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Book Chapter
Aluminum in Aircraft and Space Applications
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 30 June 2023
DOI: 10.31399/asm.tb.atia.t59340245
EISBN: 978-1-62708-427-7
... Abstract This chapter describes aluminum applications in aircraft and space vehicles and the special alloys, tempers, and product forms required to meet the unique challenges of flight. It focuses on wrought alloys and products that comprise the bulk of aluminum aircraft structure. The chapter...
Abstract
This chapter describes aluminum applications in aircraft and space vehicles and the special alloys, tempers, and product forms required to meet the unique challenges of flight. It focuses on wrought alloys and products that comprise the bulk of aluminum aircraft structure. The chapter also provides a list of the aerospace alloys and their chemical compositions in common use as well as their application on aircraft.
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Constant-ductility (% elongation) contours in time-temperature space for th...
Available to PurchasePublished: 01 December 1989
Fig. 3.12. Constant-ductility (% elongation) contours in time-temperature space for three common steels. (a) ½Mo steel ( Ref 83 ). (b) 1Cr-½Mo steel ( Ref 84 ). (c) 1Cr-1Mo-¼V steel ( Ref 83 ).
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Full-scale demonstration model of the Space-Based Interceptor (SABIR) Fligh...
Available to PurchasePublished: 01 September 2011
Fig. 7.9 Full-scale demonstration model of the Space-Based Interceptor (SABIR) Flight Experiment Propulsion System
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Space frame of the Audi A2 in extruded sections, sheet and castings. Source...
Available to PurchasePublished: 01 December 2006
Fig. 2.29 Space frame of the Audi A2 in extruded sections, sheet and castings. Source: Audi
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Image
Miller’s indices for space lattices. (a) Designation of lattice planes. (b)...
Available to PurchasePublished: 01 December 2006
Fig. 4.62 Miller’s indices for space lattices. (a) Designation of lattice planes. (b) Examples of planes in the cubic lattice. (c) Examples of directions in the cubic lattice
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Formation of a hollow space (gas pocket) under the mandrel support leg at a...
Available to PurchasePublished: 01 December 2006
Fig. 5.29 Formation of a hollow space (gas pocket) under the mandrel support leg at a low extrusion ratio (a) and a dead metal zone at a higher extrusion ratio (b). On the left, flow lines; right, lines of equal strain rate [ Wel 95 ]
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(a) Three-dimensional visualization of structure composed of space-filling ...
Available to Purchase
in Introduction to Metallographic Technique
> Metallography of Steels: Interpretation of Structure and the Effects of Processing
Published: 01 August 2018
Fig. 3.3 (a) Three-dimensional visualization of structure composed of space-filling grains, using bubbles. The interior of each bubble would be a crystal (grain), and the bubble walls would be the grain boundaries. (b) Intergranular fracture. The fracture path follows the embrittled previous
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Fabrication sequence for space shuttle carbon-carbon parts. Carbon-carbon (...
Available to PurchasePublished: 01 November 2010
Fig. 21.12 Fabrication sequence for space shuttle carbon-carbon parts. Carbon-carbon (C-C)
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Coating sequence for space shuttle carbon-carbon parts. Carbon-carbon (C-C)...
Available to PurchasePublished: 01 November 2010
Fig. 21.13 Coating sequence for space shuttle carbon-carbon parts. Carbon-carbon (C-C), silicon carbide (SiC), tetraethylortho-silicate (TEOS)
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Image
Types of solid solution. An interstitial atom occupies a space between the ...
Available to Purchase
in Introduction to Solidification and Phase Diagrams[1]
> Titanium: Physical Metallurgy, Processing, and Applications
Published: 01 January 2015
Fig. 2.6 Types of solid solution. An interstitial atom occupies a space between the atoms of the crystal lattice. Substitutional atoms replace or substitute for an atom in the crystal structure.
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Optimized blank holder force variable in space and constant in time (predic...
Available to PurchasePublished: 01 August 2012
Fig. 3.10 Optimized blank holder force variable in space and constant in time (predicted by optimization for forming the liftgate part from aluminum alloy A6111-T4 of 1 mm, or 0.04 in., thickness). Source: Ref 3.19
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in Aerospace Applications—Example Fatigue Problems
> Fatigue and Durability of Metals at High Temperatures
Published: 01 July 2009
Fig. 10.1 The United States Space Shuttle sitting on the launch pad in Florida
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Comparison of fatigue regimes encountered in the Space Shuttle Main Engines...
Available to Purchase
in Aerospace Applications—Example Fatigue Problems
> Fatigue and Durability of Metals at High Temperatures
Published: 01 July 2009
Fig. 10.2 Comparison of fatigue regimes encountered in the Space Shuttle Main Engines (SSMEs) and that encountered in aeronautical gas turbine engines
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Cut-away view of the Space Shuttle Main Engine showing components and gas p...
Available to Purchase
in Aerospace Applications—Example Fatigue Problems
> Fatigue and Durability of Metals at High Temperatures
Published: 01 July 2009
Fig. 10.3 Cut-away view of the Space Shuttle Main Engine showing components and gas paths
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A transistor schematic showing a blocked LDD implant defect under the space...
Available to PurchasePublished: 01 November 2019
Figure 49 A transistor schematic showing a blocked LDD implant defect under the spacer. The spacer acts as a thick gate oxide over the p- substrate resulting in a degraded transistor with a significantly higher Vt and resistance.
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Hydrogen embrittlement failure of a 300 M steel space shuttle orbiter nose ...
Available to PurchasePublished: 01 January 2000
Fig. 64 Hydrogen embrittlement failure of a 300 M steel space shuttle orbiter nose landing gear steering collar pin. The pin was heat treated to a 1895-MPa (275 ksi) strength level. The part was plated with chromium and titanium-cadmium. (a) Pin showing location of failure (actual size). (b
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Published: 01 October 2012
Fig. 11.11 Space Shuttle orbiter isotherms for a typical trajectory. Source: Ref 11.6
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