Abstract: A torsion seal is provided and includes a first section, a second section and a torsion section connected at opposite end portions thereof to the first and second sections and having a central portion extending between the opposite end portions to absorb differential thermal growth of vessels to which the first and second sections are coupled.

Abstract: A vacuum seal arrangement comprising a one-piece elastomeric gasket having at least first and second O-rings interconnected by a planar web, a first part having a first planar sealing surface with a dove-tail groove therein holding the first O-ring and a square walled groove therein holding the second O-ring, the first part further including at least one passage in the first planar sealing surface surrounded by the first O-ring or second O-ring.

Abstract: A seal strip (54) with a central relatively thin portion (68) and first and second thicker side portions (70, 72) that may be wedge-shaped adjacent the central portion. Each side portion may be formed of a linear array of base-in prisms (56), where each prism includes a base adjacent and normal to the central portion, and a thickness tapering distally toward an adjacent edge of the seal strip. The base-in prisms of each side portion may be separated by transverse slots (55) along the length of the strip. The transverse slots of the first side portion may be unaligned with the transverse slots of the second side portion along the length of the strip. A retention pin (58) may extend normally from an end of the seal strip. The seal strip may be mounted in tapered slots (49) of a gas turbine transition exit frame (48).

Abstract: A seal assembly includes a body having two circumferential sides, a leading end, and a trailing end. At least one of the circumferential sides includes a first channel sidewall, a second channel sidewall, and a channel bottom wall that together define a seal channel for receiving a seal. The seal channel includes a slot that cooperates with a tab on the seal to facilitate securing the seal within the seal channel.

Abstract: A container includes: a container body for storing substrates of semiconductor wafers; a door element detachably fitted to an open front portion of the container body; and a compressively deformable gasket for sealing between the container body and the door element. While a sealing surface for the gasket is formed on an inner periphery of an open front portion of the container body so that the difference between the maximum and minimum of a flatness is less than 0.50 mm, a fitting portion for the gasket is formed in a frame shape. The gasket is formed of a base fitted to the fitting portion; a flexible sealing part extended from the base toward the sealing surface; and a contact portion that is curvedly formed at a distal end of the sealing part and put in press-contact with the sealing surface.

Abstract: A vibration damper assembly for damping non-synchronous vibration between adjacent, spaced apart components comprises a vibration damper located in both of a pair of generally confronting passages in each of the components. The assembly comprises at least two spaced apart articulation surfaces for contact between damper and component, each of the articulation surfaces is arcuate in a first direction and is characterized by having a substantially linear portion in an orthogonal and second direction. Thereby the contact area is greatly enlarged and material loss minimized. The cross-sectional shape of the damper or passage is non-circular and there is a clearance between the damper and passage sufficiently small to prevent rotation of the damper in the passage during use.

Abstract: An integral seal and sealant package includes a prefabricated seal element having multiple surfaces; a high-temperature sealant composition engaged with one or more of the multiple surfaces; and a backer material enclosing the prefabricated seal element and the high-temperature sealant composition. The backer material has composition permitting the backer material to be installed with the seal element and the sealant composition between adjacent components to be sealed.

Abstract: A retainer for a gasket used to connect modular piping in a modular gas delivery system to the gas flow controlling components protects the sealing surface of the gasket from scratches before assembly by suspending the gasket at least 0.003 inches inside the retainer, regardless of orientation. Additionally, a slit in the circumference of the retainer allows the retainer to flex open for insertion of the seal gasket, and to compress to a smaller circumference, for a tight fit inside the sealing counterbore. A chamfer on the ID of the retainer aids the easier insertion of the seal into the retainer. In the ID of the retainer, a groove engages a protruding portion of the seal. The depth of this groove is such that with a complete compression of the retainer where the circumferential gap is completely closed, the protruding edge of the seal still has some clearance. This clearance acts as a stop to prevent the retainer from being overly compressed.

