An apparatus for manufacturing a container that includes a side wall (5) in the form of a tube and a base (7) at one end of the tube. The apparatus includes a tube forming unit (15) for progressively folding a length of a sheet (19) of a side wall material into an elongate tube shape (21) having a forward end (23) for receiving a base (7) of the container and welding together lengthwise extending sides of the sheet to form the tube. The apparatus also includes a base attachment unit (17) for positioning a base of the container on the forward end of the tube.

Methods of detecting and reducing error of athletic sensor readouts are disclosed. Methods relate to receiving properties, such as an athlete's body mass index and a physiological property, such as heart rate. Based on a body mass index or other parameter being outside a range, selecting a protocol, such as a heart rate measurement protocol. In further embodiments, a heart rate measurement protocol may be augmented.

A manufacturing method and an apparatus enable high productivity. A method for manufacturing an oxidized fiber bundle includes joining an upstream precursor fiber bundle and a downstream precursor fiber bundle together with a joining fiber bundle, and oxidizing the joined precursor fiber bundles by feeding the joined precursor fiber bundles through an oxidization furnace. The joining includes applying an oiling agent to a joint area of a joining target precursor fiber bundle before joining the joining target precursor fiber bundle and the joining fiber bundle together. A quantity of the oiling agent adhering to the joint area is 0.15 to 0.85 wt %.

The present invention relates to a band-like joint tape for covering a butting portion formed by butting an end portion of a one packing film to an end portion of another packing film and connecting the respective end portions of these packing films to each other. The joint tape is comprised of a laminate film formed by adhering a joint layer to a support layer at a peelable state, and covered so as to face the joint portion. to the butting portion and heat-sealed so that the joint layer is fused to the butting portion and the fused portion of the joint layer is peeled off from the support layer.

A method of applying a sealing strip onto a web of packaging material comprising advancing the web along a web advancement path; applying a first longitudinal portion of the sealing strip onto a longitudinal edge of the web, sealing the first longitudinal portion of the sealing strip onto the longitudinal edge, detecting and/or determining a correct alignment of the sealing strip with respect to the web. The detecting and/or determining of the correct alignment comprises acquiring an image of a second longitudinal portion of the sealing strip and a reference marker of a strip application apparatus, analyzing the acquired image to determine at least a first transversal distance between the reference marker and a longitudinal border of the second longitudinal portion; and evaluating the correct alignment/misalignment as a function of at least the first transversal distance.

A tape attaching machine for attaching an adhesive tape to a frame and a wafer and cutting the adhesive tape along the frame is provided. The tape attaching machine includes a tape winding unit configured to wind a remaining part of the adhesive tape left after cutting the adhesive tape, the remaining part of the adhesive tape being not attached to the frame and the wafer. The tape winding unit includes a main shaft like a roller and a pair of jigs detachably mounted on the opposite ends of the main shaft. Each of the jigs is engageable with the main shaft so as to have a tape contact area around which the remaining part of the adhesive tape is adapted to be wound and a grip area formed axially outside the tape contact area and adapted to be gripped by an operator.

The present invention relates to a method for manufacturing a composite sheet comprising an aerogel sheet, which comprises: a step (S10) of preparing the aerogel sheet (30); a step (S20) of laminating a fiber sheet (10) on each of both surfaces of the aerogel sheet (30); and a step (S30) of applying heat and a pressure to the aerogel sheet (30) and the fiber sheet (10), which are laminated, to bond the sheets to each other and to manufacture the composite sheet (40) in which the fiber sheet (10), the aerogel sheet (30), and the fiber sheet (10) are laminated.

A method and apparatus for constructing a tubular assembly (24) comprising an inner portion (21) and a further portion (22) surrounding the inner portion, the further portion being formed from a strip (50) of material comprising two opposed longitudinal marginal side portions (53). The apparatus (100) comprises an assembly station (106) having a wall (122). The apparatus (100) comprises means for advancing the inner portion (21) along a first path (111) extending past the wall, and means for advancing the strip (50) along a second path (112) and causing the strip to encircle the wall and thereby wrap about and surround the inner portion (21). The two marginal side portions (53) are disposed in overlapping relation on the side of the wall opposed to the first path (111). The apparatus (100) further comprises a system (131) for affixing the two longitudinal marginal side portions (53) together in overlapping relation to assemble the strip (50) into a tubular configuration about the inner portion (21), whereby the strip in the tubular configuration provides the further portion (22).

The terminal portion of a prefabricated skirt is connected to a casing of a thruster body in the vicinity of an end wall thereof using a method including positioning the terminal portion of the skirt with circumferential clearance around the casing of the thruster body in the vicinity of the end wall; keeping the skirt in position relative to the casing of the thruster body; closing both ends of an annular space between the terminal portion of the skirt and the casing of the thruster body; injecting elastomer into the annular space; and curing the elastomer.

Systems and methods are provided for designing composite parts. One embodiment is a method for fabricating a composite part. The method includes receiving a design that defines a stacking sequence for a composite charge comprising plies that have different fiber orientations, defining a splice zone within the design, modifying the design by splicing plies in a manner that accommodates ply slippage when the composite charge is formed to a contour, and fabricating a composite part based on the design that was modified.