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aluminum alloy 7075

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Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006737
EISBN: 978-1-62708-210-5
...Composition limits of aluminum alloy 7075 Table 1 Composition limits of aluminum alloy 7075 Element Composition, wt% Si 0.40 max Fe 0.50 max Cu 1.20–2.0 Mn 0.30 max Mg 2.1–2.9 Cr 0.18–0.28 Ti 0.20 max Zn 5.1–6.1 Other (each), max 0.05 Other (total...
Series: ASM Handbook
Volume: 12
Publisher: ASM International
Published: 01 January 1987
DOI: 10.31399/asm.hb.v12.a0000621
EISBN: 978-1-62708-181-8
... Fig. 1004 An aluminum alloy 7075-T736 aircraft main landing gear forging, similar to that described in Fig. 1002 and 1003 , which was shot peened on its inner-diameter surface to enhance fatigue resistance. The shot-peened part withstood cycles far beyond the number required for acceptance...
Series: ASM Handbook
Volume: 14A
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v14a.a0004034
EISBN: 978-1-62708-185-6
...° (+2, −1 or ±1°) Outside: 3° (+2, −1 or ±1°) (a) The suggested limits appear in publications issued by forging producers, forging users, and allied trade associations. (b) Primarily, heat treatable, high-strength aluminum alloys, such as 7075 and 7079. (c) Primarily, low-alloy, high...
Series: ASM Handbook
Volume: 13C
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v13c.a0004128
EISBN: 978-1-62708-184-9
... on the Structural Integrity of 7075-T6 Upper Wing Skins , Proc., 2003 U.S. Air Force ASIP Conference 37. Lyon S.P. , Thompson G.E. , and Johnson J.B. , Materials Evaluation Using Wet-Dry Mixed Salt Spray Tests , New Methods for Corrosion Testing of Aluminum Alloys , STP 1134, ASTM...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002406
EISBN: 978-1-62708-193-1
.... Figure 1 shows this effect in tests with 7075 aluminum alloy specimens over a range of thickness. In general, when the specimen thickness and the inplane dimensions near the crack are large enough relative to the size of the plastic zone, then the value of K at which growth begins is a constant...
Series: ASM Handbook
Volume: 14A
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v14a.a0004037
EISBN: 978-1-62708-185-6
...). The solid forging was designed with a bead at the parting line to enhance resistance to stress corrosion. The effects of beading on grain flow and end grain runout are shown in (d). See Example 2. Dimensions in figure given in inches Item Revised forging Material Aluminum alloy 7075...
Series: ASM Handbook
Volume: 13A
Publisher: ASM International
Published: 01 January 2003
DOI: 10.31399/asm.hb.v13a.a0003666
EISBN: 978-1-62708-182-5
... with samples of 7075 aluminum alloy that have been given different thermal treatments to decrease susceptibility to SCC. Analysis of these breaking stress data by extreme value statistics enables calculation of survival probabilities and the estimation of a threshold stress, without depending on failures...
Series: ASM Handbook
Volume: 14A
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v14a.a0004038
EISBN: 978-1-62708-185-6
... aluminum alloy hinge forging and (c) a corresponding section of a blocker-type finish forging. See Example 1 . Dimensions in figure given in inches Item Conventional forging Material Aluminum alloy 7075 (a) Plan area (approx) 335 cm 2 (52 in. 2 ) (a) Parting line Straight...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006549
EISBN: 978-1-62708-210-5
... with a sharp notch. Fig. 1 Comparison of fatigue strength bands for 2014-T6, 2024-T4, and 7075-T6 aluminum alloys for rotating-beam tests. Source: Ref 3 Fig. 2 Axial stress fatigue strength of 0.8 mm (0.032 in.) 2024, 7075, and clad sheet in air and seawater, R = 0. Source: Ref 4...
Series: ASM Handbook
Volume: 14A
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v14a.a0004039
EISBN: 978-1-62708-185-6
...-strength aluminum alloys, such as 7075 and 7079. (b) Series based on configurations suggesting both confined and unconfined webs. (c) Applies to unconfined webs. (d) Applies to confined webs. (e) Applies to C-channel (“bath-tub”) configuration. (f) Applies to H-channel configuration...
