Engineering Plastics in Modern Airplane Manufacturing

Plane plastic

Engineering plastics are extensively applied in aircraft due to their lightweight nature, impact resistance, high strength, excellent electrical insulation, corrosion resistance, wear resistance, and ease of molding. Nearly all types of engineering plastics and their reinforced composites can find suitable applications and play vital roles in an aircraft structure. The applications of engineering plastics in aircraft can generally be categorized into electrical components, structural parts, interior trim, and transparent components.

Plastic Electrical Components

Their superior electrical insulation properties drove the initial use of engineering plastics in aviation. They are primarily used in motors, electrical appliances, instrumentation, and power distribution systems to manufacture coil bobbins, terminal blocks, sockets, connectors, switches, as well as insulation layers and protective sleeving for wiring. For example:

  • ABS, Polycarbonate (PC), PBT, and Polyamide (PA): Used for manufacturing electrical conduits, regulators, connectors, and various switches.
  • Polyetheretherketone (PEEK): Utilized for radar components and radomes.
  • Pyromellitic Polyimide (PI) Film: Used for insulation and protective layers of aviation wires and cables due to its exceptional heat resistance and dielectric properties.
Airplane plastic parts

Plastic Structural Parts

Replacing metal with engineering plastics for structural parts in aircraft engines and various accessories is a significant trend for expanding their application. These parts include self-lubricating bearings, bushings, seals, retaining rings, fasteners, instrument housings, cams, pulleys, gears, clamps, and various gaskets. Examples include:

  • Polyetheretherketone (PEEK): Used for manufacturing various engine components.
  • Polyamide (PA) and Polyoxymethylene (POM): Used for pulleys, cams, retaining rings, clamps, and gears.
  • Polytetrafluoroethylene (PTFE): Utilized for bearings due to its excellent self-lubricating properties.
  • Polyimide Molding Compounds: Used to replace bronze for wear-resistant bushings in engine front frames.
  • Glass Fiber Reinforced Polyimide: Used for jet engine tail nozzles and flap seals (fish scales).

Plastic Interior Trim

Interior trim represents another critical area of plastic application. For instance, in a Boeing 727 with a gross weight of 77,180 kg, plastics account for 2,730 kg, of which 908 kg are used for interior trim. These components include luggage racks, flooring, liners, seats, window frames, acoustic/thermal insulation, and decorative adhesives. Large-surface panels such as decorative side walls, ceilings, storage bins, and partitions are often surfaced with Polyvinyl Fluoride (PVF) film, which offers both aesthetic appeal and flame retardancy.

MaterialProcessing methodSun visors, lamp covers, food boxes, lavatory tissue boxes, magazine racks, and projector housings
Polycarbonate (PC)Rotational molding, InjectionSun visors, lamp covers, food boxes, lavatory tissue boxes, magazine racks, and projector housings
Polycarbonate (PC)Rotational molding, InjectionWindow frames, magazine racks, waste bins, seats, passenger service units (PSU), meal trays, carpet edging
ABSInjection, ExtrusionSeat armrests, door inner panels, door trim
Polyamide (PA)Injection, ExtrusionSeat backs, elastic cushions, wall panels, carry-cots
Polysulfone (PSU)Rotational molding, ThermoformingVentilation and drainage pipes
PVF FilmCasting or ExtrusionSurface laminates for wall panels, ceilings, etc.
Polyethersulfone (PES)InjectionWindow frame channels, sunshade rails, door handles, latches, oxygen mask housings, telephones, knobs
Polyethersulfone (PES)ExtrusionDecorative panels, ejection seat covers
Polyethersulfone (PES)Vacuum forming, ThermoformingSun visors, lamp covers, food boxes, lavatory tissue boxes, magazine racks, projector housings

Transparent Plastic Components

Transparent components refer to materials used for observation and lighting, including windshields, canopy covers, nose cones, various-shaped cabin windows, transparent partitions, instrument panels, passenger lighting covers, and navigation light covers. Since these are part of the airframe structure, they must maintain an aerodynamic profile and withstand aerodynamic loads, pressurization, and kinetic heating during flight. Consequently, they serve as both structural and functional members.

