Aluminiumâlithium alloys (AlâLi 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 AlâLi alloys contain up to 2.45% lithium by mass. [1]
Alloying with lithium reduces structural mass by three effects:
The crystal structure for Al3Li and AlâLi, while based on the FCC crystal system, are very different. Al3Li shows almost the same-size lattice structure as pure aluminium, except that lithium atoms are present in the corners of the unit cell. The Al3Li structure is known as the AuCu3, L12, or Pm3m [5] and has a lattice parameter of 4.01 Ă . [3] The AlâLi structure is known as the NaTl, B32, or Fd3m [6] structure, which is made of both lithium and aluminium assuming diamond structures and has a lattice parameter of 6.37 Ă . The interatomic spacing for AlâLi (3.19 Ă ) is smaller than either pure lithium or aluminium. [7]
AlâLi alloys are primarily of interest to the aerospace industry for their weight advantage. On narrow-body airliners, Arconic (formerly Alcoa) claims up to 10% weight reduction compared to composites, leading to up to 20% better fuel efficiency, at a lower cost than titanium or composites. [8] Aluminiumâlithium alloys were first used in the wings and horizontal stabilizer of the North American A-5 Vigilante military aircraft. Other AlâLi alloys have been employed in the lower wing skins of the Airbus A380, the inner wing structure of the Airbus A350, the fuselage of the Bombardier CSeries [9] (where the alloys make up 24% of the fuselage), [10] the cargo floor of the Boeing 777X, [11] and the fan blades of the Pratt & Whitney PurePower geared turbofan aircraft engine. [12] They are also used in the fuel and oxidizer tanks in the SpaceX Falcon 9 launch vehicle, Formula One brake calipers, and the AgustaWestland EH101 helicopter. [13]
The third and final version of the US Space Shuttle's external tank was principally made of AlâLi 2195 alloy. [14] In addition, AlâLi alloys are also used in the Centaur Forward Adapter in the Atlas V rocket, [15] in the Orion Spacecraft, and were to be used in the planned Ares I and Ares V rockets (part of the cancelled Constellation program).
AlâLi alloys are generally joined by friction stir welding. Some AlâLi alloys, such as Weldalite 049, can be welded conventionally; however, this property comes at the price of density; Weldalite 049 has about the same density as 2024 aluminium and 5% higher elastic modulus.[ citation needed] AlâLi is also produced in rolls as wide as 220 inches (18 feet; 5.6 metres), which can reduce the number of joins. [16]
Although aluminiumâlithium alloys are generally superior to aluminiumâcopper or aluminiumâzinc alloys in ultimate strength-to-weight ratio, their poor fatigue strength under compression remains a problem, which is only partially solved as of 2016. [17] [13] Also, high costs (around 3 times or more than for conventional aluminium alloys), poor corrosion resistance, and strong anisotropy of mechanical properties of rolled aluminiumâlithium products has resulted in a paucity of applications.
