Aerospace materials

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Titanium support structure for a jet engine thrust reverser Rolls Royce RB.199 6.jpg
Titanium support structure for a jet engine thrust reverser

Aerospace materials are materials, frequently metal alloys, that have either been developed for, or have come to prominence through their use for aerospace purposes.

Contents

These uses often require exceptional performance, strength or heat resistance, even at the cost of considerable expense in their production or machining. Others are chosen for their long-term reliability in this safety-conscious field, particularly for their resistance to fatigue.

The field of materials engineering is an important one within aerospace engineering. Its practice is defined by the international standards bodies [1] who maintain standards for the materials and processes involved. [2] Engineers in this field may often have studied for degrees or post-graduate qualifications in it as a speciality. [3]

History

Radome over H2S radar scanner on a Halifax H2S Radome And Scanner On Halifax.jpg
Radome over H2S radar scanner on a Halifax
Honeycomb sandwich structure of Glass Reinforced Aluminium Glare honeycomb.jpg
Honeycomb sandwich structure of Glass Reinforced Aluminium

Edwardian period

The first aerospace materials were those long-established and often naturally occurring materials used to construct the first aircraft. These included such mundane materials as timber for wing structures and fabric and dope to cover them. Their quality was of utmost importance and so the timber would be of carefully selected sitka spruce and the covering of irish linen. Standards were required for the selection, manufacture, and use of these materials. These standards were developed informally by manufacturers or government groups such as HM Balloon Factory, later to become RAE Farnborough, often with the assistance of university engineering departments.

The next stage in the development of aerospace materials was to adopt newly developed materials, such as Duralumin the first age hardening aluminum alloy. These offered attributes not previously available. Many of these new materials also required study to determine the extent of these new properties, their behavior and how to make the best use of them. This work was often carried out through the new government-funded national laboratories, such as the Reichsanstalt (German Imperial Institute) [4] or the British National Physical Laboratory (NPL).

World War I

The NPL was also responsible for perhaps the first deliberately engineered aerospace material, Y alloy. [5] This first of the nickel-aluminum alloys was discovered after a series of experiments [6] during World War I, deliberately setting out to find a better material for the manufacture of pistons for aircraft engines.

Interwar period

Between the wars, many aerospace innovations were in the field of manufacturing processes, rather than just an inherently stronger material, although these too benefited from improved materials. One of the R.R. alloys, R.R.53B, had added silicon which improved its fluidity when molten. This allowed its use for applications such as die casting as well as the previous sand casting, a means of producing parts that were both far cheaper and also more accurate in shape and finish. Better control of their shape allowed designers to shape them more precisely to their tasks, leading to parts that were also thinner and lighter.

Many interwar developments were to aircraft engines, which benefited from the vast improvements being made for the growing car industry. Although not strictly an 'aerospace' innovation, the use of refractory alloys like Stellite and Brightray for the hard-facing of exhaust valves offered huge gains in the reliability of aircraft engines. [7] This itself encouraged long-range commercial flights, as the new engines were reliable enough to be considered safe for long flights across oceans or mountain ranges.

World War II

The de Havilland Albatross airliner of 1936 had a fuselage of wooden sandwich construction: wafers of birch plywood were spaced apart by a balsa sheet. This same construction achieved fame with its wartime use in the Mosquito fast bomber. As well as being a construction of light weight and high performance, it also avoided the use of aluminum, a strategic material during wartime, and could use the skills of woodworkers, rather than those of specialized aircraft metalworkers. When Germany attempted to copy this aircraft as the Moskito it was a failure, primarily for materials reasons. The original phenolic Tego film adhesive was only produced by a factory that was destroyed by bombing. Its replacement led directly to catastrophic failures and loss of the aircraft.

Radar became small enough to be carried on board aircraft, but the fragile feed horns and reflectors needed to be protected and streamlined from the airstream. Molded radomes were constructed, using the Perspex acrylic plastic that was already in use for cockpit windows. This could be heated to soften it, then molded or vacuum formed to shape. Other polymers developed at this time, notably Nylon, found uses in compact radio equipment as high-voltage insulators or dielectrics.

