Abstract: A tubular object manufacturing method comprising the steps of applying liquid heat-resistant resin containing an inorganic filler as desired onto an outer surface or inner surface of a core member which is a shaping mold to thereby form a coating layer, solidifying or hardening the applied liquid heat-resistant resin until the coating layer becomes strong enough to maintain at least a structure of the tubular object, and taking the tubular object out from the core member. In the method, liquid heat-resistant resin with a viscosity of 10 to 15000 poise at 25.degree. C. is continuously fed by means of a dispenser onto the outer surface or inner surface of the core member while rotating the core member, and a feeder part of the dispenser is moved in the direction of a rotation axis of the core member so that the fed liquid heat-resistant resin is helically wound to thereby form the coating layer.

Abstract: Supporting clamps for a tool such as, for example, a pile driver machine are used to tilt a machine support relative to a horizontal plane. The clamps include a pair of jaw elements one of which is received on a pivot and the other of which has a pair of parallel spaced pistons. The clamp jaw elements gird a fixed reference device to support the tool securely for subsequent operations. Different pressures applied to the two pistons causes the clamp to tilt about the fixed reference device, and thereby to tilt the tool to which it is attached. The difference in pressure is controlled to rotate the tool as desired. In a second embodiment of the invention, the desired angle is established by controlling an angle of a backup surface, and applying equal pressure to the two pistons. The fixed reference device is driven into the angled backup surface to establish the desired tilt angle. In a further embodiment, one piston is disposed at each side of the gap. The two pistons are spaced apart along the gap.

Abstract: An electronic component mounting apparatus for determining whether or not a nozzle replacement operation is successfully performed. A horizontal array of nozzles are accommodated in the holder in a nozzle stocker, and a light emitting device and a light receiving device are arranged so that the light path between both runs above the nozzles. The nozzle stocker is arranged in a travel path of a feeding head. The nozzle mount of the feeding head returns a used nozzle into the holder or mounts a new nozzle thereon. When any nozzle remains lifted from the holder intercepting the light path, a returning operation of the used nozzle is determined to be a failure. When a nozzle replacement is performed, its success or failure is reliably determined by detecting a intercepting height of light and release height of light by the nozzle and nozzle mount, respectively.

Abstract: A porous material of a polytetrafluoroethylene (PTFE), which can retain at least 90% of 0.109 .mu.m latex spheres and has a flow rate (IPA flow rate) of at least 0.6 ml/cm.sup.2 /min as measured with isopropyl alcohol under a differential pressure of 1 kg/cm.sup.2. A process for the production of a porous material of PTFE, which comprises, after forming a molded article from fine powder of PTFE by paste extrusion, (1) sintering the molded article, (2) rolling up the molded article thus sintered and heat-treating it at a temperature lower than the melting point of the polytetrafluoroethylene in a state as rolled up, and then (3) stretching the molded article thus heat-treated in at least an uniaxial direction. The porous material of PTFE according to the present invention has micropores and good permeability and particularly is excellent in performance of retaining fine particles.

Abstract: An electronic component mounting apparatus for determining whether or not a nozzle replacement operation is successfully performed. A horizontal array of nozzles are accommodated in the holder in a nozzle stocker, and a light emitting device and a light receiving device are arranged so that the light path between both runs above the nozzles. The nozzle stocker is arranged in a travel path of a feeding head. The nozzle mount of the feeding head returns a used nozzle into the holder or mounts a new nozzle thereon. When any nozzle remains lifted from the holder intercepting the light path, a returning operation of the used nozzle is determined to be a failure. When a nozzle replacement is performed, its success or failure is reliably determined by detecting a intercepting height of light and release height of light by the nozzle and nozzle mount, respectively.

Abstract: This invention provides a reinforcing woven fabric using as weaving threads flat and substantially nontwisted multifilaments of reinforcing fiber having less than 0.5 wt. % of sizing agent provided thereto and a binding property of 400-800 mm in hook drop value, and a method and an apparatus for manufacturing a reinforcing woven fabric by weaving the multifilaments of reinforcing fiber as warps and wefts. A reinforcing woven fabric having a small thickness and an extremely high covering factor and capable of indicating a high strength can be obtained at a low cost as a substrate for reinforcing composite materials.

Abstract: A workpiece support for a vise which is used for clamping a small workpiece on the vise and which can solve the problem that the prior art workpiece support has not versatility in clamping workpieces of various different configurations. In the workpiece support, a magnet is detachably mounted in a support plate and the support plate is fixedly attracted to a jaw plate of the vise through the magnet. Therefore, by forming a step in one side of the support plate along an edge and mounting the magnet in the support plate in a reversible manner, any one surface of the workpiece support can be selected as an attraction surface and the workpiece support can be used in many various forms depending on the workpiece configurations.

