Abstract: A turbine system is disclosed. In one embodiment, the turbine system includes a transition duct. The transition duct includes an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The transition duct further includes an interface member for interfacing with a turbine section. The turbine system further includes a flexible metallic seal contacting the interface member to provide a seal between the interface member and the turbine section.

Abstract: A waterproof structure includes a package having an opening; a lid part which is slidable between a first position that makes the opening be open and a second position that is located closer to the innermost of the opening than the first position and closes the opening; and an elastic member provided on a surface of the lid part, said surface facing an inner side of the opening, in a manner such that the elastic member is incapable of contacting the package when the lid part is positioned at the first position, and that the elastic member is pressed into the opening when the lid part is positioned at the second position.

Abstract: A moveable wall panel system is disclosed. The movable wall panel system may include a bottom drop seal assembly that maintains a constant force relative to a floor portion of an environment through a damper. The movable wall panel system may include an automatic top seal assembly that seals a gap between the movable wall panel system and a ceiling of the environment without an actuation from an operator space of the environment, the top seal assembly being positioned above the operator space of the environment. The moveable wall panel system may include a plurality of seals positioned between adjacent panels to seal a gap between the adjacent panels.

Abstract: A seal for sealing a gap between adjacent first and second components, includes a first portion for attaching to the first component and a second portion extending at an angle from the first portion, the second portion having a top extending therealong that is flat in an uninstalled position, a thickened portion beneath the top and a hinge wherein the thickened portion is disposed between the hinge and an end of the top.

Abstract: A method and structures are provided for implementing press-lock electromagnetic compatibility (EMC) gaskets. A gasket includes a plurality of fasteners received through a plurality of corresponding mounting apertures in a perforated support surface for precise placement, and retention without adhesives. The corresponding mounting apertures have a diameter smaller than 1/20th of a wavelength of the highest frequency to be suppressed to remain independent of the shielding required. The gasket defines a cavity receiving compliant foam, and includes an absorber.

Abstract: A seal aligning and retaining assembly includes a seal trough defined by a first side wall, a second side wall and a base. Also included is at least one protrusion integrally formed with the base and extending therefrom, the at least one protrusion having an outer surface. Further included is a seal having at least one aperture including a first elastically deformable inner surface, the seal also having a first elastically deformable outer wall, the seal configured to elastically deform upon disposition of the seal in the seal trough at a first interface between the first elastically deformable inner surface and the outer surface of the at least one protrusion and at a second interface between the first elastically deformable outer wall and at least one of the first side wall and the second side wall.

Abstract: Gaskets for sealing two mating surfaces are described. The gaskets have an outer portion including a core between two sealing layers and an inner portion made of a deformable material and located in an aperture in the outer portion. The thickness of the inner portion is greater than the thickness of the outer portion. The inner portion may include a chemical treatment agent that can provide chemical protection to the mating surfaces. Methods of producing the gaskets and methods of using the gaskets for sealing joints, including corroded joints, are also described.

Abstract: A gasket for a compressed gas cylinder arranged to operate with a gas cylinder having a neck with a top surface around a gas outlet and a side surface extending downwardly from the top surface. The gasket may include an upper portion arranged for positioning on the top surface of the cylinder and for making a seal with the top surface, and a lower portion extending downwardly from the upper portion and around the side surface of the neck of the cylinder, such that the lower portion is arranged to make a seal with the side surface of the gas cylinder. Face and gland seals may be established by the gasket with an opening that receives the gasket and an associated cylinder neck.

Abstract: A hermetic seal includes a spring seal compressed with a limited sealing force between sealing surfaces. The sealing surfaces surround a gas-filled cavity that houses heat sensitive components. The hermetic seal includes a film that joins the spring seal to the sealing surfaces. The film includes a material that is softenable by heat to hermetically seal the spring seal to the sealing surfaces. The hermetic seal includes an externally accessible surface for selectively application of the heat to the film, without overheating the heat sensitive components.

