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2 edition of Prototype development of an optimized, tapered-thickness, graphite/epoxy composite flywheel found in the catalog.

Prototype development of an optimized, tapered-thickness, graphite/epoxy composite flywheel

S. V. Kulkarni

Prototype development of an optimized, tapered-thickness, graphite/epoxy composite flywheel

by S. V. Kulkarni

  • 61 Want to read
  • 20 Currently reading

Published by Dept. of Energy, Lawrence Livermore Laboratory, for sale by the National Technical Information Service in Livermore, Calif, Springfield, Va .
Written in English

    Subjects:
  • Flywheels -- Design and construction,
  • Graphite,
  • Epoxy coatings

  • Edition Notes

    StatementS. V. Kulkarni, R. G. Stone, R. H. Toland
    SeriesUCRL ; 52623
    ContributionsStone, R. G. 1932- joint author, Toland, R. H., joint author, Lawrence Livermore Laboratory
    The Physical Object
    Paginationiii, 32 p. :
    Number of Pages32
    ID Numbers
    Open LibraryOL14885200M

    11 04 shear modulus, shear strength, Poisson's. ratio, composite 20 11 materials, graphite/epoxy composites. j "L T.) ABSTRACT (Continue on reverse if necessary and identify by block number)-'Off-axis tension tests were performed for coupon specimens of unidirectional graphite/ epoxy composites at various temperatures.   Stress is the amount of force on a sample divided by the cross sectional area and recorded in pounds per square inch (PSI).. Strain is the amount of stretch a material exhibits while a load is property is expressed as a percent of the original length. Toughness is a relationship between modulus, stress, and strain that corresponds to the amount of energy a specimen can absorb.

    However, when the graphite content is 35% in HDPE/graphite, the elongation at break and impact strength still remain % and J/m. respectively. Also, the yield strength increases with the increase of the graphite content, and reaches the maximum at 55% graphite content, and reduces afterwards.   Effective epoxy composite coating mechanical/fracture toughness properties improvement by incorporation of graphene oxide nano-platforms reduced by a green/biocompataible reductant. Journal of Industrial and Engineering Chemistry , 75, DOI: /

    The material studied in this investigation was a pultruded unidirectional graphite/epoxy composite, consisting of 36K tow Hercules AS2 graphite fiber and Shell Epon epoxy resin The composite panels measured cm long, 14 cm wide, and approximately mm thick. HIGH STRAIN RATE PROPERTIES OF ANGLE-PLY COMPOSITE LAMINATES ABSTRACT Angle-ply graphite/epoxy and graphite/S-glass/epoxy laminates were characterized in uniaxial tension at strain rates ranging from quasi-static to over s-l. Laminate ring specimens of [±s, [±s, [±s.


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Prototype development of an optimized, tapered-thickness, graphite/epoxy composite flywheel by S. V. Kulkarni Download PDF EPUB FB2

Get this from a library. Prototype development of an optimized, tapered-thickness, graphite/epoxy composite flywheel. [S V Kulkarni; R G Stone; R H Toland; Lawrence Livermore Laboratory.].

Prototype development of an optimized, tapered-thickness, graphite/epoxy composite flywheel Technical Report Kulkarni, S V ; Stone, R G ; Toland, R H The objective of the investigation is to design and test a prototype composite flywheel rotor and to.

The study of the curing kinetics of epoxy compositions, Fig. 8, showed the inhibitory effect of TEG on the processes of the structure formation of the epoxy composite Cited by: 3. Consider the notched T/ graphite/epoxy composite laminate plate shown in Figure (a).

Three such laminates were constructed and tested by Bogert et al. (): [0° 12], [45°/0°/−45°/0°/90°] s, and [45°/0° 2 /−45°/0° 2 /90°] s, with total thicknesses of, and in., respectively, and each with nominal v f = The progressive failure of these.

Abstract. Compression molded structural sheet molding compound (SMC) composed of S-2 Glass R and polyester resin has been used to fabricate energy storage flywheel rotors.

This technique has the potential of low cost, high throughput production of rotors for the automobile : John F. Kay. The Airbus A XWB is built of 52% CFRP including wing spars and fuselage components, overtaking the Boeing Dreamliner, for the aircraft with the highest weight ratio for CFRP, which is 50%.

This was one of the first commercial aircraft to have wing spars made from composites. The Airbus A was one of the first commercial airliners to have a central wing-box made of CFRP; it is the. tions. The use of graphite/epoxy parts reduced the satellite's weight by 25 lb.

