In engineering, aheat shieldis a component designed to protect an object or a human operator from being burnt or overheated by dissipating, reflecting, and/or absorbing heat. The term is most often used in reference toexhaust heat managementand to systems for dissipating frictional heat. Heat shields are used most commonly in automotive and aerospace.
Heat shields protect structures from extreme temperatures and thermal gradients by two primary mechanisms.Thermal insulationandradiative cooling,respectively isolate the underlying structure from high external surface temperatures, while emitting heat outwards throughthermal radiation.To achieve good functionality the three attributes required of a heat shield are lowthermal conductivity(highthermal resistance), highemissivity,and good thermal stability (refractoriness).[1]Porousceramicswith high emissivity coatings (HECs) are often employed to address these three characteristics, owing to the good thermal stability of ceramics, the thermal insulation of porous materials and the goodradiative coolingeffects offered by HECs.
Due to the large amounts of heat given off by internal combustion engines,[2]heat shields are used on most engines to protect components and bodywork from heat damage. As well as protection, effective heat shields can give a performance benefit by reducing engine bay temperatures, therefore reducing the temperature of the air entering the engine.[3]Heat shields vary widely in price, but most are easy to fit, usually by stainless steel clips, high temperature tape or specially designed metal cable ties. There are three main types of automotive heat shield:
An example of a steel heat shield on a BMW E series engineRigid heat shields have until recently commonly been made from solid steel,[4]but are now often made from aluminum. Some high-end rigid heat shields are made out of either aluminum, gold or composite, with most examples including a ceramic coating to provide athermal barrier,which improves heat insulation.
The flexible heat shield are normally made from thin aluminum or gold sheeting, most commonly sold either flat or in a roll. These heat shields are often bent by hand by the installer. High performance flexible heat shields sometimes include extras, such as ceramic insulation applied viaplasma spraying.Another common tactic in flexible heat shields is using exotic composite materials to improve thermal insulation and shave weight. These latest products are commonplace in top-end motorsports such asFormula 1.
An example of an aluminum heat shield on the Toyota Celica ST205Textile heat shields, (also known as heat wraps), are used to insulate various exhaust components by trapping the heat emitted by the exhaust inside the exhaust pipe, rather than allowing the immense heat from these components to radiate within the engine bay. These wraps are most common in motorcycle exhaust pipes.
Heat shields are often fitted by both amateur and professional personnel during the optimization phase ofengine tuning.Heat shields are also used to cool engine mount vents. When a vehicle is at higher speed there is enough ram air to cool the under the hood engine compartment, but when the vehicle is moving at lower speeds or climbing a gradient there is a need of insulating the engine heat to get transferred to other parts around it, e.g. Engine Mounts. With the help of proper thermal analysis and use of heat shields, the engine mount vents can be optimized for the best performances.[5]
Someaircraftat high speed, such as theConcordeandSR-71 Blackbird,must be designed considering similar, but lower, overheating to what occurs in spacecraft. In the case of the Concorde the aluminum nose can reach a maximum operating temperature of 127 °C (which is 180 °C higher than the ambient air outside which is below zero); the metallurgical consequences associated with the peak temperature were a significant factor in determining the maximum aircraft speed.
Recently new materials have been developed that could be superior toRCC.The prototypeSHARP(SlenderHypervelocityAerothermodynamicResearchProbe) is based onultra-high temperature ceramicssuch as zirconium diboride (ZrB2) and hafnium diboride (HfB2).[6]The thermal protection system based on these materials would allow to reach a speed ofMach number7 at sea level, Mach 11 at 35000 meters and significant improvements for vehicles designed forhypersonic speed.The materials used have thermal protection characteristics in a temperature range from 0 °C to + 2000 °C, with melting point at over 3500 °C. They are also structurally more resistant than RCC, so they do not require additional reinforcements, and are very efficient in re-irradiating the absorbed heat.NASAfunded (and subsequently discontinued) a research and development program in 2001 for testing this protection system through the University of Montana.[7][8]
Apollo 12capsule's ablative heat shield (after use) on display at theVirginia Air and Space CenterThermal soak aerodynamic heat shield used on the Space Shuttle
