in place.
Fan Nacelle with Laminar Flow Characteristics and Integrated De-Icing Element
Currently available aluminum inlets for fan nacelles cause turbulent flow of the air as it enters the fan, thereby dramatically increasing drag. To solve this problem, a plated polymer nacelle 134a is disclosed in
Currently available anti-icing systems are too hot for polymer structures and are usually made of aluminum—an inherently unfriendly surface for drag reduction through laminar flow. To avoid these problems, the inlet 193a may include a de-icing element in the form of a conducting layer 254. The conducting layer 254 may include graphite and may be flexible as well for ease of assembly. The conducting layer 254 may be in engagement with the metallic layer 196h that coats the outer polymer layer 195g. The thin outer polymer layer 195g and its respective plated metallic layers 196g, 196h may be used to conduct heat with minimal resistance.
Thus, plated polymers may also be used to construct fan nacelle inlets to promote laminar flow through the nacelle inlets for drag reduction as well as weight and cost reductions due to the various intricate shapes that are possible with the disclosed plated polymer systems. For example, a disclose fan nacelle inlet may be fabricated from a pair of plated polymers with a flexible conducting layer sandwiched therebetween. The outer metallic layer of the outer plated polymer may be polished to a mirror smoothness to promote laminar flow through the fan nacelle inlet. The conducting layer may be graphite and may be used for de-icing as the inner plated metallic layer of the outer plated polymer may be placed in contact with the conductive layer for purposed of conducting current and heat through the outer plated polymer of the fan nacelle inlet with minimal resistance.
Thin Structures with Tuned Natural Frequencies Achieved by Selective Plating
Mechanical and structural components, such as automobile parts and aircraft and/or gas turbine engine components are subject to vibration. Vibration generally has the undesirable effect of shortening the service life of a component and may result in part or component failures in a worst-case scenario. To mitigate these concerns, such components are often designed with sufficient mass and stiffness to withstand vibration. As a result, components are often designed to be heavier to shift modes of vibration outside of a critical service region. If a component may not be made with a thicker/heavier geometry, then a design or material change must be made to increase the mass or stiffness, which often leads to increased costs. Aerospace components (liners, vanes, stators, blades, etc.) also require controlled stiffness, high strength, and low weight. In addition, high fatigue life, impact resistance, load-carrying capability and erosion resistance is required. In the case of flight-critical components, expensive manufacturing methods are employed to ensure safety.
To alleviate these problems, a disclosed component may include a polymeric substrate and a plated metallic layer (or plated metallic layers on either side of the substrate). An exemplary substrate may be an injection-molded, compression-molded, or blow-molded component. Further, an exemplary substrate may be additive manufactured or it may be a composite-layup structure formed from at least one of the following: polyetherimide (PEI), polyimide, polyether ether ketone (PEEK), polyether ketone ketone (PEKK), polysulfone, polyamide, polyphenylene sulfide, polyester, polyimide, and combinations thereof. Suitable thermoset materials may include, but are not limited to, condensation polyimides, addition polyimides, epoxy cured with aliphatic and/or aromatic amines and/or anhydrides, cyanate esters, phenolics, polyesters, polybenzoxazine, polyurethanes, polyacrylates, polymethacrylates, silicones (thermoset), and combinations thereof. Optionally, the polymeric material of the polymeric substrate 195 may be structurally reinforced with materials that may include carbon, metal, or glass. The fiber-reinforced polymeric substrate 195 may include a plurality of layers to form a composite layup structure.
Such a composite-layup may be designed in concert with selective plating to achieve a desired overall vibration response. The plated metallic layer may include one or more layers. The plated metallic layer may be applied by electroless plating, electroplating, or electroforming and may have a thickness ranging from about 0.001 to about 0.05 inches (from about 25 to about 1270 microns). The average plating thickness may range from about 0.003 to about 0.002 inches (from about 76.2 to about 508 microns). This range of thickness may provide resistance to erosion, impact, foreign object damage (FOD), etc. and the option to finish more aggressively to meet tight tolerances, surface finish requirements, etc.
The plated metallic layer may include one or more layers as discussed above. Plating may be performed in multiple steps by masking certain areas to yield different thicknesses (or no plating) in areas of interest, resulting in a desired vibration response. This customized plating thickness profile can also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.). This process additionally allows for optimization of properties for the selectively tuned component with respect to fire resistance, structural support, surface characteristics, etc., without adding undue weight to the component to completely accommodate each of these properties. A component may also be selectively plated in concert with perforations in order to act as a vibration dampener as in the case of an engine acoustical liner. Some mounting features (e.g., flanges or bosses) may be bonded on using a suitable adhesive after molding but before plating to simplify the mold tooling. Selectively tuned components may be fabricated in multiple segments that may be joined by conventional processes (e.g., ultrasonic, laser, friction, friction-stir welding; traditional welding processes; adhesives; mitered joints with or without adhesive, etc.) before plating as discussed above. Furthermore, the selectively tuned components can be produced and plated separately and subsequently bonded by transient liquid phase (TLP) bonding. In addition, features such as bosses or inserts may be added (using an adhesive, riveting, etc.) to the part after the plating process. Polymeric coatings can also be applied to plated polymer selectively tuned components to produce a lightweight, stiff, and strong polymer appearing (non-conductive) component. These coatings can be applied by conventional processes, such as spray coating or dip coating, and can be applied to localized regions only, if desired.
With respect to the molding processes, the polymeric substrate thickness can range from about 0.05 to about 0.25 inches (from about 1270 to about 6350 microns) using injection molding, with localized areas ranging up to about 0.5 inches (about 1.27 cm). On the other hand, compression molding can be used to form polymeric substrate thicknesses ranging up to about 2 inches (about 5.8 cm).
Components made from selectively plated polymeric substrates have the ability to control vibration, thereby increasing the useful service life of the component and to address any risk of component failure, which may, in turn, pose safety risks if the component is an automobile part or an aircraft and/or engine component. The disclosed selectively plated polymer components may address both primary factors of vibration—mass and stiffness variation—across a component. By leveraging this dual capability to address both the mass and stiffness factors, components may be fabricated with lower weights and/or costs. This is particularly desirable for aerospace components (liners, vanes, stators, blades, etc.) which require controlled stiffness, high strength, and low weight. Plated polymer components may provide cost and/or weight savings compared to traditional materials and processes. Schedule savings can be realized given the high-throughput molding and plating processes. Complex and/or large geometries can be accommodated by producing multiple polymer segments and joining the segments together before plating.
Electromagnetic interference (EMI) and electromagnetic pulses (EMPs) may be generated by various electrical and electronic systems such as induction heads, full authority digital engine controls (FADECs), computers, radios, electrical actuators, etc. For example, radio frequency emitting induction heads with thermoplastic housings are used routinely with other sensitive equipment such as test machine load frames, linear variable displacement transducers (LVDTs), and extensometers used in fatigue and monotonic testing. Such induction heads encased in thermoplastic housings release EMI into the environment without any suppression, thereby increasing noise levels for nearby components, such as those listed above. Use of an induction head with a thermoplastic housing in conjunction with sensitive electronic and electrical equipment requires extensive grounding schemes to reduce interference and noise.
Previous induction heating systems incorporate a metal housing for the induction head. The metal housing suppresses the radio frequency emitted by the induction head by minimizing the electromagnetic interference. However, metal housings are heavy, thereby adding weight to the induction heating system. Further, ferrite foils have been used to suppress EMI, but ferrite foils are obviously not suitable for use in harsh environments where a sturdy housing is required.
As a solution to the problems noted above, plated polymer housings for induction heads, FADECs, computers, radios, electrical actuators, and other EMI or EMP generating systems. The housings or enclosures may be plated with a ferromagnetic material, i.e., a material that forms a permanent magnet or that is attracted to a magnet. Ferromagnetic materials that are suitable for plating polymers include nickel, iron, cobalt, and alloys thereof. Suitable alloys include, but are not limited to nickel-zinc alloys. Other suitable ferromagnetic alloys that may be plated onto a polymeric substrate will be apparent to those skilled in the art. The use of a ferromagnetic alloy as the plating metal enables the plated polymer housing to absorb and thereby significantly reduce or eliminate EMI and/or EMP disturbance to surrounding systems. Additionally, lightweight plated polymer or polymeric substrate housings or enclosures for electrical and electronic systems such as engine FADECs, computers, and electrical actuators may be used to provide significant weight reduction opportunities and protection to the systems within the plated polymer housings.