Honeycomb structures were developed as flat sandwich sheets used for bulkheads and decking. These were long established with wood and paper board construction, but required a more robust material for aerospace use. This was achieved towards the end of the war, with all-aluminum honeycomb sandwiches.

Post-war

New materials

New lightweight materials include Ceramic matrix composites, metal matrix composites, polymer aerogels and CNT-yarns, along the evolution of polymer composites. [8] These light weight materials have given way for stronger, more reliable structures, improved production times and increased power-to-weight ratios.

Marketing outside aerospace

Carbon fiber money clip Carbon Fiber Money Clip.jpg
Carbon fiber money clip

The term "aerospace grade" has come to be a fashionable marketing slogan for luxury goods, particularly for cars and sporting goods. Bicycles, golf clubs, sailing yachts and even flashlights are all sold on the basis of their high-performance materials, whether these are relevant or not. Since their appearance in 1979, Maglite have advertised their use of 6061 aluminum for their torch bodies, one of the first to make a deliberate feature of aerospace materials for a non-performance reason.

Some sporting uses have been for the material's actual qualities. Many ski makers have produced skis wholly from cloth and resin composite materials, using the tailorability of such construction to vary the stiffness, damping and torsional stiffness of a ski along its length. Hexcel, a manufacturer of aluminum honeycomb sheet, became well known for its branded skis, using this same advanced material.

Sporting uses may be every bit as demanding as aerospace needs. Particularly in cycling, materials may be loaded more highly than in aerospace use, the risk of possible failure being seen as more acceptable than for aircraft.

Many uses of aerospace materials for sporting goods have been as the result of a 'peace dividend'. After World War II, Hiduminium alloy appeared in bicycle brake components [9] as its maker sought to expand new markets to replace their previous military aircraft. In the 1990s, both smelters and recyclers of titanium sought new non-military markets after the end of the Cold War, finding them in both bicycle frames and golf clubs.

Carbon fiber composite, and its distinctive weave pattern, has become a popular decorative choice on cars and motorbikes, even in purely decorative contexts such as dashboards. This has extended to the use of flexible stick-on patterned vinyl to skeuomorphically reproduce the appearance without any of the physical properties.

Related Research Articles

In materials science, a metal matrix composite (MMC) is a composite material with fibers or particles dispersed in a metallic matrix, such as copper, aluminum, or steel. The secondary phase is typically a ceramic or another metal. They are typically classified according to the type of reinforcement: short discontinuous fibers (whiskers), continuous fibers, or particulates. There is some overlap between MMCs and cermets, with the latter typically consisting of less than 20% metal by volume. When at least three materials are present, it is called a hybrid composite. MMCs can have much higher strength-to-weight ratios, stiffness, and ductility than traditional materials, so they are often used in demanding applications. MMCs typically have lower thermal and electrical conductivity and poor resistance to radiation, limiting their use in the very harshest environments.

<span class="mw-page-title-main">Carbon fibers</span> Material fibers about 5–10 μm in diameter composed of carbon

Carbon fibers or carbon fibres are fibers about 5 to 10 micrometers (0.00020–0.00039 in) in diameter and composed mostly of carbon atoms. Carbon fibers have several advantages: high stiffness, high tensile strength, high strength to weight ratio, high chemical resistance, high-temperature tolerance, and low thermal expansion. These properties have made carbon fiber very popular in aerospace, civil engineering, military, motorsports, and other competition sports. However, they are relatively expensive compared to similar fibers, such as glass fiber, basalt fibers, or plastic fibers.

<span class="mw-page-title-main">Bicycle frame</span> Main component of a bicycle

A bicycle frame is the main component of a bicycle, onto which wheels and other components are fitted. The modern and most common frame design for an upright bicycle is based on the safety bicycle, and consists of two triangles: a main triangle and a paired rear triangle. This is known as the diamond frame. Frames are required to be strong, stiff and light, which they do by combining different materials and shapes.