Abstract: A sealing assembly includes a component, a polyvinyl chloride foam gasket, a double sided acrylic tape, and a butyl tape. The component has a wall, an interior space defined by the wall, and an opening extending through the wall into the interior space. The wall has a rib extending therefrom and surrounding the opening. The gasket has a base, two sides, first and second ends, a length, and a groove formed therein and defined by the two sides and the base of the gasket. The groove extends along the length of the gasket. The gasket is positioned along the rib such that the rib extends into the groove, the gasket extends around the opening and the first and second ends of the gasket abut. Accordingly, upon entry of the amendment to the abstract, the new abstract reads: A sealing assembly includes a component, a polyvinyl chloride foam gasket, a double sided acrylic tape, and a butyl tape.

Abstract: A split ring seal assembly includes a metal seal ring having two ends defining a circumferential gap therebetween. At least a first spring element is mounted to the two ends to bias the two ends circumferentially towards each other to reduce the diameter of a circumferential inner sealing surface of the metal seal ring.

Abstract: Systems involving feather seals are provided. A representative vane assembly for a gas turbine engine includes: a first mounting platform having a first slot; a first airfoil extending from the first mounting platform; and a feather seal having opposing faces, a first side extending between the faces, and a first tab, the first tab extending outwardly beyond the first side; the first slot being sized and shaped to receive the feather seal including the first tab.

Abstract: A sealing material in a closed circular shape for a dovetail groove formed on the surface of one member and to be abutted to the surface of the other member to seal a space between the both members, the sealing material for a dovetail groove in a cross-sectional shape includes: a bottom portion that comes into contact with the bottom face of the dovetail groove and that has corner portions formed slightly narrower than the narrowest width of the opening portion of the dovetail groove; a side protruding portion that is formed continuously from the bottom portion; an overhanging shoulder portion that is formed continuously from the side protruding portion; and a sealing protrusion that is formed continuously from the overhanging shoulder portion and that is protruded upward from the opening portion of the dovetail groove to seal a space between the both members in the case in which the sealing protrusion is abutted to the surface of the other member.

Abstract: A seal assembly for an electric component includes a generally cylindrical plug, a first O-ring seal and a second O-ring seal. The plug includes a sidewall extending between first and second end walls. An annular groove circumscribes the sidewall. A first O-ring seal is disposed in the annular groove. A first through-bore extends between the first end wall and the second end wall. A first counter-bore circumscribes the first through-bore in the first end wall. A second O-ring seal is disposed within the first counter-bore.

Abstract: An arrangement for sealing a turbine shroud gas path duct interface of a turbine engine comprises a static shroud surrounding a rotatable airfoil array and an annular duct downstream of the shroud with respect to a gas flow passing through the gas path. The shroud and the duct define a portion of the gas path for directing the gas flow, having an axially extending interface gap between the shroud and duct. An annular seal in use engages both the shroud and the duct, thereby sealing the annular gap.

Abstract: An improved regenerative heat exchanger and seal assembly employ a plurality of instances of a seal apparatus, with each seal apparatus including a seal member that includes a seal tab that extends from one end of the seal member and further includes a corresponding notch at the opposite end of the seal member. The seal tab is receivable in a notch of an adjacent seal apparatus, and the engagement of the seal tabs in the notches creates a labyrinth seal by providing a tortuous path that resists the flow of exhaust gases and air past the seal assembly.

Abstract: An electronic sign module housing having an overmolded gasket seal including an elastomer overmolded gasket seal with an inner and an outer lip and a base overmolded to a rearwardly located contact surface of an electronic sign module housing. Grooves on the contact surface of the electronic sign module housing provide additional bonding surfaces with a greater surface area to enhance the chemically-bonded overmolding of the overmolded gasket seal. Truncated conical projections extending forwardly from the elastomer base extend into correspondingly shaped truncated conical cavities in the electronic sign module housing in order to provide additional chemical bonding and to provide a geometrically based frictional engagement arrangement.

Abstract: An exemplary embodiment of an air blower includes an electrically powered motor including a motor housing. A blower housing has first and second housing structures, each having inwardly facing, spaced ribs, and configured to surround the motor assembly in an assembled configuration. The ribs on the first and second housing structures register the radial and axial position of the motor housing inside the housing.