Abstract: Methods of assembling wall structure include coupling first and second sealing members to a wall structural member along a first side and second side, respectively, of the wall structural member. The first sealing member and the second sealing member each include a compliant seal having a thickness and an adhesive along at least one side. The methods also include coupling a first wall sheathing element to the first side of the wall structural member so that the first sealing member contacts the first wall sheathing element and coupling a second wall sheathing element to the second side of the wall structural member so that the second sealing member contacts the second wall sheathing element. The first sealing member and the second sealing member form a restrictive fluid path between the first wall sheathing element, the wall structural member, and the second wall sheathing element.

Abstract: Methods and apparatus for a seal according to various aspects of the present invention include a seal operating in conjunction with a housing and a removable cover. A portion of the seal is attached to the housing and another portion of the seal is attached to the removable cover to enclose a joint between the housing and the removable cover. A cutter cuts the seal, which allows the removable cover to be removed.

Abstract: A seal is inserted into a space to be sealed. First and second end portions of the seal are engaged with first and second end surfaces of the space. The seal is compressed between the first and second end surfaces. The compression strains the seal. The strain includes the rotation of a cross-section of the seal so as to bias the seal into engagement with a surface forming one of an inboard surface and an outboard surface of the space.

Abstract: According to one aspect, an apparatus to provide sealing contact between first and second fueldraulic components includes a metallic member, wherein the metallic member comprises a layer of metal that is formed into a spring energized seal member. The apparatus also includes a layer disposed on an outer portion of the metallic member to provide sealing contact between the first and second fueldraulic components.

Abstract: A wing assembly for an aircraft comprising a spar, a wing cover and a rib; wherein the spar has a web portion and a flange portion joined by a radius corner; wherein a gap is formed at an interface between the spar, the wing cover and the rib; wherein the assembly further comprises a seal member which substantially covers the gap, and sealant provided between the seal member and the rib and/or the wing cover and/or the spar so as to seal the gap. Also a method for sealing a gap in an aircraft wing assembly.

Abstract: An article includes a crosslinked product of: a first crosslinked polymer and a second crosslinked polymer, wherein the article has a gradient in glass transition temperature. A process for making the article includes combining a first crosslinked polymer and a second crosslinked polymer to form a composition; compressing the composition; heating the composition; and crosslinking the composition to form the article, the article having a gradient in glass transition temperature. An article can be a seal that includes a first portion including a crosslinked product of: a first crosslinked polymer and a second crosslinked polymer; and a second portion including a polymer which is different than a constituent polymer in the first portion, wherein the seal has a gradient in glass transition temperature.

Abstract: A seal member internally seals a depressurized chamber constructed by joining a plurality of plates. The seal member includes a linear portion for sealing a linear joint of the depressurized chamber and a loop portion for sealing around a corner of the depressurized chamber by being pressed against internal walls of the plates forming the corner. The loop portion is arranged to enclose the corner of the depressurized chamber. The loop portion is fixed by using a support block held at the corner and a corner pressing member joined to the plates forming the corner. The loop portion is secured between a support surface of the support block and the corner pressing member.

Abstract: A sensor assembly for a printer arranged to displace printed material along a path, including a sensor housing and a platen assembly. The sensor housing includes top surfaces and resilient elements fixed to the top surfaces, and houses light emitting elements. The platen assembly includes transparent material and a platen housing with a plurality of steps, and is arranged to engage the sensor housing and displace in a first direction along the sensor housing toward an end of the sensor housing such that the transparent material is aligned with the light emitting elements in a direction orthogonal to the axis. As the platen assembly displaces in the first direction, the plurality of resilient elements is arranged to engage the plurality of steps to urge the piece of transparent material into contact with the sensor housing with progressively greater force such that the transparent material is sealed against the sensor housing.

Abstract: A tool for setting an annular seal, including an inner body, a first outer body coaxial with the longitudinal axis, and a second outer body coaxial with the longitudinal axis, wherein the second outer body is coupled to the first outer body. The inner body is configured to rotate about a longitudinal axis of the tool and is configure to bias a retaining ring, the first outer body is configured to couple to a potion of the mineral extraction system, and the second outer body is configured to move along the longitudinal axis to bias the annular seal.