Abstract: A method and apparatus for supplying twist free flat warp containing a plurality of carbon fibers to a plurality of wefts in a weaving loom, wherein the warp is transversely removed from a plurality of bobbins and twisted along a longitudinal travelling direction of the warps so that flat surfaces of individual flat warps are oriented at a right angle to an arranged direction. The plurality of flat warps are reeded to a desired density in relation to the arranged direction. The warps are then twisted along the longitudinal travelling direction so that the flat surfaces of the individual flat warps are oriented to the arranged direction.

Abstract: Disclosed is a process of producing a prepreg which is suited for preparing honeycomb sandwich panels, by which the formation of pores in the interlayer zones in the cured composite can be reduced. The prepreg comprises a resin composition including an epoxy resin, a curing agent and a solid rubber, and a woven fabric made of reinforcing fibers, the meshes of the woven fabric being crushed such that said prepreg has a cover factor K.sub.p of 97-99.9%. Also disclosed is a reinforcing fabric comprising warps and woofs which are multifilament yarns made of carbon fibers, the widths W (mm) and finenesses D (d:denier) of the warp and woof satisfying the equation of:W=k.multidot.(D/.rho.).sup.5/9(wherein k represents 3.5.times.10.sup.-2 -10.0.times.10.sup.-2 (mm.multidot.d.sup.-5/9) and .rho. represents specific gravity of said carbon fibers), the woven fabric having a cover factor K.sub.c of 90.0-99.8%.

Abstract: Disclosed is a prepreg which is suited for preparing honeycomb sandwich panels, by which the formation of pores in the interlayer zones in the cured composite can be reduced. The prepreg of the present invention comprises a resin composition including an epoxy resin, a curing agent and a solid rubber, and a woven fabric made of reinforcing fibers, the meshes of the woven fabric being crushed such that said prepreg has a cover factor K.sub.p of 97-99.9%. Also disclosed is a reinforcing fabric comprising warps and woofs which are multifilament yarns made of carbon fibers, the widths W (mm) and finenesses D (d:denier) of the warp and woof satisfying the equation of:W=k.multidot.(D/.rho.).sup.5/9(wherein k represents 3.5.times.10.sup.-2 -10.0.times.10.sup.-2 (mm.multidot.d.sup.-5/9) and .rho. represents specific gravity of said carbon fibers), the woven fabric having a cover factor K.sub.c of 90.0-99.8%.

Abstract: Method of making a reinforcing fabric comprising warps and woofs which are multifilament yarns made of carbon fibers. The widths W (mm) and finenesses D (d:denier) of the warps and woofs satisfy the equation:W=k.multidot.(D/.rho.).sup.5/9wherein k represents 3.5.times.10.sup.-2 to 10.0.times.10.sup.-2 (mm.multidot.d.sup.-5/9) and .rho. represents specific gravity of the carbon fibers. The woven fabric has a cover factor K.sub.c of 90.0 to 99.8%. The fabric is made by treating a precursor fabric with water jets.

Abstract: An escape device for aircrafts having a pair of gas bags and a slide member joined to the gas bags. The escape device provides a high resistance to radiation heat and reliable bonding between the sheet members. The sheet member forming the gas bags and the slide member includes a substrate of fabric and covering layers of thermosetting elastomer containing a flame retardant. The sheet members forming the gas bags are bonded together before the covering layer of one of the sheet members hardens completely. A protective layer is provided on the outer surface of the joint portion between the sheet members to reflect radiation heat.

Abstract: In an escape device for an aircraft having a pair of air bags formed of sheet members and a slide surface, the sheet members have a high tear strength and excellent flame retardancy. The sheet members forming the air bags are a rubber covered fabric having a substrate of fabric and covering layers of a thermosetting elastomer which contains a flame retardant. By using a flame retardant in the form of needle-like crystals having a high aspect ratio and a small crystal grain diameter, the flame retardant will not aggregate in the elastomer, but will be uniformly dispersed, so that the bond strength between the substrate and the covering layer is high.

Abstract: A method and apparatus for supplying twist free flat weft containing a plurality of carbon fibers to a plurality of warps in a rapier weaving loom wherein the weft is transversely removed from a bobbin by draw-off rollers and intermittently supplied to the rapier. An elastic force is applied to the length of weft accumulated between the rapier and the bobbin to take up any slack and obviate its twisting. By this technique a carbon fiber fabric is woven with flat wefts which ensure a high fabric strength since crimped yarns with non uniform densities are avoided as well as a non uniform fabric thickness caused by irregular yarn thicknesses.