Abstract: A seal assembly for an axial flow gas turbine engine includes a rotatable component having a radially extending mate face, a seal slot formed in the mate face, and a seal member slidably disposed in the seal slot. The seal slot includes a radially outer wall and an opposing radially inner wall extending into the component in a circumferential direction from the mate face. The radially outer wall is angled radially inwardly from the mate face toward an inner end portion of the seal slot. Rotation of the seal assembly during operation of the engine produces a centrifugal force on the seal member to effect movement of the seal member in the circumferential direction out of the seal slot.

Abstract: A carriage sealing structure for refrigerator car is disclosed. The carriage is composed of core carriage plates provided with a heat preservation layer that is made of polyurethane. The carriage plates include a left side plate (5), a right side plate (6), a head plate (1), a soleplate (3), a front plate (4) and a backdoor plate (2). Notches are equipped at the jointed sites of the left side Plate, the right side plate, the head plate, the soleplate and the front plate, and an injection groove (7) is formed by the notches between mutually jointed carriage plates. High density polyurethane foam material is filled in the injection grooves in a high pressure so as to provide sealed connection between carriage plates. A working method for the carriage sealing structure is also disclosed. Assembled refrigerator car carriage is simple in structure and better in connection strength of the carriage plates.

Abstract: A sealing structure in which sealing is made by a seal ring installed in a dovetail groove where only an inner surface on one side of the groove is an inclined surface. In the sealing structure, the seal ring is less likely to come out of the dovetail groove, resistance of insertion of the seal ring into the dovetail is small, and particles are less likely to occur in the structure. The seal ring is formed of a rubber-like elastic material and is installed in the dovetail groove where the first inner surface on one side of the groove is inclined falling to the inside of the groove.

Abstract: A gate valve for vacuum capable of preventing a seal member from being cracked or particles from being produced due to a stress concentration even if the seal member is repeatedly compressed in the state that the adhesive agent is separated from the open side of a seal member mounting groove and capable of suppressing particles from being produced due to the rub of the seal top part with the seal surface.

Abstract: A housing structure includes an upper housing, a lower housing, a first waterproof member and a second waterproof member. The upper housing has a first connecting portion, and the lower housing has a second connecting portion. The upper housing and the lower housing are connected to each other by the first connecting portion and the second connecting portion. The first waterproof member is disposed between the first connecting portion and the second connecting portion. The second waterproof member is disposed between the first connecting portion and the second connecting portion. Wherein, a distance is formed between the first waterproof member and the second waterproof member.

Abstract: A seal assembly is configured to seal a tile gap between a pair of tiles. Each of the tiles may include a tile side surface. At least one of the tiles may include a groove which may be formed along a length of the tile side surface. The seal assembly may comprise a gasket assembly including first and second bulb portions which may be interconnected by a web. A spacer rope may be positionable along the web. The gasket assembly may define a folded configuration for mounting within the tile gap when the web is wrapped around the spacer rope such that the second bulb portion is positioned between the spacer rope and the first bulb portion. The second bulb portion may be receivable within the groove.

Abstract: A gasket is adapted to be mounted to a structure with a connector having a head and a body. The gasket includes a sealing body and a mounting body secured to the sealing body. The mounting body defines an elongated hollow chamber adapted to receive the head of the connector that mounts the gasket to the structure.

Abstract: Disclosed are sealing apparatuses having a sealing gland for an O-ring, the sealing gland comprising a primary gland and an auxiliary gland located below the primary gland. The apparatuses may be utilized for filter cartridges in filter systems.

Abstract: Disclosed is a two-material composite gasket, preferably a two-material composite annular gasket, for sealing a gap between two opposing surfaces, one of the surfaces having a concave gap portion, which is to be sealed by the gasket, the gasket having an oblong cross-sectional shape and having projections on the top end and bottom end thereof, the gasket including an upper low-hardness elastomer molded part formed of vulcanized rubber having a Shore A hardness of 5 to 35, a lower high-hardness elastomer molded part formed of vulcanized rubber having a Shore A hardness of 45 to 80, and a parting line bonding the low-hardness elastomer molded part and the high-hardness elastomer molded part, the parting line being positioned so that the height of the low-hardness elastomer molded part is 5 to 40% of the height of the entire gasket.

Abstract: A ball valve seat arrangement is provided that permits relief of cavity pressure. The arrangement includes a valve body for receiving a resilient annular seat. First passages in the seat provide communication between the valve cavity, and a space formed between the seat and the valve body. When the cavity pressure reaches a certain level, a sealing point between the seat and the valve body is lost. Communication is thereby provided between the space and the valve passage to achieve cavity pressure relief.

