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Aerospace structures

Recently ultrasonic spectroscopy has become a more common NDE technique and specialized instruments are commercially available now for inspection of aerospace structures, ball bearings, and even concrete [2],[3]. [Pg.105]

The performance of the classifier has been verified using a number of practical applications, such as civil engineering [3], inspection of aerospace composite structures, ball bearings and aircraft multi-layer structures. Here we present shortly some results, focusing on detection of disbonds in adhesively joint multi-layer aerospace structures using Fokker Bond Tester resonance instrument, details can be found in [1]. [Pg.107]

It also has lubricating properties similar to graphite. The hydrides are easily oxidized with considerable energy liberation, and have been studied for use as rocket fuels. Demand is increasing for boron filaments, a high-strength, lightweight material chiefly employed for advanced aerospace structures. [Pg.14]

Aerospace industry Aerospace structures Aerotex Antistatic D... [Pg.20]

Johnson, G.R., Recent Developments and Analyses Associated with the EPIC-2 and EPIC-3 Codes, in 1981 Advances in Aerospace Structures and Materials— AD-01 (edited by Wang, S.S. and Renton, W.J.), the American Society of Mechanical Engineers, New York, 1981, pp. 141-147. [Pg.370]

There are two important titanium aluminides Tig A1 which has a hexagonal structure with a density of 4.20 g/cm and a melting point of 1600°C and Ti A1 which has a tetragonal structure with a density of 3.91 g/cm and a melting point of 1445°C. As do all aluminides, they have excellent high temperature oxidation resistance owing to the formation of a thin alumina layer on the surface. They have potential applications in aerospace structures. [Pg.176]

Kevlar fibers are supplied by DuPont as Kevlar-29 and 49. The former is characterized by high tensile strength and the latter by high initial modulus(4). Some Kevlar-29 end uses are in ropes and cables, which are as strong as steel at one-fifth the weight, and in ballistic vests. Some Kevlar-49 end uses are in reinforcing resins and composites for aerospace structures, boat hulls, and sport equipments. [Pg.326]

Carbon, Carbides, and Nitrides. Carbon (graphite) is a good thermal and electrical conductor. It is not easily wetted by chemical action, which is an important consideration for corrosion resistance. As an important structural material at high temperature, pyrolytic graphite has shown a strength of 280 MPa (40,600 psi). It tends to oxidize at high temperatures, but can be used up to 2760°C for short periods in neutral or reducing conditions. The use of new composite materials made of carbon fibers is expected, especially in the field of aerospace structure. When heated under... [Pg.26]

In mathematical system theory, the subject of model reduction has been studied for about 30 years. The focus is on model reduction of linear systems, in particular methods based on singular value decomposition. One of the best known of these methods is balanced truncation. It is used extensively for various engineering purposes, such as electronic chip design and the reduction of models of aerospace structures. This method does not require the type of a priori information about the system mentioned above. Only recently has it been tried out on biochemical systems [105, 106]. [Pg.410]

One of the most popular uses of radiant curing is the advancement (viscosity increase) or crosslinking of pressure-sensitive adhesives. These applications have been satisfied mostly with acrylate-based adhesive systems. With epoxy-based adhesives, the main applications are electrical and electronic components, the bonding of large aerospace structures such as composites, and the bonding of transparent substrates such as glass and plastic. [Pg.256]

Cationic cured epoxies may also be crosslinked by electron beam radiation. A major application for this technology is the repair of composite aerospace structures. Direct benefits of EB processing include rapid cure, allowing completion of a permanent repair in the same or less time than a traditionally temporary repair, and ease of material handling. Other... [Pg.264]

Wise [2] prepared selected polyimides, (I), that formed dispersions of carbon nanotubes exhibiting long-term stability. Nanocomposites produced from these dispersions were useful in the fabrication of lightweight aerospace structures. [Pg.355]

Epoxy structural adhesives are used in an extraordinarily wide range of applications. They are available in essentially all of the forms discussed above, except for primer—liquid combinations or as room temperature curing liquids. The liighest technology7 application for epoxies is in aerospace structural... [Pg.232]

Soovere, J. Drake, M. L. Aerospace Structures Technology Damping Design Guide Flight Dynamics Laboratory Wright-Patterson Air Force Base, Ohio,... [Pg.344]

Jones, D.I.G., J.P. Henderson, and 1/Lt. G.H. Bruns, "Use of Tuned Viscoelastic Dampers for Reduction of Vibrations in Aerospace Structures," Air Force Materials Laboratory, presented at the 13th Annual Air Force Science and Engineering Symposium at Arnold Air Force Station, Tennessee, September 27-29, 1966. [Pg.354]

