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  • 1
    Electronic Resource
    Electronic Resource
    Springer
    Archives of microbiology 102 (1975), S. 85-90 
    ISSN: 1432-072X
    Keywords: Intracytoplasmic Membranes ; Membrane Induction ; Hydrocarbon Oxidation ; Acinetobacter Species
    Source: Springer Online Journal Archives 1860-2000
    Topics: Biology
    Notes: Abstract 1. The induction of intracytoplasmic membranes was demonstrated to occur in Acinetobacter sp. when grown on hexadecane, heptadecane, and hexadec-1-ene. 2. Evidence for a physical relationship between the cytoplasmic hydrocarbon “pools” and the intracytoplasmic membranes is presented. 3. The specificity of the cytoplasmic pooling of hydrocarbons and the induction of intracytoplasmic membranes was investigated in relationship to hydrocarbon oxidation. 4. These results suggest that both processes are required for the growth of Acinetobacter sp. on hydrocarbons.
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 2019-06-28
    Description: Rapidly solidified alloys, based upon the Al-Fe-V-Si system and designed for elevated temperature applications, were evaluated for superplasticity and diffusion bonding behavior. Alloys with 8, 16, 27, and 36 volume percent silicide dispersoids were produced; dispersoid condition was varied by rolling at 300, 400, and 500 C (572, 752, and 932 F). Superplastic behavior was evaluated at strain rates from 1 x 10(exp -6)/s to 8.5/s at elevated temperatures. The results indicate that there was a significant increase in elongation at higher strain rates and at temperatures above 600 C (1112 F). However, the exposure of the alloys to temperatures greater than 600 C (1112 F) resulted in the coarsening of the strengthening dispersoid and the degradation of mechanical properties. Diffusion bonding was possible using low gas pressure at temperatures greater than 600 C (1112 F) which also resulted in degraded properties. The bonding of Al-Fe-V-Si alloys to 7475 aluminum alloy was performed at 516 C (960 F) without significant degradation in microstructure. Bond strengths equal to 90 percent that of the base metal shear strength were achieved. The mechanical properties and microstructural characteristics of the alloys were investigated.
    Keywords: METALLIC MATERIALS
    Type: NASA-CR-181849 , NAS 1.26:181849
    Format: application/pdf
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  • 3
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2019-07-13
    Description: A test program was carried out to evaluate several new high-temperature friction materials for use in aircraft disk brakes. A specially built test apparatus utilizing a disk brake and wheel half from a small jet aircraft was used. The apparatus enabled control of brake pressure, velocity and braking time. Tests were run under both constant and variable velocity conditions and covered a kinetic energy range similar to that encountered in aircraft brake service. The materials evaluation showed that two newly developed friction materials show potential for use in aircraft disk brakes. One of the materials is a nickel-based sintered composite, while the other is a molybdenum-based material. Both materials show much lower wear rates than conventional copper-based materials and are better able to withstand the high temperatures encountered during braking. Additional materials improvement is necessary, however, since both materials show a significant negative slope of the friction-velocity curve at low velocities.
    Keywords: METALLIC MATERIALS
    Type: ASLE PREPRINT 77-LC-6B-2 , Joint Lubrication Conference; Oct 03, 1977 - Oct 05, 1977; Kansas City, MO; US
    Format: text
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  • 4
    Publication Date: 2019-07-13
    Description: The influence of temper condition on the tensile and compressive stress-strain behavior for six boron-aluminum laminates was investigated. In addition to monotonic tension and compression tests, tension-tension, compression-compression, and tension--compression tests were conducted to study the effects of cyclic loading. Tensile strength results are a function of the laminate configuration; unidirectional laminates were affected considerably more than other laminates with some strength values increasing and others decreasing.
    Keywords: METALLIC MATERIALS
    Type: NASA-TM-X-74753 , VPI-E-77-18 , TR-8
    Format: application/pdf
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  • 5
    Publication Date: 2019-07-13
    Description: The feasibility of applying conventional hot forming and welding methods to high temperature aluminum alloy, Al-8Fe-1V-2Si (FVS812), for structural applications and the effect of thermal exposure on mechanical properties were determined. FVS812 (AA8009) sheet exhibited good hot forming and resistance welding characteristics. It was brake formed to 90 deg bends (0.5T bend radius) at temperatures greater than or equal to 390 C (730 F), indicating the feasibility of fabricating basic shapes, such as angles and zees. Hot forming of simple contoured-flanged parts was demonstrated. Resistance spot welds with good static and fatigue strength at room and elevated temperatures were readily produced. Extended vacuum degassing during billet fabrication reduced porosity in fusion and resistance welds. However, electron beam welding was not possible because of extreme degassing during welding, and gas-tungsten-arc welds were not acceptable because of severely degraded mechanical properties. The FVS812 alloy exhibited excellent high temperature strength stability after thermal exposures up to 315 C (600 F) for 1000 h. Extended billet degassing appeared to generally improve tensile ductility, fatigue strength, and notch toughness. But the effects of billet degassing and thermal exposure on properties need to be further clarified. The manufacture of zee-stiffened, riveted, and resistance-spot-welded compression panels was demonstrated.
    Keywords: METALLIC MATERIALS
    Type: NASA-CR-187575 , NAS 1.26:187575 , RE-787
    Format: application/pdf
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  • 6
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2019-07-13
    Description: A pendulum-type test device has been built for use in studying rubs between a turbine or compressor blade tip or labyrinth seal knife edge and specimens of abradable gas path seal materials. The device allows measurement of the rub energy dissipated in a single wear event, along with friction and normal forces and wear. Subsequent rubs over the same surface can also be monitored, with microscopic observation of the rub surface being possible after any of the passes. The device was used in tests of several potential abradable materials, ranging from porous to fully dense. It was shown that the rub energy dissipated in initial and subsequent passes is a fundamental parameter in the evaluation of material abradability. Rub energy was found to be influenced by such factors as: density and tensile (or yield) strength of the abradable material, prior densification or work hardening of the rub surface, and the sharpness of the leading edge of the blade tip.
    Keywords: METALLIC MATERIALS
    Type: ASLE PREPRINT 81-AM-1D-1 , Annual Meeting; May 11, 1981 - May 14, 1981; Pittsburgh, PA
    Format: text
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