Abstract: A gas turbine, a gas turbine shroud, and a method for sealing a gas turbine shroud with a non-metallic seal are provided. The gas turbine shroud includes an inner shroud and an outer shroud. A non-metallic seal is located between the inner shroud and the outer shroud while a shroud retainer clip applies a compression force upon the inner shroud and the outer shroud. The compression force compresses the non-metallic seal to fill a gap space between the inner shroud and the outer shroud to control fluid flow between a flow path and a non-flow path.

Abstract: Apparatus for sealing the gap between adjacent interconnecting mats in a reusable load-supporting surface deployed on the ground includes a seal member. The seal member includes an elongated main body and an elongated planar tail extending outwardly therefrom. The main body is positionable in the gap and the tail is configured to extend into at least a portion of the interface formed between upper and lower lips of the adjacent mats.

Abstract: According to one aspect of the invention, a turbine assembly includes a first stationary component, a second stationary component positioned radially outside the first stationary component, a first key feature on the first stationary component configured to mate to a second key feature on the second stationary component and a seal assembly positioned between the first and second key features to reduce fluid flow between the first and second key features. The seal assembly includes a V-shape member and a second member adjacent to the V-shape member, the second member and V-shape member having different rates of thermal expansion. The seal assembly also includes a latch feature coupled to the V-shape member configured to expand the seal assembly from a compressed state to an expanded sealing state when the seal assembly is subject to an elevated temperature.

Abstract: A transition piece aft-frame seal assembly may include an elongate body including a first side and a second side. The seal assembly may also include at least one feed hole disposed on the first side of the body. The seal assembly may also include at least one passageway extending through the body from the first side to the second side and in communication with the at least one feed hole. Moreover, the seal assembly may include at least one cooling hole disposed at the second side of the body and in communication with the at least one passageway. A flow of cooling fluid may enter the at least one feed hole, the at least one passageway, and the at least one cooling hole, wherein the at least one cooling hole directs the flow of cooling fluid to a recirculation zone about adjacent transition piece aft-frame assemblies.

Abstract: A glass-coated gasket comprises a gasket main body defining an inner hole and having a first contact surface and a second contact surface opposite the first contact surface, and a glass layer formed over at least a portion of one of the first contact surface and the second contact surface. The glass layer comprises a low melting temperature glass. A hermetic package comprises a substrate/glass-coated gasket/substrate structure that can be sealed using a thermo-compressive sealing step.

Abstract: An exemplary embodiment disclosed herein relates to an articulatable sealing device. The device includes a plurality of seal elements each of which is urgable against a seal-surface, a fixing member tightenable about a perimeter of the seal elements, and a retractor in operable communication with the plurality of seal elements and able to move the plurality of seal elements in a desired direction.

Abstract: The invention proposes a sealing shell (101) for partially bounding and for sealing a cavity (111), the sealing shell having a foam mold side and a tool carrier side, wherein the sealing shell is made of a material that is compressed when the cavity is closed.

Abstract: A spiral wound gasket (20) is disposed between joint members (22, 24) of a hot fluid joint to seal a gap (48) therebetween. The spiral wound gasket (20) includes a first high temperature performance metallic strip (28) formed of a thermally conductive alloy, including, Ni Cr, and Fe, spirally wound around a central axis (A) to present a first high temperature performance metallic winding (30) exposed to hot fluids. A first non-metallic filler strip (32) formed of a mica material is spirally wound outwardly of the first high temperature performance metallic winding (30) to form a first non-metallic filler winding (34). A second high temperature performance metallic strip (36) formed of a stainless steel material is spirally wound outwardly of the first non-metallic filler winding (34). A second non-metallic filler strip (40) formed of a graphite material is spirally wound outwardly of the second high temperature performance metallic winding (38).