Further, plating polymer electronic and electrical housings with a ferro-magnetic plating metal will provide lightweight, low-cost EMP and EMI suppression by effectively creating a Faraday cage that isolates the systems or components disposed within the housing. Sealing features such as compression, blade, and spring fingers disposed at the housing faying surfaces or joints may also be plated to provide electrical continuity and EMP/EMI protection at the housing joints.
By plating thermoplastic or polymeric substrate housings with a thin ferromagnetic layer, noise suppression and/or protection may be obtained while low-cost, lightweight thermoplastic housings may still be used. Further, fabricating a component such as an induction head out of a ferrite material would be cost prohibitive and would not provide the durability needed for robust applications.
Cost-effective, robust, and lightweight ferromagnetic-plated thermoplastic or polymeric substrate housings or enclosures are disclosed. Such housings are useful for electronic and electrical systems that are sensitive to EMI and EMPs. Further, such housings are also useful for containing the EMI or EMPs of systems that emit radio frequencies and that may interfere with neighboring electronic or electrical systems. For example, induction heads of welding equipment may be housed or enclosed in the disclosed plated structures. Further, expensive metal housings for testing instrumentation may be replaced with the disclosed lower-cost, thermoplastic housings that are plated with EMI and EMP absorbing material. An added benefit of the disclosed structures is the enabling of higher instrument sensitivity and measurement accuracy because the disclosed housing structures suppress interfering noise from nearby systems that emit EMI and/or EMPs.
Hydraulic or pneumatic power may be transferred to a load using a piston and rod assembly. Such piston and rod assemblies may vary in size, dependent on the amount of force required from the piston in order to perform the desired operation. Piston rods are generally made from a high strength metal. When choosing a high strength metal for a piston rod, a manufacturer often must choose between weight and cost. For example, using a lightweight metal such as titanium for a piston rod drastically increases the cost of the piston rod while keeping the weight of the rod low. Conversely, making a piston rod out of a conventional metal like plated steel or stainless steel adds significant weight to the piston rod but keeps the cost of the rod down. As a result, for weight-sensitive applications, e.g. aerospace, there is a need for piston rods that are both lightweight and cost-effective.
In satisfaction of this need, an exemplary lightweight plated polymer piston rod is disclosed. The disclosed rod may include a polymeric substrate and a metallic layer. The exemplary substrate may be an injection-molded, compression-molded, blow-molded, additively manufactured or composite-layup structure. The polymer may be selected from the group consisting of: polyetherimide (PEI), polyimide, polyether ether ketone (PEEK), polyether ketone ketone (PEKK), polysulfone, polyamide, polyphenylene sulfide, polyester, polyimide, and combinations thereof. Suitable thermoset materials may include, but are not limited to, condensation polyimides, addition polyimides, epoxy cured with aliphatic and/or aromatic amines and/or anhydrides, cyanate esters, phenolics, polyesters, polybenzoxazine, polyurethanes, polyacrylates, polymethacrylates, silicones (thermoset), and combinations thereof. Optionally, the polymeric material of the polymeric substrate 195 may be structurally reinforced with materials that may include carbon, metal, or glass. The fiber-reinforced polymeric substrate 195 may include a plurality of layers to form a composite layup structure.
The metallic layer 196 may include one or more layers. The metallic layer 196 may be applied by electroless plating, electroplating, or electroforming to a thickness ranging from about 0.001 to about 0.05 inches (from about 25.4 microns to about 1.27 mm), locally. The average plating thickness may range from about 0.004 to about 0.04 inches (from about 101.6 to about 1060 microns). However, in order to increase the strength of the rod, the plating layer thickness may be increased to any thickness necessary to support the additional strength requirements. The 0.004-0.04 inch thickness range may provide resistance to erosion, impact, FOD, etc., and the option to finish more aggressively to meet tight tolerances, surface finish requirements, etc. The plating layer may include one or more layers. Plating may be performed in multiple steps by masking certain areas of the rod to yield different thicknesses (or no plating) in areas of interest. This customized plating thickness profile can also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.). This process also allows for optimization of properties for the disclosed piston rod with respect to fire resistance, structural support, surface characteristics, etc. without adding undue weight to the part to completely accommodate each of these properties.
To simplify mold tooling, mounting features (e.g., flanges or bosses) may be bonded to the rod after molding, but before plating, using a suitable adhesive. The disclosed lightweight plated polymer piston rod may be fabricated in multiple segments that are joined before plating by a conventional process, such as: ultrasonic, laser, friction or friction-stir welding; traditional welding processes; adhesives; mitered joints, with or without adhesive. Furthermore, the disclosed piston rod may be produced and plated separately and subsequently bonded by transient liquid phase (TLP) bonding. In addition, features such as bosses or inserts may be added (using an adhesive, riveting, etc.) to the part after the plating process.
An injection molded polymeric substrate may have a thickness ranging from about 0.05 to about 0.25 inches (from about 1270 to about 6350 microns), with localized areas ranging up to about 0.5 inches (about 12.7 mm) On the other hand, a compression molded polymeric substrate may be used to form wall thicknesses ranging from about 0.050 to about 2 inches (0.127 to about 5.08 cm). In an embodiment, the polymeric substrate for the piston rod could be hollow, and filled with high-density foam to increase the strength of the rod without adding substantially to the weight of the rod.
Turning to
As shown in
Disclosed piston rods may be formed from a polymeric substrate and one or more metallic layers. The polymeric substrate may be injection-molded, compression-molded, blow-molded or additively manufactured. The polymeric substrate may also be a composite layup structure with multiple layers. The polymeric substrate may be formed from at least one of the following: polyetherimide (PEI); polyimide; polyether ether ketone (PEEK); polyether ketone ketone (PEKK); polysulfone; polyamide; polyphenylene sulfide; polyester; polyimide; and combinations thereof. Suitable thermoset materials may include, but are not limited to: condensation polyimides; addition polyimides; epoxy cured with aliphatic and/or aromatic amines and/or anhydrides; cyanate esters; phenolics; polyesters; polybenzoxazine; polyurethanes; polyacrylates; polymethacrylates; silicones (thermoset); and combinations thereof. Optionally, the polymeric material of the polymeric substrate 195 may be structurally reinforced with materials that may include carbon, metal, or glass. The fiber-reinforced polymeric substrate 195 may include a plurality of layers to form a composite layup structure.
The metallic layer(s) 196 may be applied to the polymeric substrate by electroless plating, electroplating, or electroforming. The resultant instrument piston rods are strong, lightweight and may be manufactured using a variety of techniques with minimal lead-time.
Pumps used for aircraft engines are typically enclosed in metal housings or enclosures. A pump typically includes one or more inlets and one or more outlets to control flow. The metal housings are heavy, thereby adversely affecting fuel consumption. As a result, there is a need for lightweight pump housings for use in aerospace and other applications where weight reduction is a goal.
Lightweight pump housings can be made from plated polymeric substrates wherein the outer plated metallic layer provides a durable and structural coating. As shown in
The metallic layer 312 may include one or more layers. The metallic layer(s) 312 may be applied by electroless plating, electroplating, or electroforming to a thickness ranging from about 0.01 to about 0.09 inches (from about 254 microns to about 2.29 mm), locally. An average plating thickness may range from about 0.015 to about 0.08 inches (from about 381 microns to about 2.03 mm) These thickness ranges provide resistance to erosion, impact, FOD, etc. and the option to finish more aggressively to meet tight tolerances, surface finish requirements, etc. The metallic layer 312 may be applied in multiple steps by masking certain areas of the pump housing to yield different thicknesses (or no plating) in areas of interest. Such a customized plating thickness profile can also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.). This process allows for optimization of properties for the pump housing with respect to fire resistance, structural support, surface characteristics, etc. without adding undue weight to the pump housing.
Some mounting features (e.g., flanges or bosses) may be bonded on using a suitable adhesive after molding but before plating to simplify the mold tooling. Further, the pump housing may be fabricated in multiple segments that are joined by any conventional process (e.g., ultrasonic, laser, friction and friction-stir welding processes; traditional welding processes; adhesives; mitered joints with or without adhesive) before plating. Furthermore, components of the pump housing may be produced and plated separately and subsequently bonded by transient liquid phase (TLP) bonding. In addition, features such as bosses or inserts may be added (using an adhesive, riveting, etc.) to the pump housing after the plating process. One or more polymeric coatings 314 may also be applied to plated polymer pump housing components to produce a lightweight, stiff, and strong polymer appearing (non-conductive) component. These coatings 314 may be applied by conventional processes, such as spray coating or dip coating.
Plated polymer pump housings offer cost and/or weight savings compared to traditional metal or thermoplastic pump housings. Further, plated polymer pump housings provide reduced manufacturing costs due to the high-throughput molding and plating processes used to fabricated the plated polymer pump housings. Pump housings with complex geometries can be accommodated by producing multiple polymer segments and joining the segments together before plating to simplify the mold tooling. Alternatively, the segments can be plated separately and subsequently joined using TLP.
