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wing ribs

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Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006741
EISBN: 978-1-62708-210-5
...Abstract Abstract The aluminum alloy 7099 is a Kaiser aluminum high-strength Al-Mg-Zn-Cu alloy with zirconium that offers a less quench-sensitive alloy for properties in thicker sections for airframe structures such as wing ribs, spars, and skins, as well as fuselage frames and floor beams...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003425
EISBN: 978-1-62708-195-5
... Fig. 12 Co-consolidated cockpit floor Fig. 13 Schematic for ultrasonic welder and multiunit weld machine. Source: Ref 30 , 31 Fig. 14 Schematic for resistance weld of rib to spar Fig. 15 Resistance welding wing substructure using copper foil and amorphous...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003477
EISBN: 978-1-62708-195-5
... resistance to corrosion. The A-6 wing was being designed and built by Boeing Military Airplane Company. The A-6 replacement program requires a wing structural box made of carbon- fiber-reinforced epoxy. Figure 18 shows the design configuration of laminate skin fastened to composite intermediate ribs...
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
... sponson attachment forging was originally forged with 7° draft (a); tilting made it possible to forge the high, thin rib above the trough without applied draft. See text for details. Dimensions given in inches. Fig. 16 Conventional forging for wing spar root fitting (a), designed with 5° draft...
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
.... 21 Conventional aluminum alloy forging for a wing front spar terminal fitting, with a dorsal rib that was preblocked as a web and then blocked and finished as a rib. Dimensions given in inches Fig. 22 Conventional aluminum alloy wing fold rib forgings of original and revised designs...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003455
EISBN: 978-1-62708-195-5
... was used only to carry in-plane loads. Metal fittings were used for all triaxially loaded components—the landing gear, engine mounts, control surface mounting brackets, wing-to-fuselage junction, and so on. Such a policy of avoiding triaxial or interlaminar loads on composite structures makes even more...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003457
EISBN: 978-1-62708-195-5
... Administration , May 1985 20. Harvill W.E. , Duhig J.J. , and Spencer B.R. , “Program for Establishing Long-Time Flight Service Performance of Composite Materials in Center Wing Structure of C-130 Aircraft. Phase II–Detailed Design,” NASA CR-112272, National Aeronautics and Space...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003411
EISBN: 978-1-62708-195-5
... Fig. 1 Contour skin lay-up using a gantry-type automated tape layer Fig. 2 Automated tape lay-up of a contour skin showing the integrated contour tooling Fig. 8 Contour tape lay-up on an F-22 wing skin Fig. 3 Tape head for an automated tape layer Fig. 4...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003368
EISBN: 978-1-62708-195-5
... Airbus A330-200 rudder nose ribs  sulfide Airbus A340 aileron ribs Airbus A340-500/600 fixed-wing leading-edge assemblies Airbus A340-500/600 inboard wing access panels Airbus A340-500/600 keel beam connecting angles Airbus A340-500/600 keel beam ribs Airbus A340-500/600 pylon...
Series: ASM Handbook
Volume: 14A
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v14a.a0004040
EISBN: 978-1-62708-185-6
... (a) Mechanical properties (b) Weight of forging 12.7 kg (28 lb) (c) Weight of finished part 10 kg (22 lb) (a) Plan area 600 cm 2 (93 in. 2 ) (d) Parting line Straight; along center plane of web Draft angle 1° (+1°, − 1 2 °) Minimum rib width 9 mm (0.35 in.) Maximum rib...
Book: Machining
Series: ASM Handbook
Volume: 16
Publisher: ASM International
Published: 01 January 1989
DOI: 10.31399/asm.hb.v16.a0002158
EISBN: 978-1-62708-188-7
..., and other operations that follow the traditional machining of this type of material. In one application, the abrasive WJM process significantly reduced tooling costs in the machining of irregularly shaped wing ribs made of carbon fiber. The flow rate and the pressure of the waterjet have different...
Book: Casting
Series: ASM Handbook
Volume: 15
Publisher: ASM International
Published: 01 December 2008
DOI: 10.31399/asm.hb.v15.a0009021
EISBN: 978-1-62708-187-0
... austenitic stainless steel. One section of the casting required two revisions in wall thickness to bring rejection rate to an acceptable level. Rejections were 50% with 0.060-in. wall, 25% with 0.075-in., and 5% with 0.090-in. Fig. 5 Eight stiffening ribs in this alloy steel green sand casting were...
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
...° (±2°) (a) Minimum and typical rib width (approx) 19 mm (0.75 in.) (a) Maximum rib height-to-width ratio (approx) 1:1 (a) Minimum and typical fillet radius (approx) 11.7 mm (0.46 in.) (a) Minimum and typical corner radius (approx) 9.7 mm (0.38 in.) (a) Minimum web thickness...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003125
EISBN: 978-1-62708-199-3
... sheet 5005, 5050, 5052 O, H32, H34, H36, H38 Commercial roofing and siding  Corrugated roofing and siding Sheet 3004, Alclad 3004 …  V-beam roofing and siding Sheet 3004, Alclad 3004 …  Ribbed roofing Sheet Alclad 3004 …  Ribbed siding Sheet 3004, Alclad 3004 … Duct sheet...
Book Chapter

Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006740
EISBN: 978-1-62708-210-5
... and moderate resistance to stress corrosion cracking in aerospace applications such as wing-box ribs and spars; fuselage primary structural elements such as frames, bulkheads, windshield surrounds; and structural components in landing-gear bays. Plate product has excellent flatness, consistency, and low...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002393
EISBN: 978-1-62708-193-1
... into two adjacent bays, creating the potential for a two-bay skin crack with a broken central stiffener. Figure 5(c) summarizes these damage scenarios. Figure 5(d) , another example of basic structure, shows potential cracking of a lower wing surface stiffener at fuel transfer holes or at rib...
Series: ASM Handbook
Volume: 2A
Publisher: ASM International
Published: 30 November 2018
DOI: 10.31399/asm.hb.v02a.a0006493
EISBN: 978-1-62708-207-5
..., taper (draft) angles, fillet and corner radii, rib heights, and rib and web thicknesses. Forgeability Advanced Alloys Types of Forgings Forging Equipment Forging Die Design Forged Part Design Processing of Forgings Processing of Precision Forgings Postforge Processing...
Series: ASM Handbook
Volume: 13C
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v13c.a0004127
EISBN: 978-1-62708-184-9
... Paint failure from usage and spills V RBR. Install patches if beyond negligible damage limit. BAS. Item replaced if damage is extensive Fuselage to wing fitting Stress-corrosion cracking Paint failure due to wing flex and moisture entrapment … RBR. Item replaced if damage is extensive...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003452
EISBN: 978-1-62708-195-5
... Aircraft Structure , Compos. Struct ., Vol 47 , 1999 , p 431 – 443 5. Baker A.A. , Chester R.J. , Davis M.J. , Roberts J.D. , and Retchford J.A. , Reinforcement of the F-111 Wing Pivot Fitting with a Boron/Epoxy Doubler System—Materials Engineering Aspects...
Book Chapter

Book: Casting
Series: ASM Handbook
Volume: 15
Publisher: ASM International
Published: 01 December 2008
DOI: 10.31399/asm.hb.v15.a0005299
EISBN: 978-1-62708-187-0