Abstract: Assemblies for coupling together two elements are provided and include a first coupling member and a second coupling member. The second coupling member has a body sized and adapted to be fitted into a hollow space defined by the first coupling member. The coupling members are structured to deflect the body of the second coupling member toward a first wall of the first coupling member as the body is passed into the hollow space.

Abstract: To make a plasma resistant seal excellent in both a plasma resisting performance and a sealing performance, and prevent an O-ring from protruding to a vacuum side gap, a plasma seal (6) made of PTFE having a plasma resisting performance is provided in a plasma irradiating side of an O-ring (5) as a main seal made of a rubber-like elastic material, an installation groove (4) shallower than a depth of an installation groove (3) provided in an installation member (2) is continuously provided in a plasma irradiation side of the installation groove (3), the O-ring (5) is attached to the installation groove (3), and the plasma seal (6) is attached to the installation groove (4) in a compressed state, or the O-ring is attached to the installation groove and the plasma seal is attached to the plasma irradiation side of the same installation groove (3) in a compressed state.

Abstract: A sealing device for a hydraulic assembly wherein hydraulic fluid is contained in working chamber (53) formed between body (52) and thrust member (51) of the assembly. The device comprises annular seal (63) with opposed sealing faces which are urged into sealing engagement between body (52) and thrust member (51) which have convergent sealing faces. The device may also have a pressure relief valve (100) tapped into the over-stroke end of chamber (53) to protect seal (63) from over-stroke damage comprising porous body (101) which allows fluid to bleed from chamber (53) and allows seal (63) to pass the tapping point without obstruction.

Abstract: The present invention relates to a seal carrier plate and a system of interchangeable chambers. A seal carrier plate is provided, wherein the seal carrier plate is adapted for being located between a first chamber and a second chamber and adapted for sealing the first chamber with respect to the second chamber from the environment, and wherein the seal carrier plate comprises an opening for transferring of substrates from the first chamber to the second chamber. Further, a system of interchangeable chambers is provided, wherein the chambers are adapted for accommodating a seal carrier plate on at least one side of the chamber with an opening.

Abstract: A structure for encapsulating a liquid crystal display device is disclosed. Openings are formed in a second material layer on a first substrate, exposing an underlying first material layer. The openings are substantially distributed over the perimeter of the first substrate. A sealant is placed in the openings, forming a sealant region for attachment of a second substrate to the first substrate. The sealant region is substantially perpendicular to a direction of length of the openings. In addition, the sealant contacts the first material layer and the second material layer through the openings.

Abstract: A radiation limiting opening for a structure includes a door with a gasket which seals against a door frame about the opening. Spaced apart channels in the door frame define a strike plate therebetween. A film made of a material galvanically compatible with the gasket to prevent corrosion is in intimate contact with the strike plate by a seal. This seal lodges an edge of the film in each channel to create a tortuous path for radiation.

Abstract: A seal assembly is disclosed including a support member, a first seal, a second seal spaced apart from the first seal, and a third seal, wherein the first seal militates against a leakage of fluid when an interior of an article to be sealed is subjected to at least one of temperatures below a predetermined temperature and pressures below a predetermined pressure, and the second seal and the third seal militate against the leakage of fluid when the interior of the article to be sealed is subjected to at least one of temperatures above the predetermined temperature and pressures above the predetermined pressure.

Abstract: The interturbine duct (ITD) directs hot combustion gases from a high pressure turbine stage outlet to a low pressure turbine stage inlet in a gas turbine engine. The ITD comprises an outer wall and a heat resistant non-metallic resilient annular seal provided around an end of the outer wall that is adjacent to the high pressure turbine stage outlet.

Abstract: A method and apparatus facilitates coupling a pressure vessel first mating surface to a second mating surface. The method comprises inserting a seal assembly into a groove defined in the first mating surfaces such that a portion of the seal assembly extends outwardly from the first mating surface, positioning the second mating surface in close proximity to the first mating surface such that the portion of the seal assembly extending outwardly from the first mating surface is received within a groove defined in the second mating surface, and such that the seal assembly facilitates reducing fluid leakage between the first and second mating surfaces.