Instrumentation probes may be utilized to locate and attach instrumentation needed to assess actual performance of an engine or device, e.g., a gas turbine engine. Instrumentation probes need to fit into limited available spaces and be physically attached in a stable and secure manner. Because instrumentation probes are used to troubleshoot problems associated with engines and devices that are in service, they often need to be fabricated within a relatively short lead-time.
Turning to
The metallic layer(s) 302 may be plated in multiple steps by masking certain areas of the polymeric substrate to yield different thicknesses (or no plating) in areas of interest. Such a customized plating thickness profile may also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.). Tailored racking may allow for optimization of properties for the instrumentation probe 300 with respect to structural support, surface characteristics, etc. without adding undue weight to the probe 300.
Further, some mounting features (e.g., flanges or bosses) may be bonded to the polymeric substrate using a suitable adhesive after molding but before plating to simplify the mold tooling. More broadly, the instrumentation probe may be fabricated in multiple segments before plating that are joined by any conventional process (e.g., ultrasonic, laser, friction and friction-stir welding processes; traditional welding processes; adhesives; mitered joints with or without adhesives). Furthermore, the instrumentation probe 300 may be molded as separate segments, plated separately and the plated segments may be subsequently bonded by transient liquid phase (TLP) bonding. In addition, features such as bosses or inserts may be added (using an adhesive, riveting, etc.) to the plated polymeric substrate or probe after the plating process. One or more polymeric coatings 304 may also be applied to the plated polymer instrumentation probe 300 to provide a lightweight, stiff and strong probe with a polymeric coating 304 or appearance. Such polymeric coatings 304 may be applied by conventional processes, such as spray coating or dip coating, and may be applied to localized areas.
Thus, disclosed instrument probes may be formed from a polymeric substrate and one or more metallic layers. The polymeric substrate may be injection-molded, compression-molded, blow-molded or additively manufactured. The polymeric substrate may also be a composite layup structure with multiple layers of one or more polymeric materials recited above. The metallic layer(s) may be applied to the polymeric substrate by electroless plating, electroplating, or electroforming. The resultant instrument probes are strong, lightweight and may be manufactured using a variety of techniques with minimal lead-time.
A waveguide is a structure that guides energy, such as microwave, optical, electromagnetic, acoustic, etc. Some uses for waveguides include the transmission of power between components of a system. Waveguides are also used as a fundamental method of non-destructive testing. The geometry of the waveguide controls the effectiveness of the waveguide structure, and in some cases, the geometry of the waveguide may be complex. Further, many applications require waveguides to be lightweight, stiff and/or strong. For example, structural rigidity is needed as it partially controls the energy transmission efficiency of the waveguide. In addition, typically, low costs and manufacturability are primary concerns.
Turning to
As noted above, the metallic layer(s) 312 may be plated in multiple steps by masking certain areas of the waveguide to yield different thicknesses (or no plating) in areas of interest. Such a customized plating thickness profile may also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.). Tailored racking may be used to optimize propertied of the waveguide with respect to fire resistance, structural support, surface characteristics, etc., without adding undue weight to the part to the waveguide.
Some mounting features (e.g., flanges or bosses) may be bonded to the molded polymeric substrate 311 using a suitable adhesive after molding but before plating to simplify the mold tooling. Further, the waveguide 310 may be fabricated or molded in multiple segments that are joined after molding and before plating by a conventional process (e.g., ultrasonic, laser, friction or friction-stir welding processes; traditional welding processes; adhesives; mitered joints with or without adhesive, etc.). Furthermore, the polymeric substrate 311 may be molded as separate segments, plated separately and the plated polymer segments may be subsequently bonded by transient liquid phase (TLP) bonding. Features such as bosses or inserts may be added (using an adhesive, riveting, etc.) to the plated polymeric substrate 311 after the plating process. One or more polymeric coatings 314 may be applied to plated polymeric substrate or waveguide 310 to produce a lightweight, stiff, and strong waveguide 310 with a polymer appearance. Such polymeric coatings 314 may be applied by conventional processes, such as spray coating or dip coating, and can be applied to localized regions only, if desired.
With respect to the molding processes, an injection molded polymeric substrate 311 may have a thickness ranging from about 0.05 to about 0.25 inches (from about 1270 to about 6350 microns), with localized areas ranging up to about 0.5 inches (12.7 mm) On the other hand, a compression molded polymeric substrate 311 may be formed with a thicknesses ranging from about 0.05 to about 2 inches (from about 1270 microns to about 50.8 mm).
Disclosed waveguides may be formed from a polymeric substrate and one or more metallic layers. The polymeric substrate may be injection-molded, compression-molded, blow-molded or additively manufactured. The polymeric substrate may also be a composite layup structure with multiple layers. The polymeric substrate may be formed from at least one of the following: polyetherimide (PEI); polyimide; polyether ether ketone (PEEK); polyether ketone ketone (PEKK); polysulfone; Nylon; polyphenylsulfide; polyester; and any of the foregoing with fiber reinforcement e.g., carbon-fiber or glass-fibers. The metallic layer(s) may be applied to the polymeric substrate by electroless plating, electroplating, or electroforming. The resultant waveguides are strong, lightweight and may be manufactured using a variety of techniques with minimal lead-time.
Heat exchangers are currently produced using alloys with high thermal conductivity such as copper. Heat exchangers are also typically constructed in two major forms (plate fin or shell and tube). Modern heat exchangers must be assembled using techniques such as brazing, welding, or extrusion/press fit between mating parts. For aerospace, automotive and other payload sensitive applications, the weight of a heat exchanger assembly is a major design driver. Furthermore, joints and sealing surfaces between hot and cold sides of a heat exchanger are prone to leakage, which compromises the cooling effectiveness of the heat exchanger. Accordingly, methods for producing a lightweight, high cooling effectiveness heat exchanger would have significant utility and commercial value.
Disclosed herein are heat exchangers and components of heat exchangers made from plated polymeric substrates 310 or polymeric substrates 311 that are molded or otherwise formed into a desired shape before they are plated with one or more metallic layers 312 as shown in
The metallic layer(s) 312 may be applied by electroless plating, electroplating, or electroforming to a thickness ranging from about 0.001 to about 0.03 inches (from about 25.4 to about 762 microns), locally. An average plating thickness may range from about 0.001 to about 0.02 inches (from about 25.4 to about 508 microns). These thickness ranges provide resistance to erosion, impact, FOD, etc., and the option to finish more aggressively to meet tight tolerances, surface finish requirements, etc. The metallic layer(s) may be plated in multiple steps by masking certain areas of the substrate 311 to yield different thicknesses in areas of interest. Such a customized plating thickness profile may also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.). Further, a thicker metallic layer 312 allows for more aggressive machining, finishing, etc. to achieve the desired surface roughness, tolerances, etc. This multiple-step process allows for optimization of properties for the heat exchanger or heat exchanger component with respect to fire, structural support, surface characteristics, etc., without adding undue weight to the part.
Some mounting features (e.g., flanges, bosses, etc.) may be bonded to the polymeric substrate 311 using a suitable adhesive after molding, but before plating, to simplify the mold tooling. The plates, fins, shells, tubes, fittings and cover parts of a heat exchanger may be fabricated in multiple segments, which may be joined by conventional processes (e.g., ultrasonic, laser, friction and friction-stir welding processes; traditional welding processes; adhesives; mitered joints with or without adhesive) before plating. Because the metallic layer 312 is thick enough to provide significant structural strength and rigidity, the method of joining the segments of polymeric substrate 311 will likely not limit the strength of the finished component. Furthermore, the plates, fins, shells, tubes, fittings and cover parts may be molded, plated separately and subsequently bonded together by transient liquid phase (TLP) bonding. In addition, features such as bosses or inserts may be added (using an adhesive, riveting, etc.) to the component or assembly after the plating process.
Reduced-weight heat exchangers are disclosed that may be fabricated from plated polymers or plated polymeric substrates. The disclosed manufacturing methods provide flexibility in the design of heat exchangers, especially when using additive manufacturing to create the polymeric substrate(s). Manufacturing savings may be realized given the disclosed high-throughput molding and plating processes used to fabricated the disclosed heat exchangers. Complex geometries can be accommodated by producing multiple polymer segments and joining them together before plating.
