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  • MECHANICAL ENGINEERING  (15)
  • MATERIALS, METALLIC  (3)
  • CHEMISTRY AND MATERIALS (GENERAL)  (2)
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  • 1
    Publication Date: 2006-10-26
    Description: Ceramic surface films for lubrication at temperatures to 2000 deg f
    Keywords: MATERIALS, METALLIC
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  • 2
    Publication Date: 2019-05-21
    Description: Friction, wear, and dynamic seal studies in liquid fluorine and liquid oxygen
    Keywords: MATERIALS, METALLIC
    Type: NASA-TN-D-2453
    Format: application/pdf
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  • 3
    Publication Date: 2019-05-29
    Description: Self-lubricating composite materials prepared by vacuum impregnating nickel-chromium alloy with barium fluoride-calcium fluoride eutectic composition
    Keywords: MATERIALS, METALLIC
    Type: NASA-TN-D-3484
    Format: application/pdf
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  • 4
    Publication Date: 2019-06-28
    Description: Processing-technology development of a multiphase, self-lubricating, plasma-spray powder resulted in greater uniformity and reproducibility of plasma-sprayed coats. The effect of particle-size variation, binder concentration, and reproducible processing parameters are reported. Greater adhesive strengths of coats to substrates were achieved by particle-size variation, use of an intermediate bond coat such as Ni-Cr, or heat treatment. Quantitative analyses of polished, coated specimens are also given.
    Keywords: CHEMISTRY AND MATERIALS (GENERAL)
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  • 5
    Publication Date: 2019-06-27
    Description: Oscillating, plain spherical bearings with graphite-fiber-reinforced polyimide (GFRPI) liners were tested for friction and wear from 25 to 315 C. A condensation polymer was compared with an addition polymer, and a high-modulus fiber was compared with a lower cost, low-modulus fiber. All polymer-fiber combinations gave friction coefficients from 0.05 to 0.18 and low wear. Adding CdO and CdI2 reduced the wear of degassed bearings in dry air. These additives were not needed when the bearing liners contained adsorbed moisture. Although, at 25 C, MoS2 reduced the friction and wear of the base composite at unit loads above 70,000,000 N/m squared (10,000 psi), it had no beneficial effect at lighter loads.
    Keywords: MECHANICAL ENGINEERING
    Type: NASA-TP-1229 , E-9296
    Format: application/pdf
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  • 6
    Publication Date: 2019-06-27
    Description: A plasma-sprayed coating is described with good lubricating properties over a wide temperature range. The coating, designated NASA LUBE PS101, contains silver, nichrome, calcium fluoride, and an oxidation protective glass. Oscillating tests were conducted of self-aligning, plain cylindrical bearings, in which the bore was lined with 0.025 cm (0.010 in.) thick coatings of PS101; these were conducted at a radial load of 3.5 x 10 to the 7th power N/sq m (5000 psi) in nitrogen gas at -107 C (-160 F), in vacuum at room temperature, and in air from room temperature to 870 C (1600 F). Friction coefficients were less than 0.25 in all cases and wear rates were low. The coating is not brittle, and it has adequate oxidation resistance in air to at least 870 C.
    Keywords: MECHANICAL ENGINEERING
    Type: NASA-TM-X-71798 , E-8476
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  • 7
    Publication Date: 2019-06-28
    Description: The lubricating effectiveness of solid-lubricant dispersions are investigated in both point and line contacts using surfaces with both random and directional roughness characteristics. Friction and wear data obtained at relatively low speeds and at room temperature, indicate that the existence of solid lubricants such as graphite, MoS2, and PTFE in a plain mineral oil generally will not improve the effectiveness of the oil as a lubricant for such surfaces. Under boundary lubrication conditions, the friction force, as a function of time, initially depends upon the directional roughness properties of the contacting surfaces irrespective of whether the base oil or dispersions are used as lubricants.
    Keywords: MECHANICAL ENGINEERING
    Type: ASLE PREPRINT 83-LC-4C-1
    Format: text
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  • 8
    Publication Date: 2019-07-13
    Description: (Previously announced in STAR as N82-17263)
    Keywords: MECHANICAL ENGINEERING
    Type: ASLE PREPRINT 82-AM-1A-1 , Annual Meeting; May 10, 1982 - May 13, 1982; Cincinnati, OH
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  • 9
    Publication Date: 2019-07-13
    Description: A plain spherical bearing design with a ball diameter of 28.6 mm, a race length of 12.7 mm, and a 1.7-mm-thick, molded composite liner was evaluated. The liner material is a self-lubricating composite of graphite-fiber-reinforced polyimide resin (GFRPI). The liner is prepared by transfer molding a mixture of one part chopped graphite fiber and one part partially polymerized resin into the space between the bearing ball and the outer race and then completing the polymerization under heat and pressure. Several liner compositions were evaluated: two types of polyimide, condensation and addition; two types of graphite fiber, low and high modulus; and four powder additives - cadmium oxide, cadmium iodide, graphite fluoride, and molybdenum disulfide. The bearings were oscillated + or - 15 deg at 1 Hz for 20 kilocycles under a radial unit load of 29 MN sq m (4200 psi) in dry air at 25, 200, or 315 C. Both types of fiber and polyimide gave low friction and wear. A simple equation was developed to fit the wear-time data and adequately predicted wear to 100 kilocycles.
    Keywords: MECHANICAL ENGINEERING
    Type: NASA-TM-78908 , E-9296 , Intern. Conf. on Solid Lubrication; Aug 14, 1978 - Aug 18, 1978; Denver
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  • 10
    Publication Date: 2019-07-13
    Description: Plain spherical bearings with molded liners of self-lubricating graphite fiber-polyimide composite were developed and their dynamic load capacities were determined. Liners were prepared by transfer molding a prepolymer resin-fiber mix into the space between the ball and outer race, the completing polymerization under heat and pressure. Bearing dynamic load capacities were in excess of 140 MPa (20,000 psi) from room temperature to 260 C and about 70 MPa (10,000 psi) at 320 C. Friction coefficients were about 0.20 at room temperatures and light loads and tended to decrease with increasing temperatures and loads to about 0.15. Thermal expansion of the liner at uniform bearing temperatures of 200 C or higher produced a bearing preload which could be alleviated by providing an initial internal diametral clearance of 0.05 to 0.10 mm.
    Keywords: MECHANICAL ENGINEERING
    Type: NASA-TM-78935 , E-9678 , Joint Lubrication Conf.; Oct 24, 1978 - Oct 26, 1978; Minneapolis
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