Abstract: In a casing of a rotary machine, cast components are sealingly mounted together by means of seals accommodated in (semi-) enclosed cavities. A ring seal includes an annular base and an annular skirt extending axially from the base. To ameliorate manufacturing tolerances, the seal defines circumferentially spaced, intermittent cavities to allow seal material to be deformed into the cavities as required. Land areas between cavities have cross-sectional surfaces increasing progressively from a free surface of small area to cause compressive force required for deformation to increase exponentially with an exponent larger than 1. The cavities may be peripherally spaced, being open at a radially outer surface of the seal. The seal may be of elastic material which may be incompressible. The skirt may taper away from the base. The base may have a projecting sealing lip. The skirt may have, at a free end, a slanted, peripheral lip.

Abstract: To provide a gasket (1) mounted in a mounting groove (13) formed in one of two mutually opposite members in contact with the bottom face (13a) of the groove (13) and the opposite face (12a) of the other of the two members without falling in the groove (13) and without increase of its filling rate and reaction force, the gasket (1) is provided on its side faces with protrusions (3) interfering with the side faces (13b) of the groove (13) to prevent falling, where the height of the upper portions of the protrusions (3) is more than 80% of the groove depth and is 70 to 95% of the gasket height, the height of the lower portions of the protrusions (3) is 40% or more of the gasket height, and the gasket (1) is used mainly as a waterproof seal for a mobile device.

Abstract: In a sealing device (1) installed in an installation groove (4) provided in one member (2) of two members (2, 3) facing to each other so as to be brought into close contact with the other (3), the sealing device has a seal ring (11) and a backup ring (21) arranged in a low-pressure side (L) of the seal ring (11), the installation groove (4) has a slope bottom surface (4c), the backup ring (21) has a slope surface (21a). The sealing device (1) is to be made such that the seal ring (11) made of a rubber-like elastic body is prevented from being damaged by the backup ring (21) made of a hard material. In order to achieve this object, a second backup ring (31) is arranged between the seal ring (11) and the backup ring (21), and formed by a softer material than the backup ring (21).

Abstract: A sealed, self-aligning bearing includes an inner bearing ring with race tracks for rolling bodies, and an outer bearing ring with a race track for the rolling bodies, positioned radially outside the inner bearing ring. At least at one side of the bearing, a bearing seal is arranged axially outside the race tracks and bridges the space between the inner and outer bearing rings. The bearing seal has an outer annular rim fitted in an annular groove in the inner surface of the outer bearing ring and an inner annular rim arranged to slidingly contact the outer surface of the inner bearing ring. The outer rim and the inner rim of the bearing seal are interconnected by an intermediate member formed as a bellows-like thin membrane able to alternatively be stretched and compressed for permitting the bearing rings of the self-aligning bearing to make displacements and/or angular misalignments.

Abstract: Provided is a seal structure, according to the present invention, for sealing opposite surfaces of flanges between adjacent tail ducts, which can be prevented from being worn or aged deteriorated due to a thermal deformation in a high temperature atmosphere or vibration of a gas turbine combustor, and which can maintain a satisfactory sealing function for a long time.

Abstract: The invention relates to a dashboard seal provided between the windshield (1), the sound-proofing wall (2) of the engine compartment and the dashboard (3) in the passenger compartment of the vehicle. The dashboard seal is characterised in that the upper lip (6) includes a closed pocket (8) extending along a transverse section under the latter and limited by said upper lip (6), by the clamp (5) and, at the lower portion thereof, by a connection arm (8) connected both to the upper lip (6) and to the clamp (5).

Abstract: A gas turbine engine component having an axial pin stop assembly that reduces stress around a seal pin damper slot between a platform and a buttress is disclosed. The seal pin damper slot is extended to the leading edge of the buttress and an axial pin stop seal extends into the pin damper slot to limit movement of the seal pin damper while relieving stress concentration at the interface between the buttress and platform.