[Ref. 2) Figure 5. Defense Satellite Communications System III There are many other examples from past current and future space projects which call for graphite/ epoxy composite structures.

Future planned com­ posite use include: 1. The second was the tuning of the interconnection weights of the prototype RNN to construct the soft sensor through one cure experiment with a commercial prepreg of the epoxy/graphite fiber composite.

Recurrent neural networks. Among various types of ANNs, RNNs have proved to be particularly effective in learning temporal patterns. Graphite Yarn Composite After 2-Hour Water Boil (Fiber Sample No. C) 6 VI Average Flexural Properties of 8-Ply Balanced Bidirectional Graphite Composites After 2 and 24 Hours' Water Boil (Fiber Sample No.

B) 6 ViI Inltial Epoxy Coated Graphite Yarn Handling Characteristics (Yarns Subjected to Mechanical Handling During Resin Coating) 7. Development in graphite, graphene, and graphene nanoplatelet composites with epoxy matrix is presented here.

Graphite and its modified forms propose exclusive properties to composites. Graphene has developed as subject of huge scientific attention due to excellent electron transport, mechanical properties, and high surface area.

A composite flywheel prototype was designed and manufactured from aluminum alloy, glass fiber, and carbon fiber reinforced plastics. and an optimized graphite/epoxy composite design.

Results are presented of the successful application of this model to predict creep of a unidirectional, continuous-carbon-fiber-reinforced polymer composite (AS4/) and its epoxy matrix, over. The ability to measure the thickness of paint on graphite/epoxy composite structures directly would be of benefit in the aerospace industry.

The weight reduction would increase fuel mileage for the airline customer. An additional reason for reducing the thickness of paint on graphite/epoxy composites is not as obvious as the weight savings. Graphite/epoxy composites have the potential to be used as conductive polymer composites (CPCs).

Nevertheles, graphite/epoxy composites have a low in-plane conductivity, so a large amount of conductive filler is needed to increase the in-plane conductivity.

However, other composite properties can be affected if the conductive filler content is too high. Epoxy resin held the graphite/epoxy beams and the concrete slabs in place. Composite action and effect of concrete strength on bond, stiffness, and strength were studied.

Results indicate that existing theories may be appropriate to predict the response of these beams. The use of epoxy resin as a bond was only partially effective. The Graphite-Epoxy Motor (GEM) is a series of solid rocket boosters fueled by HTPB and produced by Northrop Grumman Innovation Systems with a carbon-fiber-reinforced polymer casing.

GEM series boosters were previously used on the Delta II, Delta III, and Delta will fly on Atlas V, Vulcan, and the proposed OmegA. About Goodfellow. Goodfellow supplies metals, ceramics and other materials to meet the research, development and specialist production requirements of science and industry worldwide.

Source: Goodfellow. For more information on this source please visit Goodfellow. Graphite has a hardness rating of.5 on the mineral scale, where diamond is the top at Graphite powder won't add squat to epoxy strength- graphite fibers are another issue entirely, but what they add are flexural and compressive/tensile strength, not hardness or resistance to abrassion.

The thermal expansion behavior of unidirectional, balanced angle‐ply, and complex laminated graphite‐epoxy composites, is studied.

The expansion coefficient of the unidirectional composites is determined as a function of fiber orientation and is found to follow the simple equation. Manufacturer of graphite products, graphite composite structures, graphite/epoxy structures, & graphite gasket material.

Solid laminated panels available in carbon/epoxy construction. Standard panel sizes range from 12 in. x 18 in. to 38 in. x 50 in. Panels available in uniform thickness up to 2 in. Panels available in quasi-isotropic & bi. 17 Effects of Thermal Spiking on Graphite-Epoxy Composites ALFRED C.

LOOS AND GEORGE S. SPRINGER Department of Mechanical Engineering The University of Michigan Ann Arbor, Michigan (Received Novem ) ABSTRACT Tests were performed evaluating the effects of thermal spikes on the moisture absorption characteristics, the ultimate tensile strength, and the.().

Perspectives of Epoxy/Graphene Oxide Composite: Significant Features and Technical Applications. Polymer-Plastics Technology and Engineering: Vol.

55, No. 7. A custom formulated, heat-activated, toughened epoxy film adhesive is used to bond a carbon/epoxy composite structural stiffener to the inside of the BMW 7-Series steel B-pillar. “The adhesive cure can be as high as °C for a subminute cure time,” explains Didier Trau, project manager of advanced development at L&L’s Molsheim.