A method for bonding a contact surface of a first substrate to a contact surface of a second substrate comprising of the steps of: positioning the first substrate on a first receiving surface of a first receiving apparatus and positioning the second substrate on a second receiving surface of a second receiving apparatus; establishing contact of the contact surfaces at a bond initiation site; and bonding the first substrate to the second substrate along a bonding wave which is travelling from the bond initiation site to the side edges of the substrates, wherein the first substrate and/or the second substrate is/are deformed for alignment of the contact surfaces.

Disclosed are a method of fixing an optical fiber and a measuring apparatus using the same, in which the method includes (a) heating a fixing portion where the optical fiber is to be fixed to an object, and (b) forming a concavo-convex structure by melting the heated fixing portion. The optical fiber is fixed to the object by filling an adhesive or filler in a state in which the fixing portion having the concavo-convex structure is disposed in an insertion space formed in the object. The optical fiber and the object can be firmly fixed using the mechanical coupling structure by forming the concavo-convex portion in a part where the optical fiber is to be fixed, and slip can be prevented from occurring between the cladding and the covering jacket.

A method for applying a label to an electrical cable having an outermost sheath with convolutions defining alternating peaks and valleys, the method including attaching the label to the sheath. The label includes a label substrate, the label substrate includes an attaching side, the attaching side being attached through an adhesive; and the label attaches to the peaks and spans across the valleys and circumferentially wraps around the sheath.

A method of manufacturing a composite part having a curved or radiused corner to avoid wrinkling or bridging of outer-most composite plies during consolidation and cure, including laying up composite material on male or female tooling to form two flanges extending at a first angle relative each other and a curved or radiused corner extending between the two flanges. Then the method may include changing an orientation of one or both of the flanges of the composite material, such that the two flanges extend at a second included angle relative each other. The second included angle is smaller than the first angle. The method may also include a step of consolidating the composite material before, after, or during the step of changing the orientation of the composite material to the second angle, as well as a step of curing the composite material oriented at the second angle.

An apparatus for attaching a label to a moving cable, the apparatus comprising: a roller for pressing a label against the moving cable, wherein the label has a first attaching edge and a second attaching edge and wherein the roller comprises: a first roller for pressing the label against the moving cable, wherein the label is pressed against the moving cable with the first attaching edge and the second attaching edge of the label on opposites sides of the moving cable; a first roll down roller for folding the second edge of the label against the moving cable; and a second roll down roller for folding the first edge of the label against the moving cable.

An apparatus for laminating a fiber tow is provided. The apparatus includes a supply unit that supplies a fiber tow impregnated with resin. A laminating unit is configured to move along a surface of a lamination object and has a shock-absorption element to laminate a fiber tow supplied from the supply unit on a surface of the lamination object.

A buoy comprising: an annular upper portion disposed on a lower portion; a drain hole disposed in the upper portion proximate to the lower portion; a handhold disposed in the upper portion distal to the lower portion; an attachment member disposed in the lower portion and protruding from a bottom of the lower portion, wherein the bottom is opposite the upper portion; and wherein at least one of the upper portion and the lower portion comprises a closed cell foam.

A method for treating a field operated component is disclosed which includes providing the component including a ceramic matrix composite and removing a first portion of the component, forming a first exposed surface on the component. The method further includes providing a second portion including the composite, the second portion having a second exposed surface including a conformation adapted to mate with the first exposed surface. The second portion is positioned in association with the component so as to replace the first portion, and the second portion and the component are joined to form a treated component. Another method is disclosed wherein the component is a turbine component which further includes removing an environmental barrier coating from the component, arranging and conforming the first exposed surface and the second exposed surface to define a joint, and applying an environmental barrier coating to the treated component.

A method and apparatus for bonding a yarn to a wearable article includes bonding the yarn to the wearable article at a first portion and a second portion. A first bonding location and a second bonding location are spaced apart from one another on a surface of the wearable article and an intermediate portion of the yarn extends contiguously between the first bonding location and the second bonding location and is not bonded to the wearable article.

A method for producing a thermoplastic fiber composite component, in particular for an aircraft or spacecraft, has the following method steps: material-removing processing of a first face of a first plate, wherein the first plate comprises a thermoplastic fiber composite material and a local reduction in thickness of the first plate is made by the material-removing processing of the first face; positioning a second plate relative to the first plate such that the first face of the first plate is brought into alignment with a third face of the second plate; and joining the first plate to the second plate to form a single component, wherein the surface of the first face of the first plate is integrally bonded to the surface of the third face of the second plate.