LPC Made from Plated Polyermic Substrates
Geared turbofan (GTF) engines and other advanced aero-engines could benefit from weight reducing technologies to improve overall engine fuel burn for flight cycles. Turning to
Plated polymers are disclosed herein for use in the manufacture of the LPC 116 that include a polymeric substrate 311 plated with one or more metallic layer 312 as shown in
Useful polymeric substrates 311 may be injection-molded, compression-molded, extrusion-molded or additive-manufactured. An injection molded polymeric substrate 311 may provide a wall thickness ranging from about 0.05 to about 0.25 inches (from about 1270 to about 6350 microns), with localized areas ranging up to about 0.5 inches (about 12.7 mm) On the other hand, a compression molded polymeric substrate 311 may provide a wall thickness ranging from about 0.05 to about 2 inches (from about 1270 microns to about 50.8 mm) The polymeric substrates 311 may be fabricated using at least one polymer selected from the group consisting of: polyetherimide (PEI); polyimide; polyether ether ketone (PEEK); polyether ketone ketone (PEKK); polysulfone; Nylon; polyphenylsulfide; polyester; and any of the foregoing with fiber reinforcement e.g., carbon-fiber or glass-fibers. Passages may be formed in the polymeric substrate(s) using conventional methods (e.g., washed-out mandrels, machining, etc.).
The metallic layer 312 may be applied by electroplating, electroless plating, brush plating, spray metal deposition, or a powder spray metal process. The thickness of the metallic layer may range from about 0.005 to about 0.1 inches (from about 127 microns to about 2.54 mm) For relatively thick metallic layers 312, a secondary machining or abrasive grinding operation may be performed to shape the trailing edge 324 (
The metallic layer(s) 312 may be applied by electroless plating, electroplating or electroforming to a thickness ranging from about 0.001 to about 0.03 inches (from about 25.4 to about 762 microns), locally. An average plating thickness may range from about 0.001 to about 0.02 inches (from about 25.4 to about 508 microns). These thickness ranges provide resistance to erosion, impact, FOD, etc., and the option to finish more aggressively to meet tight tolerances, surface finish requirements, etc. The metallic layer(s) 312 may be plated in multiple steps by masking certain areas of the substrate 311 to yield different thicknesses in areas of interest. Such a customized plating thickness profile may also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.). Further, a thicker metallic layer 312 allows for more aggressive machining, finishing, etc. to achieve the desired surface roughness, tolerances, etc. This multiple-step process allows for optimization of properties for the LPC stage 320 with respect to fire, structural support, surface characteristics, etc., without adding undue weight to the stage 320.
Some mounting features (e.g., flanges, bosses, etc.) may be bonded to the polymeric substrate 311 using a suitable adhesive after molding, but before plating, to simplify the mold tooling. As noted above, the stages 320 may be fabricated separately and in multiple segments, which may be joined by conventional processes (e.g., ultrasonic, laser, friction and friction-stir welding processes; traditional welding processes; adhesives; mitered joints with or without adhesive) before plating. Because the metallic layer 312 is thick enough to provide significant structural strength and rigidity, the method of joining the segments of polymeric substrate 311 will likely not limit the strength of the finished stage 320. In addition, features such as bosses or inserts may be added (using an adhesive, riveting, etc.) to the stage 320 or to the LPC 116 after the plating process.
The metallic layer 312 may be applied by electroplating, electroless plating, brush plating, spray metal deposition, or a powder spray metal process. The thickness of the metallic layer may range from about 0.005 to about 0.100 inches (from about 127 microns to about 2.54 mm) For relatively thick metallic layers 312, a secondary machining or abrasive grinding operation may be performed to shape the trailing edge 324 (
The techniques described herein will enable lighter LPC components for any gas turbine engine because current LPCs are made of aluminum. A plated polymer LPC or LPC component that is plated with higher hardness and toughness materials such as nickel will improve compressor durability, especially for GTF engines where higher percentages of total compression work is performed in the LPC.
Some aerospace components must have conductive paths to ground electricity that is induced by events such as lightning strikes. Static electricity may also be dissipated in this manner. While polymer and composite parts are being used to replace parts on airplanes to save weight, fuel and manufacturing costs, polymers and composites are not inherently conductive materials. Some such polymer, composite or otherwise non-conductive parts or components must include a conductive path for grounding purposes. Otherwise, a lightning strike or the build-up of static electricity can have serious detrimental consequences on non-grounded components made of these lightweight non-metal materials.
As a solution to this problem, a polymer component 330 is disclosed in
The exemplary polymeric substrate may be injection-molded, compression-molded, blow-molded, additively manufactured or a composite-layup structure. The polymeric substrate may be formed from at least one of the following polymers selected from the group consisting of: polyetherimide (PEI); polyimide; polyether ether ketone (PEEK); polyether ketone ketone (PEKK); polysulfone; polyamide; polyphenylene sulfide; polyester; polyimide; and combinations thereof. Suitable thermoset materials may include, but are not limited to: condensation polyimides; addition polyimides; epoxy cured with aliphatic and/or aromatic amines and/or anhydrides; cyanate esters; phenolics; polyesters; polybenzoxazine; polyurethanes; polyacrylates; polymethacrylates; silicones (thermoset); and combinations thereof.
In addition to the selective surface plating approach described above, recesses or pockets can be machined in the polymeric substrate 331 or provided in the forming process (molding, build file) of the polymeric substrate 331 to provide for an even surface between the polymer and plating strips or metallic layers 332 to prevent increased drag or (increased) turbulence. The use of such recesses or pockets facilitates the masking of the polymeric substrate 331 for the plating process. The grounding strips or metallic layers 332 may include one or more metals including, but not limited to: nickel; cobalt; copper; iron; gold; silver; palladium; rhodium; chromium; zinc; tin; cadmium; and alloys with any of the foregoing elements comprising at least 50 wt. % of the alloy; and combinations thereof. Plating may be performed in multiple steps by masking certain areas of the molded article to yield different thicknesses or no plating in certain areas. A customized plating thickness profile can also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.).
A lightweight solution to lightning-strike grounding is provided in the form of plated grounding strips on molded polymer components. The grounding strips may be selectively plated onto a molded polymer article or component by masking areas of the article. The selective plating process is applicable to composite nacelles and other components that could be fabricated from polymer or composite materials, such as fan blades, fan cases, guide vanes, splitters, etc.
In a gas turbine engine, ducting can be fabricated using a variety of processes, such as a composite layup or forming sheet metal to the desired shape using a combination of cutting, bending, welding, and/or stamping processes. These processes tend to be expensive and/or time consuming.
Disclosed plated polymer ducts may include a polymeric substrate and a metallic layer that replaces either a sheet metal part or a composite layup baseline part. As shown in
The metallic layer 354 and the polymeric substrate 355 each may include one or more layers. The metallic layer 354 may be plated onto the polymer layer 355 in multiple steps by masking certain areas of the duct 350 to yield different thicknesses in areas of interest. For example, a thicker metallic layer 354 can be provided on the inside surface 356 or along the flow path of the duct 350 for structural integrity during an external fire. In addition, a thicker metallic layer 354 allows for more aggressive machining, finishing, etc. to achieve the desired surface roughness, tolerances, etc. This multi-step plating process allows for optimization of duct properties, with respect to fire, structural support, surface characteristics, etc. without adding undue weight to the duct 350.
The exemplary substrate 355 is injection-molded or compression molded and may be formed from at least one of the following: may include, but are not limited to: polyetherimide (PEI); polyimide; polyether ether ketone (PEEK); polyether ketone ketone (PEKK); polysulfone; polyamide; polyphenylene sulfide; polyester; polyimide; and combinations thereof. Suitable thermoset materials may include, but are not limited to: condensation polyimides; addition polyimides; epoxy cured with aliphatic and/or aromatic amines and/or anhydrides; cyanate esters; phenolics; polyesters; polybenzoxazine; polyurethanes; polyacrylates; polymethacrylates; silicones (thermoset); and combinations thereof. Optionally, the polymeric material of the polymeric substrate 195 may be structurally reinforced with materials that may include carbon, metal, or glass. The fiber-reinforced polymeric substrate 195 may include a plurality of layers to form a composite layup structure.
Some mounting features (e.g., flanges or bosses) may be bonded to the substrate 355 using a suitable adhesive after molding but before plating to simplify the mold tooling. Further, the duct 350 may be fabricated in multiple segments that are joined by any conventional process (e.g., ultrasonic, laser, friction or friction-stir welding processes; traditional welding processes; adhesives; mitered joints with or without adhesive) before plating. Because the metallic layer(s) 354 is thick enough to provide significant structural strength and rigidity, the method of joining segments will likely not be a strength limiter. In addition, features such as bosses or inserts may be added (using an adhesive, riveting, etc.) to the duct 350 after the plating process. Furthermore, the duct may be produced in a plurality of segments that are plated separately and subsequently bonded by transient liquid phase (TLP) bonding.