Aside from its formal four-digit designation derived from its element composition, an aluminiumâlithium alloy is also associated with particular generations, based primarily on when it was first produced, but secondarily on its lithium content. The first generation lasted from the initial background research in the early 20th century to their first aircraft application in the middle 20th century. Consisting of alloys that were meant to replace the popular 2024 and 7075 alloys directly, the second generation of AlâLi had high lithium content of at least 2%; this characteristic produced a large reduction in density but resulted in some negative effects, particularly in fracture toughness. The third generation is the current generation of AlâLi product that is available, and it has gained wide acceptance by aircraft manufacturers, unlike the previous two generations. This generation has reduced lithium content to 0.75â1.8% to mitigate those negative characteristics while retaining some of the density reduction; [18] third-generation AlâLi densities range from 2.63 to 2.72 grams per cubic centimetre (0.095 to 0.098 pounds per cubic inch). [19]
Alloy name/number | Applications |
---|---|
1230 (VAD23) | Tu-144 |
1420 | MiG-29 fuselages, fuel tanks, and cockpits; Su-27; Tu-156, Tu-204, and Tu-334; Yak-36, and Yak-38 fuselages |
1421 | |
2020 | A-5 Vigilante wings and horizontal stabilizers |
Alloy name/number | Applications |
---|---|
1430 | |
1440 | |
1441 | Be-103 and Be-200 |
1450 | An-124 and An-225 |
1460 | McDonnell Douglas reusable launch vehicle ( DC-X); Tu-156 |
2090 (intended to replace 7075) | Airbus A330 and Airbus A340 leading edges; C-17 Globemaster; Atlas Centaur payload adapter [21] |
2091 (CP 274) [22] (intended to replace 2024) | Fokker 28 and Fokker 100 access doors in the fuselage lower fairing [23] |
8090 (CP 271) (intended to replace 2024) | EH-101 airframe; [9] Airbus A330 and Airbus A340 leading edges; Titan IV payload adapter |
Alloy name/number | Applications |
---|---|
2050 (AirWare I-Gauge) [9] [24] | Ares I crew launch vehicle â upper stage; A350 wing ribs; [24] A380 lower wing reinforcement [25] |
2055 [26] | |
2060 (C14U) | |
2065 [9] [19] | |
2076 | [19] |
2096 | |
2098 [27] [19] | |
2099 (C460) | A380 stringers, extruded crossbeams, longitudinal beams, and seat rails; [28] Boeing 787 [9] |
2195 | Ares I crew launch vehicle â upper stage; [9] Last revision of the Space Shuttle Super Lightweight External Tank [29] Falcon 9 propellant tanks [30] |
2196 | A380 extruded crossbeams, longitudinal beams, and seat rails [28] |
2198 (AirWare I-Form) | Fuselage skin of the A350 and CSeries; [24] Falcon 9 second-stage rocket [9] |
2199 (C47A) | |
2296 | [19] |
2297 | F-16 bulkheads [19] |
2397 | F-16 bulkheads; Space Shuttle Super Lightweight External Tank intertank thrust panels [19] |
AlâLi TPâ1 | |
C99N |
Key world producers of aluminiumâlithium alloy products are Arconic, Constellium, and Kamensk-Uralsky Metallurgical Works.
Aluminiumâlithium alloys (AlâLi 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 AlâLi alloys contain up to 2.45% lithium by mass. [1]
Alloying with lithium reduces structural mass by three effects:
The crystal structure for Al3Li and AlâLi, while based on the FCC crystal system, are very different. Al3Li shows almost the same-size lattice structure as pure aluminium, except that lithium atoms are present in the corners of the unit cell. The Al3Li structure is known as the AuCu3, L12, or Pm3m [5] and has a lattice parameter of 4.01 Ă . [3] The AlâLi structure is known as the NaTl, B32, or Fd3m [6] structure, which is made of both lithium and aluminium assuming diamond structures and has a lattice parameter of 6.37 Ă . The interatomic spacing for AlâLi (3.19 Ă ) is smaller than either pure lithium or aluminium. [7]
AlâLi alloys are primarily of interest to the aerospace industry for their weight advantage. On narrow-body airliners, Arconic (formerly Alcoa) claims up to 10% weight reduction compared to composites, leading to up to 20% better fuel efficiency, at a lower cost than titanium or composites. [8] Aluminiumâlithium alloys were first used in the wings and horizontal stabilizer of the North American A-5 Vigilante military aircraft. Other AlâLi alloys have been employed in the lower wing skins of the Airbus A380, the inner wing structure of the Airbus A350, the fuselage of the Bombardier CSeries [9] (where the alloys make up 24% of the fuselage), [10] the cargo floor of the Boeing 777X, [11] and the fan blades of the Pratt & Whitney PurePower geared turbofan aircraft engine. [12] They are also used in the fuel and oxidizer tanks in the SpaceX Falcon 9 launch vehicle, Formula One brake calipers, and the AgustaWestland EH101 helicopter. [13]
The third and final version of the US Space Shuttle's external tank was principally made of AlâLi 2195 alloy. [14] In addition, AlâLi alloys are also used in the Centaur Forward Adapter in the Atlas V rocket, [15] in the Orion Spacecraft, and were to be used in the planned Ares I and Ares V rockets (part of the cancelled Constellation program).