Spacecraftthat land on aplanetwith anatmosphere,such asEarth,Mars,andVenus,currently do so by entering the atmosphere at high speeds, depending onair resistancerather than rocket power to slow them down. A side effect of this method of atmospheric re-entry isaerodynamic heating,which can be highly destructive to the structure of an unprotected or faulty spacecraft.[10]An aerodynamic heat shield consists of a protective layer of special materials to dissipate the heat. Two basic types of aerodynamic heat shield have been used:
The SovietVostok 1,the first crewed spacecraft, used ablative heat shielding made from asbestos fabric in resin.[11]The succeeding Mercury and Gemini missions both used fiber glass in the resin, while the Apollo spacecraft using a quartz fiber reinforced resin.[12]The first use of a super-light ablator (SLA) for spacecraft purposes was for theViking Landersin 1976.[12]SLA would also be utilized for thePathfinder mission.[12]Phenolic impregnated carbon ablators (PICA) was used for the Stardust mission launched in 1999.[12]
Athermal soak heat shielduses an insulating material to absorb and radiate the heat away from the spacecraft structure. This type was used on theSpace Shuttle,with the intent for the shield to be reused with minimal refurbishment in between launches.[13]The heat shield on the space shuttle consisted ofceramic or composite tilesover most of the vehicle surface, withreinforced carbon-carbonmaterial on the highestheat loadpoints (the nose and wing leading edges).[14]This protected the orbiter when it reached a temperature of 1,648 degrees Celsius during reentry.[15]The Soviet spaceplane, known as theBuran,also used TPS tiles that are similar to the American Shuttles. With the Buran also using a ceramic tiles on the bottom of the orbiter, and carbon-carbon on the nose cone.[16]
Many problems arose with the tiles used on the Space Shuttle, while minor damage to the heat shield was somewhat commonplace. Major damage to the heat shield almost caused the destruction of Space shuttle Atlantis in 1988 and did cause the loss of Columbia in 2003.[17][18][19]
With possible inflatableheat shields,as developed by the US (Low Earth Orbit Flight Test Inflatable Decelerator - LOFTID)[20]and China,[21]single-use rockets like theSpace Launch Systemare considered to be retrofitted with such heat shields to salvage the expensive engines, possibly reducing the costs of launches significantly.[22]On November 10, 2022, LOFTID was launched using anAtlas Vrocket and, then, detached in order to reenter the atmosphere.[23]The outer layer of the heat shield consisted of a silicon carbide ceramic.[24]The recovered LOFTID had minimal damage.[23]
Passive cooled protectors are used to protect spaceships duringatmospheric entryto absorb heat peaks and subsequently radiate heat to the atmosphere. Early versions included a substantial amount of metals such astitanium,berylliumandcopper.This greatly increased the mass of the vehicle. Heat absorption and ablative systems became preferable.
In modern vehicles, passive cooling can be found asreinforced carbon–carbonmaterial instead of metal. This material constitutes the thermal protection system of the nose and the front edges of the Space Shuttle and was proposed for the vehicleX-33.Carbonis the most refractory material known with a sublimation temperature (forgraphite) of 3825 °C. These characteristics make it a material particularly suitable forpassive cooling,but with the disadvantage of being very expensive and fragile. Some spacecraft also use a heat shield (in the conventional automotive sense) to protect fuel tanks and equipment from the heat produced by a largerocket engine.Such shields were used on the ApolloService ModuleandLunar Moduledescent stage. TheParker Solar Probe,designed to enter the corona of the Sun, experiences a surface temperature of 2,500 °F.[25]To withstand this temperature without damage to its body or instruments, the spacecraft uses a heat shield using a carbon-carbon ceramic with a layer of carbon foam in between.[26]The probe was launched into space on August 18, 2018.[27]
Heat shields are often affixed tosemi-automaticorautomaticrifles and shotguns asbarrel shroudsin order to protect the user's hands from the heat caused by firing shots in rapid succession. They have also often been affixed to pump-action combat shotguns, allowing the soldier to grasp the barrel while using a bayonet.[citation needed]
Heat shields are used in metallurgical industry to protect structural steel of the building or other equipment from the high temperature of nearby liquid metal.[citation needed]
^Fahrenholtz, William G; Wuchina, Eric J; Lee, William E; Zhou, Yanchun, eds. (2014). "Ultra-High Temperature Ceramics: Materials for Extreme Environment Applications".doi:10.1002/9781118700853.ISBN9781118700853.
^Leinbach, Micheal D.; Ward, Jonathan H. (2020).Bringing Columbia Home: The Untold True Story of a Lost Space Shuttle and Her Crew.New York, NY: Arcade Publishing. pp. 229–234.ISBN9781948924610.
^Leinbach, Micheal D.; Ward, Jonathan H. (2020).Bringing Columbia Home: The Untold True Story of a Lost Space Shuttle and Her Crew.New York, NY: Arcade Publishing. pp. 229–234.ISBN9781948924610.