The polymeric substrate 355 may have a wall thickness ranging from about 0.05 to about 0.25 inches (from about 1.27 to about 6.35 mm), with localized areas ranging up to about 0.5 inches (12.7 mm) for injection-molded substrates 355. On the other hand, a compression-molded substrate 355 may have a wall thicknesses ranging from about 0.05 to about 2 inches (from about 1.27 to about 50.8 mm).
Portions of the metallic layer 354 may be purposefully weakened (or the polymeric substrate can be masked before plating) to provide paths for outgassing and expansion of the polymeric substrate 355 during a fire. These portions should not reside near areas of the duct 350 that are significantly stressed or that are stress concentrations and may be masked areas, scored lines, a few large holes, many smaller holes, etc. to provide appropriate redirection of thermally induced stresses and strains away from critical load paths.
The metallic layer 354 may be applied by electroless plating, electroplating, or electroforming to a thickness ranging from about 0.002 to about 1270 microns (from about 50.8 to about 1270 microns). The metallic layer 354 may be any one or more of: nickel; cobalt; copper; iron; gold; silver; palladium; rhodium; chromium; zinc; tin; cadmium; and alloys with any of the foregoing elements comprising at least 50 wt. % of the alloy; and combinations thereof. Plating may be performed in multiple steps by masking certain areas of the molded article to yield different thicknesses or no plating in certain areas. A customized plating thickness profile can also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.).
Plated polymer ducts for gas turbine engines offer cost and/or weight savings compared to composite layup or sheet metal parts. Injection molding and plating processes provide faster and easier manufacturing of gas turbine engine ducts. Complex geometries can be accommodated by producing the ducts in multiple polymer segments and joining them together before or after plating.
A fan platform is a rotating part that defines the flow path between fan blades during normal operation of a turbofan gas turbine engine. Fan platforms must maintain sufficient structural integrity after a bird strike or fan blade-out event to preserve the rotation of the fan blades of a fan blade assembly to meet minimum thrust and/or shutdown requirements as required by FAA regulations.
Turning to
The exemplary substrate 311 may be injection-molded or compression molded and may be formed of at least one polymer selected from the group consisting of: polyetherimide (PEI); polyimide; polyether ether ketone (PEEK); polyether ketone ketone (PEKK); polysulfone; polyamide; polyphenylene sulfide; polyester; polyimide; and combinations thereof. Suitable thermoset materials may include, but are not limited to: condensation polyimides; addition polyimides; epoxy cured with aliphatic and/or aromatic amines and/or anhydrides; cyanate esters; phenolics; polyesters; polybenzoxazine; polyurethanes; polyacrylates; polymethacrylates; silicones (thermoset); and combinations thereof. Optionally, the polymeric material of the polymeric substrate 311 may be structurally reinforced with materials that may include carbon, metal, or glass. The fiber-reinforced polymeric substrate 311 may include a plurality of layers to form a composite layup structure.
Some mounting features (e.g., flanges or bosses) may be to the substrate 311 using suitable adhesives after molding but before plating to simplify the mold tooling. The platform may also be fabricated in multiple segments that are joined by a conventional process (e.g., ultrasonic, laser, friction and friction-stir welding processes; traditional welding processes; adhesives; mitered joints with or without adhesives) and before plating. It is possible to use a metallic layer 312 thick enough to provide significant structural strength and rigidity such that the method of joining segments will likely not be a strength limiter. Furthermore, the platform may be produced in a plurality of segments that are plated separately and subsequently bonded by transient liquid phase (TLP) bonding.
An injection molded polymeric substrate 311 may have a wall thickness ranging from about 0.05 inch (1.27 mm) to about 0.2 inches (5.08 mm) A compression-molded substrate 311 may have a wall thickness ranging from 0.05 inch (1.27 mm) to about 2 inches (5.08 cm). The metallic layer 312 may be applied by electroless plating, electroplating or electroforming to a thickness ranging from about 0.004 to about 0.025 inches (from about 102 to about 635 microns).
Plated polymer fan platforms may provide cost savings in comparison to fan platforms made from composite layup structures, aluminum, or titanium. The metallic layer 312 provides built-in erosion protection and structural integrity.
End walls (platforms) of advanced gas turbine engine airfoils have three-dimensional (3D) contours in order to reduce vortex flow through the engine. 3D contoured end walls are difficult and costly to fabricate.
As shown in
The thickness of the metallic layer(s) 312 may selectively be increased to form contours in the end wall 372 form a two-dimensional axisymmetric part. The method may include using traditional manufacturing technology, such as but not limited to, casting, forging, injection molding, compression molding, to create an airfoil end wall having no 3D contours (2D axisymmetric). The method may also include plating the 3D contours on top of the end wall 372 by way of selectively plating certain regions with a greater thickness than another region. The method may further include polishing the plated 3D contours to achieve desired final contour and flow path surface finish.
An exemplary polymeric substrate 311 may be injection-molded or compression molded and may include one or more polymers selected from the group consisting of: polyetherimide (PEI); polyimide; polyether ether ketone (PEEK); polyether ketone ketone (PEKK); polysulfone; polyamide; polyphenylene sulfide; polyester; polyimide; and combinations thereof. Suitable thermoset materials may include, but are not limited to: condensation polyimides; addition polyimides; epoxy cured with aliphatic and/or aromatic amines and/or anhydrides; cyanate esters; phenolics; polyesters; polybenzoxazine; polyurethanes; polyacrylates; polymethacrylates; silicones (thermoset); and combinations thereof.
The metallic layer 312 may then be applied to the polymeric substrate 311 by methods including, but not limited to, electroless plating, electroplating, or electroforming. The metallic layer 311 may be any number of different metals or alloys including, but not limited to: nickel; cobalt; copper; iron; gold; silver; palladium; rhodium; chromium; zinc; tin; cadmium; and alloys with any of the foregoing elements comprising at least 50 wt. % of the alloy; and combinations thereof. Plating may be performed in multiple steps by masking certain areas of the molded article to yield different thicknesses or no plating in certain areas. A customized plating thickness profile can also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.). The metallic layer 312 may be polished after plating to provide at least two benefits. First, a highly polished metallic layer 312 with have a high emissivity and therefore will be less subject to heating by radiant heat sources. Further, a highly polished metallic layer 312 will have improved smoothness, thereby promoting laminar flow and increased turbine and compressor efficiencies.
Thus, the disclosed plated polymer technology provides an affordable approach to forming 3D contours in platform end walls. Further, polishing the metallic layer surface increases emissivity and thus reduces heating of the platform by thermal radiation. A polished metallic layer surface also improves the gas flow path smoothness translating to gas turbine engine efficiency. A molded polymeric substrate and may be used as a fast, durable prototyping method to create 3D contours for end wall a similar 2D prototype, without the need for expensive hard tooling, or long lead time machining.
Full authority digital controls (FADECs) are used to house the engine control unit on aircraft engines. FADECs control all engine functions and communicate with the aircraft controls to ensure safe operation. FADEC housings are traditionally fabricated from aluminum castings, which are affordable but heavy. A lighter-weight more affordable FADEC (or any electrical control unit) housing could benefit any industry where weight versus payload and cost are design considerations (e.g., marine vehicle controls, automotive controls, etc.).
Referring to
The metallic layer(s) 312 may be applied by electroless plating, electroplating, or electroforming to a uniform thickness ranging from about 0.001 to about 0.05 inch (from about 25.4 microns to about 1.27 mm) The average plating thickness may range from about 0.003 to about 0.03 inches (from about 76.2 to about 762 microns). These thickness ranges provide resistance to wear, impact, FOD, etc. and the option to finish more aggressively to meet dimensional tolerances, surface finish requirements, etc. The metallic layer(s) 312 may be plated in multiple steps by masking certain areas of the electrical control unit housing to yield different thicknesses (or no plating) in areas of interest for performance or decorative purposes. Such a customized plating thickness profile can also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.). Tailored racking permits for optimization of properties for the electrical control unit housing with respect to structural support, surface characteristics, etc. without adding undue weight to the housing. Further, the electrical control unit housing may be fabricated in multiple segments that are joined by conventional process (e.g., ultrasonic, laser, friction and friction-stir welding processes; traditional welding processes; adhesives; mitered joints with or without adhesives) before plating. Furthermore, the electrical control unit housing may be produced in a plurality of segments that are plated separately and subsequently bonded by transient liquid phase (TLP) bonding.