Abstract: A carbon seal assembly includes a carbon seal element disposed about a central axis and that extends between a first end and a second end. The carbon seal element includes an inner step surface at an axial distance H1 with regard to the first end. An o-ring is adjacent to the inner step surface. The o-ring includes a cross-section diameter D2 such that a ratio H1/D2 is between 1.60-1.73.

Abstract: A system seals a filter or equipment component to a base and will continue to seal the filter or equipment component to the base in the event of hot air or fire. The system includes a first sealing material between the filter or equipment component and the base; and a second sealing material between the filter or equipment component and the base and proximate the first sealing material. The first sealing material and the second seal material are positioned relative to each other and relative to the filter or equipment component and the base to seal the filter or equipment component to the base and upon the event of fire the second sealing material will be activated and expand to continue to seal the filter or equipment component to the base in the event of hot air or fire.

Abstract: A filter setting and sealing apparatus includes a wobble plate mounted to press a filter edge into a plane defined by the top rim of a brew cup. A sealer defined by expandable sealer jaws is moveable into the filter. The jaws are actuated for radial outward expansion to seal the filter to the cup proximate the filter rim and cup edge. A second sealer is used to seal any gaps remaining in the seal after initial sealing. Methods are disclosed.

Abstract: An apparatus for attaching substrates includes a first chamber for supporting a first substrate and a second chamber for supporting a second substrate. A main seal member is placed between the first chamber and the second chamber so as to maintain a seal and a gap between the chambers. An alignment control part is placed between the first chamber and the second chamber so as to maintain the seal, and also to allow the second chamber to move with respect to the first chamber in order to align the substrates. The alignment control part may also control a gap between the chambers, to thereby maintain a uniform gap between the substrates.

Abstract: An application for an arced sealing tape has a bottom interfaced to an inner wall. The surface of the inner wall that is closest to a center point of the arc has an adhesive and the bottom surface of the bottom also has an adhesive.

Abstract: An example seal assembly includes a first seal that is configured to be placed between a fuel cell manifold and a fuel cell stack. The first seal establishes a recessed area within a side of the first seal that faces the fuel cell stack. The fuel cell seal assembly further includes a second seal that is configured to be placed between the first seal and the fuel cell stack within the recessed area. An example method of sealing a fuel cell interface includes holding a first seal within a groove established within a manifold and holding a second seal within a recessed area established within the second seal. The method limits flow of a fuel cell fluid using a first seal and the second seal.

Abstract: A system for sealing a port of a pulverizer. A pulverizer has journal assembly and a port for receiving the journal assembly. At least a portion of the journal assembly extends through the port. The system further includes a seal having a first end and a second end. The seal includes a first opening at or near the first end and a second opening at or near the second end. A bore extends between the first opening and the second opening. One of the first end and the second end is coupled to the pulverizer and the other one of the first end and the second end is coupled to the journal assembly. The seal inhibits fluid communication through the port.

Abstract: A seal assembly for a rotary machine is provided. The seal assembly includes a shim seal including multiple seal plates forming a C-shaped shim seal or a box shaped shim seal. The C-shaped shim seal includes a first side portion having a smaller width than that of an opposing second side portion, and the second side portion of the C-shaped shim seal includes a gap between at least two straight faces with an inward angle for allowing positioning within the slot between stator components. The box shaped seal includes a plurality of cuts at two opposing sides or corners for allowing high pressure fluid to occupy the cavity of the box-shaped shim seal. The seal may be inserted within one or more slots between adjacent stator components of the rotary machine.

Abstract: A spring seal assembly includes a first plate and a second plate. One or more spring elements are located between the first plate and the second plate and compressible therebetween. The spring seal assembly is insertable into a gap between two adjacent components such that at least one of the first plate and the second plate at least partially block a flow between the two adjacent components while exerting a force on the two adjacent components to prevent vibration of the seal in the gap. A method of sealing between adjacent components includes at least partially compressing a spring seal assembly. The spring seal assembly is inserted into the gap and allowed to expand in the gap thereby at least partially blocking a flow between the two adjacent components while exerting a force on the two adjacent components to prevent vibration of the seal in the gap.

