Self-sealing fuel tank

In aviation, self-sealing fuel tank is a fuel tank technology in wide use since World War II that prevents fuel tanks primarily on aircraft from leaking fuel and igniting after being damaged by enemy fire.

Self-sealing tanks have two layers of rubber, one of vulcanized rubber and one of untreated rubber that can absorb oil and expand when wet. When a fuel tank is punctured, the fuel will spill on to the layers, causing the swelling of the untreated layer, thus sealing the puncture.

Most jet fighters and all US military rotary wing aircraft have some type of self-sealing tanks. Military rotary wing fuel tanks have the additional feature of being crashworthy. High altitudes require the tanks to be pressurized, making self-sealing difficult. Newer technologies have brought advances like inert foam-filled tanks to prevent detonation. This foam is an open cell foam that effectively divides the gas space above the remaining fuel into thousands of small spaces; none of which contain sufficient vapour to support combustion. This foam also serves to reduce fuel slosh. Major manufacturers of this technology include Amfuel (Zodiac) (formerly Firestone), Engineered Fabrics Corp. (Meggitt) (formerly Goodyear), GKN USA and FPT Industries. For military use, tanks are qualified to MIL-DTL-27422 and MIL-DTL-5578.

In additions to fighter aircraft some military patrol vehicles and armoured limousines for VIP use also feature self-sealing fuel tanks.

Wingtip device

Wingtip devices are usually intended to improve the efficiency of fixed-wing aircraft. There are several types of wingtip devices, and though they function in different manners, the intended effect is always to reduce the aircraft's drag by altering the airflow near the wingtips. Wingtip devices can also improve aircraft handling characteristics and enhance safety for following aircraft. Such devices increase the effective aspect ratio of a wing without materially increasing the wingspan. An extension of span would lower lift-induced drag, but would increase parasitic drag and would require boosting the strength and weight of the wing. At some point, there is no net benefit from further increased span. There may also be operational considerations that limit the allowable wingspan (e.g., available width at airport gates).

Wingtip devices increase the lift generated at the wingtip (by smoothing the airflow across the upper wing near the tip) and reduce the lift-induced drag caused by wingtip vortices, improving lift-to-drag ratio. This increases fuel efficiency in powered aircraft and increases cross-country speed in gliders, in both cases increasing range.

Winglets are employed on many aircraft types, such as:

• Rutan VariEze, the first aircraft to use winglets (1975)
• Learjet 28/29, the first production jet aircraft to use winglets (1977)
• Glaser-Dirks DG-303, an early glider derivative design, incorporating winglets as factory standard equipment
• Airbus A310-300, the first airliner to feature wingtip fences (1985)
• Boeing 747-400, the first mainline airliner to feature winglets (1988)
• Ilyushin Il-96, first Russian and modern jet to feature winglets (1988)
• Tupolev Tu-204, first narrow body aircraft to feature winglets (1994)