| Class / Patent application number | Description | Number of patent applications / Date published |
|---|
| 277640000 | Anchoring feature extending through seal | 10 |
| 20110227297 | Railroad Car Seal for Railroad Hopper Cars - A seal is disclosed for retrofitting to an existing railroad hopper car having opposing sidewalls and at least one trough extending between the opposing sidewalls. The seal includes a first member configured to mate against a surface of a trough adjacent a sidewall, the first member including a first edge having angled sections corresponding to angled sections of where the sidewall meets the trough, and a second member integral with the first member and extending substantially upright from the first edge of the first member, the second member configured to mate against a surface of the sidewall adjacent the trough, wherein the second member is angled relative to the first member at each of the angled sections corresponding to angled sections of the sidewall adjacent the trough. | 09-22-2011 |
| 20120248714 | ASSEMBLY HAVING GASKET RESISTANT TO SIDE LOADING BY PRESSURIZED FLUID - An assembly that includes first and second housing members, a gasket and a plurality of bolts that exert a clamp force to clamp the gasket between the first and second housing members. The gasket includes a plurality of tab members that engage the interior of one or both of the first and second housing members. The gasket tabs can resist a force exerted by a pressurized fluid within one or both of the first and second housing members. A gasket that is resistant to side loading due to a pressurized fluid is also provided. | 10-04-2012 |
| 20120292860 | TURBINE COMBUSTION SYSTEM TRANSITION SEALS - Respective seals ( | 11-22-2012 |
| 20120306167 | TORSION SEAL - 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. | 12-06-2012 |
| 20120306168 | FORMED FLEXIBLE SEAL - A formed flexible seal is provided and includes a first section, a second section and a formed flexible 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. | 12-06-2012 |
| 20130049308 | Gasket Design For Molding Large Gaskets In A Deformed Shape - A gasket includes a plurality of corner sections each having a cross-section having a width of at least a first dimension. A plurality of deformable sections are disposed between a pair of the plurality of corner sections, each of the plurality of deformable sections having a cross-section having a width less than the first dimension and having a curved shape that is deformable to a straight shape in its installed condition. The deformable sections allow the gasket to be formed with a smaller molding footprint than the assembled gasket shape and the plurality of corner sections have a same angled orientation in its installed and un-installed positions. | 02-28-2013 |
| 20130292912 | UNDERWATER SWIMMING POOL LIGHT REPAIR DEVICE - A sealing ring repair device for underwater swimming pool lights is designed to fit on the water side of a sealing ring. The repair device includes a top plate with a plurality of top plate screw holes sized and positioned to match the sealing ring screw holes. The top plate has an inner side, and a repair tab extends from the top plate inner side. The repair tab can be used to secure an underwater swimming pool light in place when the ring tab of the sealing ring is damaged. | 11-07-2013 |
| 20140015204 | SPACER AND GASKET ASSEMBLY FOR USE ON AN AIRCRAFT - A spacer and gasket assembly is shown for receipt between a static structure having an outer and inner surface and fastener holes therethrough and a removable structure having a base with fastener holes and an upper surface and a lower surface. The static structure and removable structure are engaged through a multiplicity of fasteners having a shaft diameter. The fasteners are adapted to apply a compression on the gasket between the static structure and the removable structure. The static structure and the removable structure have opposed, typically flat, facing walls. The spacer and gasket assembly comprising a substantially non-compressible spacer adapted for receipt between the static structure and the removable structure having a spacer thickness. A gasket has a deformable, flowable, elastomeric body and a skeleton having a skeleton thickness, the skeleton substantially integral with the body. The gasket has an uncompressed gasket thickness. The spacer and the gasket are adapted to be placed substantially between the facing walls of the static structure and the removable structure and the removable structure will compress and deform the gasket when the fasteners are torqued down. | 01-16-2014 |
| 20160069202 | GAS TURBINE ROTOR SEALING BAND ARRANGEMENT HAVING A FRICTION WELDED PIN ELEMENT - A sealing band arrangement for a gas turbine including first and second adjoining rotor disks separated by a gap wherein the first rotor disk includes an aperture. The sealing band arrangement includes at least one seal strip segment located within the gap, wherein the seal strip segment includes a first mating surface. The sealing band arrangement further includes a block having a locking section located within the aperture to stop circumferential movement of the seal strip segment relative to the first and second disks. A tapered pin element extends through the seal strip segment and the block. The tapered pin element is friction welded to both the seal strip segment and the block to attach the block to the first mating surface of the seal strip segment. | 03-10-2016 |
| 20160186866 | AIR SEAL ASSEMBLY FOR AIRCRAFT FLAP SEAL - An air seal assembly for an aircraft control surface comprises a bulb-type air seal, a mounting bracket and a fastener. The bulb-type air seal has a hollow bulb portion, a T-shaped mounting extension, and a first through hole extending through the T-shaped mounting extension. The mounting bracket has a T-shaped channel configured to slidingly receive the T-shaped mounting extension of the air seal and a second through hole. The fastener has a head at one end and an opposite exposed end sized for extending through the first through hole in the T-shaped mounting extension and through the second through hole in the mounting bracket. The exposed end is accessible to tighten the fastener against the bracket to keep the air seal in place within the T-shaped channel. | 06-30-2016 |