Transparent components

Performance of Transparent Plastics

Transparent materials are categorized into two types:

  • Polymethyl Methacrylate (PMMA), this is a general-purpose plastic.
  • Polycarbonate (PC), this is an engineering plastic.

These materials are used for monolithic transparent parts or as structural layers in glass-plastic composite systems. Structures include single-layer, double-layer, and laminated forms. Laminated structures are further classified by material combinations: glass-glass, glass-acrylic, glass-polycarbonate, and acrylic-polycarbonate.

StructureMaterialConnection TypesFeaturesApplications
Single-layerMonolithic acrylic or PC boardVarious rigid or flexible connectionsEasy to process and manufactureWindows for small/medium aircraft and helicopters; fighter canopies and windshields; bomber nose cones and observation windows
Double-layerTwo acrylic sheets with a rubber/plastic spacer; air or nitrogen-filled cavityClamping frame or plateFail-safe structure; excellent thermal and acoustic insulationPassenger windows and door windows for large/medium aircraft; some cockpit side windows
LaminatedMultiple layers of glass, acrylic, or PC bonded with transparent interlayers; may include heating elementsClamping frame (glass); clamping plate or bolts (plastic)Bird-strike resistance or bulletproof capabilityBird-strike resistant windshields and bulletproof glass for military/civil aircraft and some helicopters; some fighter canopies

Aviation-grade Polycarbonate (PC) sheet is extruded from specific Bisphenol A type PC resin and then calendered. Compared to acrylic, its primary advantage is superior impact resistance (falling-weight impact strength is 20 times that of oriented acrylic) and higher heat resistance (heat deflection temperature is ~30°C higher). However, it has poor abrasion resistance, is prone to stress cracking under solvent exposure, and is UV-sensitive, usually requiring a hard coating for protection. In aviation, it is rarely used alone but serves as the load-bearing structural layer in laminated transparent panels.

Requirements for Transparent Materials

Transparent components must possess excellent optical properties, sufficient structural strength, wear resistance, a long service life, high reliability, and ease of maintenance.

ItemRequirements
ShapeStreamlined to reduce drag; stealth aircraft require special shapes for low radar cross-section (RCS)
Field of ViewExcellent visibility and clarity; fighters require wide front and side views, as well as downward, upward, and rear visibility
Optical PropertiesHigh light transmittance, minimal haze; critical windows must meet strict optical distortion and angular deviation standards; thick parts must account for binocular parallax and ghosting
Load CapacityStatic: withstand aerodynamic and pressurization loads; Dynamic: meet fatigue life requirements; Concentrated: bird-strike resistance for front sections and bulletproof requirements for combat aircraft
Thermal ResistanceStandard: -55 to 60°C; supersonic aircraft must withstand kinetic heating above 95°C
EnvironmentalResistance to aging, humidity, heat, and salt spray
Flame RetardancyHorizontal burn rate not exceeding 64 mm/min
ProcessabilityEasy to thermoform and machine; decomposition temperature must be significantly higher than molding temperature
MaintainabilityEasy to repair with high component interchangeability

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Typical transparent components differed by plane type:

TypeName
Attack AircraftFront windshield (bulletproof), side windshield, movable canopy
BomberBombing sight window, cockpit central/main windshields, nose cone, navigation windows, observation covers, rear gunner windows (side/front-bulletproof)
Passenger AircraftCentral/main windshields, eyebrow windows (upper fixed), clear-view windows (movable), side fixed windows, entry door windows, passenger cabin windows
HelicopterGreen filter glass, windshields, lower-view glass, pilot door windows (upper/lower), sliding glass, front/rear cabin door glass

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Frode Hoo

Frode Hoo holds a Bachelor's degree in Mechanical Engineering from Sichuan University and has over 5 years of experience in product development and manufacturing. He creates technical content and lives in Dongguan, China.

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