Major polymer applications microwave cookware, fiber optic connectors, capsules for electronic devices, watches, cameras, audiovisual equipment, under-bonnet automotive components, aerospace structures... [Pg.623]

Keywords. Cyanate ester, Polycyanurates, Phenolic-triazine, Polymer matrix composite, Cure kinetics, Polymer blends, Cyanate-epoxy blend, Bismaleimide-triazine resins, Aerospace structure... [Pg.1]

Reports on the use of cyanate ester resins in aerospace structures and related applications are scanty. Practically all the literature pertaining to their trials for potential aerospace applications are in the form of patents. All indications are... [Pg.9]

Figure 1. Specific ultimate tensile strength vs. specific stiffness of current and developmental aerospace structural materials. Data are displayed on a log-log plot in (a), where P signifies PAN-based reinforcements Gr represents graphite fibers 0 0 and 90 0 indicate data collected parallel to and transverse to the fiber direction in uniaxial composites, respectively and Q/I represents quasi-isotropic laminates. The (f represents fiber reinforcements in MMCs. The dashed line in (b) represents the combinations of specific strength and stiffness that are double those of conventional metal alloys. Figure 1. Specific ultimate tensile strength vs. specific stiffness of current and developmental aerospace structural materials. Data are displayed on a log-log plot in (a), where P signifies PAN-based reinforcements Gr represents graphite fibers 0 0 and 90 0 indicate data collected parallel to and transverse to the fiber direction in uniaxial composites, respectively and Q/I represents quasi-isotropic laminates. The (f represents fiber reinforcements in MMCs. The dashed line in (b) represents the combinations of specific strength and stiffness that are double those of conventional metal alloys.
Thermosets are often used in intimate contact with materials of much lower coefficient of linear thermal expansion p. A thermoset film may be coated on a surface, or sandwiched between two surfaces as an adhesive. A thermoset matrix may be filled with high-modulus fibers in aerospace structural materials and in other composite materials. A residual stress other material(s) to changes in temperature. The value of or typically reflects the balance between the driving force to produce residual stresses due to differential shrinkage upon cooling and the temperature-dependent capacity to relax these stresses. The worst such effects... [Pg.478]

Fiberite. (IQ Fiberite] Phenolic, epoxy, polyester, or polyimide resins to structural aiic exteitos, aircraft interiors, sandwich panels, aerospace structures, spiting goods. [Pg.144]

USE Source of neutrons when bombarded with alpha particles according to the equation jBe + JHe J C + jn This yields about 30 neutrons per million alpha particles. Also as neutron reflector and neutron moderator in nuclear reactors. In beryllium copper and beryllium aluminum alloys (by direct reduction of beryllium oxide with carbon in the presence of Cu nr Al). In radio tube parts. In aerospace structures. In inertial guidance systems. [Pg.182]


See other pages where Aerospace structures is mentioned: [Pg.105]    [Pg.977]    [Pg.401]    [Pg.426]    [Pg.244]    [Pg.1283]    [Pg.197]    [Pg.330]    [Pg.150]    [Pg.1594]    [Pg.432]    [Pg.101]    [Pg.483]    [Pg.234]    [Pg.358]    [Pg.162]    [Pg.441]    [Pg.85]    [Pg.87]    [Pg.14]    [Pg.174]    [Pg.234]    [Pg.559]   
See also in sourсe #XX -- [ Pg.13 ]

See also in sourсe #XX -- [ Pg.2 ]




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Aerospace

Aerospace A Pioneer in Structural Adhesive Bonding

Aerospace structural applications, thermoset

Aerospace structural applications, thermoset resins

Aerospace structures adhesives

Aerospace structures adhesives chemistries

Aerospace structures adhesives commercial

Aerospace structures adhesives cure temperatures

Aerospace structures adhesives curing

Aerospace structures adhesives formats

Aerospace structures adhesives formulations

Aerospace structures adhesives manufacture

Aerospace structures adhesives mechanisms

Aerospace structures adhesives primers

Composite materials aerospace structures

Fiber-metal laminates, aerospace structural

Foreword to Chapter 5 Aerospace, Pioneer in Structural Bonding

Laminate aerospace structures

Modeling the stiffness and strength of aerospace structural elements

Redux adhesives aerospace structures

Repair of damaged aerospace composite structures

Structural adhesive aerospace

Structural health monitoring (SHM) of aerospace composites

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