Abstract: A sealing method is for sealing a gap between an opening section extending through a wall in a thickness direction thereof and an insertion member inserted in the opening section, and includes a seal-member preparing step of preparing a seal member including an elastic layer, an adhesive layer laminated on a surface of the elastic layer, and a release sheet laminated on a surface of the adhesive layer, and formed with a through hole into which the insertion member is to be inserted along a direction of lamination thereof, an inserting step of inserting the insertion member into the through hole such that the insertion member comes in contact with the seal member to bring the release sheet into abutment with the wall, and a sticking step of sticking the seal member to the insertion member and the wall, while peeling the release sheet from the adhesive layer.

Abstract: An electrochemical gas sensor includes: a disc-shaped metal bottom member; a cylindrical metal side member that extends along the axial direction of the bottom member to surround the bottom member; a ring-shaped polymer gasket that includes an opening in the center and in which both sides of the opening each have an L-shaped member in cross section, with one section of the L-shaped member being in contact with the inner side of the side member and the other section of the L-shaped member being in contact with the bottom member; a gas sensor body that is located in the opening of the gasket and whose bottom surface is in contact with the bottom member and that includes a pair of electrodes and a solid electrolyte membrane or a separator retaining a liquid electrolyte; and a metal cover that is in contact with the top surface of the gas sensor body.

Abstract: An exemplary method of applying a seal to a fuel cell component includes providing a release layer on one side of a seal. The release layer has reinforcing fibers. Another side of the seal is placed against a selected portion of the fuel cell component. The seal, release layer and fuel cell component are heated. The release layer is then removed after the seal is secured to the fuel cell component.

Abstract: According to one aspect, an apparatus to provide sealing contact between first and second fueldraulic components includes a metallic member, wherein the metallic member comprises a layer of metal that is formed into a spring energized seal member. The apparatus also includes a layer disposed on an outer portion of the metallic member to provide sealing contact between the first and second fueldraulic components.

Abstract: A method of sealing a gap between first and second aerodynamic surfaces. The width of the gap between the two surfaces is measured to obtain a gap measurement. The width of a seal member is pre-formed in accordance with the gap measurement. The seal member is fitted into the gap such that the seal member is substantially flush with the first and second aerodynamic surfaces. Apparatus for performing the method is also described. The apparatus comprising: a metrology device adapted to measure the width of the gap between the first and second aerodynamic surfaces; a seal member dispenser for dispensing a seal member; and a cutter adapted to cut the seal member to size in accordance with the measurements obtained by the metrology device.

Abstract: A seal assembly for a nozzle in a gas turbine engine includes a connector having a first hinge portion for attaching to the nozzle, a flat portion for sealing against a wall of the engine; and a first hinge for attaching the connector to the flat portion wherein the connector is adapted to rotate relative to the nozzle and the flat portion is adapted to rotate relative to the connector.

Abstract: A seal is provided that includes a resilient, arc-shaped body having a pair of sealing portions movable between a pre-compressed state and a compressed state. A removable, arc-shaped pre-compression member slidingly engages the seal body along at least a portion of its length to hold the sealing portions in the pre-compressed state.

Abstract: A fiber-based gasket, a glass manufacturing system, and a method are described herein for reducing thermal cell induced blisters. In one embodiment, the fiber-based gasket is placed in a connection between a first glass manufacturing device (e.g., capsule surrounding a downcomer) and a second glass manufacturing device (e.g., fusion draw machine surrounding an inlet). The fiber-based gasket has a density and compression which results in a gas permeation rate per unit surface area that is less than 22.5 ml/min/cm2 to reduce thermal cell induced blistering within the first glass manufacturing device and the second glass manufacturing device.