AlâLi alloys are generally joined by friction stir welding. Some AlâLi alloys, such as Weldalite 049, can be welded conventionally; however, this property comes at the price of density; Weldalite 049 has about the same density as 2024 aluminium and 5% higher elastic modulus.[ citation needed] AlâLi is also produced in rolls as wide as 220 inches (18 feet; 5.6 metres), which can reduce the number of joins. [16]
Although aluminiumâlithium alloys are generally superior to aluminiumâcopper or aluminiumâzinc alloys in ultimate strength-to-weight ratio, their poor fatigue strength under compression remains a problem, which is only partially solved as of 2016. [17] [13] Also, high costs (around 3 times or more than for conventional aluminium alloys), poor corrosion resistance, and strong anisotropy of mechanical properties of rolled aluminiumâlithium products has resulted in a paucity of applications.
Aside from its formal four-digit designation derived from its element composition, an aluminiumâlithium alloy is also associated with particular generations, based primarily on when it was first produced, but secondarily on its lithium content. The first generation lasted from the initial background research in the early 20th century to their first aircraft application in the middle 20th century. Consisting of alloys that were meant to replace the popular 2024 and 7075 alloys directly, the second generation of AlâLi had high lithium content of at least 2%; this characteristic produced a large reduction in density but resulted in some negative effects, particularly in fracture toughness. The third generation is the current generation of AlâLi product that is available, and it has gained wide acceptance by aircraft manufacturers, unlike the previous two generations. This generation has reduced lithium content to 0.75â1.8% to mitigate those negative characteristics while retaining some of the density reduction; [18] third-generation AlâLi densities range from 2.63 to 2.72 grams per cubic centimetre (0.095 to 0.098 pounds per cubic inch). [19]
Alloy name/number | Applications |
---|---|
1230 (VAD23) | Tu-144 |
1420 | MiG-29 fuselages, fuel tanks, and cockpits; Su-27; Tu-156, Tu-204, and Tu-334; Yak-36, and Yak-38 fuselages |
1421 | |
2020 | A-5 Vigilante wings and horizontal stabilizers |
Alloy name/number | Applications |
---|---|
1430 | |
1440 | |
1441 | Be-103 and Be-200 |
1450 | An-124 and An-225 |
1460 | McDonnell Douglas reusable launch vehicle ( DC-X); Tu-156 |
2090 (intended to replace 7075) | Airbus A330 and Airbus A340 leading edges; C-17 Globemaster; Atlas Centaur payload adapter [21] |
2091 (CP 274) [22] (intended to replace 2024) | Fokker 28 and Fokker 100 access doors in the fuselage lower fairing [23] |
8090 (CP 271) (intended to replace 2024) | EH-101 airframe; [9] Airbus A330 and Airbus A340 leading edges; Titan IV payload adapter |
Alloy name/number | Applications |
---|---|
2050 (AirWare I-Gauge) [9] [24] | Ares I crew launch vehicle â upper stage; A350 wing ribs; [24] A380 lower wing reinforcement [25] |
2055 [26] | |
2060 (C14U) | |
2065 [9] [19] | |
2076 | [19] |
2096 | |
2098 [27] [19] | |
2099 (C460) | A380 stringers, extruded crossbeams, longitudinal beams, and seat rails; [28] Boeing 787 [9] |
2195 | Ares I crew launch vehicle â upper stage; [9] Last revision of the Space Shuttle Super Lightweight External Tank [29] Falcon 9 propellant tanks [30] |
2196 | A380 extruded crossbeams, longitudinal beams, and seat rails [28] |
2198 (AirWare I-Form) | Fuselage skin of the A350 and CSeries; [24] Falcon 9 second-stage rocket [9] |
2199 (C47A) | |
2296 | [19] |
2297 | F-16 bulkheads [19] |
2397 | F-16 bulkheads; Space Shuttle Super Lightweight External Tank intertank thrust panels [19] |
AlâLi TPâ1 | |
C99N |
Key world producers of aluminiumâlithium alloy products are Arconic, Constellium, and Kamensk-Uralsky Metallurgical Works.