Abstract: An outer ring of a clamp-type joint for vacuum apparatus is disclosed. The joint includes a base forming an outer circumferential side and a pair of brims respectively extending from the top and bottom of the base toward the center axis of the joint, the inner side of the brims on which the brims come into contact with the O-ring being in the form of a convex sector, of which the arc faces the O-ring. The radius r of the circle forming the sector is 0.6-2.5 mm and the thickness (t0) satisfies the following formula: t1?0.2?t0?t1+0.4. In the formula, t1 is a thickness (mm) of the center ring at the point at which the center ring engages with the O-ring. The clamp-type joint can exhibit stable sealing performance at a high temperature of 250° C. or more without cracking of the O-ring.

Abstract: A fluid actuated rotational coupling device is provided with improved sealing of fluid passages. The device includes a fluid actuated rotational coupling that is disposed on a rotatable shaft. The coupling defines a fluid port. A key is received within a keyway in the coupling and/or shaft and defines a fluid passage extending therethrough having fluid ports at either end aligned with the fluid port in the coupling and a fluid port in the shaft. The key also defines grooves formed in surfaces of the key and surrounding the fluid ports. Seals are disposed within the grooves in the key. By locating the fluid passage and seals in the key, the seals may be removed and replaced without removing the coupling from the shaft. Further, the seals are less likely to be damaged during installation of the coupling device on the shaft.

Abstract: An aft closure assembly manufactured from two separate and distinct pieces made from different materials is provided for a rocket motor case. The aft closure assembly includes at least a retaining ring piece made from a first material similar to or having a coefficient of thermal expansion similar to that of the motor case. The aft closure assembly includes a blast tube and closure piece that can be manufactured from a second material that does not need to be similar to nor have a coefficient of thermal expansion similar to the motor case and retaining ring piece. This is possible because the blast tube and closure piece includes a face seal that seals against a face of the retaining ring.

Abstract: There is provided a sealing structure and a gasket which can seal both of a portion where a groove for mounting the gasket is formed and a portion where a groove for mounting the gasket is not formed when the portions are connected. The gasket includes a first gasket portion 110 which has a first mounted portion 111 to be mounted in a first groove 211 to come in close contact with a bottom face 211a of the first groove 211 and which is formed in a shape along an end portion of an outer wall portion 210 and a second gasket portion 120 which has a second mounted portion 150 to be mounted in a second groove 221 near a portion connected to the first gasket portion 110 and which is formed in a shape along an end portion 220 of a partition wall 220, the second mounted portion 150 having an inclined face for coming in close contact with the inclined bottom face 221a of the second groove 221.

Abstract: A metal ring gasket provides a high-pressure temperature tolerant metal-to-metal seal between subcomponents of a threaded union. The metal ring gasket is received in an annular cavity formed between mating surfaces of the subcomponents of the threaded union. The metal ring gasket is capable of maintaining a fluid seal even at very high temperatures resulting from direct exposure to fire. At high fluid pressures the metal ring gasket is energized because hoop stress induced by the fluid pressure forces the metal ring gasket into tighter contact with the subcomponents of the threaded union.

Abstract: A heat shield according to the invention on a support structure comprises a number of heat shield elements, which are configured and arranged on the support structure such that they abut each other leaving gaps. The support structure of the heat shield according to the invention has a peripheral direction and an axial direction, the heat shield elements abutting each other in the peripheral direction of the support structure leaving a gap, hereafter referred to as a peripheral gap, and in the axial direction of the support structure leaving a gap, hereafter referred to as an axial gap. Both the peripheral gaps and the axial gaps are also sealed by sealing elements, the sealing elements sealing the axial gaps being at a different distance from the support structure from the sealing elements sealing the peripheral gaps.

Abstract: An improvement in a seal assembly for sealing with a rotatable component extending within the seal assembly and defining a longitudinal axis of rotation, the seal assembly being of a type including a seal element retained by a seal housing, where one of the seal element and the seal housing is constructed from a compressible material, where the seal element includes a seal engagement surface and where the seal housing includes a housing engagement surface. The improvement includes one of the seal engagement surface and the housing engagement surface being comprised of the compressible material and the other being oriented in a plane normal to the longitudinal axis of rotation of the component extending within the seal assembly and defining a depression for providing an isolated gap between the seal engagement surface and the housing engagement surface for receiving the compressible material to restrain movement of the seal element relative to the seal housing.