Abstract: Certain embodiments of the invention may include systems methods, and apparatus for sealing a bucket dovetail in a turbine. According to an example embodiment of the invention, a method is provided for sealing a gap between a bucket dovetail and a rotor wheel slot. The method can include providing a bucket tab associated with a bucket dovetail, wherein the bucket tab is configured to accept a seal tab; configuring the bucket tab and the seal tab to engage at least one dimension upon insertion of the seal tab into the bucket tab; and sealing a gap between the bucket dovetail and a rotor wheel slot with the seal tab; wherein at least a portion of the seal tab changes as a function of temperature for further sealing gap between the bucket dovetail and the rotor wheel slot.

Abstract: The invention relates to an arrangement (10) for sealing off a joint area (1) between a first joint partner (20, 200) and a second joint partner (30, 300) by means of at least one elastic sealing element (18, 180) disposed between a first sealing surface (12.1) of the first joint partner (20, 200) and a second sealing surface (12.2) of the second joint partner (30, 300), and an associated method for sealing off the joint area (1) between a first joint partner (20, 200) and a second joint partner (30, 300). According to the invention, at least one reservoir (14) for an anticorrosion agent (16) is introduced in a sealing zone (11) of the first and/or second sealing surface (12.1, 12.2), wherein the sealing element encloses the reservoir (14) together with the first and/or second sealing surface (12.1, 12.2).

Abstract: The present invention relates to a gasket mainly containing a non-halogen flame-retardant-containing adhesive sheet, wherein at least one surface of the gasket is an adhesive face of the non-halogen flame-retardant-containing adhesive sheet, and the non-halogen flame-retardant-containing adhesive sheet is an adhesive sheet wherein a non-halogen flame-retardant-containing adhesive layer/a nonporous core film/a non-halogen flame-retardant-containing adhesive layer are laminated in this order.

Abstract: The present invention provides a gasket comprising an adhesive sheet and a substrate sheet laminated on one surface of the adhesive sheet, which shows a distortion recovery rate according to the following compression distortion recovery test (I) of not less than 40%: Compression distortion recovery test (I): A 10 mm flat square sample is heated to 80° C., under which conditions a load is applied to compress the sample in the thickness direction such that the thickness thereof becomes 75% of the total thickness of the sample before loading, the load is lifted, the total thickness of the sample is measured 3 hr after unloading, and a distortion recovery rate is calculated according to the following formula: distortion recovery rate (%)=(total sample thickness 3 hr after unloading?(total sample thickness before compression×0.75))/(total sample thickness before compression×0.25)×100.

Abstract: Precompressed sealing tape for sealing a joint has a foam strip and a foil-type wrapping, which completely surrounds the foam strip and thus holds it in a precompressed state. A first transverse surface of the foam strip is pressed against a strip-like element, which is arranged inside the wrapping and has a certain resistance to bending in the transverse direction of the foam strip. A second transverse surface of the foam strip, which is arranged opposite to the first transverse surface, is firmly connected to the foil-type wrapping.

Abstract: The present invention relates to a gasket locating arrangement for a flow module, preferably plate reactor, comprising a gasket, locating means, a channel in a channel plate, a barrier plate, wherein the gasket consists of a sheet of soft gasket material, and said sheet has a cut through pattern corresponding to the channel in the channel plate. The present invention relates further to a use of the gasket location arrangement and also to a flow module, preferably a plate reactor, which comprises one or more gasket locating arrangements according to the invention, and one or more heat transfer means for heat transfer to and from the channel, and wherein each channel plate has one or more inlets, preferably two inlets, to the channel, and one outlet from the channel.

Abstract: A spring seal assembly includes a first plate and a second plate. One or more spring elements are located between the first plate and the second plate and compressible therebetween. The spring seal assembly is insertable into a gap between two adjacent components such that at least one of the first plate and the second plate at least partially block a flow between the two adjacent components while exerting a force on the two adjacent components to prevent vibration of the seal in the gap. A method of sealing between adjacent components includes at least partially compressing a spring seal assembly. The spring seal assembly is inserted into the gap and allowed to expand in the gap thereby at least partially blocking a flow between the two adjacent components while exerting a force on the two adjacent components to prevent vibration of the seal in the gap.