<span class="mw-page-title-main">Airframe</span> Mechanical structure of an aircraft

The mechanical structure of an aircraft is known as the airframe. This structure is typically considered to include the fuselage, undercarriage, empennage and wings, and excludes the propulsion system.

Fibre-reinforced plastic is a composite material made of a polymer matrix reinforced with fibres. The fibres are usually glass, carbon, aramid, or basalt. Rarely, other fibres such as paper, wood, boron, or asbestos have been used. The polymer is usually an epoxy, vinyl ester, or polyester thermosetting plastic, though phenol formaldehyde resins are still in use.

<span class="mw-page-title-main">Ceramic engineering</span> Science and technology of creating objects from inorganic, non-metallic materials

Ceramic engineering is the science and technology of creating objects from inorganic, non-metallic materials. This is done either by the action of heat, or at lower temperatures using precipitation reactions from high-purity chemical solutions. The term includes the purification of raw materials, the study and production of the chemical compounds concerned, their formation into components and the study of their structure, composition and properties.

<span class="mw-page-title-main">Sandwich-structured composite</span> Material composed of two thin, stiff skins around a lightweight core

In materials science, a sandwich-structured composite is a special class of composite materials that is fabricated by attaching two thin-but-stiff skins to a lightweight-but-thick core. The core material is normally of low strength, but its greater thickness provides the sandwich composite with high bending stiffness with overall low density.

<span class="mw-page-title-main">Aluminium alloy</span> Alloy in which aluminium is the predominant metal

An aluminium alloy (UK/IUPAC) or aluminum alloy is an alloy in which aluminium (Al) is the predominant metal. The typical alloying elements are copper, magnesium, manganese, silicon, tin, nickel and zinc. There are two principal classifications, namely casting alloys and wrought alloys, both of which are further subdivided into the categories heat-treatable and non-heat-treatable. About 85% of aluminium is used for wrought products, for example rolled plate, foils and extrusions. Cast aluminium alloys yield cost-effective products due to the low melting point, although they generally have lower tensile strengths than wrought alloys. The most important cast aluminium alloy system is Al–Si, where the high levels of silicon (4–13%) contribute to give good casting characteristics. Aluminium alloys are widely used in engineering structures and components where light weight or corrosion resistance is required.

<span class="mw-page-title-main">Material</span> Substance or mixture of substances that constitutes an object

A material is a substance or mixture of substances that constitutes an object. Materials can be pure or impure, living or non-living matter. Materials can be classified on the basis of their physical and chemical properties, or on their geological origin or biological function. Materials science is the study of materials, their properties and their applications.

Aluminium–lithium alloys are a set of alloys of aluminium and lithium, often also including copper and zirconium. Since lithium is the least dense elemental metal, these alloys are significantly less dense than aluminium. Commercial Al–Li alloys contain up to 2.45% lithium by mass.

6061 aluminium alloy is a precipitation-hardened aluminium alloy, containing magnesium and silicon as its major alloying elements. Originally called "Alloy 61S", it was developed in 1935. It has good mechanical properties, exhibits good weldability, and is very commonly extruded. It is one of the most common alloys of aluminium for general-purpose use.

7075 aluminium alloy (AA7075) is an aluminium alloy with zinc as the primary alloying element. It has excellent mechanical properties and exhibits good ductility, high strength, toughness, and good resistance to fatigue. It is more susceptible to embrittlement than many other aluminium alloys because of microsegregation, but has significantly better corrosion resistance than the alloys from the 2000 series. It is one of the most commonly used aluminium alloys for highly stressed structural applications and has been extensively used in aircraft structural parts.

An aerostructure is a component of an aircraft's airframe. This may include all or part of the fuselage, wings, or flight control surfaces. Companies that specialize in constructing these components are referred to as "aerostructures manufacturers", though many larger aerospace firms with a more diversified product portfolio also build aerostructures.