Abstract: A method and apparatus is provided for manufacturing a carbon fiber woven fabric by opening and closing a warp sheet formed of carbon fiber warps and by injecting wefts made of carbon fibers by water-jet into the warp sheet when the warp sheet is open. The accumulation of fluffs generated by abrasion between the weft and various guides is reduced by interrupting dispersion of water injected from the nozzle onto the weft as the weft travels from a bobbin to the nozzle, by sucking fluffs from the weft, and/or by causing contact between the weft and fluffs on the surface of the nozzle by loosening the weft, thereby making it possible to conduct a high-speed continuous operation.

Abstract: A carbon fiber woven fabric which uses a flat carbon fiber yarn consisting of many carbon fibers as at least its warp or weft, its weaving method and weaving apparatus. The flat carbon fiber yarn is twist-free, the number of its carbon fibers being 6,000 to 36,000, the yarn size being 3,000 to 30,000 deniers, the yarn width being 4 to 16 mm, the yarn thickness being 0.07 to 0.6 mm, and the ratio of yarn width to yarn thickness being 20 to 150. In the carbon fiber woven fabric, the flat carbon fiber yarn has a yarn width of 4 to 16 mm, a yarn thickness of 0.07 to 0.6 mm, a ratio of yarn width to yarn thickness of 20 to 150, and a ratio of weaving yarn pitch to yarn width of 1.0 to 1.2, the thickness of the woven fabric being 0.1 to 0.6 mm, the weight of woven fabric being 90 to 500 g/m.sup.2, and the fiber density of woven fabric being 0.8 to 1.2 g/cm.sup.3. The woven fabric is woven by a weaving apparatus provided with at least a weft supply device or a warp supply device.

Abstract: Disclosed is a reinforcing fabric comprising warps and woofs which are multifilament yarns made of carbon fibers, the widths W (mm) and finenesses D (d:denier) of the warp and woof satisfying the equation of:W=k.multidot.(D/.rho.).sup.5/9(wherein k represents 3.5.times.10.sup.-2 - 10.0.times.10.sup.-2 (mm.multidot.d.sup.-5/9) and .rho. represents specific gravity of said carbon fibers), the woven fabric having a cover factor K.sub.c of 90.0-99.8%. The warps and woofs are twisted to not more than 5 turns/m.

Abstract: A carbon fiber woven fabric which uses a flat carbon fiber yarn consisting of many carbon fibers as at least its warp or weft, its weaving method and weaving apparatus. The flat carbon fiber yarn is twist-free, the number of its carbon fibers being 6,000 to 36,000, the yarn size being 3,000 to 30,000 deniers, the yarn width being 4 to 16 mm, the yarn thickness being 0.07 to 0.6 mm, and the ratio of yarn width to yarn thickness being 20 to 150. In the carbon fiber woven fabric, the flat carbon fiber yarn has a yarn width of 4 to 16 mm, a yarn thickness of 0.07 to 0.6 mm, a ratio of yarn width to yarn thickness of 20 to 150, and a ratio of weaving yarn pitch to yarn width of 1.0 to 1.2, the thickness of the woven fabric being 0.1 to 0.6 mm, the weight of woven fabric being 90 to 500 g/m.sup.2 and the fiber density of woven fabric being 0.8 to 1.2 g/cm.sup.3. The woven fabric is woven by a weaving apparatus provided with at least a weft supply device or a warp supply device.

Abstract: This invention relates to an automation system for nuclear power plants. This system comprises operation plan making means, supervisory control means, and control means for controlling controlled objects. The operation plan making means makes a new operation plan to restore a normal operating condition which existed before the plant condition deviated from the normal operation range. The supervisory control means outputs control commands according to an operation plan under abnormal condition when the plant operating condition deviates from the normal operation range. Furthermore, the supervisory control means outputs control commands according a new operation plan prepared by the operation plan making means after an operation according to an operation plan under abnormal condition has been finished. The control means for controlling controlled objects controls the controlled objects according to control commands output from the supervisory control means.

Abstract: The present invention provides a cordless thermal vaporizer of the liquid type wherein the body of the vaporizer has a heater for heating a wick for drawing up a chemical solution from a bottle, and a socket disposed under the heater and removably fittable in the form of a cap to the bottle for attachment thereto. The body is reduced in weight and thereby made attachable to an electric outlet with stability. The solution bottle can be attached directly to the socket of the body and is therefore easy to replace.