The metallic layer(s) 312 may include of one or more metals including, but not limited: to nickel; cobalt; copper; iron; gold; silver; palladium; rhodium; chromium; zinc; tin; cadmium; and alloys with any of the foregoing elements comprising at least 50 wt. % of the alloy; and combinations thereof. Plating may be performed in multiple steps by masking certain areas of the molded article to yield different thicknesses or no plating in certain areas. A customized plating thickness profile can also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.).
One or more polymeric coatings 314 may also be applied to the metallic layer(s) 312 to produce a lightweight, stiff, and strong polymer appearing (non-conductive) housing. The polymeric coating(s) 314 may be applied by conventional processes, such as spray coating or dip coating.
A lightweight, plated polymer housing for FADECs and other electrical electronic control units provide a precisely engineered structure. The disclosed housings may be cheaper to manufacture and/or lighter than prior-art housings due to the disclosed plated polymer technology. Further, the metal appearance of the housing may increase the resale value of the unit. Polymer outer surfaces are also possible, if required.
Sound Attenuation Structures Made with Plated Polymers
There are two primary noise sources on a gas turbine engine—the fan and the turbine(s). To help attenuate fan noise, which cannot be controlled at the source, gas turbine engine makers use sound damping features in the walls of the fan duct. These features include honeycomb structures, which are both costly and difficult to manufacture.
An alternative sound-damping scheme is disclosed in the form of sound/vibration damping structures made from plated polymers. Turning to
The metallic layer 382 may include one or more layers. Plating may be performed in multiple steps by masking certain areas of the substrate 381 to yield different thicknesses (or no plating) in areas of interest for performance or for later introduction of discontinuous vibration damping materials for noise attenuating purposes. This customized plating thickness profile can also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.). Tailored racking allows for optimization of properties for the vibration/noise dampener with respect to structural support, surface characteristics, etc. without adding undue weight to the sound/vibration damper 380. The metallic layer(s) 382 may be then applied to the polymeric substrate 381 by methods such as, but not limited to, electroless plating, electroplating or electroforming. The metallic layer 381 may be formed from one or more metals including, but not limited to: nickel; cobalt; copper; iron; gold; silver; palladium; rhodium; chromium; zinc; tin; cadmium; and alloys with any of the foregoing elements comprising at least 50 wt. % of the alloy; and combinations thereof. Plating may be performed in multiple steps by masking certain areas of the molded article to yield different thicknesses or no plating in certain areas. A customized plating thickness profile can also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.).
The sound vibration damper 380 can be fabricated in multiple segments that are joined by any conventional process (e.g., ultrasonic, laser, friction and friction-stir welding processes; traditional welding processes; adhesives; mitered joints with or without adhesives) before plating. Furthermore, the vibration damper/attenuator 380 can be produced and plated separately and subsequently bonded by transient liquid phase (TLP) bonding.
One or more polymeric coatings 384 may also be applied to the metallic layer(s) 382 to produce a lightweight, stiff and strong polymer appearing (non-conductive) sound/vibration damper 380 or to enhance performance of the sound/vibration damper 380. The polymeric coating(s) 384 may be applied by conventional processes, such as spray coating or dip coating. In addition, as shown in
Thus, disclosed vibration damper/attenuators may not only reduce transmitted noise from the fan blades, but could also be used in a high-temperature exhaust system. The durability of the disclosed vibration damper/attenuator may also offer improved durability over traditional honeycomb materials.
Drive and Transmission Shafts Made from Plated Polymeric Substrates
Drive shafts, transmission shaft and rotors are used to transmit power and torque from a drive component to a driven component. Typically, such shafts are made from metal materials or alloys due to high strength and stiffness requirements. However, metal shafts are heavy and costly. Thus, high strength, high torque shafts that are lighter than metal shafts but perform as well as metal shafts would be of value to payload driven platforms.
Turning to
The metallic layer 392 may be plated in multiple steps by masking certain areas of the formed polymeric substrate 391 to vary the thickness of the metallic layer 392 for performance or handling purposes. Such a customized plating thickness profile may also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.). Tailored racking allows for optimization of properties of the shaft 390 with respect to structural support, surface characteristics, etc. without adding undue weight to the shaft 390. The shaft 390 may be fabricated in multiple segments that are joined by a conventional process (e.g., ultrasonic, laser, friction and friction-stir welding processes; traditional welding processes; adhesives; mitered joints with or without adhesive) before plating. Furthermore, the shaft 390 may be produced in multiple segments that may be plated separately and subsequently bonded together by transient liquid phase (TLP) bonding.
Thus, a hybrid metal-composite drive or torque transmission shaft can be produced which is lighter in weight than traditional all metal shafts. The hybrid construction using a plated polymers can produce a higher stiffness and lighter weight shaft, at similar or lower cost.
Valves used for aircraft engines typically employ metal housings or enclosures. A valve typically includes one or more inlets and one or more outlets to control flow. Metal valve housings are heavy and therefore add unwanted weight to the aircraft. Thus, durable, but lighter alternatives are desired.
Turning to
The metallic layer 312 may include one or more layers. The metallic layer(s) 312 may be applied by electroless plating, electroplating, or electroforming to a thickness ranging from about 0.01 to about 0.09 inches (from about 0.254 to about 2.29 mm, locally. An average plating thickness may range from about 0.015 to about 0.08 inches (from about 0.381 to about 2.03 mm) These thickness ranges provide resistance to erosion, impact, FOD, etc. and the option to finish more aggressively to meet tight tolerances, surface finish requirements, etc. The metallic layer(s) 312 may include any one or more of the following: nickel; cobalt; copper; iron; gold; silver; palladium; rhodium; chromium; zinc; tin; cadmium; and alloys with any of the foregoing elements comprising at least 50 wt. % of the alloy; and combinations thereof.
The metallic layer(s) 312 may be plated in multiple steps by masking certain areas of the formed polymeric substrate to yield different thicknesses (or no plating) in areas of interest. Such a customized plating thickness profile may also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.). Tailored racking process permits optimization of properties for the valve housing with respect to fire resistance, structural support, surface characteristics, etc. without adding undue weight to the valve housing.
Some mounting features (e.g., flanges or bosses) may be bonded to the substrate 311 using a suitable adhesive after molding but before plating to simplify the mold tooling. More broadly, the valve housing may be fabricated in multiple segments that are joined by a conventional process (e.g., ultrasonic, laser, friction and friction-stir welding processes; traditional welding processes; adhesives; mitered joints with or without adhesive) before plating. Furthermore, the valve housing may be produced and plated separately and subsequently bonded by transient liquid phase (TLP) bonding. In addition, features such as bosses or inserts may be added (using an adhesive, riveting, etc.) to the part after the plating process.
One or more polymeric coatings 314 may also be applied to the plated polymer valve housing to produce a lightweight, stiff, and strong polymer appearing (non-conductive) valve housing. The polymeric coating(s) 314 may be applied by conventional processes, such as spray coating or dip coating.
Thus, plated polymer valve housings or enclosures offer cost and/or weight savings compared to traditional metal materials. The molding of the polymeric substrate and the plating of the molded polymeric substrate are both high-throughput processes. Further, complex housing geometries may be accommodated by producing multiple polymer segments and joining them together before plating of after plating using TLP bonding.
During operation of a gas turbine engine, ice may accumulate on the fan blades before it is shed from the fan blades in a radially outward and in the aft direction. Thus, as the ice is forced radially outward and aft of the fan blades, the ice impacts the inner flow path surface of the fan case. To insure that the impact of the ice does not result in damage to the inner flow path surface of the fan case, ice impact panels are known and are installed on the fan case. Typically, an ice impact panels is a Kevlar/epoxy composite laminate. Such composite laminate ice impact panels work well at resisting damage from ice impact, but are relatively expensive to manufacture. Thus, an effective but cheaper alternative is needed.
Referring to
The substrate 401 is then coated with at least one metallic layer 402, and preferably multiple metallic layers. The metallic layers may include nickel or sulfamate nickel to improve the strength and impact resistance of the thermoplastic substrate 401 such that it can withstand the ice impact. Other suitable metals include, but are not limited to: nickel; cobalt; copper; iron; gold; silver; palladium; rhodium; chromium; zinc; tin; cadmium; and alloys with any of the foregoing elements comprising at least 50 wt. % of the alloy; and combinations thereof. Plating may be performed in multiple steps by masking certain areas of the molded article to yield different thicknesses or no plating in certain areas. A customized plating thickness profile can also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.).
Thus, plated polymer ice impact panels may be fabricated from a molded polymer substrate that may be plated to provide ice impact panels that are cheaper to make but as effective as the currently employed composite laminate ice impact panels.