<span class="mw-page-title-main">Hexcel</span> American materials company

Hexcel Corporation is an American public industrial materials company, based in Stamford, Connecticut. The company develops and manufactures structural materials. Hexcel was formed from the combination of California Reinforced Plastics, Ciba Composites and Hercules Composites Products Division. The company sells its products in commercial, military and recreational markets for use in commercial and military aircraft, space launch vehicles and satellites, wind turbine blades, sports equipment and automotive products. Hexcel works with Airbus Group, The Boeing Company, and others. Since 1980, the firm has publicly traded on the New York Stock Exchange under the ticker symbol HXL.

<span class="mw-page-title-main">Honeycomb structure</span> Natural or man-made structures that have the geometry of a honeycomb

Honeycomb structures are natural or man-made structures that have the geometry of a honeycomb to allow the minimization of the amount of used material to reach minimal weight and minimal material cost. The geometry of honeycomb structures can vary widely but the common feature of all such structures is an array of hollow cells formed between thin vertical walls. The cells are often columnar and hexagonal in shape. A honeycomb-shaped structure provides a material with minimal density and relative high out-of-plane compression properties and out-of-plane shear properties.

<span class="mw-page-title-main">Sandwich panel</span> Structure made of three layers

A sandwich panel is any structure made of three layers: a low-density core, and a thin skin-layer bonded to each side. Sandwich panels are used in applications where a combination of high structural rigidity and low weight is required.

A thermoset polymer matrix is a synthetic polymer reinforcement where polymers act as binder or matrix to secure in place incorporated particulates, fibres or other reinforcements. They were first developed for structural applications, such as glass-reinforced plastic radar domes on aircraft and graphite-epoxy payload bay doors on the Space Shuttle.

Carbon fiber-reinforced polymers, carbon-fibre-reinforced polymers, carbon-fiber-reinforced plastics, carbon-fiber reinforced-thermoplastic, also known as carbon fiber, carbon composite, or just carbon, are extremely strong and light fiber-reinforced plastics that contain carbon fibers. CFRPs can be expensive to produce, but are commonly used wherever high strength-to-weight ratio and stiffness (rigidity) are required, such as aerospace, superstructures of ships, automotive, civil engineering, sports equipment, and an increasing number of consumer and technical applications.

In materials science, advanced composite materials (ACMs) are materials that are generally characterized by unusually high strength fibres with unusually high stiffness, or modulus of elasticity characteristics, compared to other materials, while bound together by weaker matrices. These are termed "advanced composite materials" in comparison to the composite materials commonly in use such as reinforced concrete, or even concrete itself. The high strength fibers are also low density while occupying a large fraction of the volume.

<span class="mw-page-title-main">Aircraft recycling</span> Recycling industry for aircraft

Aircraft recycling is the process of scrapping and disassembling retired aircraft, and re-purposing their parts as spare parts or scrap. Airplanes are made of around 800 to 1000 parts that can be recycled, with the majority of them made from metal alloys and composite materials. The two most common metal alloys are aluminum and titanium and the main composite material is carbon fiber.

References

  1. "Aerospace Materials Division". SAE International.
  2. "Aerospace Material Standards". ASTM.
  3. "MSc(Eng) Aerospace Materials". University of Sheffield. Archived from the original on 2011-02-27.
  4. Magnello, Eileen (2000). A Century of Measurement: History of the National Physical Laboratory. HMSO. p. 16. ISBN   0-9537868-1-1.
  5. Higgins, Raymond A. (1983). Part I: Applied Physical Metallurgy (5th ed.). Hodder & Stoughton. pp. 435–438. ISBN   0-340-28524-9.{{cite book}}: |work= ignored (help)
  6. Experiment 'Y' of the series, giving the alloy its name.
  7. Clinton, Arnold C. A.F.R.AeS. (1938). Machining Operations on the 'Bristol Mercury' Engine. Aero Engineering. Vol. II, part 1. George Newnes. pp. 378–383.
  8. Richard Collins, IDTechEx (Aug 1, 2018). "Out of the lab and into a plane: The emerging materials making aircraft lighter". Aircraft Interiors.
  9. Hilary Stone. "G B brakes (Gerry Burgess Cycle Components, 1948)".