Series: ASM Handbook
Volume: 5
Publisher: ASM International
Published: 01 January 1994
DOI: 10.31399/asm.hb.v05.a0001275
EISBN: 978-1-62708-170-2
... the properties of the coating being sought. For example, in order to be used on military aircraft, aluminum alloy parts (such as those made from highly corrosive copper-containing aluminum alloy 2024-T3 or 7075-T6) must pass government specifications MIL-C-5541 and MIL-C-81706, which require that the unpainted...
Series: ASM Handbook
Volume: 12
Publisher: ASM International
Published: 01 January 1987
DOI: 10.31399/asm.hb.v12.a0001836
EISBN: 978-1-62708-181-8
... stereo pair. Both 4000× Fig. 13, 14 The first of two sets of views at increasing magnification showing four areas of the surface of a low-cycle fatigue test fractured in aluminum alloy 7075-T6 obtained with a maximum loading of 117 MPa (17 ksi) at 1900 cpm. Fracture occured at 600,000 cycles...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002371
EISBN: 978-1-62708-193-1
... residual surface stress and 10 7 cycles fatigue limit of various structural alloys for various finishing methods. (a) 4340 steel. (b) 17-4PH austenitic stainless steel, with double peaks of residual stress indicated with lines between data points. (c) Ti-6Al-4V. (d) 7075 aluminum alloy. Source: Ref 1...
Series: ASM Handbook
Volume: 22A
Publisher: ASM International
Published: 01 December 2009
DOI: 10.31399/asm.hb.v22a.a0005419
EISBN: 978-1-62708-196-2
... 04159, 1992 . 23. Newman J.C. Jr. , Brot A. , and Matias C. , Crack-Growth Calculations in 7075-T7315 Aluminum Alloy under Various Load Spectra Using an Improved Crack-Closure Model , Eng. Fract. Mech. , Vol 17 , 2004 , pp. 2347 – 2363 . 24. NASGRO Software described...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003125
EISBN: 978-1-62708-199-3
... of aluminum alloys Alloy Extrudability, % of rate for alloy 6063 1350 160 1060 135 1100 135 3003 120 6063 100 6061 60 2011 35 5086 25 2014 20 5083 20 2024 15 7075 9 7178 8 Standard manufacturing limits (in inches) for aluminum extrusions...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006545
EISBN: 978-1-62708-210-5
... Resistance of Aluminum Alloy 7075-T6 , Mater. Sci. Eng. A , Vol 103 , 1988 , p 223 – 231 10.1016/0025-5416(88)90512-5 36. Bobby-Kannan M. , Raja V.S. , Raman R. , and Mukhopadhyay A.K. , Influence of Multistep Aging on the Stress Corrosion Cracking Behavior of Aluminum Alloy...
Series: ASM Handbook
Volume: 14A
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v14a.a0004033
EISBN: 978-1-62708-185-6
... 7 0.06 2.4:1 0.75 unc nf 0.75 (b) 2.0 (b) 0.75 (b) 1:1 7 3.0 1.5:1 1.46 con md (a) Primarily heat treatable, high-strength aluminum alloys, such as 7075 and 7079. (b) Approximate. (c) Estimated. (d) Special tooling used in one rib location to achieve this thin...
Series: ASM Handbook
Volume: 13C
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v13c.a0004119
EISBN: 978-1-62708-184-9
... ). The Air Force has authorized the use of film tape type sealant to apply on spars, ribs, and decking structures. To address the problems of SCC and CF in primary structures, airframes, and skins, alloy substitution to replace corrosion-prone materials such as aluminum alloy 7075-T6 has been established...
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006260
EISBN: 978-1-62708-169-6
... and temperature of an interrupted quench on (a) yield strength of alloys 7075 and 7050 and (b) 99.5% maximum yield strength of 6351-T6 extrusion. Source: Ref 3 , 4 , 5 Fig. 4 Examples of isothermal C-curves in comparing quench sensitivity of various aluminum alloys. (a) 95% of maximum tensile stress...
Series: ASM Handbook
Volume: 2A
Publisher: ASM International
Published: 30 November 2018
DOI: 10.31399/asm.hb.v02a.a0006506
EISBN: 978-1-62708-207-5
... operations. It discusses the quenchants that are used in quenching aluminum alloys, namely, hot or cold water and polyalkylene glycol. The article also describes the racking practices for controlling distortion and the level of residual stresses induced during the quench. aluminum alloys distortion...