An oil or lubrication system of a gas turbine engine, or any similar type of engine, may provide pressurized and heated oil to one or more bearings, a gearbox, a gear train, etc. A lubrication system for an engine may include a plurality of tubes and connectors. Such tubes and connectors are normally machined out of stainless steel because of internal pressure, temperature and anti-erosion requirements and to prevent oil leaks at preformed seals. The manufacturing costs of such tubes and connectors can be high due to the high-precision machining and corrosion resistant steel used to fabricate the tubes and connectors. Because of the use of stainless steel as the material of construction, such stainless steel tubes and connectors are heavy in comparison to parts fabricated from thermoplastic materials. As a result, stainless steel or metal tubes and connectors add weight to the engine, which reduces the fuel efficiency of the engine. However, replacing the stainless steel or metal in such tubes and connectors with a lighter, different metal is problematic due to the operating conditions of many gas turbine engines, including those used to power aircraft. For example, many thermoplastic materials are not suitable for aircraft engine applications because, in the case of lubrication system tubes and connectors, the material must be able to withstand continuous operating temperatures of 177° C. (350° F.) or higher while also enduring thermal cycles and internal pressure requirements.
To provide durable and lightweight tubes and connectors for use in engines that have relatively complex geometries and that operate in relatively extreme environments, disclosed herein are tubes and connectors made from molded or machined or additively manufactured polymeric materials that are plated. The disclosed tubes and connectors have a comparably low weight and may offer reduced manufacturing costs.
To reduce the weight and cost of tubes and connectors for engines that operate in harsh environments, composite tubes, connectors, nozzles, etc. are disclosed like the exemplary tube/connector 410 shown in
After the polymeric substrate 411 is formed as shown in
The tube/connector 410 may be machined, as necessary, to the required dimensions using conventional methods. For example, the polymeric substrate 411 may be machined as necessary after molding and/or after application of the metallic layer(s) 412, 413. Tight tolerance requirements may be met with conventional machining processes. In addition, the thin metallic layer 412 provided in the above example may not be necessary.
To ensure a thick, uniform layer of metal in the internal passage 417 of the tube/connector 410, a metal tube 418 (e.g., stainless steel or a comparable metal or alloy) may be inserted into the passage 417 to provide additional support and resistance to erosion, etc. The metal tube 418 could be inserted before or after the plating process. In addition, the polymeric substrate 411 may be co-molded with the metal tube 418 in place.
The tube/connector 410 may also be a nozzle. In the case of nozzles with small holes, metal tubular inserts 418 could be used to line the internal passage 417 to ensure coverage of small channels or passages with metal.
Thus, plated polymer tubes, connectors, and nozzles are lighter in weight compared to their steel counterparts. The plating may provide dimensional stability for parts under substantial internal pressures at high temperatures. Certain complex geometries found in tubes, connectors and nozzles might be easier to fabricate using a forming process as compared to machining a part from stock material. Furthermore, formed or machined polymeric substrates may be produced separately and subsequently bonded together before plating to create a more complex plated part. Further, complex geometries may be accommodated by producing multiple polymer segments and joining them together after plating using TLP bonding. Further, plated polymer parts may be produced in high volumes with faster turnaround times than parts made by machining.
Turning to
The exemplary gearbox cover 420 may include a polymeric substrate 311 and one or more metallic layers 312 as shown in
The exemplary substrate 311 may be injection-molded or compression molded formed at least one polymer selected from the group consisting of: polyetherimide (PEI); polyimide; polyether ether ketone (PEEK); polyether ketone ketone (PEKK); polysulfone; polyamide; polyphenylene sulfide; polyester; polyimide; and combinations thereof. Suitable thermoset materials may include, but are not limited to: condensation polyimides; addition polyimides; epoxy cured with aliphatic and/or aromatic amines and/or anhydrides; cyanate esters; phenolics; polyesters; polybenzoxazine; polyurethanes; polyacrylates; polymethacrylates; silicones (thermoset); and combinations thereof. Optionally, the polymeric material of the polymeric substrate 311 may be structurally reinforced with materials that may include carbon, metal, or glass. The fiber-reinforced polymeric substrate 311 may include a plurality of layers to form a composite layup structure.
Some mounting features (e.g., flanges or bosses) may be bonded to the substrate 311 using a suitable adhesive after molding but before plating to simplify the mold tooling. Further, the cover 420 may be fabricated by molding the substrate 311 in separate, multiple segments that are subsequently joined by a conventional process (e.g., ultrasonic, laser, friction and friction-stir welding processes; traditional welding processes; adhesives; mitered joints with or without adhesive) before plating. Further, complex geometries may be accommodated by producing multiple polymer segments and joining them together after plating using TLP bonding.
An injection-molded polymeric substrate 311 may have thickness ranging from about 0.05 to about 0.2 inches (from about 1.27 to about 5.08 mm) On the other hand, a compression-molded polymeric substrate 311 may have a thickness ranging from about 0.05 to about 2 inches (from about 1.27 to about to about 50.8 mm) In addition, reinforcing fibers (e.g., glass and/or carbon fibers) may be locally added, as required, to meet structural requirements.
From about 10 to about 60 wt % of the gearbox cover 420 may be attributed to the metallic layer(s) 312. Portions of the metallic layer(s) 312 may be purposefully weakened (or the polymeric substrate can be masked before plating) to provide paths for outgassing and expansion of the polymeric substrate during a fire. The weakened portions should not reside near areas of the gearbox cover 420 that may be significantly stressed or that experience stress concentrations. Such weakened portions may be used to provide appropriate redirection of thermally-induced stresses and strains away from critical load paths. The metallic layer(s) 312 may be applied by electroplating or electroforming to a thickness ranging from about 0.01 to about 0.1 inches (from about 0.254 to about 2.54 mm) The metallic layer(s) 312 may be formed from one or more metals including, but not limited: nickel; cobalt; copper; iron; gold; silver; palladium; rhodium; chromium; zinc; tin; cadmium; and alloys with any of the foregoing elements comprising at least 50 wt. % of the alloy; and combinations thereof. Plating may be performed in multiple steps by masking certain areas of the molded article to yield different thicknesses or no plating in certain areas. A customized plating thickness profile can also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.).
Thus, gearboxes made from plated polymers may provide cost or weight savings. Further, fabricating a gearbox from a plated polymer may yield lower lead times, which is a significant advantage over the normally long lead-time required for gearbox covers. As a result, using plated polymers for gearboxes provides increased flexibility in the detailed design phase of engine development and shorter baseline schedules for cover/housing developments, which both have a significant impact on program costs, even though they do not necessarily make the gearbox itself less expensive than a metal counterpart.
Referring to
Improved light weight and stiff forward cones 440, 450, 470 are shown in
Due to the injection molding process, the ribs 441, 442, 443 may require a draft angle for removal from the mold tool (not shown), and a thickness and height of the ribs 441, 442, 443 may primarily be a function of the cone thickness due to shrinkage concerns. Regardless, the quantity and spacing of the ribs 441, 442 and the optional shear ties or ribs 443 and the overall thickness of forward cones 440, 450, 470 (with and without the ribs 441, 442 and shear ties 443) may be optimized. The ribs 441, 442, 443 do not have to be evenly spaced.
Referring back to
The plating of the polymeric substrate 311 produces lightweight forward cones 440, 450, 470 with high specific strength and resistance to certain environmental concerns, e.g., erosion. Variations in the desired wall thickness or thickness of the polymeric substrate 311 may be easily accommodated in the molding process. The exemplary substrate 311 may be injection-molded or compression-molded and formed from one or more polymers selected from the group consisting of: condensation polyimides; addition polyimides; epoxy cured with aliphatic and/or aromatic amines and/or anhydrides; cyanate esters; phenolics; polyesters; polybenzoxazine; polyurethanes; polyacrylates; polymethacrylates; silicones (thermoset); and combinations thereof. Optionally, the polymeric material of the polymeric substrate 311 may be structurally reinforced with materials that may include carbon, metal, or glass. The fiber-reinforced polymeric substrate 311 may include a plurality of layers to form a composite layup structure.
The forward cones 440, 450, 470 necessarily include mounting features (of which only a flange 471 is shown in
Thus, one-piece, injection-molded and plated forward cone (i.e., a combination nose cap and spinner) may be manufactured for a lower cost than prior art nose caps and spinners. The disclosed forward cone may be unitary, thereby replacing two parts (a nose cap and a spinner) with a single unitary forward nose cone. Disclosed one-piece, injection-molded cores that are plated with a metallic layer can be manufactured for a much lower cost than KEVLAR composites of the prior art. The disclosed forward cones are lighter and new designs may be fabricated with shorter lead times. The plated metallic layer(s) provides resistance to erosion while typical prior art spinners require an additional coating for erosion resistance. The disclosed nose cones may include reinforcing elements in the form of an internal ribbed structure designed to carry and distribute static and impact loads throughout the forward cone more efficiently than a constant thickness structure. Therefore, the wall thickness of the forward cone may be reduced to save weight.
