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2024 aluminium alloy is an aluminium alloy, ... T3 temper 2024 sheet has an ultimate tensile strength of 400–430 MPa (58–62 ksi) and yield strength of at least ...
These densities are smaller than the 2.78 g/cm 3 (0.100 lb/cu in) density of 2024-T3 aluminum alloy, [23] a common aluminum alloy in aircraft structures that is also incorporated into all but one of these Glare grades. (Glare1 uses the 7475-T761 alloy instead.)
The aircraft is made from 2024-T3 aluminum and 6061-T6 aluminum sheet. Its 8.41 m (27.6 ft) span wing has an area of 10.0 m 2 (108 sq ft) and is equipped with flaps . Standard engines available are the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant, with the 115 hp (86 kW) Rotax 914 , 141 hp (105 kW) Rotax 915 and 125 hp (93 kW) D-Motor ...
Aluminum 1100–O (annealed) 0.20: 180 2024 aluminum alloy (heat treated—T3) 0.16: 690 5052-O 0.13 210 Aluminum 6061–O (annealed) 0.20: 205 Aluminum 6061–T6: 0.05: 410 Aluminum 7075–O (annealed) 0.17: 400 Brass, Naval (annealed) 0.49: 895 Brass 70–30 (annealed) 0.49: 900 Brass 85–15 (cold-rolled) 0.34: 580 Cobalt-base alloy (heat ...
The aircraft's structure uses 2024-T3 aluminium for critical parts where extra strength is required, such as the spar, float and strut attachments as well as other critical components like the rudder horns. The R-80's structure is covered with 6061-T6 sheet of varying thicknesses; wing bottom skins are 0.016 in (0.41 mm) inches thick while the ...
Electrolytic protection, present under wet or moist conditions, is based on the appreciably higher electrode potential of commercial-purity aluminum compared to alloy 2017 or 2024 in the T3 or T4 temper. When 7075-T6 and other Al-Zn-Mg-Cu alloys appeared, an aluminum-zinc cladding alloy 7072 was developed to provide a relative electrode ...