In a gas turbine engine 110 (
An exemplary spinner attachment ring 460 is shown in
The metallic layer 312 may include one or more layers. The metallic layer(s) may be applied by electroless plating, electroplating, or electroforming to a thickness ranging from about 0.001 to about 1 inch (from about 25.4 microns to about 2.54 cm), locally. An average plating thickness may range from about 0.01 to about 0.075 inches (from about 254 microns to about 1.91 mm) These thickness ranges provide resistance to erosion, impact, etc. and the option to finish more aggressively to meet tight tolerances, surface finish requirements, etc. The metallic layer 312 may be formed from one or more metals including, but not limited: nickel; cobalt; copper; iron; gold; silver; palladium; rhodium; chromium; zinc; tin; cadmium; and alloys with any of the foregoing elements comprising at least 50 wt. % of the alloy; and combinations thereof.
The metallic layer(s) 312 may be applied in multiple steps by masking certain areas of the attachment ring to yield different thicknesses in areas of interest, such as platforms or flanges. Such a customized plating thickness profile may also be achieved by tailored racking (includes shields, thieves, etc.). In addition, a thicker metallic layer(s) 312 allows for more aggressive machining, finishing, etc. to achieve the desired surface roughness, tolerances, etc. Such a multi-step process allows for optimization of attachment ring properties, with respect to fire, structural support, surface characteristics, etc. without adding undue weight to the attachment ring 460.
Further, the attachment ring 460 may be fabricated in multiple segments that are joined by any a conventional process (e.g., ultrasonic, laser, friction and friction-stir welding processes; traditional welding processes; adhesives; mitered joints with or without adhesive) before plating. Because the metallic layer 312 is thick enough to provide significant structural strength and rigidity, the method of joining segments will likely not be a strength limiting factor.
Thus, plated polymer attachment rings are disclosed that have applications beyond attaching a spinner or forward cone to a hub. The disclosed attachment rings are relatively inexpensive to manufacture due to the high-throughput molding and plating processes used to make the rings.
Some component surfaces of gas turbine engines require protection against erosion and de-icing capability. Current materials that are relatively erosion resistant include metals, ceramics, and some polymers. It is desirable to simultaneously provide an erosion resistant material that also repels or selectively directs water and/or prevents ice buildup on the component surfaces.
Turning to
At least one metallic layer 483 is plated on top of a textured polymeric substrate 482, which can render the textured surface 480 with even more resistance to erosion and super-hydrophobicity to prevent water attachment, and thus, to minimize ice buildup/adhesion. The substrate 482 may include, but is not limited to: polyetherimide (PEI); polyimide; polyether ether ketone (PEEK); polyether ketone ketone (PEKK); polysulfone; polyamide; polyphenylene sulfide; polyester; polyimide; and combinations thereof. Suitable thermoset materials may include, but are not limited to: condensation polyimides; addition polyimides; epoxy cured with aliphatic and/or aromatic amines and/or anhydrides; cyanate esters; phenolics; polyesters; polybenzoxazine; polyurethanes; polyacrylates; polymethacrylates; silicones (thermoset); and combinations thereof. Optionally, the polymeric material of the polymeric substrate 482 may be structurally reinforced with materials that may include carbon, metal, or glass. The fiber-reinforced polymeric substrate 482 may include a plurality of layers to form a composite layup structure. The metallic layer(s) 483 may be formed from one or more metals including, but not limited: nickel; cobalt; copper; iron; gold; silver; palladium; rhodium; chromium; zinc; tin; cadmium; and alloys with any of the foregoing elements comprising at least 50 wt. % of the alloy; and combinations thereof. Plating may be performed in multiple steps by masking certain areas of the molded article to yield different thicknesses or no plating in certain areas. A customized plating thickness profile can also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.).
The metallic layer(s) 483 provide erosion and fatigue resistance. The metallic layer 483 may include one or more layers, preferably with a non-hydrophilic top-most layer. The metallic layer(s) 483 may be applied by electroless plating, electroplating, or electroforming to a thickness of about 10% of the texture dimension h.
Thus, as opposed to prior art hardening or coating techniques including nitriding and aluminizing to avoid erosion, texture plated polymer surfaces are disclosed, for example, a textured plated polymer forward cones, nose cones or spinners. The textured plated polymer design saves both weight and costs and can generate a textured metallic layer of a uniform thickness.
Many components of a gas turbine engine must be resistant to impact events from both hard objects (rocks, debris, ice, etc.) and soft objects (bird strikes, etc.). Components of other engines, such as truck, automotive, marine, etc., also must be resistant to such impact events. Components made from traditional materials such metals, polymers, composites, ceramics, etc. often must be made heavier or with more complex geometries to meet impact-resistant requirements. Heavier components and/or components with more complex geometries increase cost and manufacturing lead time as well as substantial design and manufacturing efforts.
Turning to
The metallic layer(s) 502 may include one or more layers. The metallic layer(s) 502 may be applied by electroless plating, electroplating, or electroforming to a thickness ranging from about 0.001 to about 0.5 inches (from about 25.4 microns to about 12.7 mm), locally. An average plating thickness may range from about 0.004 to about 0.3 inches (from about 101.6 microns to about 7.62 mm) These thickness ranges provides resistance to erosion, impact, FOD, etc. and the option to finish more aggressively to meet tight tolerances, surface finish requirements, etc. The plating of the metallic layer(s) 502 may be carried out in multiple steps by masking certain areas of the polymeric substrate 501 to yield different plating thicknesses (or no plating) in areas of interest. Such a customized plating thickness profile may also be achieved by tailored racking (including shields, thieves, conformal anodes, etc.). Tailored racking allows for an optimization of properties for the impact-resistant plated polymer structure 500 with respect to fire resistance, structural support, surface characteristics, etc. without adding undue weight to the structure 500. The metal layer(s) 502 may be formed from one or more metals including, but not limited: nickel; cobalt; copper; iron; gold; silver; palladium; rhodium; chromium; zinc; tin; cadmium; and alloys with any of the foregoing elements comprising at least 50 wt. % of the alloy; and combinations thereof.
The impact-resistant plated polymer structure 500 may be fabricated in multiple segments that may be are joined by a conventional process (e.g., ultrasonic, laser, friction or friction-stir welding processes; traditional welding processes; adhesives; mitered joints with or without adhesive) before plating. Such segments of a final structure 500 may be produced and plated separately, and subsequently bonded together by transient liquid phase (TLP) bonding. Features such as inserts or details may be added (using an adhesive, riveting, etc.) to the structure 500 after the plating process. One or more polymeric coatings 503 may also be applied to impact-resistant plated polymer structure 500 to yield a lightweight, stiff and strong polymer appearing (non-conductive) component. The polymeric coating(s) 503 may be applied by a conventional process, such as spray coating or dip coating, and may be applied to localized regions only, if desired.
Turning to
0.010×h1≦h2≦3.00×h1 Eq. A
0.125×h1≦w1≦0.75×h1 Eq. B
0.05 inch(1.27 mm)≦w2≦0.75×h1 Eq. C
0°≦φ≦80° Eq. D
0.025 inch (635 microns)≦r Eq. E
0.001 inch (25.4 microns)≦t≦0.5 inch (12.7 mm) Eq. F
Turning to
Plated polymer materials such as plated polymeric substrates, plated polymeric composite substrates and plated polymeric composite layup structures may be used to form lightweight but strong parts of gas turbine engines, such as a layshaft cover, a case, a component of a nacelle assembly, a fan inlet duct, a component of a thrust reverser, bulkheads, fixed panels or structures that may be used for sound attenuation, etc. The plated polymeric gas turbine engine components may offer cost and/or weight savings compared to baseline parts. The plated metallic layers provide properties such as erosion resistance that can remove the need for erosion coatings on a composite case or cover.
This application claims priority under 35 U.S.C. §119(e) to U.S. Provisional Patent Application Ser. No. 61/844,048 filed on Jul. 9, 2013, entitled “Lightweight Gas Turbine Engine Components Produced By Plating Molded Polymer Article,” and to U.S. Provisional Patent Application Ser. No. 61/844,161 filed on Jul. 9, 2013, entitled “Construction and Building Materials Formed From Plated Polymers.”
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/US2014/045998 | 7/9/2014 | WO | 00 |
| Number | Date | Country | |
|---|---|---|---|
| 61844048 | Jul 2013 | US | |
| 61844161 | Jul 2013 | US |
